ART-2000 - MAINTENANCE - 006-05332-0003- REV 4 - 2012
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Honeywell International Inc. 23500 W. 105th Street Olathe, Kansas 66061-8425 U.S.A. CAGE: 22373 Telephone: (800) 601-3099 (Toll Free U.S.A./Canada) Telephone: (602) 365-3099 (International Direct) Telephone: 00-800-601-30999 (EMEA Toll Free) Telephone: 420-234-625-500 (EMEA Direct) Website: www.myaerospace.com
Component Maintenance Manual with Illustrated Parts List
ART 2000 Color Weather Radar Antenna/Receiver /Transmitter Part Number
CAGE
071-01519-0101
22373 Legal Notice
Export Control This document contains technical data and is subject to U.S. export regulations. These commodities, technology, or software were exported from the United States in accordance with the export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 7E994, NLR Eligible
34-40-11 Publication Number 006-05332-0003, Revision 4 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page T-1 Initial 1 Jan 1999 Revised 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 Proprietary Information
Honeywell - Confidential THIS COPYRIGHTED WORK AND ALL INFORMATION ARE THE PROPERTY OF HONEYWELL INTERNATIONAL INC., CONTAIN TRADE SECRETS AND MAY NOT, IN WHOLE OR IN PART, BE USED, DUPLICATED, OR DISCLOSED FOR ANY PURPOSE WITHOUT PRIOR WRITTEN PERMISSION OF HONEYWELL INTERNATIONAL INC. ALL RIGHTS RESERVED.
Honeywell Materials License Agreement The documents and information contained herein ("the Materials") are the proprietary data of Honeywell International Inc. and Honeywell Intellectual Properties Inc. (collectively "Honeywell"). These Materials are provided for the exclusive use of Honeywell Service Centers; Honeywell-authorized repair facilities; operators of Honeywell aerospace products subject to an applicable product support agreement, their wholly owned-subsidiaries or a formally designated third party service provider; and direct recipients of Materials from Honeywell’s Aerospace Technical Publication Distribution. The terms and conditions of this License Agreement govern your use of these Materials, except to the extent that any terms and conditions of another applicable agreement with Honeywell regarding the operation, maintenance, or repair of Honeywell aerospace products conflict with the terms and conditions of this License Agreement, in which case the terms and conditions of the other agreement will govern. However, this License Agreement will govern in the event of a conflict between its terms and conditions and those of a purchase order or acknowledgement. 1. License Grant - If you are a party to an applicable product support agreement, a Honeywell Service Center agreement, or an authorized repair facility agreement, Honeywell hereby grants you a limited, non-exclusive license to use these Materials to operate, maintain, or repair Honeywell aerospace products only in accordance with that agreement. If you are a direct recipient of these Materials from Honeywell’s Aerospace Technical Publication Distribution and are not a party to an agreement related to the operation, maintenance or repair of Honeywell aerospace products, Honeywell hereby grants you a limited, non-exclusive license to use these Materials to maintain or repair the subject Honeywell aerospace products only at the facility to which these Materials have been shipped ("the Licensed Facility"). Transfer of the Materials to another facility owned by you is permitted only if the original Licensed Facility retains no copies of the Materials and you provide prior written notice to Honeywell. 2. Rights In Materials - Honeywell retains all rights in these Materials and in any copies thereof that are not expressly granted to you, including all rights in patents, copyrights, trademarks, and trade secrets. No license to use any Honeywell trademarks or patents is granted under this License Agreement. 3. Confidentiality - You acknowledge that these Materials contain information that is confidential and proprietary to Honeywell. You agree to take all reasonable efforts to maintain the confidentiality of these Materials. 4. Assignment And Transfer - This License Agreement may be assigned to a formally designated service designee or transferred to a subsequent owner or operator of an aircraft containing the subject Honeywell aerospace products. However, the recipient of any such assignment or transfer must assume all of your obligations under this License Agreement. No assignment or transfer shall relieve any party of any obligation that such party then has hereunder. 5. Copies of Materials - Unless you have the express written permission of Honeywell, you may not make or permit making of copies of the Materials. Notwithstanding the foregoing, you may make copies of only portions of the Material for your internal use. You agree to return the Materials and any copies thereof to Honeywell upon the request of Honeywell.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page T-2 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 6. Term - This License Agreement is effective until terminated as set forth herein. This License Agreement will terminate immediately, without notice from Honeywell, if you fail to comply with any provision of this License Agreement or will terminate simultaneously with the termination or expiration of your applicable product support agreement, authorized repair facility agreement, or your formal designation as a third party service provider. Upon termination of this License Agreement, you will return these Materials to Honeywell without retaining any copies and will have one of your authorized officers certify that all Materials have been returned with no copies retained. 7. Remedies - Honeywell reserves the right to pursue all available remedies and damages resulting from a breach of this License Agreement. 8. Limitation of Liability - Honeywell does not make any representation regarding the use or sufficiency of the Materials. THERE ARE NO OTHER WARRANTIES, WHETHER WRITTEN OR ORAL, EXPRESS, IMPLIED OR STATUTORY, INCLUDING, BUT NOT LIMITED TO, (i) WARRANTIES ARISING FROM COURSE OF PERFORMANCE, DEALING, USAGE, OR TRADE, WHICH ARE HEREBY EXPRESSLY DISCLAIMED, OR (ii) WARRANTIES AGAINST INFRINGEMENT OF INTELLECTUAL PROPERTY RIGHTS OF THIRD PARTIES, EVEN IF HONEYWELL HAS BEEN ADVISED OF ANY SUCH INFRINGEMENT. IN NO EVENT WILL HONEYWELL BE LIABLE FOR ANY INCIDENTAL DAMAGES, CONSEQUENTIAL DAMAGES, SPECIAL DAMAGES, INDIRECT DAMAGES, LOSS OF PROFITS, LOSS OF REVENUES, OR LOSS OF USE, EVEN IF INFORMED OF THE POSSIBILITY OF SUCH DAMAGES. TO THE EXTENT PERMITTED BY APPLICABLE LAW, THESE LIMITATIONS AND EXCLUSIONS WILL APPLY REGARDLESS OF WHETHER LIABILITY ARISES FROM BREACH OF CONTRACT, WARRANTY, TORT (INCLUDING BUT NOT LIMITED TO NEGLIGENCE), BY OPERATION OF LAW, OR OTHERWISE. 9. Controlling Law - This License shall be governed and construed in accordance with the laws of the State of New York without regard to the conflicts of laws provisions thereof. This license sets forth the entire agreement between you and Honeywell and may only be modified by a writing duly executed by the duly authorized representatives of the parties.
Safety Advisory WARNING: BEFORE THE MATERIALS CALLED OUT IN THIS PUBLICATION ARE USED, KNOW THE HANDLING, STORAGE AND DISPOSAL PRECAUTIONS RECOMMENDED BY THE MANUFACTURER OR SUPPLIER. FAILURE TO OBEY THE MANUFACTURERS’ OR SUPPLIERS’ RECOMMENDATIONS CAN RESULT IN PERSONAL INJURY OR DISEASE. This publication describes physical and chemical processes which can make it necessary to use chemicals, solvents, paints, and other commercially available materials. The user of this publication must get the Material Safety Data Sheets (OSHA Form 174 or equivalent) from the manufacturers or suppliers of the materials to be used. The user must know the manufacturer/ supplier data and obey the procedures, recommendations, warnings and cautions set forth for the safe use, handling, storage, and disposal of the materials.
Warranty/Liability Advisory WARNING: HONEYWELL ASSUMES NO RESPONSIBILITY FOR ANY HONEYWELL EQUIPMENT WHICH IS NOT MAINTAINED AND/OR REPAIRED IN ACCORDANCE WITH HONEYWELL’S PUBLISHED INSTRUCTIONS AND/OR HONEYWELL’S FAA/SFAR 36 REPAIR AUTHORIZATION. NEITHER DOES HONEYWELL ASSUME RESPONSIBILITY FOR SPECIAL TOOLS AND TEST EQUIPMENT FABRICATED BY COMPANIES OTHER THAN HONEYWELL. WARNING: INCORRECTLY REPAIRED COMPONENTS CAN AFFECT AIRWORTHINESS OR DECREASE THE LIFE OF THE COMPONENTS. INCORRECTLY FABRICATED SPECIAL TOOLING OR TEST EQUIPMENT CAN RESULT IN DAMAGE TO THE PRODUCT COMPONENTS OR GIVE UNSATISFACTORY RESULTS.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page T-3 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 WARNING: THIS EQUIPMENT GENERATES MICROWAVE RADIATION WHICH CAN BE HARMFUL TO HUMANS. DO NOT OPERATE UNTIL YOU HAVE READ AND CAREFULLY FOLLOWED ALL SAFETY PRECAUTIONS AND INSTRUCTIONS IN THE OPERATIONS AND SERVICE MANUALS. WARNING: TO PREVENT HARM TO HUMANS, MAINTAIN PRESCRIBED SAFE DISTANCE WHEN STANDING IN FRONT OF A RADIATING ANTENNA. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B. WARNING: TO PREVENT HARM TO HUMANS, NEVER EXPOSE EYES OR ANY PART OF THE BODY TO AN UNTERMINATED WAVEGUIDE. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
Copyright - Notice Copyright 1999, 2012 Honeywell International Inc. All rights reserved. Honeywell is a registered trademark of Honeywell International Inc. All other marks are owned by their respective companies. THIS IS THE CMM FOSI - DATE: 20101217
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page T-4 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
TRANSMITTAL INFORMATION REVISION NUMBER 4 DATED 3 JAN 2012 TO HOLDERS OF ART 2000 COLOR WEATHER RADAR ANTENNA/RECEIVER/TRANSMITTER CMM ATA NO. 34-40-11 ISSUED FOR USE IN SUPPORT OF THE FOLLOWING: Table TI-1. Applicable Components Component PN
Nomenclature
071-01519-0101
ART 2000 Color Weather Radar Antenna/Receiver /Transmitter
Revision History Table TI-2 shows the revision history of this CMM. Table TI-2. Revision History Revision Number
Revision Date
0
1 Jan 1999
1
Not Available
2
Not Available
3
1 Jun 2002
4
3 Jan 2012
This revision is a full replacement. All changed pages have a new date, as identified in the List of Effective Pages. Revision bars identify the changed data. See Transmittal information for history of revisions to this CMM. Remove and discard all pages of the manual and replace them with the attached pages. Write the revision number, revision date, and replacement date on the Record of Revisions page. The table of highlights tells users what has changed as a result of the revision. The table consists of three columns. The Task/Page column identifies the blocks of changed information, such as a task, subtask, graphic, or parts list, and the page on which that block starts. The block of information often includes the MTOSS code. Revision marks, when provided, identify the location of the change within the block. The Description of Change column tells about the change or changes within each block. The description of change is often preceded by a paragraph or figure reference that applies to the block of information. The Effectivity column tells the user the part number(s) to which the block of information applies. The default value for this column is "All." "All" means that the block applies to all parts. Table of Highlights Task/Page
Description of Change
Effectivity
SERVICE BULLETIN LIST
Added Service Bulletin 600-07790-0090 (SB ART 2000-9).
All
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page TI-1 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Table of Highlights (Cont) Task/Page
Description of Change
Effectivity
SERVICE BULLETIN LIST
Added Service Bulletin 600-07791-0000 (SB ART 2000-10).
All
SERVICE BULLETIN LIST
Added Service Bulletin 600-07791-0011 (SB ART 2000-11).
All
SERVICE BULLETIN LIST
Added Service Bulletin 600-07791-0020 (ART 2000-34-0012).
All
SERVICE BULLETIN LIST
Added Service Aid 601-07790-0020 (SA ART 2000-102).
All
SERVICE BULLETIN LIST
Added Service Aid 601-07790-0030 (SA ART 2000-103).
All
SERVICE BULLETIN LIST
Added Service Aid 601-07790-0040 (SA ART 2000-104).
All
SERVICE BULLETIN LIST
Added Service Aid 601-07790-0050 (SA ART 2000-105).
All
SERVICE BULLETIN LIST
Added Service Aid 601-07790-0060 (SA ART 2000-106).
All
SERVICE BULLETIN LIST
Added Service Aid 601-07790-0070 (SA ART 2000-107).
All
SERVICE BULLETIN LIST
Added Service Aid 601-07790-0080 (SA ART 2000-108).
All
SERVICE BULLETIN LIST
Added Service Aid 601-07791-0000 (SA ART 2000-110).
All
SERVICE BULLETIN LIST
Added Service Aid 601-07791-0010 (SA ART 2000-111).
All
SERVICE BULLETIN LIST
Added Software Bulletin 605-07790-0010 (SWB ART 2000-1).
All
SERVICE BULLETIN LIST
Added Software Bulletin 605-07790-0031 (SWB ART 2000-SW3).
All
SERVICE BULLETIN LIST
Added Software Bulletin 605-07790-0050 (SWB ART 2000-SW5).
All
SERVICE BULLETIN LIST
Added Service Bulletin D200904000001 (ART 2000-34-13).
All
SERVICE BULLETIN LIST
Added Service Bulletin D200906000080 (ART 2000-34-14).
All
INTRODUCTION
Reformatted section to the latest template format.
All
TASK 34-40-11-99F-801-A01 (Page INTRO-1)
Paragraph 1. Added the MPEL data.
All
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page TI-2 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Table of Highlights (Cont) Task/Page
Description of Change
Effectivity
TASK 34-40-11-99F-801-A01 (Page INTRO-1)
Paragraph 1. Added a reference to FAA Advisory Circular No. 20-68B and deleted the embedded copy.
All
Subtask 34-40-11-99F-017-A01 (Page INTRO-21)
Paragraph 7.A. Added the software version history to Table INTRO-4.
All
DESCRIPTION AND OPERATION
Reformatted section to the latest template format.
All
Subtask 34-40-11-870-004-A01 (Page 5)
Paragraph 1.D. Table 4, corrected the nomenclature of the scan sensor assembly.
All
Subtask 34-40-11-870-004-A01 (Page 5)
Paragraph 1.D. Table 4, revised the part number of the pitch motor assembly in accordance with Service Bulletin 600-07791-0011 (SB ART 2000-11).
All
Subtask 34-40-11-870-004-A01 (Page 5)
Paragraph 1.D. Table 4, corrected the part numbers of the gimbal assembly and the receiver assembly to reflect the actual part numbers.
All
Subtask 34-40-11-870-004-A01 (Page 5)
Paragraph 1.D. Table 4, added new part numbers for the preamp board, the power supply/modulator board, and the logic board in accordance with Service Bulletin 600-07790-0030 (SB ART 2000-3), and added two footnotes.
All
TESTING AND FAULT ISOLATION
Reformatted section to the latest template format.
All
Subtask 34-40-11-99C-003-A01 (Page 1001)
Paragraph 1.B. Revised Table 1001 to include the required test equipment.
All
Subtask 34-40-11-810-003-A01 (Page 1005)
Paragraph 3.A. Corrected Steps (11)(b), (e), and (f) in accordance with Service Aid 601-07790-0050 (SA ART 2000-105).
All
Subtask 34-40-11-810-003-A01 (Page 1005)
Paragraph 3.A. Updated the reference to the RDR 2000 Color Weather Radar System in Step (2).
All
Subtask 34-40-11-810-003-A01 (Page 1005)
Paragraph 3.A. Updated the target distance and signal levels in Tables 1003 and 1004.
All
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page TI-3 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Table of Highlights (Cont) Task/Page
Description of Change
Effectivity
GRAPHIC 34-40-11-99B-808-A01 (Page 1005)
Figure 1002. Revised Sheet 1 in accordance with Service Aid 601-07790-0080 (SA ART 2000-108).
All
Subtask 34-40-11-810-013-A01 (Page 1084)
Paragraph 5.E. Added the magnetron to the list of assemblies that if replaced require the receiver to be calibrated in accordance with Service Bulletin 601-07790-0040 (SA ART 2000-104).
All
Subtask 34-40-11-810-014-A01 (Page 1084)
Paragraph 5.F. Updated the target range and target width for the radar signal generator settings.
All
Subtask 34-40-11-810-015-A01 (Page 1084)
Paragraph 5.G. Updated the target range and target width for the radar signal generator settings.
All
Subtask 34-40-11-810-020-A01 (Page 1088)
Paragraph 7.D. Revised Step (3)(c) and Table 1010 to delete references to IC data sheets.
All
Subtask 34-40-11-810-020-A01 (Page 1088)
Paragraph 7.D. Deleted commonly available IC data sheets.
All
SCHEMATICS AND WIRING DIAGRAMS
Reformatted section to the latest template format.
All
Subtask 34-40-11-99C-005-A01 (Page 2001)
Paragraph 1.B. Revised Table 2002 to include the required consumables.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added the outline and detail/schematic diagram references to Table 2003.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added details from Service Bulletins 600-07790-0030 (SB ART 2000-3), 600-07790-0041 (SB ART 2000-4), 600-07790-0050 (SB ART 2000-5), 600-07790-0060 (SB ART 2000-6), 600-07790-0071 (SB ART 2000-7), 600-07790-0080 (SB ART 2000-8), 600-07790-0090 (SB ART 2000-9), 600-07791-0000 (SB ART 2000-10), 600-07791-0011 (SB ART 2000-11), and 600-07791-0020 (ART 2000-34-0012) to Table 2004.
All
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page TI-4 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Table of Highlights (Cont) Task/Page
Description of Change
Effectivity
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added details from Service Aids 601-07791-0010 (SA ART 2000-111), 601-07790-0020 (SA ART 2000-102), and 601-07790-0030 (SA ART 2000-103) to Table 2004.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added details from Software Bulletins 605-07790-0031 (SWB ART 2000-SW3), 605-07790-0041 (SWB ART 2000-SW4), and 605-07790-0050 (SWB ART 2000-SW5) to Table 2004.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added Table 2005, Summary of Changes to the Logic Board, PN 200-08549-0000.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Table 2005, added Service Bulletin D200906000080 (ART 2000-34-14).
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added details from Service Bulletins 600-07790-0041 (SB ART 2000-4), 600-07790-0050 (SB ART 2000-5), 600-07790-0060 (SB ART 2000-6), and 600-07790-0071 (SB ART 2000-7) to Table 2005.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added Table 2006, Summary of Changes to the Logic Board, PN 200-08549-0020.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added details from Service Bulletins 600-07790-0041 (SB ART 2000-4), 600-07790-0050 (SB ART 2000-5), 600-07790-0060 (SB ART 2000-6), 600-07790-0071 (SB ART 2000-7), and 600-07791-0020 (ART 2000-34-0012) to Table 2006.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added details from Service Aids 601-07791-0010 (SA ART 2000-111) and 601-07790-0030 (SA ART 2000-103) to Table 2006.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added details from Software Bulletins 605-07790-0031 (SWB ART 2000-SW3), 605-07790-0041 (SWB ART 2000-SW4), and 605-07790-0050 (SWB ART 2000-SW5) to Table 2006.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added Table 2007, Summary of Changes to the Receiver Assembly, PN 200-05553-0001.
All
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page TI-5 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Table of Highlights (Cont) Task/Page
Description of Change
Effectivity
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added Table 2008, Summary of Changes to the Preamp Board, PN 200-08545-0000.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added Table 2009, Summary of Changes to the Preamp Board, PN 200-08545-0020.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added Table 2010, Summary of Changes to the Power Supply/Modulator Board, PN 200-08548-0000.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added Table 2011, Summary of Changes to the Power Supply/Modulator Board, PN 200-08548-0020.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added details from Service Bulletins 600-07790-0080 (SB ART 2000-8) and 600-07790-0090 (SB ART 2000-9) to Table 2011.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added details from Service Aid 601-07790-0020 (SA ART 2000-102) to Table 2011.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added Table 2012, Summary of Changes to the Configuration Module Assembly, PN 071-00097-0100.
All
Subtask 34-40-11-000-002-A01 (Page 2002)
Paragraph 2.B. Added Table 2013, Summary of Changes to the Configuration Module, PN 200-08705-0000.
All
GRAPHIC 34-40-11-99B-869-A01 (Page 2010)
Figure 2003. Revised to include the latest data.
All
GRAPHIC 34-40-11-99B-870-A01 (Page 2049)
Figure 2004. Added Logic Board, PN 200-08549-0020, Detail/Schematic.
All
GRAPHIC 34-40-11-99B-871-A01 (Page 2091)
Figure 2005. Added Receiver Assembly, PN 200-05553-0001, Detail.
All
GRAPHIC 34-40-11-99B-872-A01 (Page 2095)
Figure 2006. Added Preamp Board, PN 200-08545-0000, Detail/Schematic.
All
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page TI-6 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Table of Highlights (Cont) Task/Page
Description of Change
Effectivity
GRAPHIC 34-40-11-99B-873-A01 (Page 2101)
Figure 2007. Added Preamp Board, PN 200-08545-0020, Detail/Schematic.
All
GRAPHIC 34-40-11-99B-874-A01 (Page 2107)
Figure 2008. Added Power Supply/Modulator Board, PN 200-08548-0000, Detail/Schematic.
All
GRAPHIC 34-40-11-99B-875-A01 (Page 2133)
Figure 2009. Revised to include the latest data.
All
GRAPHIC 34-40-11-99B-876-A01 (Page 2159)
Figure 2010. Added Configuration Module Assembly, PN 071-00097-0100, Detail.
All
GRAPHIC 34-40-11-99B-877-A01 (Page 2163)
Figure 2011. Added Configuration Module, PN 200-08705-0000, Detail/Schematic.
All
DISASSEMBLY
Reformatted section to the latest template format.
All
Subtask 34-40-11-99C-007-A01 (Page 3001)
Paragraph 1.B. Revised Table 3001 to include the required equipment.
All
Subtask 34-40-11-000-005-A01 (Page 3002)
Paragraph 2.B. Added the IPL figure and item numbers to the procedural steps.
All
Subtask 34-40-11-000-006-A01 (Page 3002)
Paragraph 2.C. Added the IPL figure and item numbers to the procedural steps.
All
Subtask 34-40-11-000-007-A01 (Page 3003)
Paragraph 2.D. Revised the paragraph title and added the IPL figure and item numbers to the procedural steps.
All
Subtask 34-40-11-000-008-A01 (Page 3003)
Paragraph 2.E. Added the IPL figure and item numbers to the procedural steps.
All
Subtask 34-40-11-000-009-A01 (Page 3003)
Paragraph 2.F. Added the IPL figure and item numbers to the procedural steps.
All
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page TI-7 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Table of Highlights (Cont) Task/Page
Description of Change
Effectivity
Subtask 34-40-11-000-010-A01 (Page 3004)
Paragraph 2.G. Added the IPL figure and item numbers to the procedural steps.
All
Subtask 34-40-11-000-011-A01 (Page 3004)
Paragraph 2.H. Revised the paragraph title and added the IPL figure and item numbers to the procedural steps.
All
Subtask 34-40-11-000-012-A01 (Page 3004)
Paragraph 2.I. Revised the paragraph title and added the IPL figure and item numbers to the procedural steps.
All
CLEANING
Reformatted section to the latest template format.
All
Subtask 34-40-11-99C-009-A01 (Page 4001)
Paragraph 1.B. Revised Table 4002 to include the required consumables.
All
INSPECTION/CHECK
Reformatted section to the latest template format.
All
REPAIR
Reformatted section to the latest template format.
All
Subtask 34-40-11-99C-013-A01 (Page 6001)
Paragraph 1.B. Revised Table 6002 to include the required consumables.
All
Subtask 34-40-11-300-004-A01 (Page 6003)
Paragraph 2.D. Added paragraph in accordance with Service Aid 601-07790-0030 (SA ART 2000-104).
All
ASSEMBLY
Reformatted section to the latest template format.
All
Subtask 34-40-11-99C-015-A01 (Page 7001)
Paragraph 1.B. Revised Table 7001 to include the required equipment.
All
Subtask 34-40-11-99C-015-A01 (Page 7001)
Paragraph 1.B. Revised Table 7002 to include the required consumables.
All
Subtask 34-40-11-400-002-A01 (Page 7003)
Paragraph 2.B. Revised the paragraph title and added the IPL figure and item numbers to the procedural steps.
All
Subtask 34-40-11-400-003-A01 (Page 7003)
Paragraph 2.C. Revised the paragraph title and added the IPL figure and item numbers to the procedural steps.
All
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page TI-8 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Table of Highlights (Cont) Task/Page
Description of Change
Effectivity
Subtask 34-40-11-400-004-A01 (Page 7004)
Paragraph 2.D. Added the IPL figure and item numbers to the procedural steps.
All
Subtask 34-40-11-400-004-A01 (Page 7004)
Paragraph 2.D. Added a reference to the magnetron replacement kit.
All
Subtask 34-40-11-400-004-A01 (Page 7004)
Paragraph 2.D. Added the magnetron high-voltage wiring instructions in accordance with the magnetron installation instructions provided as part of the magnetron replacement kit.
All
GRAPHIC 34-40-11-99B-878-A01 (Page 7006)
Figure 7001. Added High-Voltage Splice.
All
Subtask 34-40-11-400-005-A01 (Page 7008)
Paragraph 2.E. Added the IPL figure and item numbers to the procedural steps.
All
Subtask 34-40-11-400-006-A01 (Page 7009)
Paragraph 2.F. Added the IPL figure and item numbers to the procedural steps.
All
Subtask 34-40-11-400-007-A01 (Page 7010)
Paragraph 2.G. Revised the paragraph title and added the IPL figure and item numbers to the procedural steps.
All
Subtask 34-40-11-400-008-A01 (Page 7010)
Paragraph 2.H. Added the IPL figure and item numbers to the procedural steps.
All
Subtask 34-40-11-400-009-A01 (Page 7011)
Paragraph 2.I. Revised the paragraph title and added the IPL figure and item numbers to the procedural steps.
All
FITS AND CLEARANCES
Added FITS AND CLEARANCES section in accordance with the latest template format.
All
Subtask 34-40-11-220-002-A01 (Page 8001)
Paragraph 2.B. Added the fits and clearances to Table 8001.
All
Subtask 34-40-11-220-004-A01 (Page 8002)
Paragraph 2.D. Added the torque requirements to Table 8004.
All
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table of Highlights (Cont) Task/Page
Description of Change
Effectivity
SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES
Reformatted section to the latest template format.
All
Subtask 34-40-11-940-001-A01 (Page 9001)
Paragraph 1.B. Revised Table 9001 to include the required test equipment.
All
Subtask 34-40-11-940-001-A01 (Page 9001)
Paragraph 1.B. Revised Table 9002 to include the required consumables.
All
Subtask 34-40-11-490-002-A01 (Page 9004)
Paragraph 2.B. Added manufacturing instructions for the test harness/tester.
All
GRAPHIC 34-40-11-99B-881-A01 (Page 9004)
Figure 9001. Revised to include the latest data.
All
STORAGE (INCLUDING TRANSPORTATION)
Added STORAGE (INCLUDING TRANSPORTATION) section in accordance with the latest template format.
All
ILLUSTRATED PARTS LIST Reformatted section to the latest template format.
All
ILLUSTRATED PARTS LIST Renumbered Figure 2 thru Figure 14 as IPL Figure 1 thru IPL Figure 13 to conform to the latest ATA and template format.
All
ILLUSTRATED PARTS LIST Added item numbers in disassembly order.
All
ILLUSTRATED PARTS LIST IPL Figure 1, added pre/post notes to items 135, 135A, 140, and 140A to incorporate Service Bulletin 600-07790-0030 (SB ART 2000-3).
All
ILLUSTRATED PARTS LIST IPL Figure 2, added pre/post notes to items 215 and 215A to incorporate Service Bulletin 600-07790-0071 (SB ART 2000-7), and added pre/post notes items 810 and 810A to incorporate Service Bulletin 600-07790-0060 (SB ART 2000-6).
All
ILLUSTRATED PARTS LIST Added IPL Figure 2A, added pre/post notes to items 810 and 810A to incorporate Service Bulletin 600-07790-0060 (SB ART 2000-6), and added post note to item 815 to incorporate Software Bulletin 605-07790-0050 (SWB ART 2000-SW5).
All
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table of Highlights (Cont) Task/Page
Description of Change
Effectivity
ILLUSTRATED PARTS LIST Added IPL Figure 3A, added post note to item 20 to incorporate Service Aid 901-07790-0020 (SA ART 2000-102), and added pre/post notes to items 490 and 490A to incorporate Service Bulletin 600-07790-0090 (SB ART 2000-9).
All
ILLUSTRATED PARTS LIST IPL Figure 4, added pre/post notes to items 25 and 25A to incorporate Service Bulletin 600-07790-0030 (SB ART 2000-3).
All
ILLUSTRATED PARTS LIST Added IPL Figure 5A.
All
ILLUSTRATED PARTS LIST IPL Figure 9, added pre/post notes to items 50 and 50A to incorporate Service Bulletin 600-07791-0011 (SB ART 2000-11), and added item 175A to incorporate Service Aid 601-07790-0070 (SA ART 2000-107).
All
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
RECORD OF REVISIONS For each revision, write the revision number, revision date, date put in the manual, and your initials in the applicable column. NOTE:
Refer to the Revision History in the TRANSMITTAL INFORMATION section for revision data.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519
RECORD OF TEMPORARY REVISIONS Instructions on each page of a temporary revision tell you where to put the pages in your manual. Remove the temporary revision pages only when discard instructions are given. For each temporary revision, put the applicable data in the record columns on this page. Definition of Status column: TR may be active, cancelled, or incorporated. If TR is incorporated list the revision number. For example enter: INC Rev 7. If TR is replaced by another TR then put “Cancelled”. For example: Cancelled by TR NN-NN. “Active” is entered by the holder of manual.
Temporary Revision Number Status
EFFECTIVITY ALL
Page Number
Issue Date
Date Put in Manual
By
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Date Removed from Manual
By
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COMPONENT MAINTENANCE MANUAL 071-01519
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EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
SERVICE BULLETIN LIST Service Bulletin / Revision Number
Title
Modification
Date Put in Manual
600-07790-0010 (SB ART 2000-1)
Improve grounding of U5 and U6 of the power supply/modulator board.
1
1 Jun 2002
600-07790-0020 (SB ART 2000-2)
Elimination of inaccurate antenna fault messages (as they appear on the screen).
2
1 Jun 2002
600-07790-0030 (SB ART 2000-3)
Factory Mod changing logic board.
3
1 Jun 2002
600-07790-0041 (SB ART 2000-4)
Improves radar stabilization accuracy during small inputs of pitch and roll from the gyro.
4
1 Jun 2002
600-07790-0050 (SB ART 2000-5)
Incorporates new extended STC curves.
5
1 Jun 2002
600-07790-0060 (SB ART 2000-6)
Improves the ARL circuit.
6
1 Jun 2002
600-07790-0071 (SB ART 2000-7) with Revision 1
Replaces the J5001 connector with a more robust connector.
7
1 Jun 2002
600-07790-0080 (SB ART 2000-8)
Lowers voltage applied to U15 to reduce risk of blowing fuse F1.
8
1 Jun 2002
600-07790-0090 (SB ART 2000-9)
Replaces the capacitor C4019, PN 096-01082-0065, with a more robust capacitor, PN 097-00238-0093, on the power supply/modulator board.
9
3 Jan 2012
600-07791-0000 (SB ART 2000-10)
Replaces the pivot pins and the pivot pin nuts to prevent wear on the IF cable.
10
3 Jan 2012
600-07791-0011 (SB ART 2000-11)
Replaces the pitch/tilt motor assembly, PN 200-05173-0000, with PN 200-05173-0010 to prevent breaking of the wire leads on the pitch/tilt motor assembly.
11
3 Jan 2012
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Service Bulletin / Revision Number
Title
Modification
Date Put in Manual
600-07791-0020 (ART 2000-34-0012)
Replaces U5005, PN 53001233-1, with PN 53002736-1 on the logic board to make sure that the antenna parks correctly when the unit is put in the off position, and to make better accuracy of the maintenance logs for the EFIS display.
12
3 Jan 2012
601-07790-0020 (SA ART 2000-102)
Adds an insulator to the power supply/modulator board to prevent shorting between the leads on the power supply and the IF cover on the logic board.
3 Jan 2012
601-07790-0030 (SA ART 2000-103)
Replaces an obsolete part U5091, PN 120-08030-0002, with new PN 120-08030-0010 on the logic board.
3 Jan 2012
601-07790-0040 (SA ART 2000-104)
Clarifies the ART 2000 alignment procedures.
3 Jan 2012
601-07790-0050 (SA ART 2000-105)
Corrects the maintenance manual return-to-service procedure.
3 Jan 2012
601-07790-0060 (SA ART 2000-106)
Corrects the washer installation in the pitch drive assembly.
3 Jan 2012
601-07790-0070 (SA ART 2000-107)
Authorizes the use of the X-band limiter, PN 015-00313-0001, in the ART 2000.
3 Jan 2012
601-07790-0080 (SA ART 2000-108)
Corrects the maintenance manual return-to-service procedure.
3 Jan 2012
601-07791-0000 (SA ART 2000-110)
Changes the operating procedures to correct the shut-down procedures because of obsolete parts.
3 Jan 2012
601-07791-0010 (SA ART 2000-111)
Replaces R5066 with new PN 139-01652-0000 and R5166 with new PN 139-01502-0000 on the logic board to improve the AFC circuits.
3 Jan 2012
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Service Bulletin / Revision Number
Title
Modification
Date Put in Manual
605-07790-0010 (SWB ART 2000-1)
Replaces U5003 with PN 122-01338-0105 on the logic board to prevent the display of TX failures.
3 Jan 2012
605-07790-0021 (SWB ART 2000-SW2)
ART 2000, PN 071-01519-0101, Serial No. 2020 and below.
1 Jun 2002
605-07790-0031 (SWB ART 2000-SW3)
Replaces U5003 with PN 122-01338-0107 on the logic board to improve radar stabilization performance by optimizing the antenna startup positioning, and increasing the resolution in the stabilization algorithms. Supercedes Software Bulletin 605-07790-0021 (SWB ART 2000-SW2).
3 Jan 2012
605-07790-0041 (SWB ART 2000-SW4)
ART 2000, PN 071-01519-0101, Serial No. 2190 and below.
1 Jun 2002
605-07790-0050 (SWB ART 2000-SW5)
Replaces U5003 with PN 122-01338-0109 on the logic board to improve radar stabilization performance and AGC performance under multiple extreme environmental conditions.
3 Jan 2012
D200904000001 (ART 2000-34-13)
NAVIGATION - ART 2000 COLOR WEATHER RADAR RECEIVER/TRANSMITTER (ART 2000) - ART 2000, PN 071-01519-0101; Loose Hardware on the Radio Frequency (RF) Network, PN 015-00250-0000.
3 Jan 2012
D200906000080 (ART 2000-34-14)
NAVIGATION - ART 2000 COLOR WEATHER RADAR ANTENNA/RECEIVER/TRANSMITTER (ART 2000) - Unit Modification (MOD) 13 to ART 2000, PN 071-01519-0101; Correct Nonlinear Response to the Manual Gain Control Caused by the Installation of MOD 12.
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13
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3 Jan 2012
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COMPONENT MAINTENANCE MANUAL 071-01519
LIST OF EFFECTIVE PAGES Subheading and Page
Date
Title T-1 T-2 T-3 T-4
3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012
Transmittal Information TI-1 TI-2 TI-3 TI-4 TI-5 TI-6 TI-7 TI-8 TI-9 TI-10 TI-11 TI-12
* * * * * * * * * * * *
3 3 3 3 3 3 3 3 3 3 3 3
Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012
Record of Revisions RR-1 RR-2
3 Jan 2012 3 Jan 2012
Record of Temporary Revisions RTR-1 RTR-2
* 3 Jan 2012 * 3 Jan 2012
Service Bulletin List SBL-1 SBL-2 SBL-3 SBL-4
* * * *
3 3 3 3
Jan 2012 Jan 2012 Jan 2012 Jan 2012
* * * * * *
3 3 3 3 3 3
Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012
List of Effective Pages LEP-1 LEP-2 LEP-3 LEP-4 LEP-5 LEP-6
Subheading and Page LEP-7 LEP-8
Date * 3 Jan 2012 * 3 Jan 2012
Table of Contents TC-1 TC-2 TC-3 TC-4 TC-5 TC-6 TC-7 TC-8 TC-9 TC-10 TC-11 TC-12 TC-13 TC-14
* * * * * * * * * * * * * *
3 3 3 3 3 3 3 3 3 3 3 3 3 3
Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012
Introduction INTRO-1 INTRO-2 INTRO-3 INTRO-4 INTRO-5 INTRO-6 INTRO-7 INTRO-8 INTRO-9 INTRO-10 INTRO-11 INTRO-12 INTRO-13 INTRO-14 INTRO-15 INTRO-16 INTRO-17 INTRO-18 INTRO-19 INTRO-20
* 3 Jan 2012 * 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012
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COMPONENT MAINTENANCE MANUAL 071-01519
LIST OF EFFECTIVE PAGES (Cont) Subheading and Page INTRO-21 INTRO-22
Date * 3 Jan 2012 * 3 Jan 2012
Description and Operation
F F F F F
1 2 3 4 5 6 7 8 9 10 11 12 13/14 15/16 17/18 19/20 21/22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41
3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 * 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012
Subheading and Page 42 43 44
Date 3 Jan 2012 3 Jan 2012 3 Jan 2012
Testing and Fault Isolation 1001 1002 1003 1004 1005 1006 1007 1008 1009 1010 1011 1012 1013 1014 1015 1016 1017 1018 1019 1020 1021 1022 1023 1024 1025 1026 1027 1028 1029 1030 1031 1032 1033 1034 1035
* 3 Jan 2012 * 3 Jan 2012 3 Jan 2012 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012
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COMPONENT MAINTENANCE MANUAL 071-01519
LIST OF EFFECTIVE PAGES (Cont) Subheading and Page 1036 1037 1038 1039 1040 1041 1042 1043 1044 1045 1046 1047 1048 1049 1050 1051 1052 1053 1054 1055 1056 1057 1058 1059 1060 1061 1062 1063 1064 1065 1066 1067 1068 1069 1070 1071 1072 1073 1074
Date 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3
Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012
Subheading and Page 1075 1076 1077 1078 1079 1080 1081 1082 1083 1084 1085 1086 1087 1088 1089 1090
Date
* *
* *
3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012
Schematic and Wiring Diagrams
F F
F F F F F F F F F F F F F F
2001 2002 2003 2004 2005/2006 2007/2008 2009 2010 2011/2012 2013/2014 2015/2016 2017/2018 2019/2020 2021/2022 2023/2024 2025/2026 2027/2028 2029/2030 2031/2032 2033/2034 2035/2036 2037/2038
* 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012
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COMPONENT MAINTENANCE MANUAL 071-01519
LIST OF EFFECTIVE PAGES (Cont) Subheading and Page F F F F F
F F F F F F F F F F F F F F F F F F F F
F
F F
F F
2039/2040 2041/2042 2043/2044 2045/2046 2047/2048 2049 2050 2051/2052 2053/2054 2055/2056 2057/2058 2059/2060 2061/2062 2063/2064 2065/2066 2067/2068 2069/2070 2071/2072 2073/2074 2075/2076 2077/2078 2079/2080 2081/2082 2083/2084 2085/2086 2087/2088 2089/2090 2091 2092 2093/2094 2095 2096 2097/2098 2099/2100 2101 2102 2103/2104 2105/2106 2107
Date * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * *
3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012
Subheading and Page
F F F F F F F F F F F F
F F F F F F F F F F F F
F
F F
2108 2109/2110 2111/2112 2113/2114 2115/2116 2117/2118 2119/2120 2121/2122 2123/2124 2125/2126 2127/2128 2129/2130 2131/2132 2133 2134 2135/2136 2137/2138 2139/2140 2141/2142 2143/2144 2145/2146 2147/2148 2149/2150 2151/2152 2153/2154 2155/2156 2157/2158 2159 2160 2161/2162 2163 2164 2165/2166 2167/2168 2169 2170
Date
* * * * * * * * * * * * * * * * * * * * * * * * * * * * * *
3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012
Disassembly 3001 3002
* 3 Jan 2012 * 3 Jan 2012
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COMPONENT MAINTENANCE MANUAL 071-01519
LIST OF EFFECTIVE PAGES (Cont) Subheading and Page 3003 3004 3005 3006
Date
Subheading and Page 8003 8004
* 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 3 Jan 2012 3 Jan 2012 * 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012
F
9001 9002 9003 9004 9005/9006 9007 9008
* 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 3 Jan 2012 * 3 Jan 2012 3 Jan 2012 3 Jan 2012
Special Procedures
Inspection/Check 5001 5002 5003 5004
3 3 3 3
Jan 2012 Jan 2012 Jan 2012 Jan 2012
Repair 6001 6002 6003 6004
* 3 Jan 2012 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012
Assembly 7001 7002 7003 7004 7005 7006 7007 7008 7009 7010 7011 7012
* * * * * * * * * *
3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012
Fits and Clearances 8001 8002
* 3 Jan 2012 3 Jan 2012
Special Tools, Fixtures, Equipment, and Consumables
Cleaning 4001 4002 4003 4004 4005 4006
Date
* 3 Jan 2012 * 3 Jan 2012
11001 11002
3 Jan 2012 3 Jan 2012
Removal 12001 12002
3 Jan 2012 3 Jan 2012
Installation 13001 13002
3 Jan 2012 3 Jan 2012
Servicing 14001 14002
3 Jan 2012 3 Jan 2012
Storage (Including Transportation) 15001 15002
3 Jan 2012 3 Jan 2012
Rework (Service Bulletin Accomplishment Procedures) 16001 16002
3 Jan 2012 3 Jan 2012
Illustrated Parts List 10001 10002 10003 10004 10005
3 3 3 3 3
Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012
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COMPONENT MAINTENANCE MANUAL 071-01519
LIST OF EFFECTIVE PAGES (Cont) Subheading and Page 10006 10007 10008 10009 10010 10011 10012 10013 10014 10015 10016 10017 10018 10019 10020 10021 10022 10023 10024 10025 10026 10027 10028 10029 10030 10031 10032 10033 10034 10035 10036 10037 10038 10039 10040 10041 10042 10043 10044
Date 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3 3
Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012 Jan 2012
Subheading and Page
LF LF LF
10045 10046 10047 10048 10049 10050 10051 10052 10053 10054 10055 10056 10057 10058 10059 10060 10061 10062 10063 10064 10065 10066 10067 10068 10069 10070 10071 10072 10073/10074 10075/10076 10077/10078 10079 10080 10081 10082 10083 10084 10085 10086
Date
* * * * * * * * * * * * * * * * * *
3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012
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COMPONENT MAINTENANCE MANUAL 071-01519
LIST OF EFFECTIVE PAGES (Cont) Subheading and Page
LF LF LF
10087 10088 10089 10090 10091 10092 10093 10094 10095 10096 10097 10098 10099 10100 10101 10102 10103 10104 10105/10106 10107/10108 10109/10110 10111 10112 10113 10114 10115 10116 10117 10118 10119 10120 10121 10122 10123 10124 10125 10126 10127 10128
Date * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * *
3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012
Subheading and Page
LF LF LF
LF LF LF
10129 10130 10131 10132 10133 10134 10135 10136 10137/10138 10139/10140 10141/10142 10143 10144 10145 10146 10147 10148 10149 10150 10151 10152 10153 10154 10155 10156 10157 10158 10159 10160 10161 10162 10163 10164 10165/10166 10167/10168 10169/10170 10171 10172 10173
Date * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * *
3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012
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COMPONENT MAINTENANCE MANUAL 071-01519
LIST OF EFFECTIVE PAGES (Cont) Subheading and Page
LF
LF
LF
10174 10175 10176 10177 10178 10179 10180 10181 10182 10183 10184 10185 10186 10187 10188 10189 10190 10191 10192 10193 10194 10195/10196 10197 10198 10199/10200 10201 10202 10203/10204 10205 10206
Date * * * * * * * * * * * * * * * * * * * * * * * * * * * * * *
3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012 3 Jan 2012
Subheading and Page
LF
LF
LF
LF
LF
LF
LF
LF
10207 10208 10209/10210 10211 10212 10213/10214 10215 10216 10217/10218 10219 10220 10221 10222 10223/10224 10225 10226 10227 10228 10229/10230 10231 10232 10233/10234 10235 10236 10237/10238 10239 10240 10241/10242 10243 10244
Date * 3 Jan 2012 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012 * 3 Jan 2012
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COMPONENT MAINTENANCE MANUAL 071-01519
TABLE OF CONTENTS LIST OF SECTIONS Title
Page
INTRODUCTION 1.
2.
How to Use This Manual (TASK 34-40-11-99F-801-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-1
A.
General (Subtask 34-40-11-99F-001-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-1
B.
Observance of Manual Instructions (Subtask 34-40-11-99F-002-A01) . . . . . . . . . .
INTRO-3
C.
Symbols (Subtask 34-40-11-99F-003-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-3
D.
Units of Measure (Subtask 34-40-11-99F-004-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-3
E.
Page Number Block Explanation (Subtask 34-40-11-99F-005-A01) . . . . . . . . . . . . .
INTRO-3
F.
Illustration (Subtask 34-40-11-99F-006-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-4
G.
Application of Maintenance Task Oriented Support System (MTOSS) (Subtask 34-40-11-99F-007-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-4
H.
Standard Practices Manual (Subtask 34-40-11-99F-008-A01) . . . . . . . . . . . . . . . . . . .
INTRO-14
I.
Electrostatic Discharge (Subtask 34-40-11-99F-009-A01) . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-14
Customer Support (TASK 34-40-11-99F-802-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-14
A.
Honeywell Aerospace Online Technical Publications Web Site (Subtask 34-40-11-99F-010-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-14
Global Customer Care Center (Subtask 34-40-11-99F-011-A01) . . . . . . . . . . . . . . . .
INTRO-14
References (TASK 34-40-11-99F-803-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-14
A.
Honeywell/Vendor Publications (Subtask 34-40-11-99F-012-A01) . . . . . . . . . . . . . . .
INTRO-14
B.
Other Publications (Subtask 34-40-11-99F-013-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-15
Component Maintenance Levels (TASK 34-40-11-99F-804-A01) . . . . . . . . . . . . . . . . . . . . . .
INTRO-15
A.
General (Subtask 34-40-11-99F-014-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-15
Acronyms and Abbreviations (TASK 34-40-11-99F-805-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-16
A.
General (Subtask 34-40-11-99F-015-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-16
Process Verification (TASK 34-40-11-99F-806-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-20
A.
Verification Data (Subtask 34-40-11-99F-016-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-20
B.
Environmental Certification (Subtask 34-40-11-870-001-A01) . . . . . . . . . . . . . . . . . . . .
INTRO-20
Software History (TASK 34-40-11-99F-807-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-21
A.
Software Data (Subtask 34-40-11-99F-017-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-21
History of Changes (TASK 34-40-11-99F-808-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-22
A.
INTRO-22
B. 3.
4.
5.
6.
7.
8.
Modification/Configuration History (Subtask 34-40-11-99F-018-A01) . . . . . . . . . . . .
DESCRIPTION AND OPERATION 1.
Description (TASK 34-40-11-870-801-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
1
Page TC-1 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
TABLE OF CONTENTS (Cont) LIST OF SECTIONS (Cont) Title
Page
2.
A.
General (Subtask 34-40-11-870-002-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
B.
Job Setup Data (Subtask 34-40-11-99C-001-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4
C.
Mechanical Description (Subtask 34-40-11-870-003-A01) . . . . . . . . . . . . . . . . . . . . . . . .
4
D.
Electrical Description (Subtask 34-40-11-870-004-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . .
5
Operation (TASK 34-40-11-870-802-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6
A.
Block Diagram Theory (Subtask 34-40-11-870-005-A01) . . . . . . . . . . . . . . . . . . . . . . . . .
6
B.
Detailed Theory of Operation (Subtask 34-40-11-870-006-A01) . . . . . . . . . . . . . . . . .
23
TESTING AND FAULT ISOLATION 1.
2.
3.
4.
Planning Data (TASK 34-40-11-99C-801-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1001
A.
Reason for the Job (Subtask 34-40-11-99C-002-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1001
B.
Job Setup Data (Subtask 34-40-11-99C-003-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1001
Procedure (TASK 34-40-11-810-801-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1003
A.
General (Subtask 34-40-11-810-001-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1003
B.
Test Setup (Subtask 34-40-11-810-002-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1003
Functional Test Procedures (TASK 34-40-11-810-802-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1005
A.
Return-to-Service Test (Subtask 34-40-11-810-003-A01) . . . . . . . . . . . . . . . . . . . . . . . . .
1005
Troubleshooting Procedures (TASK 34-40-11-810-803-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . .
1012
A.
Purpose (Subtask 34-40-11-810-004-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1012
B.
Viewing System Errors with an EFIS (Subtask 34-40-11-810-005-A01) . . . . . . . . .
1012
C.
Viewing System Errors with an Indicator (Subtask 34-40-11-810-006-A01) . . . . .
1013
D.
ART 2000 Logic Board Troubleshooting Procedures (Subtask 34-40-11-810007-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1014
ART 2000 Power Supply Board Troubleshooting Procedures (Subtask 34-4011-810-008-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1035
Alignment Procedures (TASK 34-40-11-810-804-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1082
A.
General (Subtask 34-40-11-810-009-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1082
B.
Pre-alignment Set-up Procedures (Subtask 34-40-11-810-010-A01) . . . . . . . . . . . .
1082
C.
Magnetron Current Set (Subtask 34-40-11-810-011-A01) . . . . . . . . . . . . . . . . . . . . . . . .
1083
D.
59 MHz IF Alignment (Subtask 34-40-11-810-012-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . .
1083
E.
Receiver Calibration (Subtask 34-40-11-810-013-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . .
1084
F.
AFC Calibration with Software Greater than 0103 (Subtask 34-40-11-810-014A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1084
E. 5.
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page TC-2 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
TABLE OF CONTENTS (Cont) LIST OF SECTIONS (Cont) Title
Page G. 6.
7.
Detector Calibration with Software Greater than 0103 (Subtask 34-40-11-810015-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1084
Retest Procedure (TASK 34-40-11-810-805-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1086
A.
General (Subtask 34-40-11-810-016-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1086
Service Information (TASK 34-40-11-810-806-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1086
A.
Proper Test Equipment Usage (Subtask 34-40-11-810-017-A01) . . . . . . . . . . . . . . . .
1086
B.
Capacitor Testing (Subtask 34-40-11-810-018-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1086
C.
Transistor Testing (Subtask 34-40-11-810-019-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1087
D.
Integrated Circuit Testing (Subtask 34-40-11-810-020-A01) . . . . . . . . . . . . . . . . . . . . . .
1088
E.
Job Close-up (Subtask 34-40-11-810-021-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1090
SCHEMATIC AND WIRING DIAGRAMS 1.
2.
Planning Data (TASK 34-40-11-99C-802-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2001
A.
Reason for the Job (Subtask 34-40-11-99C-004-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2001
B.
Job Setup Data (Subtask 34-40-11-99C-005-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2001
Outline/Schematic Diagrams (TASK 34-40-11-000-801-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . .
2002
A.
Job Setup (Subtask 34-40-11-000-001-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2002
B.
Outline and Detail/Schematic Diagrams (Subtask 34-40-11-000-002-A01) . . . . .
2002
C.
Job Close-up (Subtask 34-40-11-000-003-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2169
Planning Data (TASK 34-40-11-99C-803-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3001
A.
Reason for the Job (Subtask 34-40-11-99C-006-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3001
B.
Job Setup Data (Subtask 34-40-11-99C-007-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3001
Procedure (TASK 34-40-11-000-802-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3002
A.
Job Setup (Subtask 34-40-11-000-004-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3002
B.
Bottom Cover Removal (Subtask 34-40-11-000-005-A01) . . . . . . . . . . . . . . . . . . . . . . . .
3002
C.
Logic Board Removal (Subtask 34-40-11-000-006-A01) . . . . . . . . . . . . . . . . . . . . . . . . . .
3002
D.
Power Supply/Modulator Board Removal (Subtask 34-40-11-000-007-A01) . . . .
3003
E.
Receiver Module Removal (Subtask 34-40-11-000-008-A01) . . . . . . . . . . . . . . . . . . . .
3003
F.
Preamp Board Removal (Subtask 34-40-11-000-009-A01) . . . . . . . . . . . . . . . . . . . . . . .
3003
G.
Magnetron Removal (Subtask 34-40-11-000-010-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . .
3004
H.
Azimuth Motor Assembly Removal (Subtask 34-40-11-000-011-A01) . . . . . . . . . . .
3004
I.
Pitch Motor Assembly Removal (Subtask 34-40-11-000-012-A01) . . . . . . . . . . . . . . .
3004
DISASSEMBLY 1.
2.
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519
TABLE OF CONTENTS (Cont) LIST OF SECTIONS (Cont) Title
Page J.
Job Close-up (Subtask 34-40-11-000-013-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3005
Planning Data (TASK 34-40-11-99C-804-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4001
A.
Reason for the Job (Subtask 34-40-11-99C-008-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4001
B.
Job Setup Data (Subtask 34-40-11-99C-009-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4001
Procedure (TASK 34-40-11-100-801-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4002
A.
Job Setup (Subtask 34-40-11-100-001-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4002
B.
External Parts (Subtask 34-40-11-100-002-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4003
C.
Electrical Parts (Subtask 34-40-11-100-003-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4003
D.
Metal Mechanical Parts (Subtask 34-40-11-100-004-A01) . . . . . . . . . . . . . . . . . . . . . . . .
4003
E.
Internal Parts (Subtask 34-40-11-100-005-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4004
F.
Job Close-up (Subtask 34-40-11-100-006-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4005
CLEANING 1.
2.
INSPECTION/CHECK 1.
2.
Planning Data (TASK 34-40-11-99C-805-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5001
A.
Reason for the Job (Subtask 34-40-11-99C-010-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5001
B.
Job Setup Data (Subtask 34-40-11-99C-011-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5001
Procedure (TASK 34-40-11-210-801-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5002
A.
Job Setup (Subtask 34-40-11-210-001-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5002
B.
General Inspection/Check Procedure of the ART 2000 (Subtask 34-40-11-210002-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5002
Job Close-up (Subtask 34-40-11-210-003-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5003
Planning Data (TASK 34-40-11-99C-806-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6001
A.
Reason for the Job (Subtask 34-40-11-99C-012-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6001
B.
Job Setup Data (Subtask 34-40-11-99C-013-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6001
Procedure (TASK 34-40-11-300-801-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6002
A.
Job Setup (Subtask 34-40-11-300-001-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6002
B.
References for Repair (Subtask 34-40-11-300-002-A01) . . . . . . . . . . . . . . . . . . . . . . . . .
6002
C.
General Repair Instructions (Subtask 34-40-11-300-003-A01) . . . . . . . . . . . . . . . . . . .
6003
D.
Special Repair Instructions (Subtask 34-40-11-300-004-A01) . . . . . . . . . . . . . . . . . . . .
6003
E.
Job Close-up (Subtask 34-40-11-300-005-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6004
C. REPAIR 1.
2.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
TABLE OF CONTENTS (Cont) LIST OF SECTIONS (Cont) Title
Page
ASSEMBLY 1.
2.
Planning Data (TASK 34-40-11-99C-807-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
7001
A.
Reason for the Job (Subtask 34-40-11-99C-014-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
7001
B.
Job Setup Data (Subtask 34-40-11-99C-015-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
7001
Procedure (TASK 34-40-11-400-801-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
7002
A.
Job Setup (Subtask 34-40-11-400-001-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
7002
B.
Pitch Motor Assembly Installation (Subtask 34-40-11-400-002-A01) . . . . . . . . . . . .
7003
C.
Azimuth Motor Assembly Installation (Subtask 34-40-11-400-003-A01) . . . . . . . . .
7003
D.
Magnetron Installation (Subtask 34-40-11-400-004-A01) . . . . . . . . . . . . . . . . . . . . . . . . .
7004
E.
Preamp Board Installation (Subtask 34-40-11-400-005-A01) . . . . . . . . . . . . . . . . . . . . .
7008
F.
Receiver Module Installation (Subtask 34-40-11-400-006-A01) . . . . . . . . . . . . . . . . . .
7009
G.
Power Supply/Modulator Board Installation (Subtask 34-40-11-400-007-A01) .
7010
H.
Logic Board Installation (Subtask 34-40-11-400-008-A01) . . . . . . . . . . . . . . . . . . . . . . . .
7010
I.
Bottom Cover Installation (Subtask 34-40-11-400-009-A01) . . . . . . . . . . . . . . . . . . . . . .
7011
J.
Job Close-up (Subtask 34-40-11-400-010-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
7011
FITS AND CLEARANCES 1.
2.
Planning Data (TASK 34-40-11-99C-808-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8001
A.
Reason for the Job (Subtask 34-40-11-99C-016-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8001
B.
Job Setup Data (Subtask 34-40-11-99C-017-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8001
Procedure (TASK 34-40-11-220-801-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8001
A.
Job Setup (Subtask 34-40-11-220-001-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8001
B.
Fits and Clearances of the ART 2000 (Subtask 34-40-11-220-002-A01) . . . . . . . .
8001
C.
Torque Values (Subtask 34-40-11-220-003-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8001
D.
Specified Torque Values (Subtask 34-40-11-220-004-A01) . . . . . . . . . . . . . . . . . . . . . . .
8002
E.
Job Close-up (Subtask 34-40-11-220-005-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8003
SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES 1.
2.
Planning Data (TASK 34-40-11-99C-809-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
9001
A.
Reason for the Job (Subtask 34-40-11-99C-018-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
9001
B.
Job Setup Data (Subtask 34-40-11-940-001-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
9001
Procedure (TASK 34-40-11-490-801-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
9004
A.
9004
EFFECTIVITY ALL
Job Setup (Subtask 34-40-11-490-001-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page TC-5 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
TABLE OF CONTENTS (Cont) LIST OF SECTIONS (Cont) Title
Page B.
Test Harness/Tester Manufacturing Instructions (Subtask 34-40-11-490-002A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
9004
C.
Job Close-up (Subtask 34-40-11-210-004-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
9007
SPECIAL PROCEDURES 1.
Not Applicable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
11001
REMOVAL 1.
Not Applicable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
12001
INSTALLATION 1.
Not Applicable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
13001
SERVICING 1.
Not Applicable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
14001
STORAGE (INCLUDING TRANSPORTATION) 1.
2.
Planning Data (TASK 34-40-11-99C-810-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15001
A.
Reason for the Job (Subtask 34-40-11-99C-019-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15001
B.
Job Setup Data (Subtask 34-40-11-99C-020-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15001
Procedure (TASK 34-40-11-550-801-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15001
A.
Job Setup (Subtask 34-40-11-550-001-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15001
B.
Storage (Subtask 34-40-11-550-002-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15001
C.
Job Close-up (Subtask 34-40-11-550-003-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15001
Not Applicable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
16001
REWORK 1.
ILLUSTRATED PARTS LIST 1.
Description (TASK 34-40-11-99C-811-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10001
A.
General (Subtask 34-40-11-99C-021-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10001
B.
Job Setup Data (Subtask 34-40-11-99C-022-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10001
Contents of the IPL (TASK 34-40-11-99C-812-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10001
A.
Vendor Code List (Subtask 34-40-11-99C-023-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10001
B.
EDI (Subtask 34-40-11-99C-024-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10001
C.
Numerical Index (Subtask 34-40-11-99C-025-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10001
D.
Detailed Parts List (Subtask 34-40-11-99C-026-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10002
3.
Vendor Code List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10009
4.
Detailed Parts List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10013
2.
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page TC-6 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
TABLE OF CONTENTS (Cont) LIST OF FIGURES Figure
Description
Page
INTRO-1
MPEL Boundary (GRAPHIC 34-40-11-99B-801-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-2
INTRO-2
Symbols (GRAPHIC 34-40-11-99B-802-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-3
INTRO-3
MTOSS Code Positions (GRAPHIC 34-40-11-99B-803-A01) . . . . . . . . . . . . . . . . . . . . . . .
INTRO-5
INTRO-4
DO-160C Environmental Qualification Form (GRAPHIC 34-40-11-99B-804-A01)
INTRO-21
1
Typical ART 2000 (GRAPHIC 34-40-11-99B-805-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3
2
ART 2000 Block Diagram (GRAPHIC 34-40-11-99B-806-A01) . . . . . . . . . . . . . . . . . . . . .
13
1001
Typical Test Setup (GRAPHIC 34-40-11-99B-807-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1004
1002
ART 2000 Test Data Sheet (GRAPHIC 34-40-11-99B-808-A01) . . . . . . . . . . . . . . . . . . . .
1006
1003
Access to DIP Switches (GRAPHIC 34-40-11-99B-809-A01) . . . . . . . . . . . . . . . . . . . . . . .
1011
1004
Normal Microprocessor and FPGA Turn-On (GRAPHIC 34-40-11-99B-810-A01)
1015
1005
FPGAs Programmed Correctly but Microprocessor is Inoperative (GRAPHIC 34-40-11-99B-811-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1016
1006
Start Sync of 453 Transmission (GRAPHIC 34-40-11-99B-812-A01) . . . . . . . . . . . . . . .
1017
1007
Stop Sync of 453 Transmission (GRAPHIC 34-40-11-99B-813-A01) . . . . . . . . . . . . . . .
1018
1008
Data Packet of 453 Transmission (GRAPHIC 34-40-11-99B-814-A01) . . . . . . . . . . . .
1019
1009
Received 429 Data (GRAPHIC 34-40-11-99B-815-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1020
1010
Discriminator Input to the Discriminator A/D Converter (GRAPHIC 34-40-1199B-816-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1022
1011
STC Curve and Manual Gain for Weather (GRAPHIC 34-40-11-99B-817-A01) . . .
1024
1012
STC Curve and Manual Gain for MAP (GRAPHIC 34-40-11-99B-818-A01) . . . . . . .
1025
1013
STC Curve and Manual Gain for Weather over Multiple MAG Fires (GRAPHIC 34-40-11-99B-819-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1026
1014
Weather Compensation Bit 0 (GRAPHIC 34-40-11-99B-820-A01) . . . . . . . . . . . . . . . . .
1027
1015
Extended STC Bit 0 (GRAPHIC 34-40-11-99B-821-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1028
1016
Compensated Weather Data Bit 3 (GRAPHIC 34-40-11-99B-822-A01) . . . . . . . . . . . .
1029
1017
Weather RAM Address 0 (GRAPHIC 34-40-11-99B-823-A01) . . . . . . . . . . . . . . . . . . . . . .
1030
1018
Radial Data Transfer from WX_RAM to 453_RAM (GRAPHIC 34-40-11-99B-824A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1031
1019
Reference, Pitch, and Roll Inputs (GRAPHIC 34-40-11-99B-825-A01) . . . . . . . . . . . .
1032
1020
Pitch Hall Sensor to MUX A/D Converter (GRAPHIC 34-40-11-99B-826-A01) . . . .
1034
1021
Azimuth Hall Sensor to MUX A/D Converter (GRAPHIC 34-40-11-99B-827-A01)
1035
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page TC-7 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
TABLE OF CONTENTS (Cont) LIST OF FIGURES (Cont) Figure 1022
Description
Page
Normal Operation of the +5 VDC Pulse Width Modulator U4005 (TP4010) (GRAPHIC 34-40-11-99B-828-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1037
Normal Operation of the +9.3 VDC Pulse Width Modulator U4006 (TP4011) (GRAPHIC 34-40-11-99B-829-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1038
Normal Operation of the -15 VDC Flyback Winding (T4005-4) (GRAPHIC 34-4011-99B-830-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1039
MAG_FIRE_OUT Pulse from Logic Board (U4020-2) (GRAPHIC 34-40-1199B-831-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1042
1026
Long Pulse Gate (U4020-13) (GRAPHIC 34-40-11-99B-832-A01) . . . . . . . . . . . . . . . . .
1043
1027
MAG Fire Pulse (TP4008) (GRAPHIC 34-40-11-99B-833-A01) . . . . . . . . . . . . . . . . . . . . .
1044
1028
Modulator Switch Drive (TP4005) (GRAPHIC 34-40-11-99B-834-A01) . . . . . . . . . . . .
1045
1029
Modulator Switch FET Gate (TP4004) (GRAPHIC 34-40-11-99B-835-A01) . . . . . . .
1046
1030
Modulator Transformer Primary Voltage (CR4005 Cathode) (GRAPHIC 34-4011-99B-836-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1047
Normal Signal for the HVPS Refresh Rate with MAG Current Set to 3 A, 100 Hz PRF Rate (Jct L4009-CR4004) (GRAPHIC 34-40-11-99B-837-A01) . . . . . . . . . . . . . . .
1048
Normal Signal at the Overvoltage Frequency Compensation Port of the HVPS PWM (TP4001) (GRAPHIC 34-40-11-99B-838-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1049
Normal Signal at the Oscillator Port of the HVPS PWM Controller (U4001-7) (GRAPHIC 34-40-11-99B-839-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1050
Normal Signal from the Output of the HVPS PWM Control to the Gate of Q4001 (U4001-10) (GRAPHIC 34-40-11-99B-840-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1051
Normal Flyback Signal at the HVPS Transformer Primary (TP4002) (GRAPHIC 34-40-11-99B-841-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1052
Normal Output Voltage from the HVPS Transformer Secondary (CR4001 Anode) (GRAPHIC 34-40-11-99B-842-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1053
Normal Signal Due to the Flyback Primary Current Flowing Through R4013 (Fly Current) (GRAPHIC 34-40-11-99B-843-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1054
Typical Current as Measured Through the Current Probe Cutout (Current Loop MAG Current) (GRAPHIC 34-40-11-99B-844-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1056
Magnetron Current Sense Delay Gate (TP4017) (GRAPHIC 34-40-11-99B-845A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1057
Magnetron Current Sense Gate (TP4016) (GRAPHIC 34-40-11-99B-846-A01) . .
1058
1023 1024 1025
1031 1032 1033 1034 1035 1036 1037 1038 1039 1040
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page TC-8 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
TABLE OF CONTENTS (Cont) LIST OF FIGURES (Cont) Figure 1041
Description
Page
Conditioned Magnetron Current Pulse (TP4020) (GRAPHIC 34-40-11-99B-847A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1059
1042
MISSING_PULSE Output (TP4015) (GRAPHIC 34-40-11-99B-848-A01) . . . . . . . . .
1060
1043
CONTROL_VOLTS Input to the HVPS PWM (TP4014) (GRAPHIC 34-40-1199B-849-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1061
Normal Current and Voltage Waveforms Expected at the Cathode of Q4007 (Jct R4014-C4012/R4014 Current) (GRAPHIC 34-40-11-99B-850-A01) . . . . . . . . . . . . . . . .
1065
Normal Current and Voltage Waveforms Expected Through CR4004 (Q4004 Drain/CR4004 Current) (GRAPHIC 34-40-11-99B-851-A01) . . . . . . . . . . . . . . . . . . . . . . . .
1066
Normal Current Expected Through the Primary of T4002 (L4009) (GRAPHIC 34-40-11-99B-852-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1067
FPGA Done Programming Pin High Upon Successful Loading of Stored ROM Program (U4011-80) (GRAPHIC 34-40-11-99B-853-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . .
1068
1048
1.025 MHz FPGA Clock (U4011-30) (GRAPHIC 34-40-11-99B-854-A01) . . . . . . . . .
1069
1049
Azimuth Current Limit Sine (U4013-2) (GRAPHIC 34-40-11-99B-855-A01) . . . . . . .
1070
1050
Azimuth Current Limit Cosine (U4013-1) (GRAPHIC 34-40-11-99B-856-A01) . . . .
1071
1051
Elevation Current Limit Sine (VP Mode, U4013-20) (GRAPHIC 34-40-1199B-857-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1072
Elevation Current Limit Cosine (VP Mode, U4013-19) (GRAPHIC 34-40-1199B-858-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1073
1053
Azimuth Current Sense Sine (U4034-10) (GRAPHIC 34-40-11-99B-859-A01) . . . .
1074
1054
Azimuth Current Sense Cosine (U4033-10) (GRAPHIC 34-40-11-99B-860-A01) .
1075
1055
Elevation Current Sense Sine (VP Mode, U4050-10) (GRAPHIC 34-40-1199B-861-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1076
Elevation Current Sense Cosine (VP Mode, U4049-10) (GRAPHIC 34-40-1199B-862-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1077
1057
Azimuth Current Reset (Sine, U4012-2) (GRAPHIC 34-40-11-99B-863-A01) . . . . .
1078
1058
Azimuth Current Reset (Cosine, U4012-1) (GRAPHIC 34-40-11-99B-864-A01) . .
1079
1059
Elevation Current Reset (Sine, VP Mode, U4012-14) (GRAPHIC 34-40-1199B-865-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1080
1060
Elevation Current Reset (Cosine, U4012-13) (GRAPHIC 34-40-11-99B-866-A01)
1081
2001
ART 2000 Outline Drawing (GRAPHIC 34-40-11-99B-867-A01) . . . . . . . . . . . . . . . . . . . .
2005
1044 1045 1046 1047
1052
1056
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519
TABLE OF CONTENTS (Cont) LIST OF FIGURES (Cont) Figure 2002
Description
Page
ART 2000 P5001 Connector Pin Function Diagram (GRAPHIC 34-40-1199B-868-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2009
Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-1199B-869-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2011
Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-1199B-870-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2051
Receiver Assembly, PN 200-05553-0001, Detail (GRAPHIC 34-40-11-99B-871A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2093
Preamp Board, PN 200-08545-0000, Detail/Schematic (GRAPHIC 34-40-1199B-872-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2097
Preamp Board, PN 200-08545-0020, Detail/Schematic (GRAPHIC 34-40-1199B-873-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2103
Power Supply/Modulator Board, PN 200-08548-0000, Detail /Schematic (GRAPHIC 34-40-11-99B-874-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2109
Power Supply/Modulator Board, PN 200-08548-0020, Detail /Schematic (GRAPHIC 34-40-11-99B-875-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2135
Configuration Module Assembly, PN 071-00097-0100, Detail (GRAPHIC 34-4011-99B-876-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2161
Configuration Module, PN 200-08705-0000, Detail/Schematic (GRAPHIC 34-4011-99B-877-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2165
7001
High-Voltage Splice (GRAPHIC 34-40-11-99B-878-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . .
7006
7002
Magnetron Cable Dressing (GRAPHIC 34-40-11-99B-879-A01) . . . . . . . . . . . . . . . . . . . .
7007
7003
Magnetron and Preamp Cable Dressing (GRAPHIC 34-40-11-99B-880-A01) . . . . .
7008
9001
Test Harness/Tester (GRAPHIC 34-40-11-99B-881-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . .
9005
10001
DPL Example (GRAPHIC 34-40-11-99B-882-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10006
1
ART 2000 Final Assembly (GRAPHIC 34-40-11-99B-883-A01) . . . . . . . . . . . . . . . . . . . . .
10066
2
Logic Board (-0000) (GRAPHIC 34-40-11-99B-884-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10073
2A
Logic Board (-0020) (GRAPHIC 34-40-11-99B-885-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10105
3
Power Supply/Modulator Board (-0000) (GRAPHIC 34-40-11-99B-886-A01) . . . . .
10137
3A
Power Supply/Modulator Board (-0020) (GRAPHIC 34-40-11-99B-887-A01) . . . . .
10165
4
Receiver Assembly (GRAPHIC 34-40-11-99B-888-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10195
2003 2004 2005 2006 2007 2008 2009 2010 2011
IPL Figure
EFFECTIVITY ALL
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TABLE OF CONTENTS (Cont) LIST OF FIGURES (Cont) Figure
Description
Page
5
Preamp Board Assembly (-0000) (GRAPHIC 34-40-11-99B-889-A01) . . . . . . . . . . . . .
10199
5A
Preamp Board Assembly (-0020) (GRAPHIC 34-40-11-99B-890-A01) . . . . . . . . . . . . .
10203
6
Magnetron Assembly (GRAPHIC 34-40-11-99B-891-A01) . . . . . . . . . . . . . . . . . . . . . . . . . .
10209
7
Pitch Motor Assembly (GRAPHIC 34-40-11-99B-892-A01) . . . . . . . . . . . . . . . . . . . . . . . . . .
10213
8
Azimuth Motor Assembly (GRAPHIC 34-40-11-99B-893-A01) . . . . . . . . . . . . . . . . . . . . . .
10217
9
Gimbal Assembly (GRAPHIC 34-40-11-99B-894-A01) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10222
10
Tilt Sensor Assembly (GRAPHIC 34-40-11-99B-895-A01) . . . . . . . . . . . . . . . . . . . . . . . . . .
10229
11
Scan Sensor Assembly (GRAPHIC 34-40-11-99B-896-A01) . . . . . . . . . . . . . . . . . . . . . . . .
10233
12
Configuration Module Assembly (GRAPHIC 34-40-11-99B-897-A01) . . . . . . . . . . . . . .
10237
13
Configuration Module Board Assembly (GRAPHIC 34-40-11-99B-898-A01) . . . . . .
10241
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
TABLE OF CONTENTS (Cont) LIST OF TABLES Table
Description
Page
INTRO-1
Page Number Blocks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-3
INTRO-2
MTOSS Function Code Definitions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-6
INTRO-3
Verification Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-20
INTRO-4
Software Version History . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRO-21
1
Leading Particulars . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
2
ART 2000 Serial Digital Input Labels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4
3
ART 2000 Serial Digital Outputs Labels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4
4
Printed Circuit Board and Assembly Designators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6
5
Low-Voltage Power Supply Outputs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
23
6
Digital Data to Color Value Conversion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
33
7
FPGA Registers Read Address . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
42
8
Write Address . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
42
1001
Special Tools, Fixtures, and Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1001
1002
Consumables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1002
1003
STC with 10-Inch Antenna . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1008
1004
STC with 12-Inch Antenna . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1008
1005
STC Levels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1085
1006
PNP Transistor Testing Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1087
1007
NPN Transistor Testing Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1087
1008
Common IC Failures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1088
1009
54/74 Series IC Alpha Character Significance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1089
1010
Index to Integrated Circuit Diagrams . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1089
2001
Special Tools, Fixtures, and Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2001
2002
Consumables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2001
2003
Outline and Detail/Schematic Diagrams . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2002
2004
Summary of Unit Modifications, PN 071-01519-0101 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2002
2005
Summary of Changes to the Logic Board, PN 200-08549-0000 . . . . . . . . . . . . . . . . . . . . .
2010
2006
Summary of Changes to the Logic Board, PN 200-08549-0020 . . . . . . . . . . . . . . . . . . . . .
2049
2007
Summary of Changes to the Receiver Assembly, PN 200-05553-0001 . . . . . . . . . . . . .
2091
2008
Summary of Changes to the Preamp Board, PN 200-08545-0000 . . . . . . . . . . . . . . . . . .
2095
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
TABLE OF CONTENTS (Cont) LIST OF TABLES (Cont) Table
Description
Page
2009
Summary of Changes to the Preamp Board, PN 200-08545-0020 . . . . . . . . . . . . . . . . . .
2101
2010
Summary of Changes to the Power Supply/Modulator Board, PN 200-08548-0000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2107
Summary of Changes to the Power Supply/Modulator Board, PN 200-08548-0020 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2133
Summary of Changes to the Configuration Module Assembly, PN 071-00097-0100 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2159
2013
Summary of Changes to the Configuration Module, PN 200-08705-0000 . . . . . . . . . .
2163
3001
Special Tools, Fixtures, and Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3001
3002
Consumables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3001
4001
Special Tools, Fixtures, and Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4001
4002
Consumables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4002
5001
Special Tools, Fixtures, and Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5001
5002
Consumables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5001
6001
Special Tools, Fixtures, and Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6001
6002
Consumables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6001
7001
Special Tools, Fixtures, and Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
7001
7002
Consumables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
7001
8001
Fits and Clearances . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8001
8002
Thread Size and Torque Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8002
8003
Final Torque Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8002
8004
Specified Torque . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8002
9001
Special Tools, Fixtures, and Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
9001
9002
Consumable Materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
9003
15001
Special Tools, Fixtures, and Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15001
15002
Consumables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15001
2011 2012
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
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Page TC-14 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
INTRODUCTION 1.
How to Use This Manual (TASK 34-40-11-99F-801-A01) A.
General (Subtask 34-40-11-99F-001-A01) (1)
WARNING:
THIS EQUIPMENT GENERATES MICROWAVE RADIATION WHICH CAN BE HARMFUL TO HUMANS. DO NOT OPERATE UNTIL YOU HAVE READ AND CAREFULLY FOLLOWED ALL SAFETY PRECAUTIONS AND INSTRUCTIONS IN THE OPERATIONS AND SERVICE MANUALS.
WARNING:
TO PREVENT HARM TO HUMANS, MAINTAIN PRESCRIBED SAFE DISTANCE WHEN STANDING IN FRONT OF A RADIATING ANTENNA. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
WARNING:
TO PREVENT HARM TO HUMANS, NEVER EXPOSE EYES OR ANY PART OF THE BODY TO AN UNTERMINATED WAVEGUIDE. REFER TO FEDERAL AVIATION ADMINISTRATION ADVISORY CIRCULAR NO. 20-68B.
(2)
EFFECTIVITY ALL
This publication gives maintenance instructions for the equipment shown on the Title page.
Aircraft weather radar is specifically designed to emit a concentrated beam of microwave energy at potentially hazardous power levels. These hazards include the possibility of injury to ground personnel, ignition of flammable materials, including fuel, and damage to sensitive electronic devices. U.S. Government standards for human exposure to microwave radiation permit a maximum level of 10 mW per square centimeter. When the radar is operating, this level may be exceeded within the area shown in Figure INTRO-1. Strict observance of this boundary whenever the radar is operating should provide adequate protection.
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure INTRO-1. (Sheet 1 of 1) MPEL Boundary (GRAPHIC 34-40-11-99B-801-A01) (3)
Standard maintenance procedures that technicians must know are not given in this manual.
(4)
This publication is written in agreement with the ATA Specification.
(5)
Refer to the Special Tools, Fixtures, and Equipment and Consumables tables in each section before the start of maintenance or repair procedures.
(6)
An explanation on how to use the ILLUSTRATED PARTS LIST (IPL 34-40-11-10000) is given in the Introduction to that section.
(7)
Honeywell recommends that you do the tests in TESTING AND FAULT ISOLATION (PGBLK 34-40-11-1000) before you disassemble the unit. These tests can show the condition of the unit or most possible cause of a malfunction. If a malfunction occurs, repair as necessary.
(8)
Warnings, cautions, and notes in this manual give the data that follows:
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519 • A WARNING gives a condition or tells personnel what part of an operation or maintenance procedure, which if not obeyed, can cause injury or death • A CAUTION gives a condition or tells personnel what part of an operation or maintenance procedure, which if not obeyed, can cause damage to the equipment • A NOTE gives data, not commands. The NOTE helps personnel when they do the related instruction. (9) B.
C.
Warnings and cautions go before the applicable paragraph or step. Notes follow the applicable paragraph or step.
Observance of Manual Instructions (Subtask 34-40-11-99F-002-A01) (1)
The procedures used must be consistent with standard shop practices and be carefully examined to make sure that all safety, efficiency, and operation procedures of the unit.
(2)
All personnel who operate equipment and do maintenance specified in this manual must know and obey the safety precautions.
Symbols (Subtask 34-40-11-99F-003-A01) (1)
The symbols and special characters are in agreement with IEEE Publication 260 and IEC Publication 27. Special characters in text are spelled out.
(2)
The signal mnemonics, unit control designators, and test designators are shown in capital letters.
(3)
The signal names followed by an “*” show an active low signal.
(4)
The symbols in Figure INTRO-2, Sheet 1 show ESDS and moisture sensitive devices.
Figure INTRO-2. (Sheet 1 of 1) Symbols (GRAPHIC 34-40-11-99B-802-A01) D.
Units of Measure (Subtask 34-40-11-99F-004-A01) (1)
E.
Measurements, weights, temperatures, dimensions, and other values are expressed in the USMS followed by the appropriate SI metric units in parentheses. Some standard tools or parts such as drills, taps, bolts, nuts, etc. do not have an equivalent.
Page Number Block Explanation (Subtask 34-40-11-99F-005-A01) (1)
The data in this manual is divided into sections. A standard page number block system is used. Page number blocks are shown in Table INTRO-1. Table INTRO-1. Page Number Blocks
Section
Page Number Block
Description and Operation
1 thru 999
Testing and Fault Isolation
1001 thru 1999
Schematic and Wiring Diagrams
2001 thru 2999
Disassembly
3001 thru 3999
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table INTRO-1. Page Number Blocks (Cont) Section
Page Number Block
Cleaning
4001 thru 4999
Inspection/Check
5001 thru 5999
Repair
6001 thru 6999
Assembly
7001 thru 7999
Fits and Clearances
8001 thru 8999
Special Tools, Fixtures, Equipment and Consumables
9001 thru 9999
Illustrated Parts List
10001 thru 10999
Special Procedures
11001 thru 11999
Removal
12001 thru 12999
Installation
13001 thru 13999
Servicing
14001 thru 14999
Storage (Including Transportation)
15001 thru 15999
Rework (Service Bulletin Accomplishment Procedures)
16001 thru 16999
NOTE: 1
F.
G.
The IPL is the last page number block in the document.
Illustration (Subtask 34-40-11-99F-006-A01) (1)
Some of the exploded view illustrations shown in the ILLUSTRATED PARTS LIST (IPL 34-40-11-10000) section are also referenced in the DISASSEMBLY (PGBLK 34-40-11-3000), CLEANING (PGBLK 34-40-11-4000), INSPECTION/CHECK (PGBLK 34-40-11-5000), REPAIR (PGBLK 34-40-11-6000), ASSEMBLY (PGBLK 34-40-11-7000), and/or FITS AND CLEARANCES (PGBLK 34-40-11-8000) sections of this manual.
(2)
Illustrations that support the individual items are shown by the item nomenclature, and in parenthesis, the item number followed by the basic figure number, i.e. washer (90, IPL Figure 1). Item numbers refer to the same IPL figure until a different IPL figure is specified.
(3)
Illustrations with no specific designation are applicable to all units.
Application of Maintenance Task Oriented Support System (MTOSS) (Subtask 34-40-1199F-007-A01) (1)
In accordance with the ATA Specification 2200, this publication uses a Maintenance Task Numbering System which make the maintenance procedures in this manual compatible with an automated shop environment.
(2)
The system uses standard and unique number combinations to identify maintenance tasks and subtasks.
(3)
The MTOSS structure is the logical approach to organizing maintenance tasks and subtasks. The MTOSS numbering system includes the ATA Chapter-Section-Subject number as well as a function code and unique identifiers. The purpose of incorporating the MTOSS numbering system is to provide a means for the automated sorting, retrieval, and management of digitized data.
EFFECTIVITY ALL
1
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COMPONENT MAINTENANCE MANUAL 071-01519 (4)
Section and Subsection Numbering System (a)
All procedures in this publication have TASK and SUBTASK numbers at key data retrieval points. The numbers provide the following: • Identification of the hardware (part or parts) primary to the TASK • Identification of the maintenance function applied to the part or parts • A unique identifier for a set of instructions (known as TASK or SUBTASK) • Identification of alternate methods and configuration differences that change the procedure applied to the TASK • Identification of airline changes to a TASK or SUBTASK.
(5)
Components of Task and Subtask Number (a)
The numbering system is an expansion of the ATA three-element numbering system. The number has seven elements. The first five elements are necessary for each TASK or SUBTASK. The sixth and seventh elements are applied only when necessary. Refer to Figure INTRO-3.
(b)
Elements 1, 2, and 3 identify the ATA Chapter-Section-Subject number of the page block.
(c)
Element 4 defines the maintenance function being performed. This element is a three position element. The third position is zero filled when further definition is not required. If required, the manufacturer will use the numbers 1 through 9 or letters A through Z, excluding the letters I and O. Refer to Table INTRO-2.
(d)
Element 5 provides a unique identification for each TASK or SUBTASK number which is similarly numbered through the first four elements. • TASKS are numbered from 801 through 999 • SUBTASKS are numbered from 001 through 800.
(e)
Element 6 is a three position alphanumeric element used for identification of differences in configurations, methods or techniques, variations of standard practice applications, etc.
(f)
Element 7 provides coding of those tasks or subtasks that have been changed by the customer (e.g., those tasks or subtasks accomplished by an outside repair source).
Figure INTRO-3. (Sheet 1 of 1) MTOSS Code Positions (GRAPHIC 34-40-11-99B-803-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519 Table INTRO-2. MTOSS Function Code Definitions Code
Function
000
REMOVAL AND DISASSEMBLY
010
Removal
Removal of the engine/component from a workstand, transport dolly, test stand, etc., or aircraft.
020
Remove Modular Sections
This is the first echelon of disassembly which consists of sectionalization of the unit/engine into primary modular sections. Modular sections are identified by the third element of the ATA number when removed from the unit/engine.
030
Disassemble Modular Sections
This is the second echelon of disassembly which consists of disassembly of the modular sections into subassemblies after removal from the unit/engine. Modular section designations appear in the second element of the ATA number for this echelon of disassembly.
040
Disassemble Subassemblies
This is the third echelon of engine disassembly which consists of disassembly of subassemblies to the piece part level. The subassemblies are identified by the third element of the ATA number.
050
Remove Accessory/Power Plant Components
This consists of removing individual accessory/power plant components from either installed or uninstalled engines.
060
Disassemble Accessory
This involves disassembly of accessories /components into subassemblies.
070
Disassemble Accessory Subassembly
This involves disassembly of accessories /components subassemblies into piece parts.
080
Remove Test Equipment
This consists of removing equipment and instrumentation after accessory/component test.
090
Disassemble Support Equipment
This consists of disassembly of support equipment required to maintain said support equipment.
100
CLEANING
110
Chemical
EFFECTIVITY ALL
Definition
Removal of surface deposits from a part by use of a chemical cleaning agent. After being dissolved, the deposit is washed or rinsed away after a soaking period. Also includes chemical power flushing.
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COMPONENT MAINTENANCE MANUAL 071-01519
Table INTRO-2. MTOSS Function Code Definitions (Cont) Code
Function
Definition
120
Abrasive
Removal of surface deposits from a part by wet or dry particle impingement.
130
Ultrasonic
Removal of surface deposits and entrapped material by use of high frequency sound waves to produce cavitation at the surface of the part. Cleaning is performed in a liquid bath that transmits the sound energy and keeps the removed material in suspension.
140
Mechanical
Removal of surface deposits from a part by use of a brush, felt bob, sandpaper, or other hand or mechanical action.
150
Unassigned
160
Miscellaneous
Removal of deposits from parts with compressed air, miscellaneous hand cleaning, and various combinations of cleaning procedures.
170
Foam/Water Wash
Removal or post emulsified fluorescent penetrant through an agitated water wash, automatic spray rinse, or an aqueous remover aerated to produce a foam.
180
Testing of Solutions
Test used to assist in identifying certain materials by electro-mechanically determining the presence or absence of known constituents.
190
Unassigned
200
INSPECTION
210
Check
EFFECTIVITY ALL
A thorough visual examination of components, accessories, subsystems, and piece parts to detect structural failure, deterioration or damage, and to determine the need for corrective action. For example: exterior surfaces, electronic circuit cards, gears, control systems, linkages, accessories, components, tubing, wiring and connections, safety wiring, fasteners, clamps, etc., are inspected to verify proper condition and acceptability for continued service.
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COMPONENT MAINTENANCE MANUAL 071-01519
Table INTRO-2. MTOSS Function Code Definitions (Cont) Code
Function
Definition
220
Visual/Dimensional
A comparison of the dimensions and material conditions of parts, subassemblies, and assemblies with the specifications contained in technical manuals and/or blueprints, to detect deviations from established standard and limits and determine the acceptability for continued service, repair, or need to discard the item. A visual/dimensional function code is also required to verify that proper corrective maintenance has been accomplished. Although some of these tasks may not require measurements, a complete spectrum of tasks/sub tasks requires a variety of measuring equipment to determine runout, concentricity, flatness, parallelism, hardness, thickness, clarity, dimensions, etc.
230
Penetrant
Fluorescent penetrant inspection to detect surface cracks.
240
Magnetic
Magnetic particle inspection to detect surface cracks in magnetic materials.
250
Eddy Current
Inspection for subsurface cracks, porosity, inclusions, or other nonhomogeneous material structure by use of high frequency electromagnetic wave equipment. Parts are scanned and compared to similar parts or test specimens having known material defects.
260
X-Ray
Inspection for subsurface cracks, porosity, inclusions, or other nonhomogeneous material structure by use of x-ray techniques.
270
Ultrasonic
Inspection for subsurface cracks, porosity, inclusions, or other nonhomogeneous material structure by use of contact pulse echo ultrasonic techniques.
280
Special
Any special inspection to determine the integrity of a part for continued operation In-Service or qualitative analysis.
290
Unassigned
300
REPAIR
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table INTRO-2. MTOSS Function Code Definitions (Cont) Code
Function
Definition
310
Welding and Brazing
The joining of pieces by welding (fusion, resistance, spot, electron beam, plasma arc), brazing (furnace, torch, induction), or soldering. This category includes hard facing.
320
Machining
The process of obtaining a desired shape or finish by grinding, turning, boring, reaming, broaching, milling, drilling, lapping, honing, sizing, polishing, buffing, cutting, forming, stamping, blanking, etc.
330
Stripping and Plating
Removing or applying a metallic coating on a surface by mechanical, chemical, or electrical means. Plating of chromium, cadmium, tin, etc., to build up the size of a part or provide surface protection. Includes masking or waxing prior to the process.
340
Plasma and Flame Spraying
The application of a protective coating to a part by feeding a powder into an ionized gas stream. Flame spraying uses a fuel oxygen flame to melt and propel metal onto parts to build up the size or provide surface protection.
350
Miscellaneous Repairs
Repairing parts by hand (cutting, drilling, polishing, grinding, lapping, riveting, blending, routing, fitting, burring, planishing, sanding, sawing, recambering, drilling, tapping, heating, chilling) and including miscellaneous disassembly and assembly required.
360
Bonding and Molding/Sealing
Joining and curing of parts with an adhesive or fusible material (including silicone, fiberglass, glues).
370
Heat Treating
Controlled heating and cooling of a material to obtain the desired physical property (includes annealing, tempering, quenching, stress relieving, solution heat treat, etc.).
380
Surface Treating
Treating the surface of a part by painting, varnishing, aluminizing, Teflon coating, zinc chromate priming, tumble finishing, shot peening, etc. Baking and masking processes are included.
390
Machine Riveting and Flaring
Joining of parts by riveting and flaring the rivet.
400
INSTALLATION AND ASSEMBLY
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table INTRO-2. MTOSS Function Code Definitions (Cont) Code
Function
Definition
410
Install
Installation of the unit/engine onto a workstand, transport dolly, test stand, or aircraft.
420
Install Modular Sections
The third echelon of assembly consisting of assembly of the modular assemblies into a complete unit/engine assembly. The modular sections are identified by the third element of the ATA number.
430
Assemble Modular Sections
The second echelon of assembly consisting of assembling subassemblies into modular sections. The modular section is identified by the second element of the ATA number.
440
Assemble Subassemblies
The first echelon of assembly consisting of assembling piece parts into subassemblies. The subassemblies are identified by the third element of the ATA number.
450
Install/Close Items Removed/Opened for Access
Installation or closing of access plates, closing of ports, installation of components, tubing or any item which was removed or opened in order to provide access to perform the task.
460
Assemble Accessory
Assemble accessory components.
470
Assemble Accessory Subassembly
Assembly of accessory subassembly components.
480
Install Test Equipment
Install equipment and instrumentation required for accessory component test.
490
Assemble Support Equipment
Any assembly required to maintain support equipment.
500
MATERIAL HANDLING
510
Shipping
The movement of any part, subassembly, assembly, or component from the time it is packaged until it reaches its destination.
520
Receiving
The receipt activity for any incoming part, subassembly, assembly, or component.
530
Packing
Installing parts, subassemblies, assemblies, or components into shipping containers.
540
Unpacking
Removing parts, subassemblies, assemblies, or components from shipping containers.
550
Storage
Safekeeping of parts, subassemblies, assemblies, or components until required for use.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table INTRO-2. MTOSS Function Code Definitions (Cont) Code
Function
Definition
560
Marshaling/Positioning
Marshaling is collection of parts, subassemblies, and accessories prior to release for assembly. Positioning is movement from one fixed state to another.
570
Engine Ferry/Pod Maintenance
Necessary preparations before and after transporting an engine by aircraft ferry method.
580
Unassigned
590
Unassigned
600
SERVICING/PRESERVING/LUBRICATING
610
Servicing
Action required to sustain a unit or system in proper operating status including priming with applicable fluids prior to use.
620
Preserving
Preparation of a unit, part, assembly, etc., for safekeeping from decomposition or deterioration. Includes preparation for storage (applying a preservative layer, desiccants, etc.).
630
Depreserving
Removing preservatives, desiccants, etc., from a unit, part, assembly, etc., prior to installation or operation.
640
Lubricating
Applying oil, grease, dry film, or silicon lubricants on moving parts to reduce friction or cool the item.
650
Unassigned
660
Unassigned
670
Unassigned
680
Unassigned
690
Unassigned
700
TESTING/CHECKING
710
Oil Flow
Measuring the flow of oil through components or compartments under specific conditions.
720
Air Flow
Measuring the flow of air through components or compartments under specific conditions.
730
Fuel Flow
Function checks and flow measurements through the part or system being tested.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table INTRO-2. MTOSS Function Code Definitions (Cont) Code
Function
Definition
740
Water Flow
Function checks and flow measurements through the part or system being tested.
750
Electrical/Return to Service
Functional tests (manual or ATE) of the system or component as well as measurement of electrical or electronic parameters designed to determine whether the item can be returned to service. May include fault isolation procedures for components that require close correlation between test results and fault indications.
760
Engine
Operation of an engine to establish systems function or operation under specific conditions to measure performance.
770
Accessory/Bite
Testing of an accessory to ensure proper operation or function.
780
Pressure Check
Testing to establish the ability of a normally pressurized component or system to operate properly.
790
Leak Check
Determine the ability of a component or system to operate without leaking.
800
MISCELLANEOUS
810
Fault Isolation
Operation of an engine at constant thrust level or identical Engine Pressure Ratio (EPR) to locate the prime suspect deficient system, operating an improperly functioning system or component to locate the cause; or performing a series of checks to isolate a failed part or component.
820
Adjusting/Aligning/Calibrating
Making a physical correction to ensure proper placement or operation of a system or component.
830
Rigging
Hooking-up, arranging, or adjusting a component or accessory linkage for proper operation.
840
Service Bulletin Incorporation
Performing the work specified in the service bulletin. Provides for identification of modification tasks at the task level with subtasks recognizing any functional changes (chemical, visual/dimensional, cleaning, machining, etc.) necessary to incorporate the service bulletin.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table INTRO-2. MTOSS Function Code Definitions (Cont) Code
Function
Definition
850
Part Number Change/Re-identification
Change of part number, application of part number by transfer, engrave repair number, etc.
860
Unassigned
870
Description and Operation
Electrical and mechanical description of the unit or component. Includes leading particulars, descriptions, limitations, specifications, and theory of operation.
880
Approved Vendor Processes
Includes processes that may be proprietary and controlled by a particular manufacturer, or by nonproprietary and approved for application by conforming vendors.
890
Airline Maintenance Program (Customer Use)
900
Unassigned
910
Special Equipment Maintenance
Identification of tasks to maintain special support equipment.
920
Standard Equipment Maintenance
Identification of tasks to maintain standard support equipment.
930
Tool Fabrication
Includes fabricating any tool for which procedures to use are included in the manual.
940
Special Tools, Equip, and Consumables Listing
Listing of all special tools, standard equipment, special equipment, and consumables required to perform maintenance on the unit or component.
94A
Consumables
94B
Special Tools/Non Std Tools
94C
Fixtures/Test Equipment
94D
Standard Tools
950
Illustrated Parts List (Detailed Parts List)
Section of IPL/IPC that contains parts description and identification in top-down break down sequence.
960
Illustrated Parts List (Equipment Designation Index)
Section of IPL/IPC that contains equipment designators cross-referenced to detailed parts list.
970
Illustrated Parts List (Numerical Index)
Section of IPL/IPC that contains an alphanumeric listing of all parts in the unit cross-referenced to the detailed parts list.
980
Illustrated Parts List (Alternate Vendor Index)
Optional section of IPL/IPC that contains an alphanumeric listing of all parts in the unit that have more than one vendor source.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table INTRO-2. MTOSS Function Code Definitions (Cont) Code
Function
990
Illustrations, Tables, Front Matter, Etc.
99A
Tables
99B
Illustrations
99C
Front Matter Pageblock (TASK Level MTOSS) Front Matter Task (Collection of Subtask MTOSS)
99D
Access
99E
References
99F
General/Introduction H.
Standard Practices Manual (Subtask 34-40-11-99F-008-A01) (1)
I.
Standard cleaning, check, repair, and assembly procedures applicable to multiple models can be found in a standard practices manual. Refer to Paragraph 3 (TASK 34-40-11-99F-803-A01).
Electrostatic Discharge (Subtask 34-40-11-99F-009-A01) (1)
2.
Definition
Touch the items susceptible to electrostatic discharge in accordance with MIL-HDBK-263. Refer to MIL-STD-1686 for definition of the standards and conditions.
Customer Support (TASK 34-40-11-99F-802-A01) A.
Honeywell Aerospace Online Technical Publications Web Site (Subtask 34-40-11-99F-010-A01) (1)
Go to the Honeywell Online Technical Publications Web site at (www.myaerospace.com). • To download or see publications online • To order a publication • To tell Honeywell of a possible data error in a publication.
B.
Global Customer Care Center (Subtask 34-40-11-99F-011-A01) (1)
If you do not have access to the Honeywell Technical Publications Web site, or if you need to speak to personnel about non-Technical Publication matters, the Honeywell Aerospace Global Customer Care Center gives 24/7 customer service to Air Transport & Regional, Business & General Aviation, and Defense & Space customers around the globe. • Telephone: 800-601-3099 (Toll Free U.S.A. / Canada) • Telephone: 602-365-3099 (International / Direct) • Telephone: 00-800-601-30999 (EMEA Toll Free) • Telephone: 420-234-625-500 (EMEA Direct).
3.
References (TASK 34-40-11-99F-803-A01) A.
Honeywell/Vendor Publications (Subtask 34-40-11-99F-012-A01) (1)
Related Honeywell publications in this manual are shown in the list that follows: • Pub. No. 006-00643-0007, IM, RDR 2000 Color Weather Radar System • Pub. No. 006-08755-0001, RDR 2000 Digital Weather Radar System Pilot’s Guide
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519 • Pub. No. 006-05392-0002, MM/OG, KPA 900 Configuration Module Programmer • ATA No. 20-00-03 (Pub. No. A09-1100-004), Standard Repair Procedures for Honeywell Avionics Equipment Instruction Manual, SOPM20-00-03. B.
Other Publications (Subtask 34-40-11-99F-013-A01) (1)
These publications are standard references: • The United States GPO Style Manual 2000 (available at http://www.gpoaccess.gov /stylemanual/browse.html) • IEEE Std 260, Standard Letter Symbols for Units of Measurement (available from the American National Standards Institute, New York, NY) • ASME Y14.38, Abbreviations for Use on Drawings and in Text (available from the American National Standards Institute, New York, NY) • ANSI/IEEE Std 91, Graphic Symbols for Logic Functions (available from the American National Standards Institute, New York, NY) • H4/H8 CAGE Codes (available at http://www.dlis.dla.mil/cage_welcome.asp) • IEEE 315/ANSI Y32.2, Graphic Symbols for Electrical and Electronics Diagrams (available from the American National Standards Institute, New York, NY) • MIL-HDBK-263, Electrostatic Discharge Control Handbook for Protection of Electrical and Electronic Parts, Assemblies and Equipment (Excluding Electrically Initiated Explosive Devices) (Metric) (available from any military standards database) • MIL-STD-1686, Electrostatic Discharge Control Program for Protection of Electrical and Electronic Parts, Assemblies and Equipment (Excluding Electrically Initiated Explosive Devices) (Metric) (available from any military standards database) • FAA Advisory Circular No. 20-68B, Recommended Radiation Safety Precautions for Ground Operation of Airborne Weather Radar (available at http://www.airweb.faa.gov/Regulatory _and_Guidance_Library/rgAdvisoryCircular.nsf/MainFrame?OpenFrameSet) • FAA Advisory Circular No. 43-14, Maintenance of Weather Radar Radomes (available at http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf /MainFrame?OpenFrameSet) • RTCA document No. DO-160C, Environmental Conditions and Test Procedures for Airborne Equipment.
4.
Component Maintenance Levels (TASK 34-40-11-99F-804-A01) A.
General (Subtask 34-40-11-99F-014-A01) (1)
This CMM contains one or more component maintenance levels for repair. The component maintenance levels of repair are shown below as specified in the ARINC Report 663.
(2)
Component maintenance level 1 is maintenance operations with an end result of determining LRU serviceability. No maintenance action is performed to repair the LRU.
(3)
Component maintenance level 1 is limited to return to service testing and configuration confirmation of the LRU, including all software loading as necessary for return to service and the preloading of field loadable software.
(4)
Component maintenance level 2 is maintenance operations with an end result of restoring LRU serviceability. Maintenance procedures are limited to the replacement of subassemblies.
(5)
Component maintenance level 2 embodies those activities necessary to:
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519 • Fault isolate to the defective subassembly • Replace such subassemblies • Return the LRU to service. (6)
Component maintenance level 2 includes programming, calibrations, alignments, tuning, etc., necessary to return the LRU to service without the replacement of basic parts.
(7)
Component maintenance level 3 is maintenance operations with an end result of restoring a LRU or a subassembly to serviceability. Maintenance includes repair of the LRU and or its subassemblies by any and all repair processes, including but not limited to, replacement of defective basic parts such as processor chips, transistors, or chassis mounted parts.
(8)
Component maintenance level 3 embodies those activities necessary to: • Fault isolate to the basic part level • Replace/repair such parts • Return the LRU or subassembly to service.
(9)
Component maintenance level 3 includes all programming, calibrations, alignments, tuning, etc., necessary to return the LRU/SRU to service.
(10) If the service location does level 3 repairs, it must have the equipment identified in Table 1001 or the equivalent alternative(s).
5.
Acronyms and Abbreviations (TASK 34-40-11-99F-805-A01) A.
General (Subtask 34-40-11-99F-015-A01) (1)
The abbreviations are used in agreement with ASME Y14.38.
(2)
Acronyms and non-standard abbreviations used in this publication are as follows. List of Acronyms and Abbreviations
EFFECTIVITY ALL
Term
Full Term
µsec
Microsecond
A/D
Analog-to-Digital
A
Ampere
ACC
Accessory
AFC
Automatic Frequency Control
AGC
Automatic Gain Control
ANSI
American National Standards Institute
ANT
Antenna
ARINC
Aeronautical Radio, Incorporated
ASCII
American Standard Code for Information Interchange
ASME
American Society of Mechanical Engineers
ATA
Air Transport Association
ATE
automated test equipment
AWG
American Wire Gage
C
Celsius
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COMPONENT MAINTENANCE MANUAL 071-01519
List of Acronyms and Abbreviations (Cont)
EFFECTIVITY ALL
Term
Full Term
CAGE
Commercial and Government Entity
cm
Centimeter
CMM
Component Maintenance Manual
CMOS
Complementary Metal-Oxide Semiconductor
DAC
Digital-to-Analog Converter
dB
Decibel
dBi
Decibel Isotropic
dBm
Decibel (Referenced to One Milliwatt)
DC
Direct Current
DIP
Dual Inline Package
DP
Done Programming
DPL
Detailed Parts List
ECCN
Export Control Classification Number
EDI
Equipment Designator Index
EEPROM
Electronically Erasable Programmable Read-Only Memory
EFIS
Electronic Flight Instrument System
EMEA
Europe, the Middle East, and Africa
EPROM
Electrically Programmable Read-Only Memory
ESDS
Electrostatic Discharge Sensitive
ESTC
Extended Sensitivity Timing Control
F
Fahrenheit
FAA
Federal Aviation Administration
FET
Field Effect Transistor
FPGA
Field-Programmable Gate Array
GHz
Gigahertz
GMAP
Ground Mapping
GPO
Government Printing Office
HDC
High During Configuration
HPN
Honeywell Part Number
HVPS
High-Voltage Power Supply
Hz
Hertz
IC
Integrated Circuit
IEC
International Electrotechnical Commission
IEEE
Institute of Electrical and Electronics Engineers
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COMPONENT MAINTENANCE MANUAL 071-01519
List of Acronyms and Abbreviations (Cont)
EFFECTIVITY ALL
Term
Full Term
IF
Intermediate Frequency
IM
Installation Manual
in-lb
Inch-Pound
IPC
illustrated parts catalog
IPL
Illustrated Parts List
Jct
Junction
kg
Kilogram
kHz
Kilohertz
km
Kilometer
kW
Kilowatt
LO
Local Oscillator
LRU
Line-Replaceable Unit
LSB
Least Significant Bit
LSI
Large Scale Integration
m
Meter
MAG
Magnetron
MDS
ENGINEERING PLEASE PROVIDE
MHz
Megahertz
MM/OG
Maintenance Manual/Operator’s Guide
mm
Millimeter
MMIC
Monolithic Microwave Integrated Circuit
MOD
Modification
MOSFET
Metal-Oxide Semiconductor Field-Effect Transistor
MPEL
Maximum Permissible Exposure Level
MSB
Most Significant Bit
msec
Millisecond
MTOSS
maintenance task oriented support system
MUX
Multiplexer
mV
Millivolt
mW
Milliwatt
N•m
Newton Meter
N/A
Not Applicable
NAV
Navigation
NHA
Next Higher Assembly
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COMPONENT MAINTENANCE MANUAL 071-01519
List of Acronyms and Abbreviations (Cont)
EFFECTIVITY ALL
Term
Full Term
NLR
No License Required
NM
Nautical Mile
Nm
Newton Meter
No.
Number
NOVRAM
Non-Volatile Random Access Memory
nsec
Nanosecond
PC
Personal Computer
PN
Part Number
PRF
Pulse Repetition Frequency
Pub.
Publication
PWM
Pulse Width Modulation
PWR
Power
R/T
Receiver/Transmitter
RAM
Random Access Memory
RF
Radio Frequency
RFI
Radio Frequency Interference
RNAV
Radio Navigation
ROM
Read-Only Memory
RTCA
Radio Technical Commission for Aeronautics
S/N
Serial Number
SBN
Service Bulletin Number
SBY
Standby
SCR
Silicon-Controlled Rectifier
SDI
Source-Destination Identifier
SI
International System of Units
SRU
Shop-Replaceable Unit
STBY
Standby
STC
Sensitivity Timing Control
Std
Standard
TCAS
Traffic Alert and Collision Avoidance System
Toll Free U.S.A.
United States of America
TR
Temporary Revision
TST
Test
TTL
Transistor-to-Transistor Logic
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Page INTRO-19 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
List of Acronyms and Abbreviations (Cont)
6.
Term
Full Term
TX
Transmitter
usec
Microsecond
USMS
United States Measurement System
VDC
Volt, Direct Current
Vp-p
Volt Peak-to-Peak
Vrms
Volts Root Mean Square
VSWR
Voltage Standing Wave Ratio
W
Watt
Wx
Weather
Process Verification (TASK 34-40-11-99F-806-A01) A.
Verification Data (Subtask 34-40-11-99F-016-A01) (1)
Honeywell does a verification of these technical instructions by performance or by simulation of the necessary procedures. Performance shows that the procedures were checked by the use of the manual. Simulation shows that the applicable personnel looked at the procedure in the manual and that the procedure is technically correct. The dates of verification for this manual are given in Table INTRO-3. Table INTRO-3. Verification Data
Section
Method
Date
Testing and Fault Isolation
Simulation
18 July 2011
Disassembly
Simulation
18 July 2011
Assembly
Simulation
18 July 2011
B.
Environmental Certification (Subtask 34-40-11-870-001-A01) (1)
EFFECTIVITY ALL
The ART 2000 meets the environmental conditions of the RTCA document No. DO-160C, Environmental Conditions and Test Procedures for Airborne Equipment.
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure INTRO-4. (Sheet 1 of 1) DO-160C Environmental Qualification Form (GRAPHIC 34-40-11-99B804-A01)
7.
Software History (TASK 34-40-11-99F-807-A01) A.
Software Data (Subtask 34-40-11-99F-017-A01) (1)
The ART 2000 incorporates operating system software. Refer to Table INTRO-4 for the software version history. Table INTRO-4. Software Version History
Software Version No.
Updated By
01/04
Originally shipped
01/05
Pub. No. 605-07790-0010 (SWB ART 2000-1)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table INTRO-4. Software Version History (Cont) Software Version No.
Updated By
01/06
Pub. No. 605-07790-0021 (SWB ART 2000-SW2)
01/07
Pub. No. 605-07790-0031 (SWB ART 2000-SW3)
01/08
Pub. No. 605-07790-0041 (SWB ART 2000-SW4)
01/09
Pub. No. 605-07790-0050 (SWB ART 2000-SW5)
8.
History of Changes (TASK 34-40-11-99F-808-A01) A.
Modification/Configuration History (Subtask 34-40-11-99F-018-A01) (1)
EFFECTIVITY ALL
Refer to the Service Bulletin list for modifications applicable to the ART 2000.
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COMPONENT MAINTENANCE MANUAL 071-01519
DESCRIPTION AND OPERATION 1.
Description (TASK 34-40-11-870-801-A01) A.
General (Subtask 34-40-11-870-002-A01) (1)
The ART 2000 is a remote mounted weather avoidance radar R/T. It is primarily intended for weather avoidance and ground mapping functions as an aid to navigation.
(2)
Refer to Table 1 for the leading particulars.
Table 1. Leading Particulars Characteristic
Specification
Temperature range
-67 to +158 F (-55 to +70 C) with antenna
Altitude
55,000 feet (16.764 m) unpressurized
Weight
9.9 pounds (4.49 kg)
Overall dimensions: Base
10.00 inches (25.40 cm)
Input power requirements
28 VDC at 2 A, 17 VDC at 2.5 A
RADAR TRANSMITTER: RF power output
4 kW magnetron peak power, 3.5 kW typical
Frequency (X-band)
9345 to 9405 MHz
Pulse repetition frequency
101.5 to 111.5 Hz
Pulse width
4 µsec nominal (GMAP and Wx modes)
Weather avoidance range capability: 10-inch antenna 12-inch antenna
279 NM maximum 305 NM maximum
RADAR RECEIVER: Sensitivity
-110 dBm typical
STC: 10-inch antenna 12-inch antenna
Effective 0 to 30 NM Effective 0 to 35 NM
Weather compensation (Wx mode only)
40 to 240 NM
Extended STC
Effective 40 to 240 NM
Variable gain
0 to -20 dB
Stabilization requirements: Reference
EFFECTIVITY ALL
400 to 5000 Hz
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COMPONENT MAINTENANCE MANUAL 071-01519
Table 1. Leading Particulars (Cont) Characteristic
Specification
Inputs
26 Vrms, 400 Hz sine wave 115 Vrms, 400 Hz sine wave 20 Vp-p, 400 Hz sine wave 20 Vp-p, 400 Hz square wave 10.7 Vp-p, 400 Hz square wave 28 Vp-p, 5 kHz square wave ARINC 429
Pitch and roll scaling
30 to 220 mV/ , 400 Hz or 5000 Hz Pitch HI in phase with gyro except on pitch up Roll HI in phase with gyro except on right roll
Stabilization rate
25 /second (pitch and roll)
Scan angle
90 or 100 (configurable)
Scan physical radius: Horizontal polarized 10-inch antenna 12-inch antenna
To 5.22 inches (13.26 cm) To 6.20 inches (15.75 cm)
Vertical polarized 10-inch antenna 12-inch antenna
To 5.31 inches (13.49 cm) To 6.28 inches (15.95 cm)
Scan rate
25 /second
Vertical profile
±30
Tilt angle
±15
Performance index: 10-inch antenna 12-inch antenna (3)
EFFECTIVITY ALL
207.4 to 212.4 dB 210.5 to 215.2 dB
Refer to Figure 1 for a typical ART 2000.
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1. (Sheet 1 of 1) Typical ART 2000 (GRAPHIC 34-40-11-99B-805-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519 (4)
Table 2 gives the serial digital input labels for the ART 2000. Table 2. ART 2000 Serial Digital Input Labels
Label
Information Contained in Label
Format
Speed
203
Altitude
BNR
Low speed
204
Baro corrected altitude
BNR
Low speed
270
Radar control word No. 1
DSC
Low speed
271
Radar control word No. 2
DSC
Low speed
273
Vertical profile control word
DSC
Low speed
275
RDR control word No. 3
DSC
Low speed
276
Radar control panel control word
DSC
Low speed
324
Pitch angle
DSC
Low speed
325
Roll angle
BNR
High speed
177
Time/temperature recorder data request
BNR
High speed
(5)
Table 3 gives the serial digital outputs from the ART 2000. Table 3. ART 2000 Serial Digital Outputs Labels
Label
Information Contained in Label
177
Time/temperature recorder data B.
Format
Speed
Job Setup Data (Subtask 34-40-11-99C-001-A01) (1)
The list that follows identifies Honeywell publications that are related to this section: • Pub. No. 006-00643-0007, IM, RDR 2000 Color Weather Radar System.
C.
Mechanical Description (Subtask 34-40-11-870-003-A01) (1)
The ART 2000 consists of a radar receiver and a radar transmitter (with applicable antenna) constructed as a single unit with a single mounting facility. A configuration module, PN 071-00097-0100 is an integral part of the unit but is not attached to it. Refer to Pub. No. 006-00643-0007, RDR 2000 Color Weather Radar System IM for more information on the configuration module. The RDR 2000 system provides for radar stabilization input for combined pitch, roll, and tilt angles of up to ±30 . In the vertical profile mode, the antenna stabilization only responds to pitch inputs.
(2)
The antenna array is attached to the microwave assembly on the ART 2000 and the two are moved together as the radar scans. The base of the ART 2000 contains the receiver and all processing and control circuits.
(3)
The antenna scan angle can be configured for a 90 or 100 scan.
(4)
Upon installation, the system can be configured to include a target alert feature. In this configuration, if the ART 2000 detects a red intensity target with a minimum size of 2 nautical miles in range and 2 in azimuth that is beyond 80 nautical miles and the selected range is 80 nautical miles or less, two red arcs separated by a black arc are displayed at the top of the display centered on the aircraft heading.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519 D.
Electrical Description (Subtask 34-40-11-870-004-A01) (1)
The ART 2000 can accommodate up to three ARINC 429 control inputs, but only two can be actively controlling the system at one time and display No. 3 must be EFIS 40/50 software level 9 or higher. It can also output information to a maximum of three displays by using SDI bits on the ARINC 453 bus. NOTE:
When an ARINC 429 altimeter is connected, display No. 3 becomes nonfunctional (the altimeter is read rather than the third controller).
(2)
The control/display unit used enables selection of basic weather, ground mapping, and self-test functions. Also, image display optimization is made possible by the use of controls for range selection, display intensity, and antenna tilt angle. All these functions are multiplexed on the ARINC 429 control bus.
(3)
Alphanumerics are displayed on-screen for the selected mode of operation and the selected range, along with the interval (nautical miles) between the displayed range rings. All controls for the system are mounted on the perimeter of the IN 182A screen. In EFIS installations, the radar is controlled through the radar control panel.
(4)
A source of attitude data is required to stabilize the ART 2000 during aircraft maneuvering. Lack of a source will not prevent the ART 2000 from operating, but performance will be compromised.
(5)
The ART 2000 will accept pitch and roll information in the form of ARINC 429 serial data or analog data at various voltage levels. Refer to Pub. No. 006-00643-0007, RDR 2000 Color Weather Radar System IM for a list of acceptable attitude sources and for complete interconnection information.
(6)
A source of altitude is required to fully utilize the AutoTilt feature of the ART 2000. Lack of a source will not prevent the AutoTilt from operating, but the function will be limited to range compensation only.
(7)
The ART 2000 will accept altitude data in the form of ARINC 429 (low speed only) serial data or ARINC 575 parallel data. Refer to Pub. No. 006-00643-0007, RDR 2000 Color Weather Radar System IM for a list of acceptable altitude sources and for complete interconnection information.
(8)
The optional IU 2023B DataNav can be used to interface numerous navigation systems to an RDR 2000 system by means of an ARINC 429 data bus.
(9)
The panel-mounted CC 2024B checklist controller can be used with the RDR 2000 to display pilot-selectable checklist information and can be used with or without the IU 2023B DataNav.
(10) The optional GC 381A radar graphics unit can be used to interface the RDR 2000 with the KNS 81 RNAV or the KNR 634 NAV equipment. When the RDR 2000 system is used with a GC 381A, the indicator will provide several pages of alphanumerical checklist data and waypoint information for display on the screen. The waypoint information is supplied by the KNS 81 (ten waypoints) or the KNR 634 (one waypoint). (11) The GC 360A radar graphics unit can be used to interface a KNS 660 NAV system to an RDR 2000 system by means of an ARINC 429 data bus. (12) The GC 362A TCAS graphics processor can be used to interface TCAS with the RDR 2000 system. (13) Table 4 lists the assemblies found in the ART 2000 along with their respective designator number series and connector designators.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519 Table 4. Printed Circuit Board and Assembly Designators PC Board or Assembly
Part Number
Reference
Connectors
Azimuth motor assembly
200-05174-0000
N/A
P4002
Scan sensor assembly
200-05313-0000
N/A
P5006
Gimbal assembly
200-05175-0020
N/A
N/A
Pitch motor assembly
200-05173-0010
N/A
P4003
Tilt sensor assembly
200-05554-0000
N/A
P5005
Receiver assembly
200-05553-0001
N/A
N/A
Preamp board
200-08545-0000
1000
J1002
200-08545-0020 Magnetron assembly
200-05310-0000
N/A
N/A
Power supply/modulator board
200-08548-0000
4000
J4001, J4002, J4003
5000
J5001, J5002, J5003, J5004,
200-08548-0020 200-08549-0000
Logic board
200-08549-0020
J5005, J5006, J5502
NOTES: 1 The logic board, PN 200-08549-0000, the preamp board, PN 200-08545-0000, and the power supply/modulator board, PN 200-08548-0000, are a matched set and are not interchangeable with boards with a part number that ends in -0020. 2 The logic board, PN 200-08549-0020, the preamp board, PN 200-08545-0020, and the power supply/modulator board, PN 200-08548-0020, are a matched set and are not interchangeable with boards with a part number that ends in -0000.
2.
Operation (TASK 34-40-11-870-802-A01) A.
Block Diagram Theory (Subtask 34-40-11-870-005-A01) (1)
Refer to Figure 2 for the following discussion.
(2)
Low-Voltage Power Supply (a)
The low-voltage power supply receives unfiltered 27.5 VDC from the aircraft bus and provides several voltages necessary to operate the unit. The low-voltage power supply consists of the following parts: • A hash filter to remove unwanted noise and spikes from the aircraft power bus • A low-voltage power supply • A timer circuit to hold the power supply on for a fixed amount of time after the unit is turned off. This time out is necessary so that the antenna is parked in the down position when the unit is turned off.
(b)
EFFECTIVITY ALL
The low voltage outputs from the power supply consist of filtered 27.5 volts, +5 volts, +15 volts, -15 volts, +24 volts, and +9.3 volts.
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COMPONENT MAINTENANCE MANUAL 071-01519 (3)
(4)
EFFECTIVITY ALL
Transmitter (a)
The transmitter portion of the radar consists of a high-voltage power supply, a pulse transformer, a magnetron, a magnetron isolator, a circulator, a harmonic filter, and the antennas.
(b)
The high-voltage power supply and the pulse transformer provide the magnetron with a pulse of 3600 volts at 3.5 amps for 4 µsec. The timing of the 4-µsec pulse is generated by the pulse timing circuit on the logic board.
(c)
Once the 4000-watt magnetron fires, the RF pulse passes through a magnetron isolator of 20 dB.
(d)
This isolator is necessary to protect the magnetron from being pulled in the case of a bad VSWR from either the antenna or radome. From the magnetron isolator, the RF pulse then passes through the three port circulator. This circulator allows the magnetron energy to pass through to the antenna and not on to the receiver. This circulator has a 20-dB reverse isolation.
(e)
From the three port circulator, the RF pulse then passes through the harmonic filter. This filter is a low-pass filter with a break point of approximately 12 GHz. This filter is necessary to reduce the power in the second harmonic of the magnetron in order to pass radiated harmonic specifications. The RF pulse is then radiated by the antenna into the atmosphere with a gain of either 26.0 dBi (10 inch) or 27.8 dBi (12 inch).
Receiver (a)
The RF pulse travels from the antenna at a rate approximately equal to the speed of light to a weather target and then is reflected back to the antenna. The antenna provides a gain to the received energy of either 26.0 dBi (10-inch antenna) or 27.8 dBi (12-inch antenna).
(b)
The received energy from the antenna is then passed through the harmonic filter into the three-port circulator. The three-port circulator prevents the received energy from passing towards the magnetron and allows the energy to pass to the receiver. From the three-port circulator, the received energy passes through the diode limiter.
(c)
The diode limiter is used to protect the receiver from the high amount of energy produced by the magnetron. Although the three-port circulator provides 20 dB of isolation to the receiver from the magnetron, there is still a very large amount of energy which is allowed to pass. The diode limiter is self biasing when a large amount of energy enters the input port. The limiter is then biased on and allows only 600 mW of power out the output port. The received signal is of low enough energy level to prevent self biasing of the limiter.
(d)
Once the received signal passes through the limiter, it is then passed on to the receiver module. The receiver module consists of a low noise amplifier, mixer, a LO, and a unity gain buffer. The total gain of the receiver module is 5 dB with a noise figure of 4.5 dB. The received signal is amplified, mixed, and the buffered 59-MHz IF is then sent to the preamp. The control of the LO will be further discussed in the AFC section of Paragraph 2.B. (Subtask 34-40-11-870-006-A01), Detailed Theory of Operation.
(e)
The preamplifier consists of a one stage amplifier with a gain of 30 dB with a noise figure of 3 dB and a temperature sensor (temperature sensor 2). This temperature sensor is used for all receiver calibration operations.
(f)
From the preamplifier the received signal is then passed to the IF section of the logic board. The IF consists of a 800-kHz band pass filter, two stages of gain, an active detector, a selectable low-pass filter of either 125 kHz or 250 kHz, and a video amplifier.
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COMPONENT MAINTENANCE MANUAL 071-01519 Also in the IF section of the logic board is the AFC sample amplifier which is used to supply a strong signal to the AFC circuit during the time the magnetron is firing.
(5)
(g)
The two stages of gain in the IF section are used to control the calibration and noise level of the receiver.
(h)
The first stage of amplification is the STC and the AGC will vary from 35 dB of gain to -5 dB of gain. The STC is used to calibrate the receiver to compensate for the two-way loss of energy through the atmosphere.
(i)
This gain level will vary with time starting with the magnetron fire and ending at either 30 nautical miles (10-inch antenna) or 35 nautical miles (12-inch antenna). Once the STC time is complete, the final gain level will be the AGC gain. The second amplifier is the manual gain control. The gain of this amplifier will vary from approximately 30 dB to 10 dB depending upon the gain setting selected by the pilot.
(j)
After the received signal is amplified to a calibrated level, it is then detected by an active detector with a gain of 20 dB. From the detector, the signal is once again filtered by a selectable low-pass filter. This filter is normally 250 kHz at the 3-dB break point, but on the 320-nautical mile range. The filter is switched to the 125-kHz low-pass filter. This switching of filters increases the receiver’s performance by reducing the noise of the signal by 3 dB. From the low-pass filter, the signal is buffered through a unity gain amplifier and passed on to the 8-bit video A/D converter.
AFC (a)
The AFC is used to control the frequency of the LO in the receiver module. The LO is mixed with the received signal and a 59-MHz IF frequency is produced. In order for the 59-MHz IF frequency to remain at 59 MHz, the AFC circuit must periodically adjust the LO to correct for magnetron frequency drift. The AFC circuitry consists of three basic parts: • Frequency sample circuit • Microprocessor • LO voltage drive circuit.
EFFECTIVITY ALL
(b)
During the magnetron fire, a small amount of energy is allowed to pass into the receiver and is mixed with the LO.
(c)
The IF signal is then amplified by the preamp and sent on to the IF section of the logic board. In the IF, the AFC amplifier increases the magnetron frequency sample to a level which activates the discriminator circuit. The output from the discriminator circuit is then passed on to a unity gain amplifier to the discriminator A/D converter. Eight samples from the discriminator A/D converter are saved in the STC RAM and recalled by the microprocessor for AFC control.
(d)
The microprocessor reads the eight samples from the STC RAM and determines if the IF is either too high, too low, or on frequency. If the LO is off by a large amount, either high or low, then the microprocessor drives the LO at large frequency steps. Once the IF is within a predetermined range from desired, then the microprocessor drives the LO by smaller frequency steps.
(e)
The LO drive circuitry consists of three 8-bit DACs. The output from these three DACs is summed together and sent to the receiver as the LO drive. The three DACs consist of the course, the fine, and the offset. The course sets up the nominal bias for the fine and offset, and has a range of approximately 24 volts. The offset is adjusted by the microprocessor in the AFC software procedure. The offset is also controlled by the microprocessor and accounts for the frequency pulling of the LO by the magnetron.
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COMPONENT MAINTENANCE MANUAL 071-01519 (6)
Weather Data Accumulator and 453 Transmitter (a)
The weather data accumulator circuit consists of the following: • Video A/D converter • Wx ROM • Weather compensation and extended STC circuit • Wx RAM • Radial sum circuit • 453 RAM • 453 serial data transmitter.
EFFECTIVITY ALL
(b)
The digitized video from the 8-bit video A/D converter is passed onto the lower eight address bits of the Wx ROM. The next six address bits of the Wx ROM are used for weather compensation control. The final four address bits of the Wx ROM are used for extended STC.
(c)
The output from the Wx ROM is an 8-bit video value adjusted for weather compensation and extended STC.
(d)
The weather compensation LSB is equivalent to 1 dB of signal attenuation due to intervening weather. The maximum amount of weather compensation is 32 dB of compensation. The ESTC increases the level of the returned signal by 10 dB at a linear rate from 40 nautical miles to 240 nautical miles. The ESTC provides additional STC range, but not at a true calibration rate.
(e)
The compensated video from the Wx ROM is then clocked into the Wx RAM at the range clock rate. The Wx RAM consists of 32 pages. Each page holds 256 bytes of compensated video from one radial for a total of 32 radials. At approximately 4 milliseconds after the magnetron fires, the radial summation starts. The radial summation sums all 32 radials and then divides the sum by 32 to obtain an average compensated video.
(f)
The 453 data format consists of 1600 bits of data. Bits 0 to 63 consist of control data and bits 64 thru 1600 consist of radial information. At the appropriate time, the microprocessor sends the first 64 bits of control data to the 453 RAM.
(g)
The average compensated video is transferred to the 453 RAM at approximately 5 milliseconds after the magnetron fires. During the transfer, the 8-bit average compensated video is converted to a 3-bit color level. Due to the nature of the 453 data format, 512 bins (3-bit color value) of radial information is sent during one transmission. Since only 256 bins of radial information have been collected, the 3-bit color value is repeated to give a total of 512 bins of information.
(h)
Once the data has been sent to the 453 RAM, the microprocessor then sends a request to the 453 transmitter to start transmitting data to the indicator. The data format of the 453 data transmission follows the modified ARINC 708 data specifications with compatibility to the RDS series radars. Refer to the Weather Accumulator and 453 Transmitter paragraph in Paragraph 2.B. (Subtask 34-40-11-870-006-A01) Detailed Theory of Operation, for more information on the 453 word.
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COMPONENT MAINTENANCE MANUAL 071-01519 (7)
Logic and Control (a)
The logic and control section consists of the microprocessor, its support circuits, and the 429 data receivers. The microprocessor is a Zilog Z8400 and is configured in a memory mapped input-output configuration.
(b)
The microprocessor and its support circuits consist of: • Microprocessor • 2 Meg of ROM • 12K of RAM • 2K of EEPROM • Reset and watchdog chip • Crystal oscillator • Four discrete 8-bit output ports • Five discrete 8-bit input ports • 16-input A/D port.
(c)
The EEPROM stores data such as: • Elapsed time of unit operation • Faults • Temperature of the unit when the fault occurred • Time when the unit failed • History of unit failure • Temperature calibration data.
(d)
The four discrete 8-bit outputs are divided into these four ports: • Mode control port • Machine cycle port • Configuration module port • General purpose port.
EFFECTIVITY ALL
(e)
The first 8-bit input port reads unit input discretes, such as R/T ON/OFF from indicators.
(f)
The second 8-bit input port is used as an R/T configuration port. This port provides inputs for configurations such as 10-inch or 12-inch antennas, transmit disable, scan disable, and several factory calibration switches.
(g)
The third 8-bit input port is used for factory calibration and gyro sign bits.
(h)
The fourth 8-bit input port is used for the configuration module.
(i)
The fifth 8-bit input port is used for altitude input.
(j)
Three of the five 429 receivers provide the microprocessor with control data from each controller/indicator. The fourth 429 receiver receives data from the pitch and roll gyro if the unit is configured to receive gyro data from the 429 receiver and not the analog ports.
(k)
The fifth 429 receiver receives altitude data.
(l)
There is one 429 transmitter, but it is used for test purposes only.
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COMPONENT MAINTENANCE MANUAL 071-01519 (m) The configuration module is mounted externally to the ART 2000 unit and remains with the aircraft when the ART 2000 is replaced on the aircraft. This configuration module stores the gain settings for the analog gyro, the ART 2000 configuration, and the type of indicator/controller being used in that particular aircraft.
(8)
(n)
This data is saved in the configuration module so that when an ART 2000 is replaced on an aircraft, the need to realign the gyro and reconfigure the newly installed ART 2000 is eliminated.
(o)
If the ART 2000 system is being installed for the first time, then a gyro alignment and equipment configuration is necessary.
Gyro and Antenna Stabilization (a)
The gyro and antenna stabilization circuit consists of three parts: • Analog gyro inputs • Azimuth and tilt motor drive circuits • Hall effect sensors.
EFFECTIVITY ALL
(b)
The analog gyro inputs consist of the 400-Hz reference, pitch, and roll. There are numerous gyro systems to which the ART 2000 must interface. Each of these systems have varying parameters from aircraft to aircraft. The gyro reference input can vary from 10 Vrms to 115 Vrms. The gyro reference input therefore has a switchable gain amplifier so that the same level of reference voltage may be applied to the detector circuit. The pitch and roll inputs are applied to fixed gain amplifiers and then detected. The detected outputs from the three signals are then integrated and multiplexed to a programmable amplifier. The gain values for the programmable amplifier are stored in the configuration module and applied to the amplifier when the appropriate input is selected.
(c)
The pitch and roll data is multiplexed by the microprocessor to the A/D converter and then read by the microprocessor. The pitch and roll data is then used to calculate the appropriate tilt of the antenna in accordance with the current azimuth setting. Once the tilt angle has been calculated, then the microprocessor determines if the tilt of the antenna should be increased or decreased from its current setting. The microprocessor in a fixed interrupt time, instructs the azimuth drive circuit and the pitch drive circuit to step their motors.
(d)
The azimuth motor drive circuit and the tilt motor drive circuit are located on the power supply/modulator/motor drive board due to the heat generated by the driver circuit. These drivers receive commands from the microprocessor to either step the motors up or down or not to step the motor at all. The azimuth and pitch motors are stepper motors and step the antenna in 0.05-degree steps.
(e)
The two Hall effect sensors are used to determine the position of the antenna in both the tilt and azimuth axis. The input voltage from the Hall effect devices is then multiplexed to the 16-input A/D converter.
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COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2. (Sheet 1 of 5) ART 2000 Block Diagram (GRAPHIC 34-40-11-99B-806-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2. (Sheet 2 of 5) ART 2000 Block Diagram (GRAPHIC 34-40-11-99B-806-A01)
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2. (Sheet 3 of 5) ART 2000 Block Diagram (GRAPHIC 34-40-11-99B-806-A01)
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2. (Sheet 4 of 5) ART 2000 Block Diagram (GRAPHIC 34-40-11-99B-806-A01)
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2. (Sheet 5 of 5) ART 2000 Block Diagram (GRAPHIC 34-40-11-99B-806-A01)
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COMPONENT MAINTENANCE MANUAL 071-01519 B.
Detailed Theory of Operation (Subtask 34-40-11-870-006-A01) (1)
General (a)
(2)
Refer to the appropriate schematics in the SCHEMATIC AND WIRING DIAGRAMS (PGBLK 34-40-11-2000) section of this manual.
Low-Voltage Power Supply (a)
The low-voltage power supply provides the voltages and approximate currents shown in Table 5. Table 5. Low-Voltage Power Supply Outputs
Voltage
Current
Wattage
+5 VDC
0.75 A
3.7 W
+15 VDC
0.18 A
2.7 W
-15 VDC
0.08 A
1.3 W
+24 VDC
0.01 A
0.2 W
+9.3 VDC
0.55 A
5.2 W
+28 VDC filtered (b)
(c)
ON_OFF and Antenna Stow Timer 1
To apply power to the ART 2000, the ON/OFF line P4001-14 is grounded which causes Q4021 and Q4023 to conduct. When Q4021 pulls the gate of Q4018 low, aircraft power is applied to the power supply. As +5 VDC is applied to the power OFF antenna stow timer, Q4023 is now on which turns Q4015 and Q4022 on. Q4015 lowers the voltage at the not_clear input which puts U4020 in the clear state and inhibits operation of the 15-second timer. The collector of Q4022 is low placing U4008 in preset. When the Q output of flip-flop U4008 is high, Q4019 is turned on in parallel with Q4021. The power supply is now in the ON state and remains unchanged during normal operation.
2
When P4001-14, the ON/OFF line, is ungrounded and allowed to go high (turned OFF), the emitter of Q4021 goes high and the collector of Q4023 goes low. Q4018 remains on because Q4019 remains on for 15 seconds as long as the Q output of U4008 is high.
3
Q4015 is off which removes the clear input and the 15-second antenna stow timer begins to charge C4054 toward the trip point of the monostable U4020. Q4022 is now off allowing the monostable circuit of U4020 to time out and trigger U4008 which is no longer held in preset. When the 15 seconds times out, the Q output of U4008 goes low turning off Q4019 which turns off Q4018 removing aircraft power from the power supply.
4
C4053, C4056, C4057, and CR4021 are used for the correct timing to assure proper turn on and off sequence.
Input Over Voltage 1
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The over-voltage sensor CR4022 does not conduct unless the aircraft power bus exceeds +36 volts. When CR4022 conducts, Q4017 conducts causing Q4018 to turn off and remain off for the duration of the transient. When the transient is removed, CR4022 no longer conducts and Q4018 is restored to normal operation.
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COMPONENT MAINTENANCE MANUAL 071-01519 CR4039 is a polarity diode for protection from negative transients as well as accidental reversing of input power polarity. Incorrect power supply polarity will blow fuse F4001. (d)
(e)
EFFECTIVITY ALL
Switching Regulators 1
Switching regulators U4005 and U4006 are used for +15 volts, -15 volts, +5 volts, +24 volts, and +9.3 volts. These regulators are capable of switching three amps each. Both are configured as Buck regulators operating at 72 kHz. Each device has an internal reference voltage of 5.05 VDC and an undervoltage lockout. A thermal shutdown circuit and a 3-amp overcurrent shutdown circuit are built-in. A frequency compensating resistor and capacitor are required at pin 5 of each regulator IC. Several voltages are supplied by one regulator by using transformer T4005. Only the 5-volt output is compared by the feedback loop and compared with the reference voltage, and is better regulated than the other voltages. The regulators provide 72-kHz pulses to the transformer or inductor which are used to temporarily store the energy.
2
When the charging pulse turns off, the current in the primary of the transformer T4005 changes direction and the circuit is completed by diode CR4015. The energy stored as flux in the transformer is transferred to the secondary and rectified by the diodes for each supply voltage. The +24 volt supply is derived from the 15-volt transformer winding by a voltage doubling rectifier CR4025 and CR4026 with C4063 and C40064. At each cycle, the 5-volt supply is sampled and compared to the reference in U4005. The pulse width is then changed to correct the output voltage. The 9.3-volt supply using U4006 is similar but has only one output voltage and an inductor L4001 is used for energy storage. C4030, C4042, C4073, and C4074 store energy for the switching regulators and, with L4004, decouple the switching spikes from the aircraft bus and reduce RFI emissions.
3
The worst case failure mode for Buck regulators is a dead short which allows the aircraft power to pass through unimpeded. An over-voltage protection circuit prevents damage if regulator failure occurs.
4
U4014 monitors the +5 VDC and U4015 monitors the +9.3 VDC. If either of these over-voltage monitors senses a high-voltage condition, SCR Q4020 is turned on which crowbars the input and blows the fuse.
Temperature Sensor 1
A temperature sensor is included to measure the internal temperature of the unit. The sensor (U4017) is an LM335 IC that behaves like a Zener diode with output voltage that is linearly proportional to absolute temperature. The output is summed with a temperature stable offset voltage from reference U4019. Amplifier U4018A is a high-impedance differential amplifier that buffers and provides DC offset for the sensor signal. U4018B is the scaling amplifier that provides a linear 0.5 to 5-volt signal for TEMP_SENSOR_1 (J4001-28) and TP4009 corresponding to -958 to +2282 F (-550 to +1250 C).
2
This DC signal is sent to the logic board (J4001-28) where it is converted to digital form for use by the microprocessor for adjusting gains.
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COMPONENT MAINTENANCE MANUAL 071-01519 (3)
Transmitter (a)
High-Voltage Power Supply 1
A flyback power supply provides the 250 to 350 VDC for the magnetron pulse modulator. U4001 is a pulse width controller IC that determines the oscillating frequency and pulse duration of the flyback power supply circuit. The operating frequency is approximately 25 kHz and the pulse width is controlled to provide the required high voltage. Power MOSFET Q4001 is switched by U4001 and provides a pulse of correct width to the flyback transformer T4001. Diode CR4001 rectifies the high voltage which is stored by low-loss film capacitors C4011 and C4013. This high voltage may be read with caution at TP4003. The multipurpose resistive divider string of R4021, R4028, R4029, R4020, and R4015 provides: • High-voltage bleeder resistor for C4011 and C4013 • Under-voltage sense to comparator U4002C for fault monitoring • Over-voltage sense to comparator U4002D for fault monitoring • Over-voltage sense to U4018/Q4028 for limiting.
2
The flyback operation is inhibited (pin 1 of U4001 low): • During the one minute start-up period • When HV_ENABLE is at logic 1 by microprocessor control • On over-voltage condition sensed at R4021.
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3
When MOSFET Q4004 turns on for 4 microseconds to create the magnetron pulse, the current demand at C4011 and C4013 is so high that the controller senses a momentary short circuit and the flyback controller restarts.
4
R4008 and C4004 cause the power supply to slow start after each modulator pulse and provide about 2 milliseconds of idle time.
5
This time is the receiver quiet time when it is desirable to have this circuit turned off to reduce switching noise. C4007 filters the internal reference voltage while R4009 and C4008 are the flyback oscillator timing elements for 25-kHz operation.
6
The waveform at TP4002 is a damped 25-kHz oscillation peculiar to flyback power supplies which is interrupted at 10-millisecond intervals by the magnetron pulse. It is difficult to view because of variation in each cycle. CR4009 clamps any negative transients that may occur. The output from the controller drives a MOSFET Q4001 which switches the primary of T4001 to ground. The transformer ratio is only 1:2.5 but flyback action provides much higher output voltage. Current is sensed across R4013 in the source path of Q4001 and supplies information to the flyback controller, U4001. Both the 25-kHz flyback switching rate and the magnetron pulse repetition rate of 106 each second place heavy demands on the energy supply capacitors C4009 and C4134. C4010 helps keep high-frequency switching noise from the input power leads. There are effectively two pi-section filters using both inductors L4004 and L4003 to prevent radiation from the high-voltage power supply through the power leads.
7
An over-voltage condition is sensed by the resistive divider (R4021, R4028, R4029, R4020, and R4015). The voltage sensed at R4021 is compared by U4018 to a reference voltage of 2.5 volts divided from 5.0 volts by R4026 and R4027. The output of the comparator U4018 controls transistor switch Q4029 to inhibit the flyback controller by pulling pin 1 of U4001 low. This happens very briefly and the
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COMPONENT MAINTENANCE MANUAL 071-01519 power supply maintains the upper voltage limit of 350 VDC if the current control loop should malfunction.
(b)
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8
Fault sensing information is provided by the over_under_voltage sensors. Over-voltage is sensed across R4021 and R4028 from ground and is compared to 5 VDC in U4002D. Under-voltage is sensed across R4021, R4028, and R4029 to ground and compared in U4002C to 5 VDC.
9
If either fault conditions exists, the OVER_UNDER_VOLTAGE output to the FPGA (U4011 pin 39) goes to logic 0.
10
The one minute turn-on timer for the magnetron warm up is initiated when the unit is turned on and is timed by R4022 and C4019. This time is normally about one minute but for short interruptions, requires about the same reset time as the duration of the interruption. The magnetron filament requires a minute to warm up when cold but can recover faster from short interruptions. The comparator U4002A holds pin 1 of U4001 (TP4001) low until the time out period expires. When the radar is turned on but in a nontransmitting mode, the HV_ENABLE input (J4001-13) is high and the high-voltage power supply will not operate. For brief power interruptions, it may require longer for the microprocessor to reset than for the high-voltage power supply to be operational again. Under these circumstances, the HV_ENABLE is high to inhibit the high voltage.
Pulse Forming Network 1
A 0.15-ohm sense resistor (R4195) is in the ground return of the secondary of the pulse transformer T4002. The pulse current for the magnetron is sampled across R4195 and the resulting voltage is differentially amplified to minimize noise by U4059. The pulse may be observed at TP4020 but will be distorted. Viewing the current pulse with a current probe is more reliable. U4058 is a dual multivibrator IC which provides the proper delay and width for a sample-hold window. Timing elements R4208 and C4146 set the delay time for the first one-shot at 2 microseconds and a 1-microsecond pulse width for the sample window is determined by R4206 and C4145 of the second one-shot.
2
This gate signal, which can be viewed at TP4015 as a positive-going logic pulse, is used to open the sample gate (U4060) for 1 microsecond and charges capacitor C4144. R4221 and C4144 integrate the error signals from several cycles. Op amp U4061A buffers the output and maintains a very high impedance so the sample capacitor C4144 is not loaded.
3
U4061B amplifier supplies the error voltage for the pulse-width flyback controller U4001. The error signal, which can be measured at TP4014, is compared to the internal reference of U4001 and the flyback pulse width is adjusted so this voltage will be forced to 2.5 volts. The gain of U4061B is adjusted by R4200 for the correct high voltage at the primary of the pulse transformer T4002 to provide a 3.0-amp magnetron pulse. U4061C and U4061D are used as comparators to establish a window to sense abnormally high or low pulse current. If current is high (shorted magnetron) or low (open magnetron), a missing pulse indication is present at TP4015 as a 4-microsecond, 5-volt positive pulse. The MISSING_PULSE signal is sent to the FPGA (U4011) pin 40 for processing. A missing pulse indication may also be caused by loss of filament voltage, shorted or open wires, arcing, or other problems.
4
The pulse width and repetition rate is determined on the logic board and applied to the modulator as MAG_FIRE_OUT (J4001-12). Diode CR4008 holds the one-shot
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COMPONENT MAINTENANCE MANUAL 071-01519 U4020 in clear so no pulses pass unless the HV_ENABLE and 1-minute start-up timer are satisfied. A one-shot (U4020) is started by the MAG_FIRE_OUT pulse and limits the pulse width to less than 6 microseconds. An accidental pulse of longer duration would damage the receiver/limiter and possibly the magnetron. 5
The MAG_FIRE_OUT pulse shape is kept square by the DRIVER U4003 which provides sufficient current to drive the power MOSFET Q4004. This rectangular pulse may be observed as a 15-volt rectangular pulse at TP4004 with a turn-on distortion caused by driving the MOSFET switch.
6
The modulating pulse may be seen at TP4008 as an undistorted 5-volt logic pulse. The power MOSFET switches the primary of the pulse-modulation transformer T4002 to ground.
7
The SCR circuit Q4007 is a tail-chopper to speed the fall time of the pulse and help reset the pulse transformer core for the next pulse. When the pulse voltage across the transformer begins to fall, the gate turns on and fires the SCR, dumping any remaining charge rapidly into R4014. Diodes CR4009 and CR4010 are reverse-spike clamp diodes to prevent damage to the MOSFET from negative transients.
8
Pulse transformer T4002 with a turn ratio of about 1:11, steps the pulse voltage up to 4600 volts nominal. All connections are insulated so there is no point to measure the pulse voltage out of the transformer. The secondary of the pulse modulation transformer carries the filament voltage for the magnetron and the high-voltage negative pulse. Approximately 3.7 volts of the filament voltage are lost in the transformer resistance and diode CR4040 which leaves 6.3 VDC at the filaments.
9
It is not recommended to measure the filament voltage at the magnetron because of the high-pulse voltage. Diode CR4040 helps isolate the secondary so all the current passes through the sense resistor R4195.
10
Since it is impossible to measure the magnetron current by placing a current probe over the shielded leads, a port has been cut in the power supply board to accommodate a Tektronix current probe. The probe can be used from either side of the board but polarity will be reversed from the component side.
11
Filament current for the magnetron flows both directions in these paths and will NOT be added to the pulse current measurement. The current probe should be used when adjusting R4200 for the correct high voltage required for 3.5 amps of magnetron current and to select the best inductance value for L4009 to minimize the slope of the pulse. NOTE:
(c)
Magnetron 1
(d)
ALL
The negative pulses are applied to the cathode of a grounded anode, fixed frequency, X-band, pulse magnetron. The output of the magnetron is nominally 6 kilowatts at 9375 MHz for 4 microseconds. The filaments require 6.3 VDC at 550 milliamps. There are no adjustments to the magnetron.
RF Network 1
EFFECTIVITY
Pulse modulation causes extremely high currents to circulate in ground paths. Nominal currents of 30 amps are present in the pulse transformer primary. Troubleshooting with scope or voltmeter is difficult.
An E-plane isolator, an E-plane three-port circulator, and a harmonic filter are combined in an integral unit. The diode limiter, magnetron, and antenna are
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COMPONENT MAINTENANCE MANUAL 071-01519 mounted to the RF network with waveguide connections. The isolator section provides 20 dB of magnetron isolation to reduce the pulling effects of bad load caused by radome or antenna problems. The circulator passes the transmitted pulse to the antenna and block the path to the receiver. The circulator has 20 dB of isolation between the two parts. Filter sections are located between the circulator and the antenna to prevent radiation of harmonics. Signals that return from a target are passed by the circulator to the receiver and blocked from the magnetron. (e)
(4)
Diode Limiter 1
The circulator provides 20 dB of isolation between the magnetron and the receiver but this would be enough RF to damage the receiver. A diode limiter is inserted at this point to limit the RF entering the receiver to 100 mW maximum. The diodes are self-biasing from the RF and require no connections other that the waveguide. There are no adjustments and the diodes are not replaceable.
2
A filter is included in the diode limiter to prevent the destruction of the receiver from any off-frequency RF caused by a magnetron misfire.
Receiver (a)
Low-Noise Front End 1
(b)
59-MHz Low-Noise Preamplifier 1
(c)
A low-noise MMIC, I1001, provides a noise figure of less than 3 dB and gain of 31 dB. Power is supplied from the logic board through the coaxial cable center conductor. This coax also takes the output signal from the preamp to the IF section on the logic board. The input is isolated by capacitor C1002. The IC amplifier is designed for 50-ohm terminations and grounding is extremely important.
Temperature Sensor 1
(d)
The X-band receiver module is not repairable and has no adjustments. It consists of a low-noise preamplifier, an image canceling mixer, a LO, and buffer amplifier. The LO frequency is 59 MHz above the received frequency and is tuned with a voltage derived from the AFC circuit. The noise figure is 4.5 dB at 9375 MHz and the 59-MHz output has an overall gain of about 5 dB.
The casting temperature is sampled by a sensor to supply data enabling the software to make gain corrections. The sensor, U1002, is an LM35 which is similar to a zener diode with a voltage output that increases linearly 10 millivolts/ C. The voltage from a temperature-compensated reference, U1004, is divided by R1002 and R1003 then buffered by amplifier U1003A to provide a reference voltage of 0.5 volts. Amplifier U1003B has unity gain and provides a high-input impedance and signal inversion for the temperature sensor. Output at J1002-2 is 1.85 volts to 0.6 volts changing linearly with temperature from -67 to +158 F (-55 to +70 C).
59-MHz IF Strip 1
The 59-MHz IF section receives down-converted signals from the receiver module through the preamplifier and the coax cable to jack J5502. There is approximately 48 dB of gain in the receiver/preamp assembly. The actual amplitude of these signals depends upon the amount of moisture in clouds or the reflective surface in map mode, and the distance to the target.
2
The video IF section performs: • IF passband filtering
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519 • Main IF amplification and detection • Manual gain, automatic gain, and STC • Video buffering and limiting • Video bandwidth filter switching.
(e)
EFFECTIVITY ALL
a
A resistive divider (R5551, R5552, R5555) splits the input signal from J5502 for the main video IF and the AFC limiting IF amplifier that drives the discriminator. Resistors R5511 and R5512 are used to supply operating current to the preamp board through the signal coax cable.
b
Two capacitively-matched and coupled inductor-capacitor pairs, L5501/C5527, C5501, or C5528, and L5502/C5543, C5504, C5503, or C5529, with coupling capacitor C5502 provide most of the filtering for the main IF. C5528, C5529, and C5543 are temperature-compensating capacitors to minimize changes at temperature extremes.
c
Amplifier U5501 provides up to 45 dB of gain and is gain controlled by the STC/AGC control voltage received from amplifier U5122A. Input to this amplifier is high-impedance and single-ended from the bandpass filter. Differential output through T5501 provides a match to I5502 and helps shape the IF passband. STC gain control is applied to pin 5 of this amplifier.
d
IC U5502 is gain controlled by the MAN_GAIN_DRIVE voltage received from amplifier U5028C. It provides up to 45 dB of gain.
e
Both the input and the output are differential with T5502 providing additional passband shaping and impedance matching into the detector, Q5501.
f
Q5502 is connected as a bias diode for the detector, Q5501. L5506 and C5517 trap the 59-MHz IF signal and pass the video. The detected output pulse from Q5501 may be as high as 12 volts at the detector so it is voltage divided by R5510 and R5509 to a level below 5 volts.
g
Detector video output is filtered above 125 kHz by C5520 when transistor Q5503 is turned on. This integrates the return signal and the pulse viewed at TP5023 is rounded. Normal operation with Q5503 turned off will have at least 250-kHz bandwidth.
h
Video buffer amplifier U5503 has unity gain and the output a signal of less than 5 volts for the A/D converter U5036. R5550 helps isolate the amplifier from spikes generated in the A/D converter.
Receiver Gain Control 1
The receiver gain control consists of two major functions, the manual gain and the STC/AGC. Manual gain is used by the pilot to decrease the gain of the receiver to reduce target saturation. The manual gain is to be decremented the gain of the receiver 20 dB in 1-dB steps. The STC/AGC is used to account for the attenuation of the RF energy through the atmosphere and then to control the final gain of the receiver.
2
The manual gain circuit consists of three major sections. The first section is the manual gain drive circuit consisting of the quad DAC (U5027) and an op amp (U5028). Section two consists of the IF amplifier (U5502). The third section is the microprocessor and the 429 control word from the indicator/controller.
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COMPONENT MAINTENANCE MANUAL 071-01519
EFFECTIVITY ALL
3
When the pilot varies the manual gain at the controller, the gain value which is sent by 429 digital data bus will vary from 0 dB of attenuation to a maximum of 20 dB of attenuation. The microprocessor reads the manual gain value from the 429 receiver and then sends a digital value to the manual gain DAC. This 8-bit value varies the voltage out of U5027-pin 19 from 0 volts to 5 volts. This voltage is then amplified by U5028 to a voltage range from 0 volts to 12 volts as measured at test point TP5007. The manual gain voltage is then applied to R5505 which converts the voltage to a current and then onto U5502 (manual gain amp). U5502 is an IF amplifier with controllable gain. The gain of U5502 will vary from approximately 30 dB to 10 dB in 1-dB steps.
4
The STC/AGC circuit consists of four major sections. The first section is the STC/AGC drive circuit which consists of the STC RAM (U5118), the STC DAC (U5119), the STC op amp (U5122), and the STC output controller (U5037). Section two consists of the gain-controlled IF amplifier (U5501). The third section is the video A/D converter (U5036) which is used to sample the video noise level. The last section is the microprocessor which reads the video level and then sends a new control voltage to the IF amp through the STC/AGC drive circuit.
5
The STC RAM (U5118) is used for three functions. The first eight memory locations hold the discriminator A/D converter samples during magnetron fire. This is further discussed in the AFC paragraph of this section. The second function is to hold the STC curves for both weather and map. The third function is to hold the current AGC value in the last STC location.
6
Memory locations 8 thru 224 (10-inch antenna) or 255 (12-inch antenna) hold the STC curves. The STC RAM (U5118) is further divided into two pages. Page 1 is for weather STC curves and Page 2 is for MAP curves.
7
When the mode is changed from weather to MAP or MAP to weather, the MSB of the STC RAM is toggled to change the current page.
8
Once the magnetron has fired, the STC curves are clocked out of the STC RAM by the STC circuit, U5037. This circuit controls the output so that each memory location is approximately equal to one third of a nautical mile. Due to the dynamic range of the receiver being approximately 38 dB, the STC can only control the receiver’s gain for the first 30 nautical miles for the 10-inch antenna, or 35 nautical miles for the 12-inch antenna. Beyond the this range, a second receiver calibration method is used. This second calibration method is called the ESTC. The ESTC will be discussed in the Weather Accumulator and 453 Transmitter paragraph of this section.
9
Once the STC curve reaches the maximum limit, the last value to be output is the AGC setting. This level is set so that the receiver is at maximum gain. When the receiver is at maximum gain, the noise at the front end of the receiver is amplified to a level that should not cross the green threshold. If the green threshold is exceeded by the noise, then the radar screen will show false targets. In order to reduce false targets, the AGC alters the gain of the receiver so that the noise floor is just at the threshold of green, but not exceeding it.
10
During the radar quiet time, approximately 7 milliseconds after the magnetron fired, the microprocessor reads the video voltage from the video A/D converter, U5036.
11
This video value is filtered by the microprocessor and then compared to a noise threshold value. If the filtered value is not equal to the noise threshold value, then
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COMPONENT MAINTENANCE MANUAL 071-01519 the microprocessor will then either increase or decrease the value written to the AGC memory location, last STC value. (f)
EFFECTIVITY ALL
AFC 1
The AFC function consists of five major sections. The first section is the LO drive circuit which consists of the LO DAC (U5027), the gain adjust op amp (U5028), and the summing op amp (U5144). The second section is the frequency discriminator circuit which consists of the limiting amplifiers (U5504 and U5505), the discriminator (U5506), the discriminator adjust coil (L5524), and the discriminator buffer (U5507). The third section is the discriminator A/D converter (U5030) and STC RAM (U5118). The fourth section is the LO within the receiver module. The fifth section is the transmitter fault section which consists of the missing pulse detection circuit and the high/low voltage fault. The fault detection circuits are discussed in the Power Supply paragraph of this section.
2
The AFC circuit is used to maintain a 59-MHz separation between the magnetron and the LO. When the magnetron frequency is mixed with the LO frequency, the 59-MHz IF is produced. This 59 MHz is amplified and sent on to the discriminator circuit in the IF section of the logic board.
3
The first AFC IF amplifier, U5504, has single-ended coupling both in and out and provides about 40 dB of fixed gain with the gain control connected to ground through R5525. The second amplifier, U5505, is also single ended both in and out with gain fixed at maximum by R5527. These stages do not have tunable matching elements and therefore have less gain than the video IF section.
4
A network of L5539 and C5568 matches the IF amplifier to the discriminator. U5506 is a four-quadrant multiplier connected as a quadrature detector with amplitude-limited IF signals applied to both ports of a balanced mixer with one port shifted in-phase by L5524/C5542/C5576, a temperature-compensated L/C phase-shift network.
5
C5576 is a temperature-compensating capacitor that minimizes the changes at temperature extremes and assures that the discriminator tracks the IF filter. The output as seen at TP503 and TP504 is a differential voltage. U5507A amplifier has a differential input. The output signal is buffered and referenced to the 2.5-volt reference level in U5507B, then sent to the A/D converter U5030. The frequency error pulse can be viewed at TP5018 which is the signal read by the A/D converter but it may contain noise spikes from the A/D conversion process.
6
The output from the discriminator buffer, U5507, is then sent to the discriminator A/D converter, U5030. The digitized value is temporarily stored in the STC RAM, U5118, during the magnetron fire time frame. The 4-microsecond pulse from the magnetron is sampled eight times at a 2-microsecond delay from the beginning of the pulse. Due to the speed of the samples, the microprocessor can not read eight samples this quickly and so the STC RAM is used.
7
At approximately 6 milliseconds after the magnetron has fired, the microprocessor reads the missing pulse fault flag and the high/low voltage flag from the power supply board. If no faults occurred, then the microprocessor reads the contents of the first eight memory locations of the STC RAM which holds the discriminator frequency data. The microprocessor then filters the data and determines if the LO is on frequency. If the LO is either too high or too low, then the microprocessor adjusts the digital value being sent to the LO drive circuit.
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COMPONENT MAINTENANCE MANUAL 071-01519
(5)
EFFECTIVITY ALL
8
The LO drive circuit consists of three DACs. The first DAC, U5027-pin 20, is used to establish the course setting or initial bias of the LO drive. The second DAC, U5027-pin 1, is used for frequency offset. The frequency offset is used to compensate for the fact that during the magnetron fire period, the magnetron produces so much energy that it tends to pull the LO towards the magnetron’s frequency.
9
This pulling causes the LO to be off frequency during the AFC sample period which produces an erroneous AFC sample. Since the LO pulling is a fixed frequency, the offset is set to a fixed value depending upon the amount of pulling. Both the course and offset values are determined by the AFC calibration procedure. The third DAC, U5027-pin 2, is the fine adjust. The fine adjust is the active AFC output during normal radar operation. This value is generated by the microprocessor as determined by the values received from the discriminator circuit. The outputs from the three DACs is then summed at the LO drive op amp, U5144, and then sent to the receiver module.
Weather Accumulator and 453 Transmitter (a)
The weather accumulator and 453 transmitter circuit receives video data from the video buffer and produces ARINC 453 data at the output. This conversion process involves the steps that follow.
(b)
Step 1 1
The first step is to convert the analog video to compensated digital data. This is accomplished by the video A/D converter (U5036), the Wx ROM (U5038), the Wx RAM (U5039), and the STC FPGA (U5037).
2
From the video A/D converter the data is then applied to the Wx ROM (U5038). The Wx ROM has three separate input parameters. The first input parameter is the raw digitized video. The second input parameter is weather compensation and the third input parameter is ESTC.
3
These three parameters (raw video, weather compensation, and ESTC) are applied to the Wx ROM address lines. When the appropriate address is selected, a compensated digital value is sent to the Wx RAM (U5039) and saved at the range clock rate.
4
Weather compensation and ESTC are firmware functions embedded in the STC FPGA (U5037).
5
Weather compensation is used to increase the strength of the video due to the attenuation caused by intervening weather.
6
The weather compensation algorithm sums up the weather returns in a weighted fashion. Yellow is the LSB value, red is a value of six, and magenta is a value of 37.
7
The sum is located in a 12-bit register. The lower four bits are truncated leaving the upper eight bits. The LSB of the weather compensation output to the Wx ROM is equivalent to 1 dB of intervening weather attenuation. When these values increase in number, they cause the Wx ROM to increase the digital value of the video sent to the Wx RAM.
8
The ESTC is used to increase the amplitude of the signal once the dynamic range of the STC has been exhausted, approximately 30 to 35 nautical miles.
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COMPONENT MAINTENANCE MANUAL 071-01519
(c)
(d)
9
From 40 nautical miles to 240 nautical miles, the address sent to the Wx ROM will increase every 10 nautical miles. This change in address increases the compensated video being sent to the Wx RAM.
10
This is not a calibrated compensation such as STC, but it is an attempt to provide the pilot with a more accurate presentation of the weather beyond the STC range.
Step 2 1
The second step in the process of converting analog video into ARINC 453 data is to filter the data using the weather accumulator.
2
The weather accumulator (U5057) provides a filter algorithm which sums 32 radials and produces the filtered output.
3
This filtered output is then stored back into the Wx RAM and is ready to be converted to ARINC 453 data.
Step 3 1
The third step in the conversion process is to transfer the weather data from the Wx RAM to the 453 RAM. The weather data to 453 data transfer is performed by the 453 FPGA (U5041).
2
This transfer process consists of converting the 8-bit digital data value to a 3-bit color value as shown in Table 6. Table 6. Digital Data to Color Value Conversion
8-Bit Digital Data Value
3-Bit Color Value
000
Black
001
Green
010
Yellow
011
Red
100
Magenta
(6)
3
Once the color value has been determined, the value is then repeated to conform to the format of the ARINC 453 word. (The 453 data word allows for 512 range bits. Since only 256 range bit samples have been collected, the number must be doubled to fill in the unused range bits.)
4
The microprocessor fills the 453 RAM with the first 64 bits of control data. Once the 453 RAM is filled with data, the microprocessor commands the 453 FPGA to start transmitting data to the indicator through the 453 data transmitters (U5125).
5
The 453 data consists of 1,600 bits of data being sent at a 1-MHz rate. The total word transmission time is 1.6 milliseconds. The transmission rate between words is approximately 7.5 milliseconds.
Logic and Control (a)
The logic and control section consists of four major sections: • Microprocessor and the microprocessor support circuits • Discrete input/output ports
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519 • ARINC 429 receivers and transmitter • Multiplexed A/D converter. (b)
The microprocessor and supporting circuits consist of the following chips: • Z8400 microprocessor (U5001) • Software ROM (U5003) • Microprocessor RAM (U5004) • Microprocessor nonvolatile RAM (U5005) • Reset and watchdog chip (U5002) • Microprocessor chip select FPGA (U5012) • FPGA ROM (U5013) • Microprocessor clock (Y5001) • Data bus buffers (U5014, U5015, U5016, and U5126).
(c)
Upon unit power up or reset, the reset/watchdog chip (U5002) holds the reset output low until the 5-volt supply becomes stable.
(d)
The output of the reset/watchdog chip is applied to an open collector NAND chip (U5125). This output is wired in an OR configuration to the four FPGA DP lines which are also open collector outputs.
(e)
The four FPGAs (U5012, U537, U5041, and U5057) hold their DP lines low until they have been programmed.
(f)
Once all four FPGAs have been programmed and the 5-volt supply is stable, the microprocessor reset line is pulled high by R5157.
(g)
The programming of the four FPGAs is controlled by the master FPGA (U5012).
(h)
The three slaved FPGAs (U5037, U5041, and U5057) are programmed by the master. When power up or reset occurs, the reset circuit in the master FPGA causes the FPGA to go into a self-programming mode.
(i)
In this mode, the master FPGA reads programming data from the FPGA ROM (U5013). This data is sent in serial format from the DOUT pin of U5012 to the DIN pin of U5041. From the DOUT pin of U5041 the serial data is sent to the DIN pin of U5037. The data is then sent out the DOUT pin of U5037 to the DIN pin of U5057.
(j)
After an FPGA has been programmed, the DP line is allowed to go high. When all four FPGAs have been programmed, the LCA DONE line, or microprocessor reset, goes high bringing the microprocessor out of reset.
(k)
Once the microprocessor is out of reset, it will start to execute software code which is stored in the microprocessor ROM (U5003).
(l)
The microprocessor accesses two RAMs, the first being the static RAM (U5004) and second being the nonvolatile RAM (U5005).
(m) The static RAM is used to store variables which are used during normal microprocessor operation and can be lost when the unit is powered down. (n)
EFFECTIVITY ALL
The nonvolatile RAM holds data that the microprocessor must save even when the unit is power downed. This data consists of, but not limited to, time of unit operation, unit fault history, and receiver calibration data.
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COMPONENT MAINTENANCE MANUAL 071-01519 (o)
The microprocessor data bus is buffered by U5014, U5015, U5016, and U5126. Due to the number of devices connected to the microprocessor data bus, the microprocessor data bus is divided into four separate data buses to prevent bus loading. The four buses consist of: • IOD bus which drives the discrete input/output ports • SLD bus which controls the slower chips on the data bus • ALD bus which controls the gyro and 453 data bus • SD bus which controls the frequency discriminator and the STC bus.
(p)
During normal operation, the microprocessor is interrupted at a 409-microsecond rate. This rate causes the microprocessor to execute a predefined task. These tasks are repeated every 60 interrupts.
(q)
On interrupts 0, 20, and 40, the microprocessor sends a request to the chip select FPGA to generate the 4-microsecond magnetron fire pulse. This magnetron fire pulse is then sent to the pulse-forming network on the power supply board.
(r)
The discrete input/output ports consist of U5006 thru U5011, U5017, U5019, and U5043.
(s)
There are five discrete input ports (U5006, U5007, U5017, U5019, and U5043) and four discrete output ports (U5008 thru U5011). 1
2
Input Port 1 a
Input port 1 (U5006) is the indicator ON/OFF port. This port tells the microprocessor which indicators are on and which ARINC 429 channel to listen to.
b
This port also is connected to the strut switch. The strut switch will shut off the transmitter, if connected to the aircraft strut switch (not in radar indicator only installations), when the aircraft is on ground.
Input Port 2 a
3
EFFECTIVITY ALL
Input port 2 (U5017) is the DIP switch input port. All but DIP switch 4 and 5 are used for bench test purposes only. (1)
DIP switches 1 and 2 turn off the transmitter and the antenna motors.
(2)
DIP switch 3, the equipment configuration enable, allows the installer to change the contents of the configuration module if enabled.
(3)
DIP switches 4 and 5 determine the antenna size and tells the microprocessor what size of antenna is connected to the radar.
(4)
DIP switch 6 is used in test mode only when the time, temperature, and fault history needs to be read from the ARINC 429 transmitter.
(5)
DIP switch 7 is reserved for a recalibration or a hard start switch.
(6)
DIP switch 8, the receiver calibration enable, allows the radar to be calibrated when enabled.
Input Port 3 a
Input port 3 (U5007) is the receiver calibration port. These inputs, in conjunction with DIP switch 8, allow the radar to be calibrated. The calibration procedures consist of the AFC calibration and the receiver calibration.
b
Also connected to input port 3 is the gyro sign bits. These bits will be discussed in the gyro input section.
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COMPONENT MAINTENANCE MANUAL 071-01519 4
5
Input Port 4 a
Input port 4 (U5019) is a general purpose input port. This port accepts input serial data from the configuration module.
b
Also input into this port is the target alert bit from the STC FPGA. When the STC FPGA detects a target beyond the selected range, this bit is set.
Input Port 5 a
6
7
8
EFFECTIVITY ALL
Input port 5 (U5043) is the altitude input port. The altitude information is received in ARINC 575 gray code format. This information is used in the AutoTilt function of the ART 2000.
Output Port 1 a
Output port 1 (U5008) is the mode control port. When the range or mode is changed, this port directs the hardware to react according to the new outputs.
b
When the 320-nautical mile range is selected, the bandwidth switch goes high enabling the narrow bandwidth in the IF section.
Output Port 2 a
Output port 2 (U5009) is the machine cycle port. This port controls the timing of the hardware throughout a machine cycle (a machine cycle is the time between magnetron fires).
b
If range or mode is changed, the STC circuit, the ARINC 453 circuit, and the weather accumulator circuits are reset.
c
After the magnetron has fired, the radial sum enable toggles from low to high and then back to low. This causes the Wx ACC FPGA (U5057) to start the video filtering.
d
Once the video filtering has been completed, the microprocessor toggles the weather to the ARINC 453 transfer bit which initiates the transfer of weather data to the ARINC 453 RAM.
e
When the 453 data is ready to be transmitted, the 453 enable bit toggles low to cause the 453 FPGA to start 453 transmission.
f
The 429 reset bit resets the 429 LSI chip (U5091) when it is toggled from high to low.
Output Port 3 a
Output port 3 (U5010) is a general purpose port. The microprocessor reads input port 2 to determine what size of antenna the unit has been configured for.
b
If an improper code has been entered at input port 2, the microprocessor sets the output bits at output port 3 to a 10-inch antenna by default.
c
The RDS type output bit is reserved for future use.
d
Wx compensation disable is also reserved for future use.
e
The high-voltage disable goes high 60 seconds after the microprocessor has been reset. This bit causes the high voltage to be disabled while the magnetron is warming up.
f
The 429 select bit is used to multiplex 429 ports 3 and 5 to the 429 LSI. Since the 429 LSI has only four input ports, it is necessary to multiplex two ports into one.
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COMPONENT MAINTENANCE MANUAL 071-01519 9
(t)
(u)
(7)
Output Port 4 a
Output port 4 (U5011) is the configuration module port. The configuration module is mounted externally to the radar and is intended to stay with the aircraft.
b
This module holds the analog gyro gain settings and aircraft equipment configuration. This port along with input port 4, talks and listens to the serial nonvolatile RAM in the configuration module.
The third major section of logic and control is the ARINC 429 receivers and transmitter consisting of U5091 and U5025. There are five receivers and one transmitter. 1
The first three receivers are connected to the indicator/controllers. The forth receiver is used in the aircraft for 429 pitch and roll data input and on the bench for self-test and calibration purposes. The fifth 429 receiver is used for altitude data input.
2
Since the 429 LSI (U5091) has only four input ports, the third and fifth inputs are multiplexed through U5025 to the 429 LSI.
3
The 429 transmitter is used for bench test purposes only.
The fourth major section of logic and control is the multiplexed A/D converter which consists of U5022, U5023, and U5024. Fourteen separate analog inputs are multiplexed through U5022 and U5023 to the A/D converter U5024. 1
Two of the inputs are the temperature sensors which monitor the temperature of the power supply and the preamplifier. Another two inputs are used to read the Hall effect sensors.
2
The Hall effect sensors are used by the microprocessor to determine the position of the antenna. The sensors themselves are located in the gimbal assembly.
3
The output from the Hall effect sensors are then amplified through U5021 and U5022 and applied to the multiplex A/D converter. The output from the Hall effect circuit will vary from approximately 0.5 volts to 4.5 volts.
4
The gyro input has been multiplexed by the gyro circuit so that the gyro input line may consist of reference, pitch, and roll.
5
The remaining inputs are unit voltages. These voltages are monitored for fault detection.
Analog Gyro Input (a)
The analog gyro (gyro) input consists of four major sections: • Reference input • Pitch input • Roll input • Programmable amplifier.
EFFECTIVITY ALL
1
The reference input consists of the differential input amplifiers (U5159a and U5163), the rectifier and integrator (U5159b, CR5022, R5294, and C5085), the gain adjust amplifier (U5159c), and the reference chop circuit (U5033b).
2
The pitch input consists of the input differential amplifier (U5034a), the rectifier and integrator (U5034b, CR5019, R5083, and C5041), the gain adjust amplifier (U5034c), and the pitch sign bit (U5034d, U5163a, and U5033a).
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COMPONENT MAINTENANCE MANUAL 071-01519
EFFECTIVITY ALL
3
The roll input consists of the input differential amplifier (U5035a), the rectifier and integrator (U5035b, CR5011, R5105, and C5056), the gain adjust amplifier (U5035c), and the roll sign bit (U5035d, U5163d, and U5033d).
4
The programmable amplifier consists of the analog multiplex chip (U5162), the gain data buffers (U5169 and U5168), the multiplying DAC (U5165), the unity gain current-to-voltage operational amplifier (U5160d), and the fixed gain amplifier (U5160a).
5
The gyro inputs are used to stabilize the antenna so that the antenna scans parallel to the earth while the aircraft is in a pitch or roll attitude.
6
The reference input can vary from 10 Vrms to 115 Vrms. Since the reference voltage is of such a large range, the input amplifier has switchable gains. The configuration module contains data on which range of reference voltages are applied to the unit.
7
There are three different selections which consist of 115 volts, 26 volts, and 10 volts. a
If 115 volts is selected, U5163-pin 9 will go high and place R5224 in parallel with R5223 to establish the proper gain.
b
If 26 volts is selected, U5163-pin 8 will go high and place R5225 in parallel with R5223.
c
If 10 volts is selected, R5223 will be the only resistor in the operational amplifier feedback network.
8
Once the reference gain has been established at the differential input operational amplifier (U5159a), the signal is then applied to the detector and integration circuits, and the chopper circuit.
9
The detector and integration circuit converts the sign wave into a DC value which is applied to the fixed gain operational amplifier (U5159c). This DC value is then multiplexed to the programmable gain amplifier (U5165).
10
The reference input differential operational amplifier also drives the chopper circuit (U5033a).
11
The output from the chopper circuit is used in the pitch and roll circuits to determine the phase of the pitch or roll inputs. When the pitch input is in-phase with the reference, the aircraft is pitched up. When the pitch input is 180 degrees out-of-phase with the reference input, the aircraft is pitched down.
12
When the roll input is in-phase with the reference, the aircraft is in a right roll. When the roll input is 180 degrees out-of-phase with the reference, the aircraft is in a left roll.
13
Once all three analog input signals have been rectified and integrated, the DC values are then multiplexed (U5162) and applied to the programmable amplifier (U5165, U5160d, and U5160a).
14
The programmable amplifier consists of a 10-bit DAC, a unity gain operational amplifier, and a gain-of-3 operational amplifier. The total gain of the programmable amplifier can vary from 0 to 3 in 1024 steps.
15
The multiplexed DC value is applied to the reference voltage input of the multiplying DAC. When the digital data value is applied to the DAC, the reference voltage is then either amplified or attenuated depending upon the digital data. The gain parameters, which are determined by the digital data, are stored in the configuration module.
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COMPONENT MAINTENANCE MANUAL 071-01519
(8)
16
When the gyros are being calibrated, the digital values being applied to the programmable amplifier are varied until the desired gain is achieved. The output from the programmable amplifier are then sent to the multiplexed A/D converter.
17
The multiplexed A/D converter is discussed in the Logic and Control paragraph of this section.
Antenna Stabilization and Control (a)
(b)
FPGA Overview 1
IC U4011 is an FPGA which is used to control the antenna azimuth and elevation-positioning stepper motors and to provide interfacing for OVER_UNDER VOLTAGE, MISSING_PULSE, and MOD_TIMEOUT to the microprocessor on the logic board.
2
Every time power is applied, the FPGAs configure themselves by reading the configuration information from an external EPROM (U4010).
3
After the information has been read and stored in the FPGA, the EPROM is no longer needed. This design takes advantage of an available resource by storing the required sine/cosine lookup tables in the EPROM.
Microstepping Motor Controller 1
The controller provides a register-based interface to the microprocessor and utilizes microstepping to provide smooth, quiet scanning action.
2
Two separate two-phase stepper motors (one for azimuth and one for tilt) are controlled to position the antenna. The motor drive operation is similar so only the azimuth axis motor will be described.
3
Rather than driving the motor windings with pulses of current to step the position, sinusoidal currents are used.
4
The current flowing in each winding of the two motors passes through sense resistors (R4139, R4140, R4130, and R4142, R4143, R4031) producing a voltage (AZ_SENS1 and AZ_SENS2) which is proportional to the motor current.
5
This voltage is compared to the voltage programmed by the FPGA into U4013, a quad DAC. The controller uses a pulse-width modulated drive system to keep the two voltages equal.
6
By using a sequence of values which produces a sine wave when written to the DAC, the motor current produced is also a sine wave.
7
Therefore, by controlling the phase between the two windings, the motor can be moved in either direction.
8
One full cycle of the sine/cosine currents applied to the motors represents four full steps or 128 microsteps. Each step of the motor (1.8 degrees) through the gearing of 36:1, produces a rotation of the antenna of 0.05 degrees. Each microstep is then equal to 0.0015625 degrees.
9
To produce the required 25-degree/second scanning rate, the microstep clocking rate must be 16 kHz: • 1.8 degrees/step/36 = 0.05 degrees/step • 0.05 degrees/32 microsteps = 0.0015625 degrees/microstep • 25 degrees/second/0.0015625 degrees/microstep = 16000 microstep/second equals 16 kHz.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
(c)
(d)
EFFECTIVITY ALL
10
Lower clocking rates are used in soft-start and soft-stop modes to provide accelerated starting and deaccelerated stopping for smoother operation.
11
Counters are used to hold the current position of each axis. The outputs from these counters not only address the sine/cosine table in the EPROM, but are also made available to the processor for monitoring the present position of the antenna.
12
These counters are 18 bits in length and have a range of 218X0.0015625 = 409.6 x, or ±204.8 x. The upper 13 bits are returned to the system providing a range of ±204.8 x, with a resolution of 0.05 x. The lower seven bits of each axis counter are used to address the sine/cosine table in the EPROM to get the values to be written to the current controlling DACs.
Motor Controller Timing 1
The system timing is derived from a 1.025-MHz oscillator (Y4001) which is connected to pin 30 of the FPGA (U4011). Internally, this main clock input is fed to an 8-bit counter.
2
The outputs of this counter form the main system state machine, scheduling all events which occur. The lower six bits cycle at a 16-kHz rate, forming the main DAC update cycle. Each of the four DACs is updated once each cycle.
3
The PWM outputs and chopper drives to the motors are updated at a 32-kHz rate, thus the motor current is corrected twice for each new value written to the DAC.
4
The upper two bits are utilized in the tilt and azimuth clock generator functions to allow 1/4 and 1/2-rate scanning for the soft-start and soft-stop modes.
5
All interactions with the microprocessor occur asynchronously to the FPGA controller. These interactions take the form of single byte read/write cycles, transferring data from/to the FPGA.
6
When the transfer affects the mode of the controller, the inputs are synchronized to the controller before allowing the controller to respond to them, guaranteeing synchronous transition between different modes.
7
When the transfer reads one of the motor counters, the value being returned is latched at the beginning of the transfer to prevent it from changing during the transfer.
EPROM/DAC Interface 1
The FPGA requires that a certain subset of the pins be connected to an external memory device from which it can download configuration information after power is applied.
2
Since this design also accesses sine/cosine lookup tables from the same memory device, those same pins are used for the signals which the controller uses to access the tables.
3
A signal from the FPGA (EA16 = HDC) is a logical 1 during configuration and driven to a logical 0 during normal operation. This is used for the MSB of the EPROM address, thus the lower half of the EPROM contains the sine/cosine tables and the upper half contains the configuration data.
4
During configuration, the FPGA downloads data from the EPROM, sequentially outputting an address and clocking the returned data into one of the internal registers to define the circuit to be implemented.
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COMPONENT MAINTENANCE MANUAL 071-01519
(e)
5
During normal operation, the FPGA outputs an address (EA0 thru EA15) composed of the lower seven bits of each motor counter and two additional bits, from the main system state machine which selects one of four outputs to be updated. The EPROM must then have 17 address inputs, (2 × 7) + 2 + 1 = 17.
6
This design utilizes a 27C010, 128K × 8 EPROM for this purpose. The EPROM data lines (ED0 thru ED7) are not used inside the FPGA except during normal operation. The FPGA outputs the address of a given row from the table.
7
The data from the EPROM then goes directly to the DAC where it awaits the write strobe and channel select bits from the FPGA, to clock it into the appropriate DAC.
Motor Interface 1
The controller interfaces to the motor with four comparators (U4012A and U4012B for azimuth and U4012C and U4012D for elevation) which compare the programmed DAC voltages and the voltages developed across the four current sense resistors.
2
The outputs of the four comparators form reset signals AZ_RST1(2) and EL_RST1(2) which modulate the width (time on) of their respective driver by clearing the drive signals when the current level exceeds the programmed level.
3
Each driver requires three signals to control the driver operation, two direction controls and a strobe. The FPGA outputs these signals, synchronized to the main system state machine. a
The direction controls select which direction the current flows through the motor when enabled by the strobe. When current flow is desired, one of the driver direction signals will be set to a logical high (1),the other will be set to a logical low (0).
b
Current begins to flow and will continue to increase until the value exceeds the programmed value. The reset signal then clears both direction signals which connect both sides of the motor to ground, allowing the current to continue to flow and decrease.
c
This process is repeated at a 32-kHz rate for each of the four drivers. These signals include: • AZ_OUT1A(B) • AZ_OUT2A(B) • EL_OUT1A(B) • EL_OUT2A(B).
EFFECTIVITY ALL
d
The third signal needed is the strobe which forms the chopper drive to enable the driver.
e
The motor drivers (U4033 and U4034 for azimuth and U4049 and U4050 for elevation) are power MOSFET H-bridge configurations. The chopper uses different duty cycles depending on what portion of the sine wave is being produced.
f
During the current charge quarter cycle, the chopper duty cycle is 100 percent allowing the PWM reset signals to fully control the final conduction time.
g
During the first half of the current decay quarter cycle, the chopper duty cycle is reduced to 75 percent. The second half of this quarter cycle reduces the duty cycle further to 50 percent. These signals include:
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COMPONENT MAINTENANCE MANUAL 071-01519 • AZ_EN • AZ_EN(NOT) • EL_EN • EL_EN(NOT). (f)
Microprocessor Interface 1
The microprocessor interfaces to the controller by accessing four registers within the FPGA. The interface consists of the microprocessor data bus (D0 thru D7), the address bus (A0 and A1), the timing strobes (RD/WR), and the address strobe (MTR_SEL). The four registers are detailed in Table 7. Table 7. FPGA Registers Read Address
Read Address
Function
D7
D6
D5
D4
D3
D2
D1
D0
Base+0
Az count low byte
12
11
10
09
08
07
06
05
Base+1
Az count high byte
P1
P2
AB
17
16
15
14
13
Base+2
Ti count low byte
12
11
10
09
08
07
06
05
Base+3
Ti count high byte
P3
x
TB
17
16
15
14
13
2
AB is azimuth busy and TB is tilt busy. The 1 indicates that the controller is in the process of starting or stopping.
3
P1, P2, and P3 are discrete inputs to the FPGA which are made available for monitoring by the processor. P1 and P2 are sampled on the trailing edge of the AFC_SAMPLE pulse input to the FPGA. P1, P2, and P3 are as follows: • P1 = OVER_UNDER_VOLTAGE, 0 = ERROR • P2 = MISSING_PULSE, 1 = ERROR • P3 = MODULATOR_TIME_OUT, 1 = TIME OUT.
4
The write addresses are shown in Table 8. Table 8. Write Address
Write Address
Function
D7
D6
D5
D4
D3
D2
D1
D0
Base+0
Azimuth command
C7
C6
C5
C4
C3
C2
C1
C0
Base+1
Ignored
Base+2
Tilt command
C7
C6
C5
C4
C3
C2
C1
C0
Base+3
Ignored
NOTES: 1 Hold mode (C2 = 0) allows all motor functions to work as normal with the exception that the chopper signals to the output drivers are never activated. This mode is intended for diagnostic purposes only. 2 Hard stop (C1 = 1, C3 = 0) causes the motor to stop at the next available full-step position, microstep = 0. The rate changes directly from full (16 kHz) to zero. 3 Hard start (C1 = 1, C3 = 1) causes the motor to start moving. The rate changes directly from zero to full (16kHz). 4 Soft stop (C1 = 0, C3 = 0) causes the motor to perform a soft-stop sequence consisting of one full step (32 microsteps) at 1/2 rate (8 kHz), followed by one full step at 1/4 rate (4 kHz), and then stop.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table 8. Write Address (Cont) 5
6
Soft start (C1 = 0, C3 = 1) causes the motor to perform a soft-start sequence consisting of one full step (32 microsteps) at 1/4 rate (4 kHz), followed by one full step at 1/2 rate (8 kHz), and then full rate (16 kHz) until stopped. C7 = counter reset, 1 = reset. C6 = not used. C5 = not used. C4 = not used. C3 = stop motor, 0 = stop. C2 = hold motor, 0 = hold. C1 = hard start/stop, 1 = hard. C0 = direction, 1 = right, up.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
TESTING AND FAULT ISOLATION 1.
Planning Data (TASK 34-40-11-99C-801-A01) A.
B.
Reason for the Job (Subtask 34-40-11-99C-002-A01) (1)
Use the test procedures in this section to test and isolate faults.
(2)
The function of the test procedures is to find if there is a failure in the operation of the ART 2000.
Job Setup Data (Subtask 34-40-11-99C-003-A01) (1)
You can use equivalent alternatives for the special tools, fixtures, equipment, and consumable materials. The user must find equivalent alternatives.
(2)
Refer to Table 1001 for the specified special tools, fixtures, and equipment in this section.
(3)
Refer to H4/H8 CAGE Codes (available at http://www.dlis.dla.mil/cage_welcome.asp) for manufacturer’s address. Table 1001. Special Tools, Fixtures, and Equipment
Number
Description
006-3086-XX
color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373)
050-03299-0000
bench test kit (CAGE 22373)
050-03311-0000
configuration module programmer, KPA 900 (CAGE 22373)
071-00097-0100
configuration module (CAGE 22373)
1425-4
dummy load (CAGE 93459)
429E
receiver/transmitter, ARNIC 429 (CAGE ER649)
465
oscilloscope (CAGE 80009)
8000A
digital multimeter (CAGE 89536)
Source
PC, IBM-compatible, 386 or higher, MS DOS 3.3 or higher, 3.5-inch drive, greater than 10 M HDD (commercially available) power supply, +28 VDC, regulated to 40 VDC at 20 A (commercially available) signal generator, capable of 60 MHz (commercially available) stop watch (commercially available)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table 1001. Special Tools, Fixtures, and Equipment (Cont) Number
Description
Source
test harness/tester (user built, refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES section) vertical gyro simulator, capable of 50 mV/degree (commercially available) HP 8593A
spectrum analyzer (CAGE 28480)
HP X281A
waveguide adapter (CAGE 28480)
P6000
probe, X10, 10 megohm (CAGE 80009)
P6021
current probe (CAGE 80009)
RD 300/301/301A
radar test set with option 1 (CAGE 88379)
WR109
radar test set (CAGE KCQU2)
NOTE: 1
The WR109 radar test set is optional to the RD 300/301/301A radar test set.
WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
(4)
Refer to Table 1002 for the specified consumable materials in this section. Table 1002. Consumables
Number
Description
Source
Not applicable
Not applicable
Not applicable
(5)
The list that follows identifies Honeywell publications that are related to this section: • Pub. No. 006-00643-0007, IM, RDR 2000 Color Weather Radar System • Pub. No. 006-05392-0002, MM/OG, KPA 900 Configuration Module Programmer.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
2.
Procedure (TASK 34-40-11-810-801-A01) A.
B.
General (Subtask 34-40-11-810-001-A01) WARNING:
THIS EQUIPMENT GENERATES MICROWAVE RADIATION WHICH CAN BE HARMFUL TO HUMANS. DO NOT OPERATE UNTIL YOU HAVE READ AND CAREFULLY FOLLOWED ALL SAFETY PRECAUTIONS AND INSTRUCTIONS IN THE OPERATIONS AND SERVICE MANUALS.
WARNING:
TO PREVENT HARM TO HUMANS, MAINTAIN PRESCRIBED SAFE DISTANCE WHEN STANDING IN FRONT OF A RADIATING ANTENNA. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
WARNING:
TO PREVENT HARM TO HUMANS, NEVER EXPOSE EYES OR ANY PART OF THE BODY TO AN UNTERMINATED WAVEGUIDE. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
CAUTION:
USE INDUSTRY APPROVED ELECTROSTATIC DISCHARGE SENSITIVE PRECAUTIONS. THE ART 2000 CONTAINS ELECTROSTATIC DISCHARGE SENSITIVE ITEMS.
CAUTION:
DO NOT DROP OR HIT THE ART 2000 DURING THESE PROCEDURES. THE ART 2000 CONTAINS AN ASSEMBLY THAT CAN BE DAMAGED FROM INCORRECT USE.
(1)
Obey the precautions.
(2)
The test procedure gives instructions to make the test setup.
Test Setup (Subtask 34-40-11-810-002-A01) (1)
The purpose of the functional test is to determine the operational status of the ART 2000. The functional test may be used to check a new unit, a unit which has been in storage, or a unit which has been removed from an aircraft or storage.
(2)
The functional test must be performed with the unit fully assembled and no internal adjustments can be made to the unit. Refer to Figure 1001 for a suggested test setup.
(3)
If the ART 2000 tests within the limits given, no further testing is required and the unit is considered suitable for installation in an aircraft. If the unit fails any portion of the functional test, the fault must be isolated and repaired before operation.
(4)
The alignment procedures are only performed after a misalignment has been isolated during troubleshooting, when a module or component that requires alignment has been replaced, or to set adjustable parameters to customer specifications.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1001. (Sheet 1 of 1) Typical Test Setup (GRAPHIC 34-40-11-99B-807-A01) WARNING:
THIS EQUIPMENT GENERATES MICROWAVE RADIATION WHICH CAN BE HARMFUL TO HUMANS. DO NOT OPERATE UNTIL YOU HAVE READ AND CAREFULLY FOLLOWED ALL SAFETY PRECAUTIONS AND INSTRUCTIONS IN THE OPERATIONS AND SERVICE MANUALS.
WARNING:
TO PREVENT HARM TO HUMANS, MAINTAIN PRESCRIBED SAFE DISTANCE WHEN STANDING IN FRONT OF A RADIATING ANTENNA. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
WARNING:
TO PREVENT HARM TO HUMANS, NEVER EXPOSE EYES OR ANY PART OF THE BODY TO AN UNTERMINATED WAVEGUIDE. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
WARNING:
OPERATION OF THIS EQUIPMENT INVOLVES THE USE OF HIGH VOLTAGES. THE TECHNICIAN OR OPERATOR MUST OBSERVE ALL SAFETY PRECAUTIONS WHEN PERFORMING ANY TESTS OUTLINED IN THIS SECTION. RF LOAD MUST BE CONNECTED BEFORE TRANSMITTING.
CAUTION:
THIS EQUIPMENT CONTAINS ELECTROSTATIC DISCHARGE SENSITIVE (ESDS) DEVICES. UNIT MODULES AND INDIVIDUAL ESDS DEVICES MUST BE HANDLED IN ACCORDANCE WITH SPECIAL ESDS HANDLING PROCEDURES. FAILURE TO DO SO CAN RESULT IN DAMAGE TO ESDS DEVICES.
(5)
Set the 006-3086-XX color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373) function selector to the off position.
(6)
Connect the ART 2000 to the test harness/tester (user built, refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES section).
(7)
Connect the 1425-4 dummy load (CAGE 93459) to the ART 2000 using the adapter plate in the 050-03299-0000 bench test kit (CAGE 22373).
(8)
Set S1 on the RD 300/301/301A radar test set with option 1 (CAGE 88379) for RT ON/OFF No. 1 and S2 for input to control bus No. 1.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
3.
Functional Test Procedures (TASK 34-40-11-810-802-A01) A.
Return-to-Service Test (Subtask 34-40-11-810-003-A01)
WARNING:
THIS EQUIPMENT GENERATES MICROWAVE RADIATION WHICH CAN BE HARMFUL TO HUMANS. DO NOT OPERATE UNTIL YOU HAVE READ AND CAREFULLY FOLLOWED ALL SAFETY PRECAUTIONS AND INSTRUCTIONS IN THE OPERATIONS AND SERVICE MANUALS.
WARNING:
TO PREVENT HARM TO HUMANS, MAINTAIN PRESCRIBED SAFE DISTANCE WHEN STANDING IN FRONT OF A RADIATING ANTENNA. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
WARNING:
TO PREVENT HARM TO HUMANS, NEVER EXPOSE EYES OR ANY PART OF THE BODY TO AN UNTERMINATED WAVEGUIDE. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
NOTE:
(1)
Voltage and Current Check (a)
Turn on the test equipment, leave the 006-3086-XX color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373) function selector in the OFF position.
(b)
Check the ammeter on the power supply, +28 VDC, regulated to 40 VDC at 20 A (commercially available). It should read less than 25 milliamps.
(c)
Set the 006-3086-XX color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373) to the ON position.
(d)
Set the power supply, +28 VDC, regulated to 40 VDC at 20 A (commercially available) to 27.5 VDC.
(e)
The ammeter should read less than 3.0 amps.
(2)
Follow the procedures outlined in the RDR 2000 Color Weather Radar System IM, (Pub. No. 006-00643-0007 Section 2.4).
(3)
STC
EFFECTIVITY ALL
Contained in this section is the ART 2000 Weather Avoidance Radar Return-to-Service Checklist. Record all findings on a test data sheet. A sample test data sheet is shown in Figure 1002.
(a)
Set the function selector on the 006-3086-XX color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373) to the ON position and select Wx mode.
(b)
Set the range to 40 nautical miles.
(c)
Set the target width to 35 microseconds.
(d)
If the ART 2000 being tested is configured for a 10-inch antenna, refer to Table 1003 for target distance, signal level, and color relationship. If the ART 2000 is configured for a 12-inch antenna, refer to Table 1004.
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1002. (Sheet 1 of 2) ART 2000 Test Data Sheet (GRAPHIC 34-40-11-99B-808-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1002. (Sheet 2 of 2) ART 2000 Test Data Sheet (GRAPHIC 34-40-11-99B-808-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519 Table 1003. STC with 10-Inch Antenna Target Distance (NM)
Signal Level (±3 dBm)
Color (30%)
10
-80
Magenta
10
-84
Red
10
-92
Yellow
10
-101
Green
NOTE: 1
Be aware that threshold levels and tolerance ranges might overlap.
Table 1004. STC with 12-Inch Antenna Target Distance (NM)
Signal Level (±3 dBm)
Color (30%)
10
-78
Magenta
10
-82
Red
10
-90
Yellow
10
-99
Green
NOTE: 1
Be aware that threshold levels and tolerance ranges might overlap.
(4)
(5)
(6)
PRF (a)
Connect the output of the RD 300/301/301A radar test set with option 1 (CAGE 88379) to the 465 oscilloscope (CAGE 80009). Set the PWR/ F control on the RD 300/301/301A radar test set with option 1 (CAGE 88379) to the PWR position. Set the PRF/RF switch to the PRF position.
(b)
Set the 006-3086-XX color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373) function selector to the ON position and set to Wx mode.
(c)
The frequency should read 101 to 111 Hz.
Transmitter Frequency and Power (a)
Set the PRF/RF switch on the RD 300/301/301A radar test set with option 1 (CAGE 88379) to the RF position.
(b)
The frequency should read 9345 to 9405 MHz.
(c)
The power output should be from 2.5 kW to 6 kW.
Transmitted Pulse Width (a)
(7)
EFFECTIVITY ALL
The pulse width shown on the 465 oscilloscope (CAGE 80009) should be 3.85 to 4.35 microseconds.
AGC (a)
Set the RD 300/301/301A radar test set with option 1 (CAGE 88379) for an RF level of -120 dBm.
(b)
Set the 006-3086-XX color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373) to Wx mode with a range of 240 nautical miles.
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COMPONENT MAINTENANCE MANUAL 071-01519 (c) (8)
(9)
There should be a maximum of five noise dots averaged over several sweeps.
AFC (a)
Set the PWR/ F switch on the RD 300/301/301A radar test set with option 1 (CAGE 88379) to F.
(b)
Set the
(c)
Adjust the F OFFSET for a maximum peak. There should be less than 200-kHz difference from the CAL position.
F OFFSET to CAL. The meter should be centered at 0.
Antenna Scan (a)
Set the 006-3086-XX color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373) to the ON position in horizontal scan. Verify full deflection of 100 degree. Verify that the scan time for one sweep is 3.5 to 4.5 seconds.
(b)
Push the VP button on the 006-3086-XX color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373) to vertical profile. Verify full bottom-to-top motion.
(c)
Set the 006-3086-XX color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373) to the SBY position. Verify that the antenna parks with 0 degree azimuth and tilt at -30 degree.
(10) High and Low Voltage Check (a)
Set the power supply, +28 VDC, regulated to 40 VDC at 20 A (commercially available) voltage to 32 VDC. The unit should operate normally.
(b)
Set the power supply, +28 VDC, regulated to 40 VDC at 20 A (commercially available) voltage to 20 VDC. The unit should operated normally.
(c)
Set the power supply, +28 VDC, regulated to 40 VDC at 20 A (commercially available) voltage to 27.5 VDC.
(11) R/T ON/OFF Discretes (a)
Set the 006-3086-XX color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373) function selector to the OFF position.
(b)
Set S1 and S2 on the test harness/tester (user built, refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES section) to the No. 2 input.
(c)
Set the 006-3086-XX color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373) function selector to the ON position. The ART 2000 will come on and function normally.
(d)
Set the 006-3086-XX color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373) function selector to the OFF position. The ART 2000 will power down after reaching the park position.
(e)
Set S1 and S2 on the test harness/tester (user built, refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES section) to the No. 3 position and repeat Steps (c) and (d).
(f)
Set S1 and S2 on the test harness/tester (user built, refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES section) to the No. 1 input.
(12) Strut Switch (a)
EFFECTIVITY ALL
Remove the 071-00097-0100 configuration module (CAGE 22373) from the test setup. Place the module in the 050-03311-0000 configuration module programmer, KPA 900
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COMPONENT MAINTENANCE MANUAL 071-01519 (CAGE 22373). Configure the 071-00097-0100 configuration module (CAGE 22373) to disable the strut switch override. Refer to Pub. No. 006-05392-0002, KPA 900 Configuration Module Programmer MM/OG for this procedure. Return the module to the test setup. 1
Power up. Go to the ON mode.
2
Apply 3.5 VDC to the test harness/tester (user built, refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES section) STRUT SWITCH IN. The ART 2000 should stop transmitting and show a TX_FLT on the indicator screen.
3
Remove the 3.5 VDC. The ART 2000 should begin transmitting.
(13) Gyro Fault Program Configuration Module for Analog Gyros (a)
Set the 006-3086-XX color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373) to Wx mode. Activate the stabilization (STAB ON) by pushing in the tilt knob.
(b)
Remove all gyro inputs. The word STAB OFF should be displayed on the screen.
(c)
Reconnect the gyro inputs.
(14) DIP Switch (a)
Check the DIP switch on the logic board. It is accessible through the small window near the connector harness. Refer to Figure 1003. • S5001 - 1, 2, and 7 should be ON. • S5001 - 3, 6, and 8 should be OFF. • Switch - 4 and 5 should be set for attached antenna. Refer to Pub. No. 006-00643-0007, RDR 2000 Color Weather Radar System IM.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1003. (Sheet 1 of 1) Access to DIP Switches (GRAPHIC 34-40-11-99B-809-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
4.
Troubleshooting Procedures (TASK 34-40-11-810-803-A01) A.
Purpose (Subtask 34-40-11-810-004-A01)
WARNING:
THIS EQUIPMENT GENERATES MICROWAVE RADIATION WHICH CAN BE HARMFUL TO HUMANS. DO NOT OPERATE UNTIL YOU HAVE READ AND CAREFULLY FOLLOWED ALL SAFETY PRECAUTIONS AND INSTRUCTIONS IN THE OPERATIONS AND SERVICE MANUALS.
WARNING:
TO PREVENT HARM TO HUMANS, MAINTAIN PRESCRIBED SAFE DISTANCE WHEN STANDING IN FRONT OF A RADIATING ANTENNA. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
WARNING:
TO PREVENT HARM TO HUMANS, NEVER EXPOSE EYES OR ANY PART OF THE BODY TO AN UNTERMINATED WAVEGUIDE. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
(1)
General (a)
(2)
(3)
(4)
Objectives (a)
The objective of this document is to inform those investigating and maintaining the RDR 2000 of tools available to assist diagnosis of problems.
(b)
This document is to provide a concise diagnostic reference for engineering and service personnel. Refer to the applicable schematics in the SCHEMATIC AND WIRING DIAGRAMS (PGBLK 34-40-11-2000) section when following troubleshooting procedures detailed in this section.
Background (a)
The RDR 2000 has internal diagnostic software which interrogates itself to determine problems or potential problems.
(b)
When a failure is located, a flag is set and the failure is annunciated by alternating ANT/TX faults in TEST mode.
(c)
An EFIS simply enters the ASCII text pages and all diagnostics may be evaluated. The indicators, such as the IN 182A do not have text pages. A special provision has been created in the maintenance pages.
Scope (a)
B.
This document outlines the procedures to determine the extended error codes for system faults. EFIS ASCII text pages are briefly outlined but are not explicitly walked through. The extended error codes from an indicator are explained.
Viewing System Errors with an EFIS (Subtask 34-40-11-810-005-A01) (1)
This is simply the case of entering the EFIS ASCII text pages and selecting the ARINC 453 radar bus. The ART 2000 will provide text to allow the operator to navigate and to investigate all functionality of the ART 2000.
(2)
The screens exist to display hours of operation, temperatures, failures, voltage levels, etc.
(3)
Consult the EFIS Manual for more information.
EFFECTIVITY ALL
The purpose of this procedure is to investigate system faults within the RDR 2000. System level faults are annunciated by an alternating (flashing) ANT and TX fault on the indicator display when in TEST mode.
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COMPONENT MAINTENANCE MANUAL 071-01519 C.
Viewing System Errors with an Indicator (Subtask 34-40-11-810-006-A01) (1)
An indicator such as the IN 182A does not provide text pages. Therefore, a flashing code system has been implemented. The codes flash with a header followed by a four code sequence.
(2)
When TEST mode is entered, a system fault is indicated by alternating ANT and TX faults. The maintenance mode is entered by simultaneously depressing the Wx and VP buttons. To begin receiving the extended codes change tilt to +15 degrees.
EFFECTIVITY ALL
GYRO
H Volt
AFC
AGC
/* ROM FAULT*/
GYRO
H Volt
AGC
AFC
/* RAM FAULT*/
GYRO
AFC
H Volt
AGC
/* NVRAM FAULT*/
GYRO
AFC
AGC
H Volt
/* STC RAM FAULT*/
GYRO
AGC
H Volt
AFC
/* CM HW FAULT*/
GYRO
AGC
AFC
H Volt
/* CM DATA FAULT*/
H Volt
GYRO
AFC
AGC
/* AIR TEMP ALARM*/
H Volt
GYRO
AGC
AFC
/* UNIT TEMP ALARM*/
H Volt
AFC
AGC
GYRO
/* +5V FAULT*/
H Volt
AFC
GYRO
AGC
/* +8V FAULT*/
H Volt
AGC
GYRO
AFC
/* +9V FAULT*/
H Volt
AGC
AFC
GYRO
/* +15V FAULT*/
AFC
H Volt
GYRO
AGC
/* -15V FAULT*/
AFC
H Volt
AGC
GYRO
/* 24V FAULT*/
AFC
GYRO
H Volt
AGC
/* 28V FAULT*/
AFC
GYRO
AGC
H Volt
/* Tuning Voltage*/
AFC
AGC
H Volt
GYRO
/*AGC FAULT*/
AFC
AGC
GYRO
H Volt
/*Spare*/
AGC
H Volt
AFC
GYRO
/*Spare*/
AGC
H Volt
GYRO
AFC
/*Spare*/
AGC
AFC
H Volt
GYRO
/*High Voltage FAULT*/
AGC
AFC
GYRO
H Volt
/*Missing Pulse FAULT*/
AGC
GYRO
H Volt
AFC
/*AFC FAULT*/
AGC
GYRO
AFC
H Volt
/*SPARE FAULT*/
GYRO
H Volt
AFC
400 Hz
/*H/W Counter FAULT*/
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COMPONENT MAINTENANCE MANUAL 071-01519
D.
GYRO
H Volt
400 Hz
AFC
/*Limit Exceeded FAULT*/
GYRO
AFC
H Volt
400 Hz
/*No Ant Movement FAULT*
GYRO
AFC
400 Hz
H Volt
/*Tracking exceeds limit FAULT*/
GYRO
400 Hz
H Volt
AFC
/*ANT 5 FAULT*/
GYRO
400 Hz
AFC
H Volt
/*SPARE FAULT*/
ART 2000 Logic Board Troubleshooting Procedures (Subtask 34-40-11-810-007-A01) (1)
Logic Board Troubleshooting (a)
The following is a recommended sequence of events when troubleshooting a logic board for the ART 2000. It is recommended that the logic board be placed in a unit with a known good power supply, receiver, magnetron, and gymbol assembly.
(b)
Turn on power to unit and set the indicator to standby. If the indicator shows IN FLT 6 in the lower right corner, then do Steps (c) thru (i). If not, the motors should go through an initialization which will cause the antenna to bounce against the mechanical stops. Then go to Step (j).
(c)
Check the power supply voltages at the following test points: • TP 5010, +5 volts • TP 5011, +15 volts • TP 5012, -15 volts • TP 5013, +24 volts.
EFFECTIVITY ALL
(d)
If there are no voltages, check the ON/OFF line at J2-P14 for a low voltage. Check for solder shorts. If the 5-volt line is low, all other voltages will be low.
(e)
Check signal at TP 5022 (LCA_DONE). When the power is cycled from OFF to ON, the LCA_DONE signal should be observed.
(f)
If the LCA_DONE (TP 5022) line goes high and stays high after approximately 1.7 seconds, then the FPGAs and microprocessor are working (refer to Figure 1004).
(g)
If the LCA_DONE line does not go high after approximately 1.7 seconds, then the FPGAs did not load correctly. Check the soldering of the FPGA pins and also U5013.
(h)
If the LCA_DONE line goes high after approximately 1 second but then goes low again, the FPGAs have loaded correctly, but the microprocessor is not working (refer to Figure 1005). Check the soldering of the microprocessor (U5001), the microprocessor ROM socket (U5003), and the microprocessor RAM (U5004).
(i)
Check 453 transmitter at TP 5020 and TP 5015 for ARINC 453 data (refer to Figure 1006, Figure 1007, and Figure 1008). The 453 data consists of 1600 bits at a 1-MHz rate. The packet of data should last 1.6 milliseconds. The amplitude of the voltage should be at least 2 volts. Check the soldering of pins on the 453 FPGA (U5041), 453 RAM (U5059), and the 453 Driver (U5125).
(j)
Turn the indicator function knob from SBY to TST and check to see if the unit changes modes. If the unit stays in standby then no test pattern will be displayed and there will be no antenna movement.
(k)
Check the 429 receiver circuits (refer to Figure 2004, Sheet 10). Waveform is shown in Figure 1009.
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Page 1014 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 (l)
If the IF alignment has not been performed, then it should be done at this time. If the IF does not align, check for open inductor on the +15 volt inputs into each stage.
(m) Check the manual gain and STC/AGC voltage at TP 5007 and TP 5002. With the unit in standby or test, the voltages should be around 7 volts. (n)
If the manual gain is not working properly, then check the soldering of U5027 and U5028.
(o)
If the STC/AGC is not working properly, check the soldering of STC FPGA (U5037), STC RAM (U5118), STC DAC (U5119), and STC driver (U5122).
Figure 1004. (Sheet 1 of 1) Normal Microprocessor and FPGA Turn-On (GRAPHIC 34-40-11-99B-810-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1005. (Sheet 1 of 1) FPGAs Programmed Correctly but Microprocessor is Inoperative (GRAPHIC 34-40-11-99B-811-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1006. (Sheet 1 of 1) Start Sync of 453 Transmission (GRAPHIC 34-40-11-99B-812-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1007. (Sheet 1 of 1) Stop Sync of 453 Transmission (GRAPHIC 34-40-11-99B-813-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1008. (Sheet 1 of 1) Data Packet of 453 Transmission (GRAPHIC 34-40-11-99B-814-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1009. (Sheet 1 of 1) Received 429 Data (GRAPHIC 34-40-11-99B-815-A01) (2)
AFC Calibration Procedure (a)
EFFECTIVITY ALL
The following is the AFC calibration procedure sequence of events. 1
AFC course - Local oscillator tuning voltage starts at approximately +15 volts and sweeps down.
2
AFC fine - This voltage (U5027-P2) will start at +5 volts and sweep down to +2.5 volts.
3
AFC offset - This voltage will start at +5 volts (U5027-P1) and sweep down to 0 volts.
(b)
Check the local oscillator tuning voltage at TP 5006. This voltage should be around 8 volts.
(c)
If AFC course does not lock, then check the following. 1
The quad DAC (U5027) should output 0 to 5 volts on pins 1, 2, 19, and 20.
2
The AFC course (U5027-P20) should start at 5 volts and sweep down. If the LO-tuning voltage stops at approximately 8 volts, then the AFC course should be at approximately 3.4 volts.
3
If the AFC course does not lock, then check the signal at the video A/D converter (TP 5023). The AFC course circuit will read the video A/D converter (TP5023).
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Page 1020 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 The AFC course circuit will read the video A/D converter in search of a signal at approximately 200 nautical miles. 4 (d)
(3)
If the AFC course calibration procedure does not find a target at 100 nautical miles, then it will continue to sweep.
If AFC fine does not lock, then check the following. 1
If the AFC fine keeps on sweeping, check the input signal to the discriminator A/D converter. If this signal is correct (refer to Figure 1010, Figure 1011, Figure 1012, and Figure 1013), then check the A/D converter’s outputs.
2
The discriminator A/D converter’s output will be stored in the first eight locations of the STC RAM. If the outputs from the A/D converter are correct, then check the operation of the STC RAM.
Detector Calibration Procedures (a)
The detector calibration will calibrate the STC curves, manual gain curves, color thresholds, and weather compensation thresholds.
(b)
Check the STC and manual gain voltage at TP5002 and TP5007. If the voltages are not correct, do the steps that follow. 1
Check the manual gain and STC/AGC voltage at TP 5007 and TP 5002. With the unit in standby or test, the voltages should be around 7 volts.
2
If the manual gain is not working properly, then check the soldering of U5027 and U5028.
3
If the STC/AGC is not working properly, check the soldering of the STC FPGA (U5037), the STC RAM (U5118), the STC DAC (U5119), and the STC driver (U5122).
(c)
Check to see if the indicator is showing a target at 100 nautical miles. With a target of approximately -100 dBm, a green band should be displayed at 100 nautical miles.
(d)
If the indicator is not displaying a target at 100 nautical miles, then check the following. 1
2
Check the video for a signal at TP 5023, if no signal, do the steps that follow. a
Check the manual gain and STC/AGC voltage at TP 5007 and TP 5002. With the unit in standby or test, the voltages should be around 7 volts.
b
If the manual gain is not working properly, then check the soldering of U5027 and U5028.
c
If the STC/AGC is not working properly, check the soldering of the STC FPGA (U5037), the STC RAM (U5118), the STC DAC (U5119), and the STC driver (U5122).
Check out the three sources of data to the Wx ROM (U5038): • Weather data from the video A/D (U5036 - VID_0 to VID_7) • Weather Compensation from STC FPGA (U5037 - WCAO to WCA5) (refer to Figure 1014) • ESTC data from STC FPGA (U5037 - ESA0 to ESA3) (refer to Figure 1015).
EFFECTIVITY ALL
3
Check the output from the Wx ROM (U5038) to the input of Wx RAM (U5039) (refer to Figure 1016).
4
Check the address to the Wx RAM (U5039) (refer to Figure 1017).
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Page 1021 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 5
Check the radial summation (refer to Figure 1016 and Figure 1017).
6
Check the radial transfer from Wx RAM (U5039) to the ARINC 453 RAM (U5059) (refer to Figure 1018).
(e)
Apply the gyro input signals to the unit. Check the voltages at TP 5027. These voltages shall vary as the gyro simulator is changed in pitch or roll or reference (refer to Figure 1019).
(f)
If the configuration module has been read correctly, the gyro outputs should be of proper amplitudes (reference should be around 2.5 volts).
(g)
Turn the unit OFF and then back ON to the test mode. Check to see if the antenna soft starts. This will check the Hall sensor input circuits and the multiplexed A/D converter (refer to Figure 1020 and Figure 1021).
(h)
Now select the 80-nautical mile range in the test mode. Check the temperature of the unit to see if the logic board temperature sensor circuit is working (red band at approximately 25 nautical miles).
Figure 1010. (Sheet 1 of 2) Discriminator Input to the Discriminator A/D Converter (GRAPHIC 34-40-11-99B-816-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1010. (Sheet 2 of 2) Discriminator Input to the Discriminator A/D Converter (GRAPHIC 34-40-11-99B-816-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1011. (Sheet 1 of 1) STC Curve and Manual Gain for Weather (GRAPHIC 34-40-11-99B-817-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1012. (Sheet 1 of 1) STC Curve and Manual Gain for MAP (GRAPHIC 34-40-11-99B-818-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1013. (Sheet 1 of 1) STC Curve and Manual Gain for Weather over Multiple MAG Fires (GRAPHIC 34-40-11-99B-819-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1014. (Sheet 1 of 1) Weather Compensation Bit 0 (GRAPHIC 34-40-11-99B-820-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1015. (Sheet 1 of 1) Extended STC Bit 0 (GRAPHIC 34-40-11-99B-821-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1016. (Sheet 1 of 1) Compensated Weather Data Bit 3 (GRAPHIC 34-40-11-99B-822-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1017. (Sheet 1 of 1) Weather RAM Address 0 (GRAPHIC 34-40-11-99B-823-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1018. (Sheet 1 of 1) Radial Data Transfer from WX_RAM to 453_RAM (GRAPHIC 34-40-11-99B824-A01)
EFFECTIVITY ALL
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Page 1031 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1019. (Sheet 1 of 2) Reference, Pitch, and Roll Inputs (GRAPHIC 34-40-11-99B-825-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1019. (Sheet 2 of 2) Reference, Pitch, and Roll Inputs (GRAPHIC 34-40-11-99B-825-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1020. (Sheet 1 of 1) Pitch Hall Sensor to MUX A/D Converter (GRAPHIC 34-40-11-99B-826-A01)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1021. (Sheet 1 of 1) Azimuth Hall Sensor to MUX A/D Converter (GRAPHIC 34-40-11-99B-827-A01) E.
ART 2000 Power Supply Board Troubleshooting Procedures (Subtask 34-40-11-810-008-A01) (1)
The sequence for the testing and troubleshooting of the power supply board for the ART 2000 should proceed as follows. It is recommended that a known good logic board be placed in the unit prior to testing the motor drive circuitry.
(2)
Turn on the power to the unit and set the indicator to STBY. Check the power supply voltages at the following test points:
EFFECTIVITY ALL
L4005
=
+5.2 V
±
0.25 VDC
L4008
=
+9.7 V
±
1.00 VDC
L4007
=
+24 V
±
2.5 VDC
L4006
=
+26.25 V
±
0.5 VDC/-1.0 VDC
CR4016-Anode
=
-15 V
±
1.5 VDC
CR4017-Cathode
=
+15 V
±
1.5 VDC
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Page 1035 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 (a)
If there are no voltages at any of the above test points, check the fuse (F4001), the ON/ OFF circuitry associated with Q4018, and confirm that the aircraft +28 volt bus is not greater than +36 VDC.
(b)
If +28 volts is present at L4006 but either the +5 volt or +9.3 volt line is low or absent, check for shorts to ground on all the low voltage supply outputs. Also confirm the presence of the correct waveforms at TP4010, TP4011, and T4005-4. Refer to Figure 1022, Figure 1023, and Figure 1024.
(c)
If the +28 volt line is low at L4006 and both the +5 volt and the +9.3 volt lines are present, check for a shorted motor driver (U4033, U4034, U4049, or U4050), a shorted flyback switch (Q4001), a short on the +28 volt filtered line, or a failure in the ON/OFF latching circuitry (U4008, U4020, and associated circuitry).
(d)
If the +5 volt line is low, check for shorts on the +5 volt, -15 volt, +15 volt, and the +24 volt buses, or that the FPGA (U4011) has not booted up correctly.
CAUTION:
EFFECTIVITY ALL
IF (U4011) DOES NOT BOOT UP CORRECTLY, IT WILL BECOME EXTREMELY HOT. OPERATION IN THIS CONDITION FOR AN EXCESS OF FIFTEEN (15) MINUTES MAY CAUSE DAMAGE AND REQUIRE IT TO BE REPLACED.
(e)
If the +9.3 volt line is low, check for shorts on the outputs of T4002 and J4001.
(f)
If the fuse blows repeatedly upon turn-on, check for line to line shorts on the output of the +5 volt or the 0.3 volt supplies, incorrect polarity of the aircraft +28 volt bus, or a short to ground through a filter capacitor on the aircraft +28 volt bus.
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Page 1036 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1022. (Sheet 1 of 1) Normal Operation of the +5 VDC Pulse Width Modulator U4005 (TP4010) (GRAPHIC 34-40-11-99B-828-A01) Key for Figure 1022. (Sheet 1 of 1) Signal:
+5 VDC Pulse Width Modulator Output
Location:
TP4010
Volts/Div:
10 V/Div
Time/Div:
5 µsec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1023. (Sheet 1 of 1) Normal Operation of the +9.3 VDC Pulse Width Modulator U4006 (TP4011) (GRAPHIC 34-40-11-99B-829-A01) Key for Figure 1023. (Sheet 1 of 1) Signal:
+9.3 VDC Pulse Width Modulator Output
Location:
TP4011
Volts/Div:
10 V/Div
Time/Div:
5 µsec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1024. (Sheet 1 of 1) Normal Operation of the -15 VDC Flyback Winding (T4005-4) (GRAPHIC 34-40-11-99B-830-A01) Key for Figure 1024. (Sheet 1 of 1) Signal:
-15 VDC Flyback Output
Location:
T4005-4
Volts/Div:
20 V/Div
Time/Div:
5 µsec/Div
Probe:
X 10
Trigger:
Internal Positive (3)
To check the transmitter time-out timer, turn the indicator function switch to OFF and allow it to remain OFF for 30 seconds. Cycle through STBY to ON while monitoring the time period until either the transmitter fires or U4002-2 goes high. This time period may vary from 40-90 seconds. If the output at U4002-2 does not go high after a reasonable period of time, check the circuitry in and around U4002A.
(4)
In the event that the transmitter does not fire after the time-out period has expired, either no transmit pulse is present or no high voltage is present. Proceed through the following steps.
EFFECTIVITY ALL
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Page 1039 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 (a)
(b)
(5)
No Detected RF Pulse 1
Confirm that there is a valid MAG_FIRE_OUT signal from the Logic board. Refer to Figure 1025.
2
Confirm that there is a valid Long Pulse Gate at U4020-13. Refer to Figure 1026(U4020-13). This gate enables U4054A to pass a valid MAG_FIRE_OUT signal while at the same time preventing a DC level from triggering the transmitter on continuously.
3
Confirm that there is a MAG_FIRE pulse at TP4008. Refer to Figure 1027.
4
Confirm that there is a valid Modulator Switch Drive pulse at TP4005. Refer to Figure 1028. A continuous low here could indicate that Q4003 is shorted, while a continuous high could indicate that Q4002 is shorted. If Q4002 is shorted, suspect a Drain to Gate failure of Q4004 caused by overvoltage.
5
If an overvoltage condition is suspected, open the circuit to troubleshoot by removing Q4004 and verifying the operation of both the Modulator Switch FET Gate and High Voltage Overvoltage circuitry on TP4004. (High Voltage = 375 VDC Maximum). Refer to Figure 1029.
6
Confirm that you have a high-voltage pulse at the Drain of Q4004 by monitoring the cathode of CR4005. Refer to Figure 1030. If there is no high voltage pulse, check for shorts to ground on the primary side of T4002. Also check the operation of the high-voltage supply.
In the event that a pulse is present at the gate of Q4004 but not at the drain, the next step is to check the high-voltage power supply.
No Detected RF Pulse WARNING:
EFFECTIVITY ALL
OPERATION OF THIS EQUIPMENT INVOLVES THE USE OF HIGH VOLTAGES. THE TECHNICIAN OR OPERATOR MUST OBSERVE ALL SAFETY PRECAUTIONS WHEN PERFORMING ANY TESTS OUTLINED IN THIS SECTION.
(a)
Check the high-voltage supply after time-out at CR4004-Cathode or at L4009. The voltage should be between 285 to 375 VDC. Refer to Figure 1031.
(b)
If the voltage is absent, shut down the power to the unit and check for short circuits on the primary of T4002. If a short is found, suspect a shorted Q4004, CR4001, C4011, C4013, or a short from the primary of T4002 to ground. If no short circuits are found, then the highvoltage supply and its controlling circuitry are suspect.
(c)
Check that the HV_ENABLE input from the logic board is low. If there is a low present, check for the correct waveform at TP4001. Refer to Figure 1032. If this voltage is +1.5 to 2.5 VDC, then continue.
(d)
If the voltage at TP4001 is 0 VDC, check Q4010, Q4028, or U4018C and their associated circuitries. These components make up the overvoltage sense circuit and a short circuit failure here can cause the power supply to shut down completely.
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Page 1040 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 CAUTION:
EFFECTIVITY ALL
AN OPEN CIRCUIT FAILURE HERE CAN CAUSE THE OUTPUT OF THE HIGH-VOLTAGE SUPPLY TO REACH 800 VOLT, DIRECT CURRENT OR MORE DEPENDING ON THE INPUT VOLTAGE. THIS CONDITION EVEN MOMENTARILY, WILL PROBABLY REQUIRE THE REPLACEMENT OF SEVERAL COMPONENTS IN THE HIGH-VOLTAGE POWER SUPPLY CIRCUITRY.
(e)
If the high-voltage is absent or low but TP4001 has the correct waveform, check that TP4014 has a higher voltage than TP4001. If TP4014 does not have a higher voltage than TP4001, remove power from the unit and remove R4204 from the circuit. This will open the pulse height regulator servo loop in order to complete troubleshooting the high-voltage supply.
(f)
After turn-on and time-out, the high-voltage output at L4009 should be 365 to 375 VDC. If not, troubleshoot the high-voltage power supply controller oscillator at U4001-7. Refer to Figure 1033.
(g)
If the oscillator is functioning check the output of the pulse width modulator at U4001- 10. Refer to Figure 1034.
(h)
If there is an output present at U4001-10 (even if much narrower than Figure 1034), consider the pulse width modulator okay and continue checking the high-voltage power supply by verifying that the waveform at TP4002 is similar to Figure 1035.
(i)
This waveform is the flyback signal and is true during the period of time that Q4001 is turned OFF. The amplitude of this signal varies with the input signal and the output load. An open circuit here will cause this voltage to dramatically increase in value while a short circuit would dramatically lower this signal.
(j)
Operating the ART 2000 without a MAG_FIRE pulse (no load) will force the Pulse Width Modulator to burst cycle and lower the duty cycle dramatically.
(k)
The flyback transformer secondary is shown in Figure 1036 (CR4001-Anode). The same rules for the primary apply to the secondary as well. Figure 1037 (Flyback Current) is an example of the expected voltage developed across R4013 due to Flyback Primary Current.
(l)
A short circuit on the secondary will cause this signal to be much higher which in turn will activate the over-current point on the Pulse Width Modulator (U4001-5) thus shortening the duration of the PWM output pulse.
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Page 1041 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1025. (Sheet 1 of 1) MAG_FIRE_OUT Pulse from Logic Board (U4020-2) (GRAPHIC 34-40-1199B-831-A01) Key for Figure 1025. (Sheet 1 of 1) Signal:
Logic Board MAG_FIRE_OUT
Location:
U4020-2
Volts/Div:
1 V/Div
Time/Div:
1 µsec/Div
Probe:
X 10
Trigger:
External TP4008 Positive
EFFECTIVITY ALL
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Page 1042 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1026. (Sheet 1 of 1) Long Pulse Gate (U4020-13) (GRAPHIC 34-40-11-99B-832-A01) Key for Figure 1026. (Sheet 1 of 1) Signal:
Modulator Trigger Long Pulse Gate
Location:
U4020-13
Volts/Div:
1 V/Div
Time/Div:
1 µsec/Div
Probe:
X 10
Trigger:
External TP4008 Positive
EFFECTIVITY ALL
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Page 1043 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1027. (Sheet 1 of 1) MAG Fire Pulse (TP4008) (GRAPHIC 34-40-11-99B-833-A01) Key for Figure 1027. (Sheet 1 of 1) Signal:
Modulator Trigger
Location:
TP4008
Volts/Div:
1 V/Div
Time/Div:
1 µsec/Div
Probe:
X 10
Trigger:
External TP4008 Positive
EFFECTIVITY ALL
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Page 1044 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1028. (Sheet 1 of 1) Modulator Switch Drive (TP4005) (GRAPHIC 34-40-11-99B-834-A01) Key for Figure 1028. (Sheet 1 of 1) Signal:
Modulator Switch Drive
Location:
TP4005
Volts/Div:
5 V/Div
Time/Div:
1 µsec/Div
Probe:
X 10
Trigger:
External TP4008 Positive
EFFECTIVITY ALL
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Page 1045 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1029. (Sheet 1 of 1) Modulator Switch FET Gate (TP4004) (GRAPHIC 34-40-11-99B-835-A01) Key for Figure 1029. (Sheet 1 of 1) Signal:
Modulator Switch Drive
Location:
TP4004
Volts/Div:
5 V/Div
Time/Div:
1 µsec/Div
Probe:
X 10
Trigger:
External TP4008 Positive
EFFECTIVITY ALL
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Page 1046 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1030. (Sheet 1 of 1) Modulator Transformer Primary Voltage (CR4005 Cathode) (GRAPHIC 34-40-11-99B-836-A01) Key for Figure 1030. (Sheet 1 of 1) Signal:
Modulator Switch Voltage
Location:
Drain Q4004
Volts/Div:
100 V/Div
Time/Div:
1 µsec/Div
Probe:
X 10
Trigger:
External TP4008 Positive
EFFECTIVITY ALL
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Page 1047 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1031. (Sheet 1 of 1) Normal Signal for the HVPS Refresh Rate with MAG Current Set to 3 A, 100 Hz PRF Rate (Jct L4009-CR4004) (GRAPHIC 34-40-11-99B-837-A01) Key for Figure 1031. (Sheet 1 of 1) Signal:
HVPS Refresh Rate
Location:
Jct L4009-CR4004
Volts/Div:
10 V/Div AC coupled
Time/Div:
2 msec/Div
Probe:
X 10
Trigger:
External TP4008 Positive
EFFECTIVITY ALL
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Page 1048 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1032. (Sheet 1 of 1) Normal Signal at the Overvoltage Frequency Compensation Port of the HVPS PWM (TP4001) (GRAPHIC 34-40-11-99B-838-A01) Key for Figure 1032. (Sheet 1 of 1) Signal:
HVPS Controller Output Compensation
Location:
TP4001
Volts/Div:
500 mV/Div
Time/Div:
2 µsec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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Page 1049 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1033. (Sheet 1 of 1) Normal Signal at the Oscillator Port of the HVPS PWM Controller (U4001-7) (GRAPHIC 34-40-11-99B-839-A01) Key for Figure 1033. (Sheet 1 of 1) Signal:
HVPS Controller Oscillator
Location:
U4001-7
Volts/Div:
500 mV/Div
Time/Div:
5 µsec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1034. (Sheet 1 of 1) Normal Signal from the Output of the HVPS PWM Control to the Gate of Q4001 (U4001-10) (GRAPHIC 34-40-11-99B-840-A01) Key for Figure 1034. (Sheet 1 of 1) Signal:
HVPS Controller Output
Location:
U4001-10
Volts/Div:
5 V/Div
Time/Div:
5 µsec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1035. (Sheet 1 of 1) Normal Flyback Signal at the HVPS Transformer Primary (TP4002) (GRAPHIC 34-40-11-99B-841-A01) Key for Figure 1035. (Sheet 1 of 1) Signal:
HVPS Flyback Primary Voltage
Location:
TP4002
Volts/Div:
50 V/Div
Time/Div:
5 µsec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1036. (Sheet 1 of 1) Normal Output Voltage from the HVPS Transformer Secondary (CR4001 Anode) (GRAPHIC 34-40-11-99B-842-A01) Key for Figure 1036. (Sheet 1 of 1) Signal:
HVPS Flyback Secondary Voltage
Location:
CR4001 Anode
Volts/Div:
100 V/Div
Time/Div:
5 µsec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1037. (Sheet 1 of 1) Normal Signal Due to the Flyback Primary Current Flowing Through R4013 (Fly Current) (GRAPHIC 34-40-11-99B-843-A01) Key for Figure 1037. (Sheet 1 of 1) Signal:
T4001 Primary Current
Location:
Jct R4013-Q4001 Source
Volts/Div:
100 mV/Div
Time/Div:
2 µsec/Div
Probe:
X 10
Trigger:
Internal Positive (6)
EFFECTIVITY ALL
In the event that a pulse is present at the drain of Q4004, and the high-voltage power supply output (measured at L4009) is within the specified limits (285 to 375 VDC), the next step is to measure and set the magnetron current through the magnetron current loop cutout provided on the board.
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COMPONENT MAINTENANCE MANUAL 071-01519 (7)
This cutout, located directly below the pulse transformer (T4002), is designed to accept a standard current probe from the non-component side of the board. The expected current at this point is 3.0 amperes peak. An adjustment is provided (R4200) to set the Magnetron current for a horizontal detected pulse. Refer to Figure 1038. (a)
If no RF pulse is detected or the magnetron current level is incorrect, perform the steps that follow. 1
If the current measured through the magnetron current cutout is below 1.5 Amps, suspect a relatively high impedance in the primary of T4002.
2
A current measurement of 0 amperes, of course, would indicate an open circuit in the secondary of T4002.
3
A current measurement of 5 to 10 amperes would indicate a short circuit to ground on the secondary of T4002 or a short to ground in the magnetron.
4
A current measurement of 4 amperes which is not adjustable by R4200 but with the high-voltage power supply output within specifications (365 to 375 VDC) would indicate a failure in the pulse height regulator circuitry or the absence of R4204 if it was removed earlier for trouble-shooting.
5
If R4204 has been removed, confirm that the voltage at TP4014 is below TP4001 but not below 1.5 VDC. If so, reinstall R4204 and adjust the magnetron current to a flat (horizontal) level of 3.0 amperes.
6
If the current cannot be adjusted by the use R4200 or the voltage at TP4014 is out of limits, check the magnetron current sense delay gate at TP4017 (U4058-pin 4) for the proper signal. Refer to Figure 1039.
7
This gate generates a delay until the middle of the magnetron current pulse and triggers U4058-pin 10 which generates the magnetron current sense gate, a 1 microsecond wide pulse at U4058-pin 5, which enables the magnetron current sample and the hold switch (U4060). Refer to Figure 1040.
8
The other inputs to U4060 are the conditioned magnetron current pulse, the HV_ENABLE discrete, and the -5 VDC. Refer to Figure 1041.
9
When U4060 is enabled by the magnetron current sense gate, it samples the magnetron current pulse U4060-pin 3, and charges the hold capacitors C4144 through R4221 to the sampled level.
10
The output of U4061A is expected to be a constant voltage with an amplitude equal to the input voltage during the sample time period. This signal is then buffered through U4061A, and drives U4061B which inverts and amplifies this control voltage for the high-voltage power supply pulse width modulator (U4001-pin 3). Refer to Figure 1043. NOTE:
EFFECTIVITY ALL
The input impedance of U4061A is extremely high. The oscilloscope probe should be used to monitor the output rather than the input to prevent loading C4144.
11
R4200 is used to set the gain for U4061B, and its range allows for the compensation of different magnetrons which may be utilized.
12
The HV_ENABLE discrete is used as the enable for U4060B. Its purpose is to set the quiescent condition for C4144 to -5 VDC. It also forces the magnetron current pulse to start below 3 amperes and regulate up to the desired value rather than to overshoot high and regulate down to the desired level.
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COMPONENT MAINTENANCE MANUAL 071-01519 13
The missing pulse detector, U4061C, U4061D, and their associated circuitry (refer to Figure 1042), comprises a peak current detector which monitors the conditioned magnetron current. If the current is between the limits of 1.5 and 3.4 amperes, the missing pulse detector outputs a negative going pulse.
14
This pulse is an input to the Logic Board Microprocessor. If its absence is detected for 16 transmit cycles, the microprocessor flags the indicator with a TX_FLT.
Figure 1038. (Sheet 1 of 1) Typical Current as Measured Through the Current Probe Cutout (Current Loop MAG Current) (GRAPHIC 34-40-11-99B-844-A01) Key for Figure 1038. (Sheet 1 of 1) Signal:
Magnetron Current
Location:
Magnetron Current Loop Cutout
Volts/Div:
100 mV/Div 50 Ohms
Time/Div:
1 µsec/Div
Probe:
Tek P6021 Probe (10 mA/Div)
Trigger:
External TP4008 Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1039. (Sheet 1 of 1) Magnetron Current Sense Delay Gate (TP4017) (GRAPHIC 34-40-11-99B845-A01) Key for Figure 1039. (Sheet 1 of 1) Signal:
Magnetron Current Sense Delay Gate
Location:
TP4017
Volts/Div:
2 V/Div
Time/Div:
400 nsec/Div
Probe:
X 10
Trigger:
External TP4008 Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1040. (Sheet 1 of 1) Magnetron Current Sense Gate (TP4016) (GRAPHIC 34-40-11-99B-846-A01) Key for Figure 1040. (Sheet 1 of 1) Signal:
Magnetron Current Sense Gate
Location:
TP4016
Location:
2 V/Div
Time/Div:
400 nsec/Div
Probe:
X 10
Trigger:
External TP4008 Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1041. (Sheet 1 of 1) Conditioned Magnetron Current Pulse (TP4020) (GRAPHIC 34-40-11-99B847-A01) Key for Figure 1041. (Sheet 1 of 1) Signal:
Amplified Magnetron Current
Location:
TP4020
Volts/Div:
1 V/Div
Time/Div:
1 µsec/Div
Probe:
X 10
Trigger:
External TP4008 Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1042. (Sheet 1 of 1) MISSING_PULSE Output (TP4015) (GRAPHIC 34-40-11-99B-848-A01) Key for Figure 1042. (Sheet 1 of 1) Signal:
Missing Pulse Detector
Location:
TP4015
Volts/Div:
1 V/Div
Time/Div:
1 µsec/Div
Probe:
X 10
Trigger:
External TP4008 Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1043. (Sheet 1 of 1) CONTROL_VOLTS Input to the HVPS PWM (TP4014) (GRAPHIC 34-40-11-99B-849-A01)
Key for Figure 1043. (Sheet 1 of 1) Signal:
Pulse Height Control Voltage
Location:
TP4014
Volts/Div:
1 V/Div
Time/Div:
1 µsec/Div
Probe:
X 10
Trigger:
External TP4008 Positive (8)
EFFECTIVITY ALL
In the event that the high-voltage power supply voltage is low, the magnetron current cannot be adjusted to 3.0 amperes, and the correct operation of the HVPS controller as well as the correct drive signal at TP4004 has been confirmed; excessive current draw from the high voltage power supply may be suspected.
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COMPONENT MAINTENANCE MANUAL 071-01519 (9)
One of the quickest ways to confirm this is to monitor the voltage at the Drain of Q4004. Refer to Figure 1030 (CR4005 Cathode) and Figure 1045 (Q4004 Drain Voltage/CR4004 Current). (a)
Monitor closely the dc offset from ground for this signal over the period of the pulse. Ascertain a relative measurement of the current flow across the RDS_ON of Q4004. Normally, Q4004 will pull down to less than 30 VDC over the entire pulse.
(b)
If this voltage tails upward towards the end of the pulse above 60 volts, troubleshoot for excessive current flow from the high-voltage power supply.
(c)
Confirm and isolate the failure by lifting R4014 and CR4004 from the circuit and rechecking the Magnetron Current. Refer to Figure 1044.
(d)
Figure 1044 is included to show the relationship between the voltage and the current through R4014 and Q4007. Q4007 is used to reset the core of T4002 after every pulse. It can best be described as a damper or pulse tail clipper.
(e)
When T4002 reverses polarity after Q4004 turns off, the positive ringback above the highvoltage supply turns on Q4007 as well as CR4004. The cathode of Q4007 is held low due to a charge stored in C4012. When the gate of Q4007 exceeds this charge by the turn-on voltage of Q4007, it discharges the energy stored in the core of T4002.
(f)
CR4004 will only turn on momentarily. Its voltage and current waveforms are shown in Figure 1045 (Q4004 Drain/CR4004 Current).
(g)
In both cases, if the current waveform differs markedly from the plots shown, it indicates a failure.
(h)
The current flowing in the primary of T4002 can be measured by lifting L4009, attaching a current probe, and reinstalling L4009. The expected current is shown in Figure 1046 (L4009 Current). A short on the secondary would be reflected back to the primary and 90 amperes or greater may be measured at this point during a failure.
(10) The following is a recommended sequence of events when troubleshooting the motor drive circuitry of the ART 2000 power supply board. It is recommended that a known good logic board be used for the following tests, as well as checking the motor windings themselves before you apply power, especially if the failure is related to the azimuth or elevation antenna drive. (a)
EFFECTIVITY ALL
There will be no antenna movement in either azimuth or elevation upon turn-on. 1
Confirm that the motor drive switch on the logic board is in the ON position.
2
Confirm that there is +26.25 VDC (FILTERED_MOTOR_A+) present at L4006.
3
Confirm that +4.95 to 5.45 VDC is present at TP4010.
4
Confirm continuity from the Power Supply connector (J4001-pin 31 through J4001-pin 40) to the Logic Board connector (J4002- pin 31 through J4002-pin 40).
5
Check the Azimuth and Elevation motor windings themselves for opens or shorts.
6
If an open or shorted winding is found, check for a shorted Motor Driver (U4033, U4034, U4049, U4050).
7
If a shorted Motor Driver is found, check that the FPGA is being programmed and is running by monitoring U4011-pin 80 the Done Programming pin. Refer to Figure 1047.
8
Upon unit turn-on, U4011-pin 80 should be low and after two (2) seconds go high and remain high. Failure to do this indicates that the FPGA is not being programmed by its ROM U4010.
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COMPONENT MAINTENANCE MANUAL 071-01519 9
Confirm continuity between U4010 and U4011, also check for shorts between adjacent pins of the FPGA (U4011). Check the operation of the FPGA clock (U4011- pin 30), refer to Figure 1048.
CAUTION:
EFFECTIVITY ALL
OPERATION OF THE POWER SUPPLY BOARD FOR A PERIOD EXCEEDING 15 MINUTES WITH THE FIELD-PROGRAMMABLE GATE ARRAY RUNNING UNPROGRAMMED WILL OVERHEAT THE FIELD-PROGRAMMABLE GATE ARRAY, POSSIBLY CAUSING ITS FAILURE, AND MAY DAMAGE THE MOUNTING AREA.
10
Once it has been determined that the FPGA is being programmed and is running, the next step is to check that the FPGA has the correct output by checking the sine DAC and the cosine DAC.
11
There is a sine and a cosine DAC (U4013) for both the Azimuth and Elevation motors. The data input lines to these DACs come from the ROM (U4010), while the timing and address information comes from the FPGA. a
Begin troubleshooting by confirming that U4013-pin 4 has +2.5 VDC reference, if so, monitor U4013-2 (Azimuth Current Limit Sine) and U4013- 1 (Azimuth Current Limit Cosine).
b
Refer to Figure 1049 and Figure 1050.
c
These points set the maximum current limit for the Motor Drivers. The Motor Driver Current is compared to this voltage in U4012. The expected waveform at these points is a rectified sinewave.
d
The output from U4012, in turn, is used by the FPGA to control the ontime of the Motor Drivers. A nonsinusoidal waveform at any of the DAC outputs can be caused by one or more of the data lines being open from the ROM (U4010).
e
The lack of a rectified sinusoid can be caused by one or more open address lines or an open between the FPGA (U4011) and the Logic Board connector (J4001-pin31 through J4001-pin 40 and J4001-pin 1 through J4001-pin4).
12
Next, switch the Indicator to VP mode and check the output of U4013-pin 20 (refer to Figure 1051) and U4013-pin 19 (refer to Figure 1052). A correct waveform from these pins indicates that the FPGA is being loaded with the correct program and is operational.
13
A problem with one or more of these waveforms indicates a problem on the bus between the FPGA and the DAC or between the power supply board and the logic board.
14
Monitor the output from the motor drivers themselves. The current flowing from azimuth current sense (sine) and the azimuth current sense (cosine) develop a voltage across their respective sense resistors. (Refer to Figure 1052; U4034- pin 10 and Figure 1053; U4033-pin 10)
15
Likewise, in VP mode, elevation current sense (sine) and elevation current sense (cosine) develop a voltage across their respective sense resistors. (Refer to Figure 1055; U4050- pin 10 and Figure 1054, U4049-pin 10.)
16
The voltage developed across the current sense resistor is analogous to 1.1 amperes per volt.
17
This voltage is used as one input to the quad reset comparator (U4012). For each comparator the appropriate current limit output from the DAC is paired with its
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COMPONENT MAINTENANCE MANUAL 071-01519 appropriate motor driver current sense output. (Refer to Figure 1057 thru Figure 1060.)
EFFECTIVITY ALL
18
The output from the comparator is used to terminate the FPGA output to that motor driver thus maintaining motor current and generating a quasi-sinewave drive for the antenna.
19
The absence of an output at pin 10 of the motor drivers could indicate an open winding, an open sense resistor, or lack of a drive signal from the FPGA. Check pins 11, 7, and 5 of the motor drivers for the presence of a drive signal from the FPGA.
20
There will be no signal present on U4049 or U4050 unless in VP mode, conversely no drive signals will be present on U4033 or U4034 during VP mode. A continuous high drive signal to one or more of the motor drivers will in all likelihood cause its failure as well as a failure of the motor winding(s) it drives.
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1044. (Sheet 1 of 1) Normal Current and Voltage Waveforms Expected at the Cathode of Q4007 (Jct R4014-C4012/R4014 Current) (GRAPHIC 34-40-11-99B-850-A01) Key for Figure 1044. (Sheet 1 of 1) Top Trace
Bottom Trace
Signal:
Q4007 Cathode Voltage
Q4007 Cathode Current
Location:
Q4007 Cathode
R4014
Volts/Div:
100 V/Div
10 mV/Div 50 Ohms (5 A/Div)
Time/Div:
1 µsec/Div
1 µsec/Div
Probe:
X 10
Tek TM502A/A6302 (5 A/Div)
Trigger:
External TP4008 Pos.
External TP4008 Pos.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1045. (Sheet 1 of 1) Normal Current and Voltage Waveforms Expected Through CR4004 (Q4004 Drain/CR4004 Current) (GRAPHIC 34-40-11-99B-851-A01) Key for Figure 1045. (Sheet 1 of 1) Top Trace
Bottom Trace
Signal:
Q4004 Drain Voltage
CR4004 Current
Location:
CR4005 Cathode
CR4004
Volts/Div:
100 V/Div
10 mV/Div 50 Ohms (1 A/Div)
Time/Div:
1 µsec/Div
1 µsec/Div
Probe:
X 10
Tek TM502A/A6302 (1 A/Div)
Trigger:
External TP4008 Pos.
External TP4008 Pos.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1046. (Sheet 1 of 1) Normal Current Expected Through the Primary of T4002 (L4009) (GRAPHIC 34-40-11-99B-852-A01) Key for Figure 1046. (Sheet 1 of 1) Signal:
T4002 Primary Current
Location:
L4009
Volts/Div:
20 mV/Div 50 Ohms (10 A/Div)
Time/Div:
1 µsec/Div
Probe:
Tek AM503A/A6302 (5 A/Div)
Trigger:
External TP4008 Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1047. (Sheet 1 of 1) FPGA Done Programming Pin High Upon Successful Loading of Stored ROM Program (U4011-80) (GRAPHIC 34-40-11-99B-853-A01) Key for Figure 1047. (Sheet 1 of 1) Signal:
DP (Done Programming)
Location:
U4011-80
Volts/Div:
1 V/Div
Time/Div:
2 sec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1048. (Sheet 1 of 1) 1.025 MHz FPGA Clock (U4011-30) (GRAPHIC 34-40-11-99B-854-A01) Key for Figure 1048. (Sheet 1 of 1) Signal:
FPGA Clock
Location:
U4011-30
Volts/Div:
2 V/Div
Time/Div:
400 nsec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1049. (Sheet 1 of 1) Azimuth Current Limit Sine (U4013-2) (GRAPHIC 34-40-11-99B-855-A01) Key for Figure 1049. (Sheet 1 of 1) Signal:
V Out A (Azimuth Current Limit Sine)
Location:
U4013-2
Volts/Div:
200 mV/Div
Time/Div:
2 msec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1050. (Sheet 1 of 1) Azimuth Current Limit Cosine (U4013-1) (GRAPHIC 34-40-11-99B-856-A01) Key for Figure 1050. (Sheet 1 of 1) Signal:
V Out B (Azimuth Current Limit Cosine)
Location:
U4013-1
Volts/Div:
200 mV/Div
Time/Div:
2 msec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1051. (Sheet 1 of 1) Elevation Current Limit Sine (VP Mode, U4013-20) (GRAPHIC 34-40-1199B-857-A01) Key for Figure 1051. (Sheet 1 of 1) Signal:
V Out C (Elevation Current Limit Sine - VP)
Location:
U4013-20
Volts/Div:
200 mV/Div
Time/Div:
2 msec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1052. (Sheet 1 of 1) Elevation Current Limit Cosine (VP Mode, U4013-19) (GRAPHIC 34-40-11-99B-858-A01) Key for Figure 1052. (Sheet 1 of 1) Signal:
V Out D (Elevation Current Limit Cosine - VP)
Location:
U4013-19 (VP)
Volts/Div:
200 mV/Div
Time/Div:
2 msec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1053. (Sheet 1 of 1) Azimuth Current Sense Sine (U4034-10) (GRAPHIC 34-40-11-99B-859-A01) Key for Figure 1053. (Sheet 1 of 1) Signal:
Azimuth Current Sense (Sine)
Location:
U4034-10
Volts/Div:
500 mV/Div
Time/Div:
2 msec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1054. (Sheet 1 of 1) Azimuth Current Sense Cosine (U4033-10) (GRAPHIC 34-40-11-99B-860-A01) Key for Figure 1054. (Sheet 1 of 1) Signal:
Azimuth Current Sense (Cosine)
Location:
U4033-10
Volts/Div:
500 mV/Div
Time/Div:
2 msec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1055. (Sheet 1 of 1) Elevation Current Sense Sine (VP Mode, U4050-10) (GRAPHIC 34-4011-99B-861-A01) Key for Figure 1055. (Sheet 1 of 1) Signal:
Elevation Current Sense (Sine)
Location:
U4050-10
Volts/Div:
500 mV/Div
Time/Div:
2 msec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1056. (Sheet 1 of 1) Elevation Current Sense Cosine (VP Mode, U4049-10) (GRAPHIC 34-40-11-99B-862-A01) Key for Figure 1056. (Sheet 1 of 1) Signal:
Elevation Current Sense (Cosine)
Location:
U4049-10
Volts/Div:
500 mV/Div
Time/Div:
2 msec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1057. (Sheet 1 of 1) Azimuth Current Reset (Sine, U4012-2) (GRAPHIC 34-40-11-99B-863-A01) Key for Figure 1057. (Sheet 1 of 1) Signal:
Azimuth Current Reset (Sine)
Location:
U4012-2
Volts/Div:
1 V/Div
Time/Div:
2 msec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1058. (Sheet 1 of 1) Azimuth Current Reset (Cosine, U4012-1) (GRAPHIC 34-40-11-99B-864-A01) Key for Figure 1058. (Sheet 1 of 1) Signal:
Azimuth Current Reset (Cosine)
Location:
U4012-1
Volts/Div:
1 V/Div
Time/Div:
20 msec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1059. (Sheet 1 of 1) Elevation Current Reset (Sine, VP Mode, U4012-14) (GRAPHIC 34-40-1199B-865-A01) Key for Figure 1059. (Sheet 1 of 1) Signal:
Elevation Current Reset (Sine)
Location:
U4012-14
Volts/Div:
1 V/Div
Time/Div:
2- msec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 1060. (Sheet 1 of 1) Elevation Current Reset (Cosine, U4012-13) (GRAPHIC 34-40-11-99B-866-A01) Key for Figure 1060. (Sheet 1 of 1) Signal:
Elevation Current Reset (Cosine)
Location:
U4012-13
Volts/Div:
1 V/Div
Time/Div:
20 msec/Div
Probe:
X 10
Trigger:
Internal Positive
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
5.
Alignment Procedures (TASK 34-40-11-810-804-A01) A.
General (Subtask 34-40-11-810-009-A01)
WARNING:
THIS EQUIPMENT GENERATES MICROWAVE RADIATION WHICH CAN BE HARMFUL TO HUMANS. DO NOT OPERATE UNTIL YOU HAVE READ AND CAREFULLY FOLLOWED ALL SAFETY PRECAUTIONS AND INSTRUCTIONS IN THE OPERATIONS AND SERVICE MANUALS.
WARNING:
TO PREVENT HARM TO HUMANS, MAINTAIN PRESCRIBED SAFE DISTANCE WHEN STANDING IN FRONT OF A RADIATING ANTENNA. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
WARNING:
TO PREVENT HARM TO HUMANS, NEVER EXPOSE EYES OR ANY PART OF THE BODY TO AN UNTERMINATED WAVEGUIDE. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
WARNING:
OPERATION OF THIS EQUIPMENT INVOLVES THE USE OF HIGH VOLTAGES. THE TECHNICIAN OR OPERATOR MUST OBSERVE ALL SAFETY PRECAUTIONS WHEN PER- FORMING ANY TESTS OUTLINED IN THIS SECTION.
CAUTION:
THIS EQUIPMENT CONTAINS ELECTROSTATIC DISCHARGE SENSITIVE DEVICES. UNIT MODULES AND INDIVIDUAL ELECTROSTATIC DISCHARGE SENSITIVE DEVICES MUST BE HANDLED IN ACCORDANCE WITH SPECIAL ELECTROSTATIC DISCHARGE SENSITIVE HANDLING PROCEDURES. FAILURE TO DO SO CAN RESULT IN DAMAGE TO ELECTROSTATIC DISCHARGE SENSITIVE DEVICES.
(1)
The alignment of the ART 2000 consists of the alignment of the magnetron, video IF and receiver.
(2)
Alignment of the ART 2000 must be performed with all circuit modules and dummy load in place. All voltage readings at test points are referenced to ground unless otherwise stated.
(3)
Environmental Conditions (a)
Alignment must be performed under ambient conditions with temperature of 68 to 86 F (20 to 30 C) except where the receiver calibration requires alignment at the temperatures as follows: • -67 F (-55 C) • -22 F (-30 C) • +23 F (-5 C) • +68 F (+20 C) • +113 F (+45 C) • +158 F (+70 C).
B.
Pre-alignment Set-up Procedures (Subtask 34-40-11-810-010-A01) (1)
EFFECTIVITY ALL
Before you apply power to the unit, set the test harness/tester (user built, refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES section) to the following parameters. (a)
Set the power supply to 27.5 VDC.
(b)
Set S1 on the test harness/tester (user built, refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES section) for RT ON/ OFF No. 1.
(c)
Set S2 on the test harness/tester (user built, refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES section) for ARINC 429 control bus No. 1 operation.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519 (d) C.
Set S4 on the test harness/tester (user built, refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES section) to the open position.
Magnetron Current Set (Subtask 34-40-11-810-011-A01) (1)
Remove cover and fold logic board down.
(2)
Install a cross-coupler and load at the antenna port.
(3)
Insert current probe in cutout port on the power supply board. NOTE:
The wave-form will be inverted if the probe is used from the component side of the board.
(4)
Turn the unit on and wait for the one (1) minute warm-up period.
(5)
Adjust R4200 for a peak current of 2.5 to 3.5 Amps. NOTE: (a)
The peak current should be adjusted for best spectrum and power output. If the power output is above 3.0 kW, then adjust the peak current for best spectrum.
Spectrum: • Only one primary peak. • Symmetrical first side lobes (within 2 dB of each other). • First side lobes at least 6 dB down. • Tune the peak current to try and get the first sidelobes as close in amplitude as possible and still keep both of them as far down as possible from the primary peak.
D.
(6)
Select a value for L4009 that provides the least slope of the detected pulse.
(7)
Voltage at TP4003 will be in the range of 270 to 340 VDC.
(8)
Allow the unit to run ten (10) minutes and verify the settings.
(9)
Verify the correct power output.
59 MHz IF Alignment (Subtask 34-40-11-810-012-A01) (1)
Install the IF compartment cover.
(2)
Place the unit in TEST or STBY Mode. This will cause the STC/AGC and the Man_Gain to be fixed at 7 volts. (a)
Using a coax, apply a signal from the Radar Signal Generator to the IF. This coax must provide a dc block from the IF to the Radar Signal Generator. The following procedure must be performed with the IF cover installed. NOTE:
(b)
The following procedure must be performed with the IF cover installed.
Set the Radar Signal Generator to the following: • Mode: CW • Frequency: 59 MHz • Power out level: -20 dBm.
(c)
Adjust L5524 for 2.33 to 2.43 VDC at TP5018.
(d)
Set the Radar Signal Generator to the following: • Mode: CW • Frequency: 59 MHz • Power out level: -60 dBm.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
E.
(e)
Tune L5501, L5502, T5501, and T5502 for peak at TP5023.
(f)
Adjust the signal input level to maintain 2.5 to 3.5 VDC.
(g)
Sweep the input signal from 58 to 60 MHz and adjust L5501 and L5502 for the best bandpass symmetry and minimum ripple as viewed with an oscilloscope at TP5023.
(h)
Verify that the half-voltage bandwidth is 700 to 1100 kHz and that the half-voltage symmetry is about 58.9 to 59.1 MHz.
Receiver Calibration (Subtask 34-40-11-810-013-A01) NOTE:
(1)
If the magnetron, logic board, or receiver assembly is replaced, the ART 2000 will need a complete temperature range calibration at -67 , -22 , +23 , +68 , +113 , and +158 F (-55 , -30 , -5 , +20 , +45 , and +70 C). This will require the use of a calibrated temperature chamber, Thermatron or similar. If a calibrated temperature chamber is not available, the ART 2000 will need to be returned to the Honeywell Repair and Overhaul Facility.
Receiver calibration includes AFC, AGC, STC, MAN_GAIN and detector profiling in the following procedure. The following must be done before calibration: (a)
Toggle RCVR CAL ENABLE (SW5001-8) to the ON position.
(b)
Stabilization must be OFF during receiver calibration.
(c)
Turn MOTORS OFF with SCAN DISABLE (S5001-2). NOTE:
F.
When calibrating the receiver in ambient conditions +77 F (+25 C), the default values will be loaded into all other temperature zones if SW5001-3 is in the OFF position. IF SW5001-3 is in the ON position, then the default values will not be loaded.
AFC Calibration with Software Greater than 0103 (Subtask 34-40-11-810-014-A01) (1)
Radar Signal Generator Settings: • TARGET RANGE 40 NM (495 usec) • TARGET LEVEL OFF or -120 dBm (minimum signal input) • TARGET WIDTH 200 NM (2.4 msec).
(2)
Ground AFC_CAL (J5001-16).
(3)
Wait until CAL_LIGHT (J5001-38) goes high.
(4)
Set the TARGET LEVEL to -85 dBm. NOTE:
G.
If AGC calibration does not lock, repeat calibration using -75 dBm.
(5)
Momentarily ground CAL_INC (J5001-15).
(6)
CAL_LIGHT (J5001-38) will go high in approximately 15 seconds.
(7)
Remove ground from AFC_CAL (J5001-16).
(8)
Measure the AFC Offset to see if calibration is in tolerance. If calibration is out of tolerance, then repeat Steps (1) thru (7). If the unit fails to pass after several tries, then the unit may require repair or IF filter realignment.
Detector Calibration with Software Greater than 0103 (Subtask 34-40-11-810-015-A01) (1)
Radar Signal Generator Settings: • TARGET RANGE 40 NM (495 usec)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519 • TARGET LEVEL -115 dBm • TARGET WIDTH 200 NM (2.4 msec). (2)
Ground DET_CAL (J5001-14).
(3)
Momentarily ground CAL_INC (J5001-15) and wait until CAL_LIGHT (J5001-38) goes high.
(4)
Increment Radar Signal Generators TARGET LEVEL by 1 dB.
(5)
Momentarily ground CAL_INC (J5001-15).
(6)
CAL_LIGHT (J5001-38) will go low.
(7)
Wait until the CAL_LIGHT (J5001-38) goes high and then repeat Steps 5.G.(3), (4), (5), and (6) 40 times.
(8)
CAL_LIGHT (J5001-38) will FLASH after 40 times.
(9)
Set the TARGET LEVEL to minimum signal input (OFF or -120 dBm).
(10) Momentarily ground CAL_INC (J5001-15) and wait for CAL_LIGHT (J5001-38) to FLASH. (11) Set the TARGET LEVEL to -110 dBm (MDS) and then momentarily ground CAL_INC (J5001-15). (12) The CAL_LIGHT (J5001-38) will stay ON. (13) Remove the ground from DET_CAL (J5001-14). (14) Now test MDS, STC, and manual gain to determine if the calibration was successful. If not, then repeat Steps (1) thru (13). (15) STC Levels (a)
Set the indicator to 40 NM Wx mode and verify the 30 percent color levels ±3 dB of Table 1005. Table 1005. STC Levels
Antenna Size
Display Range
Target Distance
Target Width
ART 2000Level
Color Level (30%)
12 inch
40 NM
10 NM
35 µsec
-97 dBm
Green
12 inch
40 NM
10 NM
35 µsec
-88 dBm
Yellow
12 inch
40 NM
10 NM
35 µsec
-80 dBm
Red
12 inch
40 NM
10 NM
35 µsec
-76 dBm
Magenta
12 inch
40 NM
20 NM
35 µsec
-86 dBm
Red
(16) If the calibration was not successful, the guidelines that follow can be helpful: • If at +158 F (+70 C), start at -112 dBm • If at -67 F (-55 C), start at -118 dBm. (17) Toggle RCVR CAL ENABLE (SW5001-8) to the OFF position. (18) Turn MOTORS ON with SCAN DISABLE (S5001-2).
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
6.
Retest Procedure (TASK 34-40-11-810-805-A01) A.
General (Subtask 34-40-11-810-016-A01)
WARNING:
THIS EQUIPMENT GENERATES MICROWAVE RADIATION WHICH CAN BE HARMFUL TO HUMANS. DO NOT OPERATE UNTIL YOU HAVE READ AND CAREFULLY FOLLOWED ALL SAFETY PRECAUTIONS AND INSTRUCTIONS IN THE OPERATIONS AND SERVICE MANUALS.
WARNING:
TO PREVENT HARM TO HUMANS, MAINTAIN PRESCRIBED SAFE DISTANCE WHEN STANDING IN FRONT OF A RADIATING ANTENNA. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
WARNING:
TO PREVENT HARM TO HUMANS, NEVER EXPOSE EYES OR ANY PART OF THE BODY TO AN UNTERMINATED WAVEGUIDE. REFER TO FAA ADVISORY CIRCULAR NO. 20-68B.
(1)
7.
Service Information (TASK 34-40-11-810-806-A01) A.
Proper Test Equipment Usage (Subtask 34-40-11-810-017-A01) (1)
B.
Failure of semiconductor devices and integrated circuits by accidental application of excessive voltage or current is reduced with proper test equipment usage. (a)
Do not use multimeters with sensitivities less than 5000-ohms-per-volt. Use at least a 20,000-ohms-pervolt multimeter or a vacuum tube voltmeter.
(b)
Do not use test equipment with transformerless power supplies unless an isolation transformer is used in the ac power line.
(c)
Use a conductive table top for testing and connect the table top to the ground conductor of the 60Hz power line.
(d)
Test equipment with a line filter across the ac input can accidentally apply 55 Vac to semiconductor devices. Always connect a ground wire from the test equipment chassis to the chassis of the unit-under test before making any other connections.
(e)
All low impedance equipment (such as pulse generators, etc.) should be disconnected before DC power supplies are turned off.
Capacitor Testing (Subtask 34-40-11-810-018-A01) (1)
Check all capacitors with proper voltage polarity. Polarized capacitors are damaged by reverse voltage and should be replaced if that occurs.
(2)
Check all capacitors with proper voltage level. A capacitor may be damaged if the voltage applied exceeds the dc working voltage of that capacitor.
(3)
When checking tantalum capacitors, use a series resistor to limit the charge and discharge rates to prevent surge damage to the capacitor. The value of the series resistor should be 10 ohms for each volt applied to the capacitor.
EFFECTIVITY ALL
After a fault has been isolated and repaired, the unit should be subjected to the functional test in the Testing section of this manual to ensure that the repaired area is operating correctly and that other areas have not been damaged during the repair procedure.
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COMPONENT MAINTENANCE MANUAL 071-01519 C.
Transistor Testing (Subtask 34-40-11-810-019-A01) BEFORE INSTALLING A REPLACEMENT TRANSISTOR, MAKE SURE THAT OTHER ELEMENTS OF THE CIRCUIT ARE IN GOOD OPERATING ORDER. IF A DEFECT EXISTS IN THE CIRCUIT, THE REPLACEMENT TRANSISTOR MAY ALSO FAIL.
CAUTION:
(1)
Tables Table 1006 and Table 1007 provide typical testing data for PNP and NPN transistors. Connect the ohmmeter per polarity indicated by base, collector and emitter columns of the tables. Table 1006. PNP Transistor Testing Procedure
Check No.
Base
Emitter
Range
Relative Resistance
1
-
+
RX100 or RX1,000
Low (1,000 ohms or less)
2
+
-
RX10,000
High (100,000 ohms or more)
Collector
3
-
+
RX10,000
High (100,000 ohms or more)
4
+
-
RX10,000
High (100,000 ohms or more)
5
-
+
RX100 or RX1,000
Low (1,000 ohms or less)
6
+
-
RX10,000
High (100,000 ohms or more)
7 Connect base to collector
-
+
RX100 or RX1,000
Resistance should decrease from that obtained in Check No. 3
8 Connect base to emitter
-
+
RX10,000
High (100,000 ohms or more)
Table 1007. NPN Transistor Testing Procedure Check No.
Base
Emitter
Range
Relative Resistance
1
+
-
RX100 or RX1,000
Low (1,000 ohms or less)
2
-
+
RX10,000
High (100,000 ohms or more)
Collector
3
+
-
RX10,000
High (100,000 ohms or more)
4
-
+
RX10,000
High (100,000 ohms or more)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table 1007. NPN Transistor Testing Procedure (Cont) Check No.
Base
Collector
5
+
6
-
Emitter
Range
Relative Resistance
-
RX100 or RX1,000
Low (1,000 ohms or less)
+
RX10,000
High (100,000 ohms or more)
7 Connect base to collector
+
-
RX100 or RX1,000
Resistance should decrease from that obtained in check 3.
8 Connect base to emitter
+
-
RX10,000
High (100,000 ohms or more)
D.
Integrated Circuit Testing (Subtask 34-40-11-810-020-A01)
CAUTION:
BEFORE INSTALLING A REPLACEMENT IC, VERIFY THERE IS NO VOLTAGE 10 PERCENT GREATER THAN +VCC OR -VCC ON ANY OF THE IC HOLES ON THE BOARD. VERIFY THERE IS NO GROUND ON ANY IC HOLE THAT MUST NOT BE GROUNDED.
CAUTION:
BEFORE INSTALLING A REPLACEMENT IC, MAKE SURE THAT OTHER ELEMENTS OF THE CIRCUIT ARE IN GOOD OPERATING ORDER. IF A DEFECT EXISTS IN THE CIRCUIT, THE REPLACEMENT IC MAY ALSO FAIL.
(1)
Common digital IC failures are listed in following table. Table 1008. Common IC Failures
Symptom
Possible Cause
Constant LO
Input(s) or output shorted to ground pin of IC.
Constant HI
Input(s) or output shorted to Vcc pin of IC.
Approx. 1.5 VDC
Open input(s) or output.
Output cannot go LO
Ground pin open.
Output cannot go HI
Vcc pin open.
Output cannot change
Inputs shorted together.
(2)
EFFECTIVITY ALL
Series 54/74 Integrated Circuits (a)
Type-number identification is becoming increasingly complex for the 54/74 series of integrated circuits. These chips were originally referred to as TTL but many different type numbers now apply to chips that perform the same logical function, although specifications (temperature, speed, power, etc.) and interior configurations may be different.
(b)
Usually, the only difference in the type numbers involves the alpha characters immediately following the 54/74 designation. Refer to Table 1009 as a guideline in determining the specific specifications of each type.
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COMPONENT MAINTENANCE MANUAL 071-01519 (c)
Most chips are available in both 54 series and 74 series type numbers. The 54 series have an operating temperature specification of -67 to 257 F (-55 to 125 C), and the 74 series have a temperature specification of 32 to 158 F (0 to 70 C). Table 1009. 54/74 Series IC Alpha Character Significance
Alpha Character
Significance
None
Standard TTL
S
Schottky-clamped TTL device. Contains the integrated Schottky-Barrier diode-clamped transistor circuitry.
LS
Low-power Schottky TTL device.
AS
Advanced Schottky TTL device.
ALS
Advanced Low-power Schottky TTL device.
HC
High-speed CMOS device. Requires special ESDS handling.
HCT
High-speed CMOS with TTL input voltage level compatibility. Requires special ESDS handling.
AC
Advanced CMOS device. Requires special ESDS handling.
ACT
Advanced CMOS with input TTL compatibility. Requires special ESDS handling. (3)
Integrated Circuit Functional Diagrams (a)
The truth table of a logic element is a primary fault isolation tool. A HI level on all digital logic elements used in the unit is between +2 VDC and +5 VDC in TTL circuits and +3.5 VDC to +5 VDC in CMOS circuits.
(b)
A LO level is less than +0.8 VDC in TTL and +1.5 VDC in CMOS circuits. When checking input and output levels of a logic element under question it should be remembered that an input or output may not agree with its truth table, not because it has malfunctioned, but because some other component connected to the same point has shorted to ground or to (Vcc). This is not uncommon when an output of one element is connected to an input of another. It may be necessary to isolate the gate under question by unsoldering the necessary IC pins.
(c)
Table 1010 is an index of Honeywell PNs to standard type numbers for certain integrated circuits. Information on these and other basic logic elements, operational amplifiers, and other circuits is readily available from publications such as general IC data books or basic electronic theory. Table 1010. Index to Integrated Circuit Diagrams
HPN
Type No.
Description
120-02213-0002
Z84C00
Microprocessor
120-02363-0009
6206BNJC35
32X8 static RAM
120-02452-0000
MAX699EWE
Watchdog controller
120-02494-0000
X20C16JI-55
2KX8 NOVRAM
120-03285-0002
CA3306CM
A/D Converter
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table 1010. Index to Integrated Circuit Diagrams (Cont) HPN
Type No.
Description
120-03475-0003
C0820
8-bit A/D converter
120-03488-0000
PM7224FS
DAC
120-03520-0000
MC3423D
Overvoltage sensor
120-03569-0000
L6203
Full bridge driver
120-03592-0000
AD7226KR
Quad 8-bit DAC
120-03598-0000
HI9P-5700A-9
Flash 8-bit A/D converter
120-06065-0002
AD7533KR
10-bit DAC
120-08030-0002
N/A
429 transceiver
E.
Job Close-up (Subtask 34-40-11-810-021-A01) (1)
EFFECTIVITY ALL
Not applicable.
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COMPONENT MAINTENANCE MANUAL 071-01519
SCHEMATIC AND WIRING DIAGRAMS 1.
Planning Data (TASK 34-40-11-99C-802-A01) A.
B.
Reason for the Job (Subtask 34-40-11-99C-004-A01) (1)
This section gives schematic and wiring diagrams for the ART 2000.
(2)
Use these diagrams as an aid to fault isolate the ART 2000.
Job Setup Data (Subtask 34-40-11-99C-005-A01) (1)
You can use equivalent alternatives for the special tools, fixtures, equipment, and consumable materials. The user must find equivalent alternatives.
(2)
Refer to Table 2001 for the specified special tools, fixtures, and equipment in this section.
(3)
Refer to H4/H8 CAGE Codes (available at http://www.dlis.dla.mil/cage_welcome.asp) for manufacturer’s address. Table 2001. Special Tools, Fixtures, and Equipment
Number
Description
Source
Not applicable
Not applicable
Not applicable
WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
(4)
Refer to Table 2002 for the specified consumable materials in this section. Table 2002. Consumables
Number
Description
17631
RTV sealant (CAGE 1UCL7)
425
locking compound (CAGE 1UCL7)
4444
instant adhesive (CAGE 1UCL7)
73
locking compound (CAGE 1UCL7)
Source
lacing tape, 1/16 inch, 20-pound strength (commercially available) protective coating, Type AR, fluorescent, MIL-I-46058 (commercially available) E-6000
adhesive sealant, encapsulate (CAGE 04065) (5)
The list that follows identifies Honeywell publications that are related to this section: • Not applicable.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
2.
Outline/Schematic Diagrams (TASK 34-40-11-000-801-A01) A.
Job Setup (Subtask 34-40-11-000-001-A01) (1)
B.
Not applicable.
Outline and Detail/Schematic Diagrams (Subtask 34-40-11-000-002-A01) (1)
Table 2003 shows the outline and detail/schematic diagrams in this section. Table 2003. Outline and Detail/Schematic Diagrams
Nomenclature
PN
Figure No.
ART 2000
071-01519-0101
Figure 2001
ART 2000 rear connector
N/A
Figure 2002
Logic board
200-08549-0000
Figure 2003
Logic board
200-08549-0020
Figure 2004
Receiver assembly
200-05553-0001
Figure 2005
Preamp board
200-08545-0000
Figure 2006
Preamp board
200-08545-0020
Figure 2007
Power supply/modulator board
200-08548-0000
Figure 2008
Power supply/modulator board
200-08548-0020
Figure 2009
Configuration module assembly
071-00097-0100
Figure 2010
Configuration module
200-08705-0000
Figure 2011
Table 2004. Summary of Unit Modifications, PN 071-01519-0101 1
Unit MOD No.
Affected Module(s)
Description of Change
SBN
3
Logic board, Preamp board, and Power supply /modulator board
Improves manufacturability of the of the Logic board, Preamp board, and the Power supply/modulator board.
600-07790-0030 (SB ART 2000-3)
1719 and below
4
Logic board
Improves radar stabilization accuracy during small inputs of pitch and roll from gyro.
600-07790-0041 (SB ART 2000-4)
1833 and below
5
Logic board
Incorporates new STC curves.
600-07790-0050 (SB ART 2000-5)
2190 and below
6
Logic board
Improves the ARL circuit.
600-07790-0060 (SB ART 2000-6)
2499 and below
7
Logic board
Provides a more robust connector.
600-07790-0071 (SB ART 2000-7)
4429 and below
EFFECTIVITY ALL
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S/N Effectivity
Page 2002 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Table 2004. Summary of Unit Modifications, PN 071-01519-0101 (Cont) 1
Unit MOD No.
Affected Module(s)
Description of Change
SBN
8
Power supply /modulator board
Reduces the risk of blowing fuse F1.
600-07790-0080 (SB ART 2000-8)
4408 and below
9
Power supply /modulator board
Provides a more robust capacitor.
600-07790-0090 (SB ART 2000-9)
6242 and below
10
Replaces pivot pins and pivot pin nuts to prevent wear on the IF cable.
600-07791-0000 (SB ART 2000-10)
9566 and below
11
Replaces pitch/tilt motor assembly to prevent breaking wire leads on the pitch/tilt motor assembly.
600-07791-0011 (SB ART 2000-11)
11674 and below
Logic board
Makes sure that antenna parks correctly when unit is put in OFF position and to make more accurate maintenance logs for EFIS display.
600-07791-0020 (ART 2000-340012)
N/A
Logic board
Replaces R5066 with new PN 139-01652-0000 and R5166 with new PN 139-01502-0000 to improve the AFC circuits.
601-07791-0010 (SA ART 2000-111)
All
Power supply /modulator board
Adds an insulator, PN 012-01673-001, to the board.
601-07790-0020 (SA ART 2000-102)
All
Logic board
U5091, PN 120-08030-0002, is no longer available, use PN 120-08030-0010 if required.
601-07790-0030 (SA ART 2000-103)
All
Logic board
Improves radar stabilization performance by optimizing antenna startup positioning and increasing resolution in the stabilization algorithms.
605-07790-0031 (SWB ART 2000-SW3)
2100 and below
Logic board
Improves radar stabilization performance by optimizing antenna startup positioning and increasing resolution in the stabilization algorithms.
605-07790-0041 (SWB ART 2000-SW4)
2190 and below
Logic board
Improves radar stabilization performance by optimizing antenna startup positioning and increasing resolution in the stabilization algorithms.
605-07790-0050 (SWB ART 2000-SW5)
2482 and below
12
NOTE: 1
Refer to the SERVICE BULLETIN LIST in this manual.
EFFECTIVITY ALL
S/N Effectivity
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2003 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2004 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2001. (Sheet 1 of 2) ART 2000 Outline Drawing (GRAPHIC 34-40-11-99B-867-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2005/2006 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2001. (Sheet 2 of 2) ART 2000 Outline Drawing (GRAPHIC 34-40-11-99B-867-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2007/2008 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2002. (Sheet 1 of 1) ART 2000 P5001 Connector Pin Function Diagram (GRAPHIC 34-40-1199B-868-A01) Key for Figure 2002. (Sheet 1 of 1) Pin I/O
Signal Name
Pin I/O
Signal Name
1
Input
STRUT SWITCH IN
26
Output
ARINC 575 ALTITUDE B-2
2
Input
CONTROL 1 429 RECEIVER A
27
Output
ARINC 575 ALTITUDE B-4
3
Input
CONTROL 1 429 RECEIVER B
28
Output
ARINC 575 ALTITUDE D-4
4
Input
CONTROL 2 429 RECEIVER A
29
5
Input
CONTROL 2 429 RECEIVER B
30
Output
ARINC 575 SUPER FLAG
6
Input
CONTROL 3 429 RECEIVER A
31
Input
IND No. 1 ON/OFF (ON=GND)
7
Input
CONTROL 3 429 RECEIVER B
32
Input
IND No. 2 ON/OFF (ON=GND)
8
Input
ARINC 429 STABILIZATION A
33
Input
IND No. 3 ON/OFF (ON=GND)
9
Input
ARINC 429 STABILIZATION B
34
Input
+28 VDC AIRCRAFT POWER
10
Input
ARINC 429 ALTITUDE A
35
Input
+28 VDC AIRCRAFT POWER
11
Input
ARINC 429 ALTITUDE B
36
POWER AND CHASSIS GROUND
12
Output
TIME/TEMP OUT A (MAINT ONLY)
37
POWER AND CHASSIS GROUND
13
Output
TIME/TEMP OUT B (MAINT ONLY)
38
CAL LIGHT (MAINT ONLY)
14
DETECTOR CAL (MAINT ONLY)
39
SPARE
15
CALIBRATION INC (MAINT ONLY)
40
16
AFC ADJUST (MAINT ONLY)
41
ARINC 575 COMMON
Input
GYRO REFERENCE HI GYRO REFERENCE COMMON
17
Input
ALTITUDE VALID
42
Output
ARINC 453 DATA BUS 1A
18
Input
PITCH STABILIZATION HI
43
Output
ARINC 453 DATA BUS 1B
19
Input
PITCH STABILIZATION LO
44
Output
+5 VDC CONF MODULE VOLTAGE
20
Input
ROLL STABILIZATION HI
45
Output
CONF MODULE CLOCK
21
Input
ROLL STABILIZATION LO
46
Output
CONF MODULE CHIP SELECT 1
22
Output
ARINC 575 ALTITUDE A-1
47
Output
CONF MODULE CHIP SELECT 2
23
Output
ARINC 575 ALTITUDE A-2
48
Output
CONF MODULE DATA OUT
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2009 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Key for Figure 2002. (Sheet 1 of 1) (Cont) Pin I/O
Signal Name
Pin I/O
Signal Name
24
Output
ARINC 575 ALTITUDE A-4
49
CONF MODULE DATA IN
25
Output
ARINC 575 ALTITUDE B-1
50
Input
CONF MODULE GROUND
Table 2005. Summary of Changes to the Logic Board, PN 200-08549-0000 1
Subassembly MOD No.
Description of Change
SBN
4
Cuts a path from CR5014 pin 1 to the via hole.
600-07790-0041 (SB ART 2000-4)
1833 and below
5
Replaces U5013 with PN 122-30049-0004 and U5038 with PN 122-30048-0002.
600-07790-0050 (SB ART 2000-5)
2190 and below
6
Replaces U5038 with PN 122-30048-0003.
600-07790-0060 (SB ART 2000-6)
2499 and below
7
Replaces J5001 with a more robust connector PN 030-03252-0008.
600-07790-0071 (SB ART 2000-7)
4429 and below
13
Cut trace and install wire between Pin 1 and Pin 23 on U5.
D200906000080 (SB ART 2000-34-14)
12724 and below
NOTE: 1
Refer to the SERVICE BULLETIN LIST in this manual.
EFFECTIVITY ALL
S/N Effectivity
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2010 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 1 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2011/2012 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 2 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2013/2014 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 3 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2015/2016 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 4 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2017/2018 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 5 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2019/2020 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 6 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2021/2022 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 7 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2023/2024 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 8 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2025/2026 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 9 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2027/2028 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 10 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2029/2030 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 11 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2031/2032 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 12 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2033/2034 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 13 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2035/2036 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 14 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2037/2038 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 15 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2039/2040 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 16 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2041/2042 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 17 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2043/2044 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 18 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2045/2046 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2003. (Sheet 19 of 19) Logic Board, PN 200-08549-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-869-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2047/2048 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 Table 2006. Summary of Changes to the Logic Board, PN 200-08549-0020 1
Subassembly MOD No.
Description of Change
SBN
4
Cuts a path from CR5014 pin 1 to the via hole.
600-07790-0041 (SB ART 2000-4)
1833 and below
5
Replaces U5013 with PN 122-30049-0004 and U5038 with PN 122-30048-0002.
600-07790-0050 (SB ART 2000-5)
2190 and below
6
Replaces U5038 with PN 122-30048-0003.
600-07790-0060 (SB ART 2000-6)
2499 and below
7
Replaces J5001 with a more robust connector PN 030-03252-0008.
600-07790-0071 (SB ART 2000-7)
4429 and below
12
Replaces U5005 with PN 53002736-1.
600-07791-0020 (ART 2000-340012)
N/A
Replaces R5066 with new PN 139-01652-0000 and R5166 with new PN 139-01502-0000 to improve the AFC circuits
601-07791-0010 (SA ART 2000-111)
All
U5091 PN 120-08030-0002 is no longer available, use PN 120-08030-0010, if required.
601-07790-0030 (SA ART 2000-103)
All
Replaces U5003 with PN 122-01338-0107.
605-07790-0031 (SWB ART 2000-SW3)
2100 and below
Replaces U5003 with PN 122-01338-0108.
605-07790-0041 (SWB ART 2000-SW4)
2190 and below
Replaces U5003 with PN 122-01338-0109.
605-07790-0050 (SWB ART 2000-SW5)
2482 and below
NOTE: 1
Refer to the SERVICE BULLETIN LIST in this manual.
EFFECTIVITY ALL
S/N Effectivity
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2049 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2050 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 1 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2051/2052 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 2 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2053/2054 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 3 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2055/2056 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 4 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2057/2058 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 5 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2059/2060 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 6 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2061/2062 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 7 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2063/2064 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 8 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2065/2066 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 9 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2067/2068 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 10 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2069/2070 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 11 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2071/2072 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 12 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2073/2074 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 13 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2075/2076 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 14 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2077/2078 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 15 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2079/2080 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 16 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2081/2082 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 17 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2083/2084 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 18 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2085/2086 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 19 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2087/2088 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2004. (Sheet 20 of 20) Logic Board, PN 200-08549-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-870-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2089/2090 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 Table 2007. Summary of Changes to the Receiver Assembly, PN 200-05553-0001 Subassembly MOD No.
NOTE: 1
SBN
1
S/N Effectivity
Refer to the SERVICE BULLETIN LIST in this manual.
EFFECTIVITY ALL
Description of Change
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2091 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2092 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2005. (Sheet 1 of 1) Receiver Assembly, PN 200-05553-0001, Detail (GRAPHIC 34-40-11-99B-871-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2093/2094 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 Table 2008. Summary of Changes to the Preamp Board, PN 200-08545-0000 Subassembly MOD No.
NOTE: 1
SBN
1
S/N Effectivity
Refer to the SERVICE BULLETIN LIST in this manual.
EFFECTIVITY ALL
Description of Change
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2095 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2096 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2006. (Sheet 1 of 2) Preamp Board, PN 200-08545-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-872-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2097/2098 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2006. (Sheet 2 of 2) Preamp Board, PN 200-08545-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-872-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2099/2100 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 Table 2009. Summary of Changes to the Preamp Board, PN 200-08545-0020 Subassembly MOD No.
NOTE: 1
SBN
1
S/N Effectivity
Refer to the SERVICE BULLETIN LIST in this manual.
EFFECTIVITY ALL
Description of Change
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2101 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2102 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2007. (Sheet 1 of 2) Preamp Board, PN 200-08545-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-873-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2103/2104 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2007. (Sheet 2 of 2) Preamp Board, PN 200-08545-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-873-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2105/2106 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 Table 2010. Summary of Changes to the Power Supply/Modulator Board, PN 200-08548-0000 Subassembly MOD No.
NOTE: 1
SBN
1
S/N Effectivity
Refer to the SERVICE BULLETIN LIST in this manual.
EFFECTIVITY ALL
Description of Change
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2107 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2108 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2008. (Sheet 1 of 12) Power Supply/Modulator Board, PN 200-08548-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-874-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2109/2110 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2008. (Sheet 2 of 12) Power Supply/Modulator Board, PN 200-08548-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-874-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2111/2112 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2008. (Sheet 3 of 12) Power Supply/Modulator Board, PN 200-08548-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-874-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2113/2114 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2008. (Sheet 4 of 12) Power Supply/Modulator Board, PN 200-08548-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-874-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2115/2116 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2008. (Sheet 5 of 12) Power Supply/Modulator Board, PN 200-08548-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-874-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2117/2118 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2008. (Sheet 6 of 12) Power Supply/Modulator Board, PN 200-08548-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-874-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2119/2120 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2008. (Sheet 7 of 12) Power Supply/Modulator Board, PN 200-08548-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-874-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2121/2122 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2008. (Sheet 8 of 12) Power Supply/Modulator Board, PN 200-08548-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-874-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2123/2124 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2008. (Sheet 9 of 12) Power Supply/Modulator Board, PN 200-08548-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-874-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2125/2126 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2008. (Sheet 10 of 12) Power Supply/Modulator Board, PN 200-08548-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-874-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2127/2128 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2008. (Sheet 11 of 12) Power Supply/Modulator Board, PN 200-08548-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-874-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2129/2130 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2008. (Sheet 12 of 12) Power Supply/Modulator Board, PN 200-08548-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-874-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2131/2132 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 Table 2011. Summary of Changes to the Power Supply/Modulator Board, PN 200-08548-0020 1
Subassembly MOD No.
Description of Change
SBN
8
Reduces U4015 pin 1, from 9.2 volts to 5 volts by jumpering to U4014 pin 1.
600-07790-0080 (SB ART 2000-8)
4408 and below
9
Replace C4019 with a more robust capacitor PN 097-00238-0093.
600-07790-0090 (SB ART 2000-9)
6242 and below
Adds an insulator PN 012-01673-001 to the board.
601-07790-0020 (SA ART 2000-102)
All
NOTE: 1
Refer to the SERVICE BULLETIN LIST in this manual.
EFFECTIVITY ALL
S/N Effectivity
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2133 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2134 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2009. (Sheet 1 of 12) Power Supply/Modulator Board, PN 200-08548-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-875-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2135/2136 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2009. (Sheet 2 of 12) Power Supply/Modulator Board, PN 200-08548-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-875-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2137/2138 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2009. (Sheet 3 of 12) Power Supply/Modulator Board, PN 200-08548-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-875-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2139/2140 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2009. (Sheet 4 of 12) Power Supply/Modulator Board, PN 200-08548-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-875-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2141/2142 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2009. (Sheet 5 of 12) Power Supply/Modulator Board, PN 200-08548-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-875-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2143/2144 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2009. (Sheet 6 of 12) Power Supply/Modulator Board, PN 200-08548-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-875-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2145/2146 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2009. (Sheet 7 of 12) Power Supply/Modulator Board, PN 200-08548-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-875-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2147/2148 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2009. (Sheet 8 of 12) Power Supply/Modulator Board, PN 200-08548-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-875-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2149/2150 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2009. (Sheet 9 of 12) Power Supply/Modulator Board, PN 200-08548-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-875-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2151/2152 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2009. (Sheet 10 of 12) Power Supply/Modulator Board, PN 200-08548-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-875-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2153/2154 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2009. (Sheet 11 of 12) Power Supply/Modulator Board, PN 200-08548-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-875-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2155/2156 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2009. (Sheet 12 of 12) Power Supply/Modulator Board, PN 200-08548-0020, Detail/Schematic (GRAPHIC 34-40-11-99B-875-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2157/2158 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 Table 2012. Summary of Changes to the Configuration Module Assembly, PN 071-00097-0100 Subassembly MOD No.
NOTE: 1
SBN
1
S/N Effectivity
Refer to the SERVICE BULLETIN LIST in this manual.
EFFECTIVITY ALL
Description of Change
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2159 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2160 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2010. (Sheet 1 of 1) Configuration Module Assembly, PN 071-00097-0100, Detail (GRAPHIC 34-40-11-99B-876-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2161/2162 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 Table 2013. Summary of Changes to the Configuration Module, PN 200-08705-0000 Subassembly MOD No.
NOTE: 1
SBN
1
S/N Effectivity
Refer to the SERVICE BULLETIN LIST in this manual.
EFFECTIVITY ALL
Description of Change
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2163 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2164 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2011. (Sheet 1 of 2) Configuration Module, PN 200-08705-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-877-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2165/2166 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 2011. (Sheet 2 of 2) Configuration Module, PN 200-08705-0000, Detail/Schematic (GRAPHIC 34-40-11-99B-877-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 2167/2168 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 C.
Job Close-up (Subtask 34-40-11-000-003-A01) (1)
EFFECTIVITY ALL
Not applicable.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2169 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 2170 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
DISASSEMBLY 1.
Planning Data (TASK 34-40-11-99C-803-A01) A.
Reason for the Job (Subtask 34-40-11-99C-006-A01) (1)
B.
Use these procedures to remove parts from the ART 2000 to do the cleaning, checks, and repair. Do only those procedures of disassembly that are necessary to remove the defective parts.
Job Setup Data (Subtask 34-40-11-99C-007-A01) (1)
You can use equivalent alternatives for the special tools, fixtures, equipment, and consumable materials. The user must find equivalent alternatives.
(2)
Refer to Table 3001 for the specified special tools, fixtures, and equipment in this section.
(3)
Refer to H4/H8 CAGE Codes (available at http://www.dlis.dla.mil/cage_welcome.asp) for manufacturer’s address. Table 3001. Special Tools, Fixtures, and Equipment
Number
Description
Source
allen wrench, 9/64-inch, beryllium copper (commercially available) WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
(4)
Refer to Table 3002 for the specified consumable materials in this section. Table 3002. Consumables
Number
Description
Source
Not applicable
Not applicable
Not applicable
(5)
The list that follows identifies Honeywell publications that are related to this section: (a)
EFFECTIVITY ALL
Not applicable.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 3001 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
2.
Procedure (TASK 34-40-11-000-802-A01) A.
B.
C.
Job Setup (Subtask 34-40-11-000-004-A01) WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
WARNING:
REMOVE ALL POWER FROM THE UNIT BEFORE DISASSEMBLY OF ANY MODULE. BESIDES BEING DANGEROUS TO LIFE, VOLTAGE TRANSIENTS CAN CAUSE CONSIDERABLE DAMAGE TO THE EQUIPMENT.
CAUTION:
EXERCISE EXTREME CARE WHEN DISCONNECTING AND RECONNECTING THE MULTIPLE PIN CONNECTORS TO ENSURE THAT THE CONNECTORS ARE NOT DAMAGED BY MISALIGNMENT OF THE PINS.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
CAUTION:
USE INDUSTRY APPROVED ELECTROSTATIC DISCHARGE SENSITIVE PRECAUTIONS. THE ART 2000 CONTAINS ELECTROSTATIC DISCHARGE SENSITIVE ITEMS.
CAUTION:
DO NOT DROP OR HIT THE ART 2000 DURING THESE PROCEDURES. THE ART 2000 CONTAINS AN ASSEMBLY THAT CAN BE DAMAGED FROM INCORRECT USE.
CAUTION:
DO THESE PROCEDURES IN A CLEAN ENVIRONMENT TO PREVENT DAMAGE TO MECHANICAL COMPONENTS.
(1)
Obey the precautions.
(2)
The item numbers shown in the DPL are the same as the item numbers on the exploded view illustration(s). To find a PN, find the part on the illustration and note the item number. Find the item number in the parts list and read the correct PN. Item numbers refer to the same figure until a different figure is specified.
(3)
Before disassembly, use TESTING AND FAULT ISOLATION to examine the condition of the unit or to find the malfunction. Do this to prevent disassembly that is not necessary.
(4)
As an aid for assembly, tag the items that are disconnected to show where the connections were made.
(5)
Include data for special conditions of a connection such as the polarity and the position of the items.
(6)
Identify the tie points for the wire assembly to prevent damage to the wire insulation during assembly.
Bottom Cover Removal (Subtask 34-40-11-000-005-A01) (1)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(2)
Remove the nine screws (45) from the cover (35).
(3)
Remove the two screws (40) on either side of the connector.
(4)
Remove the cover (35) from the base (290).
Logic Board Removal (Subtask 34-40-11-000-006-A01) (1)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(2)
Remove the cover (35) as described in Paragraph 2.B. (Subtask 34-40-11-000-005-A01).
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 3002 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
D.
(3)
Remove the screw (60) located toward the center of the logic board (135).
(4)
Remove the two screws (65) that fasten the connector to the base (290).
(5)
Remove the IF cover (85).
(6)
Make a note of all the cable connections for reassembly. Disconnect all the cables.
Power Supply/Modulator Board Removal (Subtask 34-40-11-000-007-A01) (1)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(2)
Remove the cover (35) as described in Paragraph 2.B. (Subtask 34-40-11-000-005-A01).
(3)
Remove the logic board (135) as described in Paragraph 2.C. (Subtask 34-40-11-000-006-A01).
(4)
Remove the two screws (100) from the power supply/modulator board (140).
(5)
Remove the five screws (95), the two spacers (70), and the two spacers (75). Refer to the decal on the bottom cover to identify the screws to be removed.
(6)
Make note of all the cable routes and connections for reassembly. Disconnect all the cables.
(7)
Remove the power supply/modulator board (140) from the base (290). NOTE:
E.
F.
Receiver Module Removal (Subtask 34-40-11-000-008-A01) (1)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(2)
Remove the cover (35) as described in Paragraph 2.B. (Subtask 34-40-11-000-005-A01).
(3)
Remove the logic board (135) as described in Paragraph 2.C. (Subtask 34-40-11-000-006-A01).
(4)
Remove the power supply/modulator board (140) as described in Paragraph 2.D. (Subtask 34-40-11-000-007-A01).
(5)
Tilt the gimbal assembly (230) to the side with the pitch motor (50, IPL Figure 9) up.
(6)
Remove the four cap screws (120, IPL Figure 9) which fasten the cable guard (115, IPL Figure 9), the receiver assembly (140, IPL Figure 9), the shroud cable (135, IPL Figure 9), and the limiter (175, IPL Figure 9) to the RF network (165, IPL Figure 9).
(7)
Separate the receiver assembly (140, IPL Figure 9) from the limiter (175, IPL Figure 9).
(8)
Remove the three screws (275) and the clamp (270) that enclose the cable ferrules from the base (290).
(9)
Separate the cable ferrules from the base (290) and remove the receiver assembly (140, IPL Figure 9).
Preamp Board Removal (Subtask 34-40-11-000-009-A01) (1)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(2)
Remove the cover (35) as described in Paragraph 2.B. (Subtask 34-40-11-000-005-A01).
(3)
Remove the logic board (135) as described in Paragraph 2.C. (Subtask 34-40-11-000-006-A01).
(4)
Remove the receiver assembly (140, IPL Figure 9) as described in Paragraph 2.E. (Subtask 34-40-11-000-008-A01).
(5)
Remove the screw (10, IPL Figure 4), the two screws (15, IPL Figure 4) and the cover (5, IPL Figure 4).
(6)
Disconnect P1001 from J1001 and P1002 from J1002.
(7)
Desolder E1001, E1002, E1003, and E1004.
EFFECTIVITY ALL
If the high-voltage transformer is to be replaced, cut the magnetron cable at the center of the splice.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 3003 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
G.
(8)
Remove the two spacers (35 and 40, IPL Figure 4) and the two washers (45, IPL Figure 4) from the preamp housing (55, IPL Figure 4).
(9)
Remove the screw (30, IPL Figure 4), the preamp board (25, IPL Figure 4), and the microwave absorber (50, IPL Figure 4) from the preamp housing (55, IPL Figure 4).
Magnetron Removal (Subtask 34-40-11-000-010-A01) NOTE:
H.
I.
(1)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(2)
Remove the cover (35) as described in Paragraph 2.B. (Subtask 34-40-11-000-005-A01).
(3)
Remove the logic board (135) as described in Paragraph 2.C. (Subtask 34-40-11-000-006-A01).
(4)
Remove the power supply/modulator board (140) as described in Paragraph 2.D. (Subtask 34-40-11-000-007-A01).
(5)
Remove the receiver assembly (140, IPL Figure 9) as described in Paragraph 2.E. (Subtask 34-40-11-000-008-A01).
(6)
Use a allen wrench, 9/64-inch, beryllium copper (commercially available) and remove the four cap screws (145, IPL Figure 9) and the magnetron assembly (155, IPL Figure 9) from the RF network (165, IPL Figure 9).
(7)
Remove the three screws (275) and the clamp (270) that enclose the cable ferrules from the base (290).
(8)
Separate the cable ferrules from the base (290) and remove the magnetron assembly (155, IPL Figure 9).
Azimuth Motor Assembly Removal (Subtask 34-40-11-000-011-A01) (1)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(2)
Remove the cover (35) as described in Paragraph 2.B. (Subtask 34-40-11-000-005-A01).
(3)
Remove the logic board (135) as described in Paragraph 2.C. (Subtask 34-40-11-000-006-A01).
(4)
Remove the power supply/modulator board (140) as described in Paragraph 2.D. (Subtask 34-40-11-000-007-A01).
(5)
Remove the two lock nuts (160), the two azimuth pivot pins (145), and the four washers (150 and 155) that secure the gimbal assembly (230) to the bottom pivot bracket (210).
(6)
Remove the four screws (165) and the seven washers (170 and 175) that secure the bottom pivot bracket (210) to the base (290). Separate the bottom pivot bracket (210) and azimuth motor assembly (200) from the base (290).
(7)
Remove the screw (180), the stop plate (185), and the ground spring (190) that secure the cable to the base (290).
(8)
Remove the four screws (205) that secure the azimuth motor assembly (200) to the bottom pivot bracket (210), and remove the azimuth motor assembly (200).
Pitch Motor Assembly Removal (Subtask 34-40-11-000-012-A01) (1)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(2)
Remove the cover (35) as described in Paragraph 2.B. (Subtask 34-40-11-000-005-A01).
(3)
Remove the logic board (135) as described in Paragraph 2.C. (Subtask 34-40-11-000-006-A01).
(4)
Remove the power supply/modulator board (140) as described in Paragraph 2.D. (Subtask 34-40-11-000-007-A01).
EFFECTIVITY ALL
Never use tools that contain ferrous metal when you work with the magnetron.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 3004 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
J.
(5)
Remove the four screws (40, IPL Figure 9) that secure the mounting plate (75, IPL Figure 9) to the tilt sensor assembly (170, IPL Figure 9).
(6)
Remove the four screws (55, IPL Figure 9) and the pitch motor assembly (50, IPL Figure 9) from the mounting plate (75, IPL Figure 9).
(7)
Remove the screw (180), the stop plate (185), and the ground spring (190) that secure the cable to the base (290).
Job Close-up (Subtask 34-40-11-000-013-A01) (1)
EFFECTIVITY ALL
Remove all tools, equipment, and unwanted materials from the work area.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 3005 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 3006 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
CLEANING 1.
Planning Data (TASK 34-40-11-99C-804-A01) A.
Reason for the Job (Subtask 34-40-11-99C-008-A01) (1)
B.
Use these procedures to remove dust, dirt, and unwanted oil and grease. Be careful not to cause damage to the parts when you do these procedures.
Job Setup Data (Subtask 34-40-11-99C-009-A01) (1)
You can use equivalent alternatives for the special tools, fixtures, equipment, and consumable materials. The user must find equivalent alternatives.
(2)
Refer to Table 4001 for the specified special tools, fixtures, and equipment in this section.
(3)
Refer to H4/H8 CAGE Codes (available at http://www.dlis.dla.mil/cage_welcome.asp) for manufacturer’s address. Table 4001. Special Tools, Fixtures, and Equipment
Number
Description
Source
non-synthetic brush (commercially available) soft-bristle brush (commercially available) stiff-bristle brush (commercially available) WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
WARNING:
GOGGLES MUST BE WORN WHEN USING PRESSURIZED AIR TO BLOW DUST AND DIRT FROM EQUIPMENT. ALL PERSONNEL MUST BE CLEARED FROM THE IMMEDIATE AREA.
WARNING:
USE A VENTILATED HOOD WHEN USING A CLEANING SOLVENT. AVOID BREATHING SOLVENT VAPOR AND FUMES. AVOID CONTINUOUS CONTACT WITH CLEANING SOLVENT. WEAR A SUITABLE MASK, GOGGLES, GLOVES, AND AN APRON WHEN NECESSARY. CHANGE CLOTHING UPON WHICH SOLVENTS HAVE BEEN SPILLED.
WARNING:
OBSERVE ALL FIRE PRECAUTIONS FOR FLAMMABLE MATERIALS. USE FLAMMABLE MATERIALS IN A HOOD PROVIDED WITH EXPLOSION-PROOF ELECTRICAL EQUIPMENT AND AN EXHAUST FAN WITH SPARKPROOF BLADES.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
(4)
EFFECTIVITY ALL
Refer to Table 4002 for the specified consumable materials in this section.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 4001 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 Table 4002. Consumables Number
Description
4/0
crocus cloth (commercially available)
Source
isopropanol, technical, per MIL TT-I-735, Grade B (commercially available) Vertrel SMT (5)
cleaning solvent (CAGE S3299) The list that follows identifies Honeywell publications that are related to this section: • ATA No. 20-00-03 (Pub. No. A09-1100-004), Standard Repair Procedures for Honeywell Avionics Equipment Instruction Manual, SOPM20-00-03.
2.
Procedure (TASK 34-40-11-100-801-A01) A.
Job Setup (Subtask 34-40-11-100-001-A01) WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
CAUTION:
USE INDUSTRY APPROVED ELECTROSTATIC DISCHARGE SENSITIVE PRECAUTIONS. THE ART 2000 CONTAINS ELECTROSTATIC DISCHARGE SENSITIVE ITEMS.
CAUTION:
DO NOT DROP OR HIT THE ART 2000 DURING THESE PROCEDURES. THE ART 2000 CONTAINS AN ASSEMBLY THAT CAN BE DAMAGED FROM INCORRECT USE.
CAUTION:
DO THESE PROCEDURES IN A CLEAN ENVIRONMENT TO PREVENT DAMAGE TO MECHANICAL COMPONENTS.
CAUTION:
BEFORE YOU USE ISOPROPANOL, DO A TEST TO MAKE SURE THAT IT DOES NOT CAUSE DAMAGE TO THE PAINTED SURFACES.
CAUTION:
DO NOT LET THE ISOPROPANOL TOUCH THE CONNECTOR BODY. IT CAN CAUSE DAMAGE TO THE PARTS. USE ISOPROPANOL CAREFULLY WHEN YOU CLEAN FLUX FROM THE SOLDER CONNECTIONS.
(1)
Obey the precautions.
(2)
Do the procedures in a clean location.
(3)
When you use pressurized air to clean assemblies and parts, do not use more air pressure than is necessary.
(4)
After you clean the assemblies and parts, supply protection from moisture, dust, and other contamination until you do a visual check and assemble the component.
(5)
Refer to the Standard Repair Procedures for Honeywell Avionics Equipment Instruction Manual, Honeywell Pub. No. A09-1100-004, for more cleaning procedures. Use the standard repair procedures and approved local shop procedures.
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 4002 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 B.
C.
External Parts (Subtask 34-40-11-100-002-A01) (1)
Remove dirt and dust with pressurized air or a soft-bristle brush (commercially available).
(2)
Remove oil and grease that has collected on the ART 2000. Use a clean cloth or cotton swab that is moist with isopropanol, technical, per MIL TT-I-735, Grade B (commercially available) or Vertrel SMT cleaning solvent (CAGE S3299).
(3)
Remove unwanted material on painted surfaces that show index marks, numerals, or letters. Use a clean cloth that is moist with a weak detergent.
(4)
To clean an area in a recess, use a stiff-bristle brush (commercially available) that is moist with a weak detergent.
Electrical Parts (Subtask 34-40-11-100-003-A01) CAUTION:
D.
(1)
Remove dirt and dust around the connector pins with ionized, pressurized air.
(2)
Remove dirt and dust on the electrical parts with a soft-bristle brush (commercially available) or cotton swab that is moist with isopropanol, technical, per MIL TT-I-735, Grade B (commercially available).
Metal Mechanical Parts (Subtask 34-40-11-100-004-A01) CAUTION:
WHEN YOU REMOVE CORROSION, MOVE THE CROCUS CLOTH PARALLEL TO THE AXIS OF THE PART. IF YOU MOVE THE CROCUS CLOTH ACROSS THE AXIS, YOU CAN CAUSE DAMAGE TO THE FINISH.
(1)
Remove corrosion from the metal parts with a 4/0 crocus cloth (commercially available).
(2)
Use isopropanol, technical, per MIL TT-I-735, Grade B (commercially available) or Vertrel SMT cleaning solvent (CAGE S3299) to clean the metal parts.
(3)
Dry the part with pressurized air.
EFFECTIVITY ALL
IF YOU CLEAN ELECTROSTATIC DISCHARGE SENSITIVE PARTS WITH PRESSURIZED AIR, USE IONIZED AIR. AN ELECTROSTATIC CHARGE CAN CAUSE DAMAGE TO THE PARTS IF YOU DO NOT USE IONIZED AIR.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 4003 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 E.
Internal Parts (Subtask 34-40-11-100-005-A01) CAUTION:
DO NOT USE SOLVENT TO CLEAN PARTS COMPOSED OF OR CONTAINING NYLON OR RUBBER GROMMETS. CLEAN THESE ITEMS WITH MILD LIQUID DISHWASHING DETERGENT AND WATER. USE DETERGENT FOR THIS PURPOSE ONLY.
CAUTION:
VERTREL SMT SOLVENT, CLEANING (CAGE S3299) DOES HAVE GENERAL MATERIAL COMPATIBILITY PROBLEMS WITH POLYCARBONATE, POLYSTYRENE, AND RUBBER. IT IS RECOMMENDED THAT THESE MATERIALS BE CLEANED WITH ISOPROPANOL, TECHNICAL, PER MIL TT-I-735, GRADE B (COMMERCIALLY AVAILABLE).
CAUTION:
DO NOT ALLOW EXCESS CLEANING SOLVENT TO ACCUMULATE IN ANY OF THE ADJUSTMENT SCREW CREVICES AND THEREBY SOFTEN OR DISSOLVE THE ADJUSTMENT SCREW EPOXY SEALANT.
CAUTION:
AVOID AIR-BLASTING SMALL TUNING COILS AND OTHER DELICATE PARTS BY HOLDING THE AIR JET NOZZLE TOO CLOSE. USE BRUSHES CAREFULLY ON DELICATE PARTS.
CAUTION:
IMPROPER CLEANING CAN RESULT IN SURFACE LEAKAGE AND CONDUCTIVE PARTICULATES, SUCH AS SOLDER BALLS OR METALLIC CHIPS, WHICH CAN CAUSE ELECTRICAL SHORTS. SEVERE IONIC CONTAMINATION FROM HANDLING AND FROM ENVIRONMENTAL CONDITIONS CAN RESULT IN HIGH RESISTANCE OR OPEN CIRCUITS.
CAUTION:
ULTRASONIC CLEANING CAN DAMAGE CERTAIN PARTS AND MUST GENERALLY BE AVOIDED.
(1)
(2)
(3)
Remove each module subassembly. Then remove any foreign matter from the casting. NOTE:
Solvents may be physically applied in several ways including agitation, spraying, brushing, and vapor degreasing. The cleaning solvents and methods used can have no deleterious effect on the parts, connections, and materials being used. If sensitive components are being used, spray is recommended. Uniformity of solvent spray flow should be maximized and wait-time between soldering and cleaning should be minimized.
NOTE:
Clean miscellaneous metal parts i.e. fasteners, handles, mounting hardware, etc. with a suitable cleaning machine.
Casting covers and shields should be cleaned as follows. (a)
Remove surface grease with a lint-free cloth.
(b)
Blow dust from surfaces, holes, and recesses with ionized, pressurized air.
(c)
If necessary, use a solvent and scrub until clean, working over all surfaces and into all holes and recesses with a suitable non-metallic stiff-bristle brush (commercially available)
(d)
Position the part to dry so that solvent is not trapped in holes or recesses. Use ionized, pressurized air to blow out any trapped solvent.
(e)
When thoroughly clean, touch up any minor damage to the finish.
Modules (circuit card assemblies) containing resistors, capacitors, RF coils, inductors, transformers, and other wired parts should be cleaned as follows. (a)
EFFECTIVITY ALL
Remove dust and dirt from all surfaces, including all parts and wiring, using a soft-bristle brush (commercially available) in conjunction with ionized, pressurized air.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 4004 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
(4)
(b)
Any dirt that cannot be removed in this way should be removed with a non-synthetic brush (commercially available) saturated with isopropanol, technical, per MIL TT-I-735, Grade B (commercially available) or Vertrel SMT cleaning solvent (CAGE S3299). Use ionized, pressurized air to remove any excess solvent.
(c)
Remove flux residue, metallic chips, and/or solder balls with isopropanol, technical, per MIL TT-I-735, Grade B (commercially available) or Vertrel SMT cleaning solvent (CAGE S3299).
Wired chassis devices containing terminal boards, resistor and capacitor assemblies, RF coils, switches, sockets, inductors, transformers, and other wired parts should be cleaned as follows. NOTE:
(5)
F.
(a)
Blow dust from surfaces, holes, and recesses using ionized, pressurized air.
(b)
Finish cleaning chassis by wiping finished surfaces with a lint-free cloth moistened with isopropanol, technical, per MIL TT-I-735, Grade B (commercially available) or Vertrel SMT cleaning solvent (CAGE S3299).
(c)
Dry with a clean, dry, lint-free cloth.
(d)
When thoroughly clean, touch-up any minor damage to the finish.
(e)
Protect the chassis from dust, moisture, and damage pending inspection.
Ceramic and plastic parts should be cleaned as follows. (a)
Blow dust from surfaces, holes, and recesses using ionized, pressurized air.
(b)
Finish cleaning chassis by wiping finished surfaces with a lint-free cloth moistened with isopropanol, technical, per MIL TT-I-735, Grade B (commercially available) or Vertrel SMT cleaning solvent (CAGE S3299).
(c)
Dry with a clean, dry, lint-free cloth.
Job Close-up (Subtask 34-40-11-100-006-A01) (1)
EFFECTIVITY ALL
When necessary to disturb the dress of wires and cables, note the positions before disturbing and restore them to proper dress after cleaning.
Remove all tools, equipment, and unwanted materials from the work area.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 4005 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 4006 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
INSPECTION/CHECK 1.
Planning Data (TASK 34-40-11-99C-805-A01) A.
Reason for the Job (Subtask 34-40-11-99C-010-A01) (1)
B.
Use these procedures to find damage or worn parts and parts that show signs of near failure.
Job Setup Data (Subtask 34-40-11-99C-011-A01) (1)
You can use equivalent alternatives for the special tools, fixtures, equipment, and consumable materials. The user must find equivalent alternatives.
(2)
Refer to Table 5001 for the specified special tools, fixtures, and equipment in this section.
(3)
Refer to H4/H8 CAGE Codes (available at http://www.dlis.dla.mil/cage_welcome.asp) for manufacturer’s address. Table 5001. Special Tools, Fixtures, and Equipment
Number
Description
Source
Not applicable
Not applicable
Not applicable
WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
(4)
Refer to Table 5002 for the specified consumable materials in this section. Table 5002. Consumables
Number
Description
Source
Not applicable
Not applicable
Not applicable
(5)
The list that follows identifies Honeywell publications that are related to this section: (a)
EFFECTIVITY ALL
Not applicable.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 5001 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
2.
Procedure (TASK 34-40-11-210-801-A01) A.
B.
Job Setup (Subtask 34-40-11-210-001-A01) WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
CAUTION:
USE INDUSTRY APPROVED ELECTROSTATIC DISCHARGE SENSITIVE PRECAUTIONS. THE ART 2000 CONTAINS ELECTROSTATIC DISCHARGE SENSITIVE ITEMS.
CAUTION:
DO NOT DROP OR HIT THE ART 2000 DURING THESE PROCEDURES. THE ART 2000 CONTAINS AN ASSEMBLY THAT CAN BE DAMAGED FROM INCORRECT USE.
CAUTION:
DO THESE PROCEDURES IN A CLEAN ENVIRONMENT TO PREVENT DAMAGE TO MECHANICAL COMPONENTS.
CAUTION:
BEFORE YOU USE ISOPROPANOL, DO A TEST TO MAKE SURE THAT IT DOES NOT CAUSE DAMAGE TO THE PAINTED SURFACES.
CAUTION:
DO NOT LET THE ISOPROPANOL TOUCH THE CONNECTOR BODY. IT CAN CAUSE DAMAGE TO THE PARTS. USE ISOPROPANOL CAREFULLY WHEN YOU CLEAN FLUX FROM THE SOLDER CONNECTIONS.
(1)
Obey the precautions.
(2)
Replace all damaged or worn parts. This prevents possible failures of the equipment.
General Inspection/Check Procedure of the ART 2000 (Subtask 34-40-11-210-002-A01) (1)
Cover (a)
(2)
Front Panel (a)
(3)
ALL
Inspect for bent, warped, stripped, dented or corroded parts. Check for damaged fasteners. Check plating, painting, and identification stencils for worn, exposed, or scratched surfaces.
Circuit Boards (a)
EFFECTIVITY
Inspect chassis for loose or missing mounting hardware, deformation, dents, damaged fasteners, or damaged connectors. Check for corrosion or damage to the finish that should be repaired.
Hardware, Covers, and Shields (a)
(5)
Check that name, serial number, and plates or stickers are secure and hardware is tight.
Chassis (a)
(4)
Inspect the cover for dents, deformation, or damage to the finish that should be repaired.
Inspect for loose, broken or corroded terminal connections and damage; such as cracks, burns, or charred track. Check for insufficient solder, proper bonding, fungus, mold or other deposits that should be repaired.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 5002 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 (6)
Connectors (a)
(7)
Terminal Connections (a)
(8)
(9)
Inspect connector bodies for broken parts, check insulation for cracks, and check contacts for damage, misalignment, corrosion, or bad plating. Check for broken, loose, or poorly soldered connections to connector terminals. Inspect connector hoods and cable clamps for crimped wires.
Inspect for corrosion or loose connections.
Terminal Connections, Soldered (a)
Inspect for cold soldered or rosin joints. Bad joints can be recognized by a dull porous appearance.
(b)
Check for excessive solder, insufficient solder, or solder splashes resulting from previous repair.
(c)
Check for corrosion at the terminal connections.
Wiring (a)
Inspect wiring of the chassis and subassemblies for any signs of physical damage or charring.
(10) Capacitors (a)
Inspect capacitors for case or body damage and for loose, broken, or corroded terminal connections.
(11) Resistors and Diodes (a)
Inspect for blistered, charred, or cracked bodies. Check for loose, broken, or corroded terminal connections.
(12) Filters and Inductors (a)
Inspect for damage to body or casting and for loose, broken, or corroded terminal connections. Check for secure mounting to chassis.
(13) Transformers (a)
Inspect for damage to case and for signs of excessive heating. Check for loose, broken, or corroded terminal connections.
(14) Transistors and Integrated Circuits (a)
Inspect for damage to body or casing. Check for proper and secure attachment to sockets.
(15) Rotary Switches (a)
Check for proper mechanical operation: no binding or looseness should be evidenced.
(16) Insulators (a) C.
Job Close-up (Subtask 34-40-11-210-003-A01) (1)
EFFECTIVITY ALL
Inspect for looseness and/or evidence of damage such as burned areas, cracks, and broken or chipped edges.
Remove all tools, equipment, and unwanted materials from the work area.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 5003 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 5004 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
REPAIR 1.
Planning Data (TASK 34-40-11-99C-806-A01) A.
B.
Reason for the Job (Subtask 34-40-11-99C-012-A01) (1)
Use these procedures for the ART 2000 to replace defective parts and replace or repair defective subassemblies.
(2)
Do only those procedures of DISASSEMBLY (PGBLK 34-40-11-3000) that are necessary to make repairs. When new parts are necessary, refer to the ILLUSTRATED PARTS LIST (IPL 34-40-11-10000) for the correct PNs and quantities.
Job Setup Data (Subtask 34-40-11-99C-013-A01) (1)
You can use equivalent alternatives for the special tools, fixtures, equipment, and consumable materials. The user must find equivalent alternatives.
(2)
Refer to Table 6001 for the specified special tools, fixtures, and equipment in this section.
(3)
Refer to H4/H8 CAGE Codes (available at http://www.dlis.dla.mil/cage_welcome.asp) for manufacturer’s address. Table 6001. Special Tools, Fixtures, and Equipment
Number
Description
Source
Not applicable
Not applicable
Not applicable
WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
(4)
Refer to Table 6002 for the specified consumable materials in this section. Table 6002. Consumables
Number
Description
HYSOL 1B-31
conformal coating (CAGE 99109)
(5)
Source
The list that follows identifies Honeywell publications that are related to this section: • ATA No. 20-00-03 (Pub. No. A09-1100-004), Standard Repair Procedures for Honeywell Avionics Equipment Instruction Manual, SOPM20-00-03.
(6)
Perform repairs and replace components with power disconnected from equipment.
(7)
Use a conductive table top for repairs. Connect table to ground conductors of 60Hz and 400Hz power lines.
(8)
Replace connectors, shield conductors, and twisted pairs ONLY with identical items.
(9)
Standard references to printed circuit boards in this manual include the following terms. "Component side" and "nearside" refer to the side components are located on. "Solder side" and "farside" refer to the side opposite component side. "Nearside" on surface mount boards with components on both sides is the side with J#### and P#### connector numbers.
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 6001 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 (10) When you replace parts, carefully observe lead dress and component orientation. Keep leads as short as possible and observe correct repair techniques. (11) Surface mount components require special soldering techniques. The soldering iron tip should not touch the ceramic component body. The iron should be applied only to the termination-solder filet. (12) Observe cable routing within unit prior to disassembly, to enable proper routing of cables during reassembly.
2.
Procedure (TASK 34-40-11-300-801-A01) A.
Job Setup (Subtask 34-40-11-300-001-A01) WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
CAUTION:
USE INDUSTRY APPROVED ELECTROSTATIC DISCHARGE SENSITIVE PRECAUTIONS. THE ART 2000 CONTAINS ELECTROSTATIC DISCHARGE SENSITIVE ITEMS.
CAUTION:
DO NOT DROP OR HIT THE ART 2000 DURING THESE PROCEDURES. THE ART 2000 CONTAINS AN ASSEMBLY THAT CAN BE DAMAGED FROM INCORRECT USE.
CAUTION:
DO THESE PROCEDURES IN A CLEAN ENVIRONMENT TO PREVENT DAMAGE TO MECHANICAL COMPONENTS.
(1) B.
Obey the precautions.
References for Repair (Subtask 34-40-11-300-002-A01) (1)
These references show where to find repair data that is located in other sections of this manual and in other manuals. The data in other sections of this manual is necessary for repair of the ART 2000 and its primary subassemblies. The data in other manuals gives procedures that are not included in this manual.
(2)
Refer to SCHEMATIC AND WIRING DIAGRAMS (PGBLK 34-40-11-2000) for reference drawings for the ART 2000 and its primary subassemblies. The drawings give data about: • Buswires • Consumable materials • Component layout • Component termination • Cut runs • Schematic diagrams.
(3)
Refer to SCHEMATIC AND WIRING DIAGRAMS (PGBLK 34-40-11-2000) for wire list tables and for harness, cable, and lead assemblies. The tables give data about wire: • Terminations • Type
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 6002 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 • Size (AWG) • Color. (4)
Refer to FITS AND CLEARANCES (PGBLK 34-40-11-8000) for: • Component clearance • Maximum component height • Maximum lead length • Torque limits.
(5)
Refer to ILLUSTRATED PARTS LIST (IPL 34-40-11-10000) for: • Figure and item numbers • Subassembly and component locations • Correct PNs • Correct quantities.
(6)
C.
Refer to the Standard Repair Procedures for Honeywell Avionics Equipment Instruction Manual, Honeywell Pub. No. A09-1100-004, for shop repairs that use the same procedures on many types of assemblies. Use the standard repair procedures and approved local shop procedures.
General Repair Instructions (Subtask 34-40-11-300-003-A01) (1)
(2)
Replacement of Printed Circuit Board Protective Coating (a)
Clean the repaired area of the printed circuit board as listed in the CLEANING (PGBLK 34-40-11-4000) section.
(b)
Apply HYSOL 1B-31 conformal coating (CAGE 99109) as follows. Shake container well before using.
2
Spray or brush surfaces with smooth, even strokes: if spraying, hold nozzle 10 to 15 inches (25.4 to 38.1 cm) from work surface.
3
Cure time is ten minutes at room temperature.
Programmable Read Only Memory (PROM) Replacement (a)
(3)
1
The read only memory packages are specially programmed devices to provide specific logic outputs required for the operation in the control unit. The manufacturer’s part (type) number is for the unprogrammed device and cannot be used. The Honeywell part number must be used to obtain the correctly programmed device. Refer to the ILLUSTRATED PARTS LIST (IPL 34-40-11-10000) section.
Coaxial Cable Connectors NOTE: (a)
D.
Replacement coaxial cable assemblies are available.
The following are connectors used on the KRA 405B unit. The cables, PN 155-02881-0001/0002, are not field serviceable and are included for reference only. Cable, PN 155-02831-0000 is field serviceable.
Special Repair Instructions (Subtask 34-40-11-300-004-A01) (1)
When the magnetron is replaced in an ART 2000, the unit must be altitude tested to 55,000 feet (16.76 km). Also, the AFC and STC curves must be recalibrated at the temperatures as follows: • -67 F (-55 C) • -22 F (-30 C)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 6003 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 • +23 F (-5 C) • +68 F (+20 C) • +113 F (+45 C) • +158 F (+70 C).
E.
(2)
If any work is done that affects the frequency, power, or spectrum of the ART 2000, the AFC and STC curves must be recalibrated over the same temperature range. This must be done even if the magnetron is not replaced.
(3)
Calibrated altitude and environmental chambers are needed for the servicing mentioned above. If your service center does not have the required equipment, we recommend that you return the unit to a Honeywell Customer Service for repair.
Job Close-up (Subtask 34-40-11-300-005-A01) (1)
EFFECTIVITY ALL
Remove all tools, equipment, and unwanted materials from the work area.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 6004 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
ASSEMBLY 1.
Planning Data (TASK 34-40-11-99C-807-A01) A.
Reason for the Job (Subtask 34-40-11-99C-014-A01) (1)
B.
Use these procedures to assemble the ART 2000. Do only those procedures that are applicable to the disassembly done.
Job Setup Data (Subtask 34-40-11-99C-015-A01) (1)
You can use equivalent alternatives for the special tools, fixtures, equipment, and consumable materials. The user must find equivalent alternatives.
(2)
Refer to Table 7001 for the specified special tools, fixtures, and equipment in this section.
(3)
Refer to H4/H8 CAGE Codes (available at http://www.dlis.dla.mil/cage_welcome.asp) for manufacturer’s address. Table 7001. Special Tools, Fixtures, and Equipment
Number
Description
2598-5342-54
engagement/disengagement tool (CAGE 96341)
Source
allen wrench, 9/64-inch, beryllium copper (commercially available) torque wrench, capable of 0.94 to 25.0 in-lb (0.11 to 2.82 N•m) (commercially available) WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
(4)
Refer to Table 7002 for the specified consumable materials in this section. Table 7002. Consumables
Number
Description
150-00096-0000
shrink tubing, black, 0.125 inch (3.17 mm) (CAGE 22373)
150-00096-0001
shrink tubing, black, 0.1875 inch (4.76 mm) (CAGE 22373)
150-00096-0002
shrink tubing, black, 0.25 inch (6.35 mm) (CAGE 22373)
271
locking compound (CAGE 1UCL7)
3145
adhesive sealant (CAGE 71984)
425
locking compound (CAGE 1UCL7)
EFFECTIVITY ALL
Source
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 7001 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Table 7002. Consumables (Cont) Number
Description
Source
isopropanol, technical, per MIL TT-I-735, Grade B (commercially available) lacing tape, 1/16 inch, 20-pound strength (commercially available) wire, AWG 22, black, MIL-W-16878/4 (commercially available) wire, AWG 22, solid copper, tinned (commercially available) Aeroshell 22
(5)
grease, multipurpose (CAGE 4LR76) The list that follows identifies Honeywell publications that are related to this section: (a)
2.
Procedure (TASK 34-40-11-400-801-A01) A.
Job Setup (Subtask 34-40-11-400-001-A01) WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
CAUTION:
USE INDUSTRY APPROVED ELECTROSTATIC DISCHARGE SENSITIVE PRECAUTIONS. THE ART 2000 CONTAINS ELECTROSTATIC DISCHARGE SENSITIVE ITEMS.
CAUTION:
DO NOT DROP OR HIT THE ART 2000 DURING THESE PROCEDURES. THE ART 2000 CONTAINS AN ASSEMBLY THAT CAN BE DAMAGED FROM INCORRECT USE.
CAUTION:
DO THESE PROCEDURES IN A CLEAN ENVIRONMENT TO PREVENT DAMAGE TO MECHANICAL COMPONENTS.
CAUTION:
BEFORE YOU USE ISOPROPANOL, DO A TEST TO MAKE SURE THAT IT DOES NOT CAUSE DAMAGE TO THE PAINTED SURFACES.
CAUTION:
DO NOT LET THE ISOPROPANOL TOUCH THE CONNECTOR BODY. IT CAN CAUSE DAMAGE TO THE PARTS. USE ISOPROPANOL CAREFULLY WHEN YOU CLEAN FLUX FROM THE SOLDER CONNECTIONS.
(1)
EFFECTIVITY ALL
Not applicable.
Obey the precautions.
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Page 7002 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
B.
(2)
The item numbers shown in the DPL are the same as the item numbers on the exploded view illustration(s). To find a PN, find the part on the illustration and note the item number. Find the item number in the parts list and read the correct PN. Item numbers refer to the same figure until a different figure is specified.
(3)
Refer to the data written during disassembly for the location of the tie points and where to connect the components and wires.
Pitch Motor Assembly Installation (Subtask 34-40-11-400-002-A01) (1)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(2)
Apply 425 locking compound (CAGE 1UCL7) to the threads of the four screws (55, IPL Figure 9).
(3)
Install the four screws (55, IPL Figure 9) that fasten the pitch motor assembly (50, IPL Figure 9) to the mounting plate (75, IPL Figure 9). Make sure that you attach the ground lug to one of the screws (55, IPL Figure 9).
(4)
Torque the four screws (55, IPL Figure 9) to 6 to 7 in-lb (0.68 to 0.79 N•m).
(5)
Apply 425 locking compound (CAGE 1UCL7) to the threads of the four screws (40, IPL Figure 9).
(6)
Install the four screws (40, IPL Figure 9) and secure the mounting plate (75, IPL Figure 9) to the tilt sensor assembly (170, IPL Figure 9).
(7)
Torque the four screws (40, IPL Figure 9) to 6 to 7 in-lb (0.68 to 0.79 N•m).
(8)
Reroute the cable as originally found and secure with two cable ties (285).
(9)
Apply 425 locking compound (CAGE 1UCL7) to the threads of the screw (180).
(10) Secure the cable to the base (290) with the screw (180), the stop plate (185), and the ground spring (190). (11) Torque the screw (180) to 6 to 7 in-lb (0.68 to 0.79 N•m). (12) Install the power supply/modulator board (140) as described in Paragraph 2.G. (Subtask 34-40-11-400-007-A01) (13) Install the logic board (135) as described in Paragraph 2.H. (Subtask 34-40-11-400-008-A01) (14) Install the cover (35) as described in Paragraph 2.I. (Subtask 34-40-11-400-009-A01) C.
Azimuth Motor Assembly Installation (Subtask 34-40-11-400-003-A01) (1)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(2)
Apply a coat of Aeroshell 22 grease, multipurpose (CAGE 4LR76) to all the gear teeth.
(3)
Put the bottom pivot bracket (210) into position on the base (290).
(4)
Apply a coat of Aeroshell 22 grease, multipurpose (CAGE 4LR76) to both sides of the washers (150 and 155).
(5)
Apply 271 locking compound (CAGE 1UCL7) to the threads of the two azimuth pivot pins (145).
(6)
Install the two azimuth pivot pins (145), the four washers (150 and 155), and the two azimuth nuts (160) on the gimbal assembly (230).
(7)
Torque the two azimuth nuts (160) to 17 to 19 in-lb (1.92 to 2.15 N•m).
(8)
Apply 425 locking compound (CAGE 1UCL7) to the threads of the four screws (205).
(9)
Install the four screws (205) that secure the azimuth motor assembly (200) to the bottom pivot bracket (210). Make sure that you attach the ground lug to one of the screws (205).
EFFECTIVITY ALL
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Page 7003 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 (10) Torque the four screws (205) to 6 to 7 in-lb (0.68 to 0.79 N•m). (11) Apply 425 locking compound (CAGE 1UCL7) to the threads of the four screws (165). (12) Install the bottom pivot bracket (210), the four screws (165), and the seven washers (170 and 175). (13) Torque the four screws (165) to 17 to 19 in-lb (1.92 to 2.15 N•m). (14) Reroute the cable as originally found and secure with two cable ties (285). (15) Apply 425 locking compound (CAGE 1UCL7) to the threads of the screw (180). (16) Secure the cable to the base (290) with the screw (180), the stop plate (185), and the ground spring (190). (17) Torque the screw (180) to 6 to 7 in-lb (0.68 to 0.79 N•m). (18) Install the power supply/modulator board (140) as described in Paragraph 2.G. (Subtask 34-40-11-400-007-A01). (19) Install the logic board (135) as described in Paragraph 2.H. (Subtask 34-40-11-400-008-A01). (20) Install the cover (35) as described in Paragraph 2.I. (Subtask 34-40-11-400-009-A01). D.
Magnetron Installation (Subtask 34-40-11-400-004-A01) NOTE:
Never use tools that contain ferrous metal when you work with the magnetron.
(1)
Refer to Paragraph 2.D. (Subtask 34-40-11-300-004-A01) in the REPAIR (PGBLK 34-40-11-6000) section for additional information when you replace the magnetron.
(2)
A magnetron replacement kit (PN 050-03298-0000) is available that includes a new magnetron, required miscellaneous wiring hardware, and specific wiring instructions.
(3)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(4)
Apply 425 locking compound (CAGE 1UCL7) to the threads of the four cap screws (145, IPL Figure 9).
(5)
Use a allen wrench, 9/64-inch, beryllium copper (commercially available) and attach the magnetron (155, IPL Figure 9) to the RF network (165, IPL Figure 9) with the four cap screws (145, IPL Figure 9). Make sure that you route the ground lug under the liner (180, IPL Figure 9) and attach it with the cap screw (145, IPL Figure 9) as shown IPL Figure 9.
(6)
Torque the four cap screws (145, IPL Figure 9) to 17 to 19 in-lb (1.92 to 2.15 N•m).
(7)
Refer to Figure 7001 and make the high-voltage connection to the magnetron as follows. (a)
Remove the outer covering on the coax to expose 1.25 inches (31.75 mm) of braid on each cable.
(b)
Trim back the braid on each cable to leave 0.20 inch (5.08 mm) of braid exposed. Be careful not to nick the inner insulation.
(c)
Trim back the insulation on each cable to leave 0.70 inch (17.78 mm) of insulation exposed. Be careful not to nick the inner conductor.
(d)
Tin the inner conductor wire of both cables with solder. Be sure that the outline of the wire strands is visible.
(e)
On each cable, slide a 2.50-inch (63.50-mm) long piece of 150-00096-0002 shrink tubing, black, 0.25 inch (6.35 mm) (CAGE 22373) on to the cable. NOTE:
EFFECTIVITY ALL
The shrink tubing has a layer of adhesive sealant inside. Make sure debris does not enter and contaminate the inside of the tubing.
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Page 7004 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 (f)
On each cable, slide a 1.25 inch (31.75 mm) long piece of 150-00096-0001 shrink tubing, black, 0.1875 inch (4.76 mm) (CAGE 22373) on to the cable. NOTE:
(g)
On each cable, slide a 1.50-inches (38.10-mm) long piece of 150-00096-0000 shrink tubing, black, 0.125 inch (3.17 mm) (CAGE 22373) on to the cable. NOTE:
(h)
The shrink tubing has a layer of adhesive sealant inside. Make sure debris does not enter and contaminate the inside of the tubing.
The shrink tubing has a layer of adhesive sealant inside. Make sure debris does not enter and contaminate the inside of the tubing.
Make hooks on the ends of the inner conductors of each cable so that the wire extends 0.125 inch (3.17 mm) from the insulation.
CAUTION:
IF THE TAILS OF THE HOOKED PORTIONS OF THE WIRES ARE ALLOWED TO PROTRUDE OUTWARD, ARCING CAN OCCUR.
(i)
Hook each wire to the corresponding high-voltage wire. Cut off any access lead from one wire and wrap the hook around the other wire. Make sure you, tuck the tail inward. The wire must wrap at least halfway around the other wire. Cut off any excess lead from the other wire and wrap the hook around the first wire. Make sure you tuck the tail inward. The wire must wrap at least halfway around the other wire. The space between the inner insulation can not exceed 0.25 inch (6.35 mm).
(j)
Apply solder to the connections so that a ball forms around the connection. Remove the soldering iron and the solder at the same time so that the solder ball will remain smooth.
(k)
Check for any solder peaks, spurs, or burrs. Check that the tails of the hooks do not protrude from the solder ball. The solder ball should be smooth with no projections.
(l)
Clean the connection areas and cable ends thoroughly with isopropanol, technical, per MIL TT-I-735, Grade B (commercially available). NOTE:
If the area is not cleaned thoroughly, corona will be allowed to escape.
(m) Center the 150-00096-0000 shrink tubing, black, 0.125 inch (3.17 mm) (CAGE 22373) over each splice and shrink it in place. Work from the center outwards so you do not trap air inside the tubing. NOTE:
(n)
Clean the connection areas and cable ends thoroughly with isopropanol, technical, per MIL TT-I-735, Grade B (commercially available). NOTE:
ALL
If the area is not cleaned thoroughly, corona will be allowed to escape.
(o)
Center the 150-00096-0001 shrink tubing, black, 0.1875 inch (4.76 mm) (CAGE 22373) over each splice and shrink it in place. Work from the center outwards so you do not trap air inside the tubing.
(p)
Wrap and solder the leads from a 2.25-inch (57.15-mm) long piece of wire, AWG 22, black, MIL-W-16878/4 (commercially available) around the coax braid on each side of the splice. Put a heat sink on the braid next to the outer covering on both sides to prevent the solder from wicking under the outer covering.
(q)
Clean the connection area and cables ends thoroughly with isopropanol, technical, per MIL TT-I-735, Grade B (commercially available). NOTE:
EFFECTIVITY
The shrink tubing must be heated to 275 F (135 C) for proper flow of the sealant. Sealant should seep from the edges of the shrink tubing when sufficiently heated.
If the area is not cleaned thoroughly, corona will be allowed to escape.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 7005 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 (r)
Center the 150-00096-0002 shrink tubing, black, 0.25 inch (6.35 mm) (CAGE 22373) over each splice and shrink it in place. Work from the center outwards so you do not trap air inside the tubing.
Figure 7001. (Sheet 1 of 1) High-Voltage Splice (GRAPHIC 34-40-11-99B-878-A01) (8)
Reroute and tie the cables exactly as shown in Figure 7002 and Figure 7003 with the cable ties (150, IPL Figure 9) and lacing tape, 1/16 inch, 20-pound strength (commercially available). NOTE:
EFFECTIVITY ALL
Be careful of the order and orientation of the cables and the cable clip (125, IPL Figure 9). The route and position of the cables and the ties are critical to prevent interference through the full range of movement of the gimbal and premature wear of the cables.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 7006 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Figure 7002. (Sheet 1 of 1) Magnetron Cable Dressing (GRAPHIC 34-40-11-99B-879-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 7003. (Sheet 1 of 1) Magnetron and Preamp Cable Dressing (GRAPHIC 34-40-11-99B-880-A01) (9)
Put the cable ferrules into the channels at the top of the base (290) in the order shown in Figure 7003.
(10) Apply 425 locking compound (CAGE 1UCL7) to the threads of the three screws (275). (11) Install the three screws (275) and the clamp (270) that enclose the cable ferrules on the base (290). (12) Torque the three screws (275) to 2 to 3 in-lb (0.23 to 0.34 N•m). (13) Install the receiver assembly (140, IPL Figure 9) as described in Paragraph 2.F. (Subtask 34-40-11-400-006-A01). (14) Install the power supply/modulator board (140) as described in Paragraph 2.G. (Subtask 34-40-11-400-007-A01). (15) Install the logic board (135) as described in Paragraph 2.H. (Subtask 34-40-11-400-008-A01). (16) Install the cover (35) as described in Paragraph 2.I. (Subtask 34-40-11-400-009-A01). E.
Preamp Board Installation (Subtask 34-40-11-400-005-A01) (1)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(2)
Replace the bus wire on E1001, E1002, E1003, and E1004 of the X-band radar front end (80, IPL Figure 4) with new wire, AWG 22, solid copper, tinned (commercially available) each 1 inch (2.54 cm) long.
(3)
Put the microwave absorber (50, IPL Figure 4) into the preamp housing (55, IPL Figure 4). Thread the bus wire through the microwave absorber (50, IPL Figure 4).
(4)
Put the preamp board (25, IPL Figure 4) into the preamp housing (55, IPL Figure 4). Thread the bus wire through E1001, E1002, E1003, and E1004 on the preamp board (25, IPL Figure 4).
(5)
Apply 425 locking compound (CAGE 1UCL7) to the threads of the two spacers (35 and 40, IPL Figure 4) and the screw (30, IPL Figure 4).
(6)
Secure the preamp board (25, IPL Figure 4) with the two spacers (35 and 40, IPL Figure 4), the two washers (45, IPL Figure 4), and the screw (30, IPL Figure 4).
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 7008 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 (7)
Torque the two spacers (35 and 40, IPL Figure 4) and the screw (30, IPL Figure 4) to 2 to 3 in-lb (0.23 to 0.34 N•m).
(8)
Apply solder to E1001, E1002, E1003, and E1004, and clean the connections.
CAUTION:
(9)
USE EXTREME CARE WHEN YOU REPLACE P1001. MAKE SURE THAT THE CONNECTOR IS CENTERED AND SQUARE WITH THE PIN BEFORE YOU APPLY PRESSURE TO INSERT.
Reconnect P1001 to J1001 and P1002 to J1002.
(10) Apply 425 locking compound (CAGE 1UCL7) to the threads of the screw (10, IPL Figure 4) and the two screws (15, IPL Figure 4). (11) Install the cover (5, IPL Figure 4) and secure with the screw (10, IPL Figure 4) and the two screws (15, IPL Figure 4). (12) Torque the screw (10, IPL Figure 4) and the two screws (15, IPL Figure 4) to 2 to 3 in-lb (0.23 to 0.34 N•m). (13) Install the receiver assembly (140) as described in Paragraph 2.F. (Subtask 34-40-11-400006-A01). (14) Install the logic board (135) as described in Paragraph 2.H. (Subtask 34-40-11-400-008-A01). (15) Install the cover (35) as described in Paragraph 2.I. (Subtask 34-40-11-400-009-A01). F.
Receiver Module Installation (Subtask 34-40-11-400-006-A01) (1)
Refer to Paragraph 2.D. (Subtask 34-40-11-300-004-A01) in the REPAIR (PGBLK 34-40-11-6000) section for additional information when you replace the receiver module.
(2)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(3)
Put the limiter (175, IPL Figure 9) with the cable shroud (135, IPL Figure 9) between the receiver assembly (140, IPL Figure 9) and the RF network (165, IPL Figure 9) with the arrow pointing toward the receiver assembly.
(4)
Apply 425 locking compound (CAGE 1UCL7) to the threads of the four cap screws (120, IPL Figure 9).
(5)
Put the cable guard (115, IPL Figure 9) against the receiver assembly (140, IPL Figure 9) and install the four cap screws (120, IPL Figure 9).
(6)
Torque the four cap screws (120, IPL Figure 9) to 17 to 19 in-lb (1.92 to 2.15 N•m).
(7)
Reroute and tie the cables exactly as shown in Figure 7003 with the cable ties (150, IPL Figure 9). NOTE:
Be careful of the order and orientation of the cables and the cable clip (125, IPL Figure 9). The route and position of the cables and the ties are critical to prevent interference through the full range of movement of the gimbal and premature wear of the cables.
(8)
Put the cable ferrules into the channels at the top of the base (290) in the order shown in Figure 7003.
(9)
Apply 425 locking compound (CAGE 1UCL7) to the threads of the three screws (275).
(10) Install the three screws (275) and the clamp (270) that enclose the cable ferrules on the base (290). (11) Torque the three screws (275) to 2 to 3 in-lb (0.23 to 0.34 N•m).
EFFECTIVITY ALL
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Page 7009 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 (12) Install the power supply/modulator board (140) as described in Paragraph 2.G. (Subtask 34-40-11-400-007-A01). (13) Install the logic board (135) as described in Paragraph 2.H. (Subtask 34-40-11-400-008-A01). (14) Install the cover (35) as described in Paragraph 2.I. (Subtask 34-40-11-400-009-A01). G.
Power Supply/Modulator Board Installation (Subtask 34-40-11-400-007-A01) (1)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(2)
Reconnect and reroute all the cables.
(3)
Put the power supply/modulator board (140) into the base (290). NOTE:
Make sure that no cables have been pinched.
(4)
Apply 425 locking compound (CAGE 1UCL7) to the threads of the two spacers (75) and the two spacers (70).
(5)
Install the two spacers (75) in the two holes on the transformer end of the board. Do not tighten.
(6)
Install the two spacers (70) on either side of the fan. Do not tighten.
(7)
Apply 425 locking compound (CAGE 1UCL7) to the threads of the five screws (95) and the two screws (100).
(8)
Install the five screws (95). Do not tighten.
(9)
Install the two screws (100). Do not tighten.
(10) Torque the five screws (95), the two screws (100), the two spacers (70), and the two spacers (75) to 6 to 7 in-lb (0.68 to 0.79 N•m). (11) Install the logic board (135) as described in Paragraph 2.H. (Subtask 34-40-11-400-008-A01). (12) Install the cover (35) as described in Paragraph 2.I. (Subtask 34-40-11-400-009-A01). H.
Logic Board Installation (Subtask 34-40-11-400-008-A01) (1)
Refer to Paragraph 2.D. (Subtask 34-40-11-300-004-A01) in the REPAIR (PGBLK 34-40-11-6000) section for additional information when you replace the logic board.
(2)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
CAUTION:
(3)
Reconnect all the cables.
(4)
Apply 3145 adhesive sealant (CAGE 71984) to two sides of P5005 and P5506 to a height of 0.14 to 0.02 inch (3.56 to 5.08 mm) above the logic board (135) to secure the connectors to the board.
(5)
Install the IF cover (85).
(6)
Put the logic board (135) into the base (290). NOTE:
Make sure that no cables have been pinched.
(7)
Apply 425 locking compound (CAGE 1UCL7) to the threads of the two screws (65) and the screw (60).
(8)
Install the two screws (65) that secure the connector to the base (290). Do not tighten the screws.
(9)
Install the screw (60) in the center of the logic board.
EFFECTIVITY ALL
USE EXTREME CARE WHEN YOU REPLACE P5502. MAKE SURE THAT THE CONNECTOR IS CENTERED AND SQUARE WITH THE PIN BEFORE YOU APPLY PRESSURE TO INSERT.
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COMPONENT MAINTENANCE MANUAL 071-01519 (10) Torque the two screws (65) and the screw (60) to 6 to 7 in-lb (0.68 to 0.79 N•m). (11) Install the cover (35) as described in Paragraph 2.I. (Subtask 34-40-11-400-009-A01). I.
J.
Bottom Cover Installation (Subtask 34-40-11-400-009-A01) (1)
Refer to IPL Figure 1 for all the item numbers unless specified differently.
(2)
Put the cover (35) on the base (290) with the handle toward the connector side.
(3)
Apply 425 locking compound (CAGE 1UCL7) to the threads of the two screws (40) and the nine screws (45).
(4)
Install the two screws (40) on either side of the connector. Do not tighten.
(5)
Install the nine screws (45).
(6)
Torque the two screws (40) and the nine screws (45) to 6 to 7 in-lb (0.68 to 0.79 N•m).
Job Close-up (Subtask 34-40-11-400-010-A01) (1)
EFFECTIVITY ALL
Remove all tools, equipment, and unwanted materials from the work area.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 7012 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FITS AND CLEARANCES 1.
Planning Data (TASK 34-40-11-99C-808-A01) A.
B.
Reason for the Job (Subtask 34-40-11-99C-016-A01) (1)
This section gives the fits and clearances used when the ART 2000 was made.
(2)
This section gives the torque data required for repair and assembly of the ART 2000.
Job Setup Data (Subtask 34-40-11-99C-017-A01) (1)
2.
Not applicable.
Procedure (TASK 34-40-11-220-801-A01) A.
Job Setup (Subtask 34-40-11-220-001-A01) (1)
B.
Not applicable.
Fits and Clearances of the ART 2000 (Subtask 34-40-11-220-002-A01) (1)
Refer to Table 8001 when you do the procedures in REPAIR (PGBLK 34-40-11-6000) and ASSEMBLY (PGBLK 34-40-11-7000). Table 8001. Fits and Clearances
Figure - Item
Condition to Measure
Limits
Figure 2004, Figure 2007, Figure 2009, and Figure 2011 - Protective coating
Thickness of protective coating
0.002 to 0.004 inch (0.05 to 0.10 mm)
Figure 2005 - insert
Distance between insert and face of X-band radar
Flush to 0.03 inch (0.8 mm) below
Figure 2009 - T2
Height of T2 above board
1.25 inches (31.8 mm) maximum
Figure 2009 - component leads
Height of component leads above board
0.04 inch (1.0 mm) maximum
Figure 2009 - C18
Height of C18 above board
0.70 inch (17.8 mm) maximum
Figure 2009 - C11 and C13
Facing surface separation of C11 and C13
2.21 inches (56.1 mm)
Figure 2011 - J1 flange
Height of flange above board
0.22 to 0.23 inch (5.6 to 5.8 mm) maximum
C.
Torque Values (Subtask 34-40-11-220-003-A01) (1)
Tighten nuts, bolts, screws, and tube fittings to the standard torque unless specified differently. Refer to FAA Manual AC65-9A, Airframe and Powerplant Mechanics General Handbook, for standard torque.
(2)
Tighten nuts, bolts, screws, and tube fittings to the standard torque unless specified differently.
(3)
Tighten fasteners installed through non-elastic boundaries to remove visible clearance between the parts. Monitor the rundown torque necessary just before the fastener becomes tight. Then tighten to the final torque (refer to Table 8002 for the correct thread size) and add the rundown torque. This procedure is sufficient for all fasteners not shown under torque values below. Refer to Table Table 8003 for final torque data after rundown torque.
EFFECTIVITY ALL
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Page 8001 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 (4)
Tighten fasteners installed through elastic boundaries (sealed by means of a diaphragm or similar elastomeric gasket) equally to get a pressure tight seal. Table 8002. Thread Size and Torque Data Torque in-lb (Nm)
Thread Size
Aluminum Fastener
Cres Fastener
6-32
5 (0.565)
10 (1.13)
8-32
10 (1.13)
20 (2.26)
10-24
15 (1.695)
35 (3.955)
1/4-20
45 (5.085)
75 (8.475)
5/16-10
80 (9.04)
160 (18.08)
3/8-24
140 (15.82)
275 (31.075)
Table 8003. Final Torque Data Thread Size
Approximate Turn After Run-Down
6-32
45 deg
8-32
60 deg
10-24
40 deg
1/4-20
40 deg
5/16-18
40 deg
3/8-24
60 deg
D.
Specified Torque Values (Subtask 34-40-11-220-004-A01) (1)
Table 8004 gives information necessary to tighten fasteners to specified torque. Values shown do not include frictional torque caused by self-locking devices or rundown resistance. Frictional torque values must be added to the specified torque. Table 8004. Specified Torque
Figure Number
Item Number
Nomenclature
Torque in-lb (N•m)
IPL Figure 1
40 and 45
Screw
6 to 7 (0.68 to 0.79)
IPL Figure 1
60 and 65
Screw
6 to 7 (0.68 to 0.79)
IPL Figure 1
70 and 75
Spacer
6 to 7 (0.68 to 0.79)
IPL Figure 1
95 and 100
Screw
6 to 7 (0.68 to 0.79)
IPL Figure 1
160
Azimuth nut
17 to 19 (1.92 to 2.15)
IPL Figure 1
165
Screw
17 to 19 (1.92 to 2.15)
IPL Figure 1
180
Screw
6 to 7 (0.68 to 0.79)
IPL Figure 1
205
Screw
6 to 7 (0.68 to 0.79)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table 8004. Specified Torque (Cont) Figure Number
Item Number
Nomenclature
Torque in-lb (N•m)
IPL Figure 1
275
Screw
2 to 3 (0.23 to 0.34)
IPL Figure 4
10 and 15
Screw
2 to 3 (0.23 to 0.34)
IPL Figure 4
30
Screw
2 to 3 (0.23 to 0.34)
IPL Figure 4
35 and 40
Spacer
2 to 3 (0.23 to 0.34)
IPL Figure 9
40
Screw
6 to 7 (0.68 to 0.79)
IPL Figure 9
55
Screw
6 to 7 (0.68 to 0.79)
IPL Figure 9
120
Cap screw
17 to 19 (1.92 to 2.15)
IPL Figure 9
145
Cap screw
17 to 19 (1.92 to 2.15)
E.
Job Close-up (Subtask 34-40-11-220-005-A01) (1)
EFFECTIVITY ALL
Not applicable.
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EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES 1.
Planning Data (TASK 34-40-11-99C-809-A01) A.
Reason for the Job (Subtask 34-40-11-99C-018-A01) (1)
B.
This section gives the special tools, fixtures, equipment, and consumable materials that are necessary for ART 2000 maintenance.
Job Setup Data (Subtask 34-40-11-940-001-A01) (1)
You can use equivalent alternatives for the special tools, fixtures, equipment, and consumable materials. The user must find equivalent alternatives.
(2)
Refer to Table 9001 for the specified special tools, fixtures, and equipment in this section.
(3)
Refer to H4/H8 CAGE Codes (available at http://www.dlis.dla.mil/cage_welcome.asp) for manufacturer’s address. Table 9001. Special Tools, Fixtures, and Equipment
Number
Description
006-3086-XX
color radar indicator, IN 182A, part of RDR 2000 Color Weather Radar System (CAGE 22373)
050-03299-0000
bench test kit (CAGE 22373)
050-03311-0000
configuration module programmer, KPA 900 (CAGE 22373)
071-00097-0100
configuration module (CAGE 22373)
1425-4
dummy load (CAGE 93459)
2598-5342-54
engagement/disengagement tool (CAGE 96341)
429E
receiver/transmitter, ARNIC 429 (CAGE ER649)
465
oscilloscope (CAGE 80009)
8000A
digital multimeter (CAGE 89536)
Source
allen wrench, 9/64-inch, beryllium copper (commercially available) non-synthetic brush (commercially available) PC, IBM-compatible, 386 or higher, MS DOS 3.3 or higher, 3.5-inch drive, greater than 10 M HDD (commercially available) power supply, +28 VDC, regulated to 40 VDC at 20 A (commercially available)
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
Table 9001. Special Tools, Fixtures, and Equipment (Cont) Number
Description
Source
signal generator, capable of 60 MHz (commercially available) soft-bristle brush (commercially available) stiff-bristle brush (commercially available) stop watch (commercially available) test harness/tester (user built, refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES section) torque wrench, capable of 0.94 to 25.0 in-lb (0.11 to 2.82 N•m) (commercially available) vertical gyro simulator, capable of 50 mV/degree (commercially available) HP 8593A
spectrum analyzer (CAGE 28480)
HP X281A
waveguide adapter (CAGE 28480)
P6000
probe, X10, 10 megohm (CAGE 80009)
P6021
current probe (CAGE 80009)
RD 300/301/301A
radar test set with option 1 (CAGE 88379)
WR109
radar test set (CAGE KCQU2) WARNING:
BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
CAUTION:
DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE.
(4)
EFFECTIVITY ALL
Refer to Table 9002 for the specified consumable materials in this section.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519 Table 9002. Consumable Materials Number
Description
150-00096-0000
shrink tubing, black, 0.125 inch (3.17 mm) (CAGE 22373)
150-00096-0001
shrink tubing, black, 0.1875 inch (4.76 mm) (CAGE 22373)
150-00096-0002
shrink tubing, black, 0.25 inch (6.35 mm) (CAGE 22373)
17631
RTV sealant (CAGE 1UCL7)
271
locking compound (CAGE 1UCL7)
3145
adhesive sealant (CAGE 71984)
4/0
crocus cloth (commercially available)
425
locking compound (CAGE 1UCL7)
4444
instant adhesive (CAGE 1UCL7)
73
locking compound (CAGE 1UCL7)
Source
isopropanol, technical, per MIL TT-I-735, Grade B (commercially available) lacing tape, 1/16 inch, 20-pound strength (commercially available) protective coating, Type AR, fluorescent, MIL-I-46058 (commercially available) wire, AWG 22, black, MIL-W-16878/4 (commercially available) wire, AWG 22, solid copper, tinned (commercially available) Aeroshell 22
grease, multipurpose (CAGE 4LR76)
E-6000
adhesive sealant, encapsulate (CAGE 04065)
HYSOL 1B-31
conformal coating (CAGE 99109)
Vertrel SMT
cleaning solvent (CAGE S3299)
(5)
The list that follows identifies Honeywell publications that are related to this section: • Not applicable.
EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
2.
Procedure (TASK 34-40-11-490-801-A01) A.
Job Setup (Subtask 34-40-11-490-001-A01) (1)
B.
Test Harness/Tester Manufacturing Instructions (Subtask 34-40-11-490-002-A01) (1)
EFFECTIVITY ALL
The following paragraphs provide manufacturing and assembly instructions to make the required test cable.
The interconnects for the test harness/tester are shown in Figure 9001 along with the materials required to manufacture the cable.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 9001. (Sheet 1 of 1) Test Harness/Tester (GRAPHIC 34-40-11-99B-881-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 9005/9006 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 C.
Job Close-up (Subtask 34-40-11-210-004-A01) (1)
EFFECTIVITY ALL
Remove all tools, equipment, and unwanted materials from the work area.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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EFFECTIVITY ALL
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SPECIAL PROCEDURES 1.
Not Applicable
EFFECTIVITY ALL
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EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519
REMOVAL 1.
Not Applicable
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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INSTALLATION 1.
Not Applicable
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519
SERVICING 1.
Not Applicable
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
STORAGE (INCLUDING TRANSPORTATION) 1.
Planning Data (TASK 34-40-11-99C-810-A01) A.
Reason for the Job (Subtask 34-40-11-99C-019-A01) (1)
B.
Use these procedures to prepare the ART 2000 for storage or transportation. The function of these procedures is to make sure that the ART 2000 has protection from dust, moisture, and other contamination.
Job Setup Data (Subtask 34-40-11-99C-020-A01) (1)
You can use equivalent alternatives for the special tools, fixtures, equipment, and consumable materials. The user must find equivalent alternatives.
(2)
Refer to Table 15001 for the specified special tools, fixtures, and equipment in this section.
(3)
Refer to H4/H8 CAGE Codes (available at http://www.dlis.dla.mil/cage_welcome.asp) for manufacturer’s address. Table 15001. Special Tools, Fixtures, and Equipment
Number
Description
Source
Not applicable
Not applicable
Not applicable
(4)
Refer to Table 15002 for the specified consumable materials in this section. Table 15002. Consumables
Number
Description
Source
Not applicable
Not applicable
Not applicable
(5)
The list that follows identifies Honeywell publications that are related to this section: • Not applicable.
2.
Procedure (TASK 34-40-11-550-801-A01) A.
Job Setup (Subtask 34-40-11-550-001-A01) CAUTION:
(1) B.
If the ART 2000 must be in storage for a long time, keep it in a location with a temperature range of -20 to +131 F (-30 to +55 C).
Job Close-up (Subtask 34-40-11-550-003-A01) (1)
EFFECTIVITY ALL
Obey the precautions.
Storage (Subtask 34-40-11-550-002-A01) (1)
C.
USE INDUSTRY APPROVED ELECTROSTATIC DISCHARGE SENSITIVE PRECAUTIONS. THE ART 2000 CONTAINS ELECTROSTATIC DISCHARGE SENSITIVE ITEMS.
Not applicable.
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EFFECTIVITY ALL
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REWORK (SERVICE BULLETIN ACCOMPLISHMENT PROCEDURES) 1.
Not Applicable
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
ILLUSTRATED PARTS LIST 1.
Description (TASK 34-40-11-99C-811-A01) A.
B.
General (Subtask 34-40-11-99C-021-A01) (1)
This section gives the parts that are used to make the ART 2000. It also supplies the necessary data to get replacement parts for REPAIR (PGBLK 34-40-11-6000) and TESTING AND FAULT ISOLATION (PGBLK 34-40-11-1000).
(2)
The DPL part of the ILLUSTRATED PARTS LIST (IPL 34-40-11-10000) gives a breakdown, in disassembly sequence, of assemblies and detail parts of the unit.
(3)
The illustrations show where you can find each part and are an important aid in DISASSEMBLY (PGBLK 34-40-11-3000) and ASSEMBLY (PGBLK 34-40-11-7000).
(4)
The item numbers shown in the DPL are the same as the item numbers on the exploded view illustration(s). To find a PN, find the part on the illustration and record the item number. Go to the DPL to find the item number and related PN.
Job Setup Data (Subtask 34-40-11-99C-022-A01) (1)
The list that follows identifies references that are related to this section: • H4/H8 CAGE Codes (available at http://www.dlis.dla.mil/cage_welcome.asp).
2.
Contents of the IPL (TASK 34-40-11-99C-812-A01) A.
B.
C.
Vendor Code List (Subtask 34-40-11-99C-023-A01) (1)
The vendor code list shows the vendor CAGE code, name, and address in numerical sequence for all vendors shown in the IPL. Refer to the Vendor Code List.
(2)
The vendor CAGE code is given in the nomenclature column of the DPL to identify the vendor.
EDI (Subtask 34-40-11-99C-024-A01) (1)
The EDI is an alphanumeric list of the equipment designators given to the subassemblies and electrical/electronic parts. The designators are an aid to identify parts in SCHEMATIC AND WIRING DIAGRAMS (PGBLK 34-40-11-2000). Refer to the Equipment Designation Index List.
(2)
Each entry in the EDI identifies the figure and item numbers where the part is found in the DPL. The EDI can also identify a geographical location of the equipment designator found on the graphic illustration. A hyphen between two designators shows a continuous sequence of designators (example: A1-A5 is the same as A1 thru A5).
Numerical Index (Subtask 34-40-11-99C-025-A01) (1)
The Numerical Index is an alphanumeric list of all the PNs shown in the part number column of the DPL.
(2)
Also included in the index are the Honeywell PNs that are equivalent to the manufacturer PN. Optional manufacturer PNs are not included in the index.
(3)
The figure item column gives all of the locations of a part. If a PN is in more than one figure item location, the PN is shown only one time in the part number column.
(4)
The total required column shows the total number of parts that are used at each figure item location.
(5)
The airline stock number column has space for customers to use.
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519 D.
Detailed Parts List (Subtask 34-40-11-99C-026-A01) NOTE: (1)
An item number is given to each part in the DPL and on the related illustration. The item numbers show the general disassembly sequence.
(2)
To find a PN in the DPL.
(3)
(a)
If the PN is known, refer to the Numerical Index to find the figure and item numbers in the DPL.
(b)
If the PN is not known, turn to the illustration; locate the part, and record the item number. The PN is shown opposite the item number in the DPL.
(c)
If the equipment designator is known, refer to the EDI to find the figure and item numbers in the DPL.
Revision codes for added, changed, or deleted data. (a)
(4)
(5)
(6)
EFFECTIVITY
Revision bars (I) in the left margin show technical changes.
Figure item column. (a)
A part not shown on the illustration is identified in the DPL as non-illustrated by a dash (-) before the item number.
(b)
When two or more items that are visually alike are listed in sequence, only the first item is illustrated. The illustration, however, is applicable to both items.
(c)
When the detailed parts of an assembly or installation are illustrated, they can be identified by a bracket. The bracket identifies the next higher assembly or installation. If brackets are not used, the detail parts are illustrated, but the next higher assembly or installation is not.
(d)
The parts that make up a select-from range group (i.e. calibration resistor assortments) have a non-illustrated item number or a different figure.
Part number column. (a)
A PN that is prefixed usually indicates a type of part or method of procurement. Examples of these prefixes are AN, MS, and NAS. These standard PNs may be suffixed by numbers only or numbers and letters. Suffix numbers usually indicate configuration or design difference. Suffix letters usually indicate material, color, or finish differences.
(b)
All procurable components manufactured by Honeywell have a PN. The PN is stamped, etched, or cast on the part at time of manufacture when size, space, or shape is available. More manufacturing symbol(s), letter(s), or number(s) can be shown with the PN to identify a manufacturing process, a design change, or for a proprietary repair. Do not use this data to order a part. Use only the item PN and nomenclature as shown in the DPL.
(c)
The letter “S” prefix of a PN designates a Honeywell standard PN. These standard PNs have suffix letters and numbers.
(d)
Honeywell commercial standard numbers are used in the parts lists to identify off-the-shelf items procured from another manufacturer. A commercial standard number can be a ten or eleven digit number.
Airline stock number column. (a)
ALL
Refer to Figure 10001.
The airline stock number column has space for customers to use.
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COMPONENT MAINTENANCE MANUAL 071-01519 (7)
Nomenclature column. (a)
The indenture code shows the relationship of each item to its NHA. 1
Each item goes in the nomenclature column one indenture (one dot) to the right of the assembly to which it belongs.
2
The items at the same indenture are all components of a single assembly or subassembly. An example of the indenture code system is shown below. 1 2 3 4 5 6 7 Assembly or installation descriptive title • Detail parts • Assembly • Attaching parts for assembly • • Detail parts for assembly • • Subassembly • • Attaching parts for subassembly • • • Detail parts for subassembly • • • Sub-subassembly • • • Attaching parts for sub-subassembly • • • • Detail parts for sub-subassembly
EFFECTIVITY ALL
(b)
Wherever possible, abbreviations will agree with the ASME Y14.38 specification. The non-standard abbreviations that spell words are not used.
(c)
The vendor code data are as follows. 1
The vendors with a code number have the letter V before the number. This code, from H4/H8 CAGE Codes, identifies where to get that item.
2
No vendor code is shown in the nomenclature column of the DPL if the item is a U.S. standard part or Honeywell is the vendor.
3
The vendors with no code number (NCN) are identified by (VNCN__).
4
The vendors with no code number are shown in the nomenclature column of the DPL with the vendor’s full name and address.
(d)
A Honeywell specification drawing number will be shown if applicable.
(e)
Refer to this list of possible explanation terms. These terms may be abbreviated. 1
OPTIONAL shows that the part is an optional alternative to other parts in the same item number variant group.
2
ALTERNATE shows that the part is an alternative to other parts in the same item number variant group.
3
SUPERSEDED BY shows that the part is replaced by the PN or item number shown and is not interchangeable.
4
SUPERSEDES shows that the part replaces the PN or item number shown and is not interchangeable.
5
REPLACED BY shows that the part is replaced by the PN or item number shown and is interchangeable. Part can be used until the supply is gone.
6
REPLACES shows that the part replaces the PN or item number shown and is interchangeable.
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COMPONENT MAINTENANCE MANUAL 071-01519
(f) (8)
EFFECTIVITY ALL
7
PRE SERVICE BULLETIN XXXX shows that the part is used if service bulletin XXXX was not done.
8
POST SERVICE BULLETIN XXXX shows that the part is used if service bulletin XXXX was done.
9
PRE SPARE PARTS BULLETIN XXXX shows that the part is used if spare parts bulletin XXXX was not done.
10
POST SPARE PARTS BULLETIN XXXX shows that the part is used if spare parts bulletin XXXX was done.
11
NONREPAIRABLE shows that the part cannot be repaired.
12
NONPROCURABLE shows that the part or assembled parts cannot be purchased. The term NONPROC is used in the PART NUMBER column when no PN exists for the assembly. The components of the assembled parts can be ordered unless differently specified.
13
ORDER NEXT HIGHER ASSEMBLY shows that the PN is part of a matched set and cannot be ordered independently. The next higher assembly can be ordered.
14
REFERENCE (GAREF, TUCREF, AIREF, TORREF etc.) shows the procurable PN that exceeds 15 digits in the NOMENCLATURE column as ORDER PN NNNN.
15
ORDER PART NUMBER shows a nonstandard or reference PN.
16
DELETED shows the part is not available for use.
17
SEE FIGURE FOR BREAKDOWN shows the PN details in a different figure.
18
SEE FIGURE FOR NEXT HIGHER ASSEMBLY refers the PN to the next higher assembly.
19
USE WITH (ITEM or PART NUMBER) shows a part is used with a different part.
20
COMPONENT OF (ITEM or PART NUMBER) shows that the part is a component of a different part.
21
SEE NOTE (N) is used to give more data for a part. The NOTE location is after the last item of the figure.
22
MAY BE SUBSTITUTED shows that the part in the Nomenclature column with its vendor code is an equivalent alternative for the part in the Part Number column.
23
REFER TO ATA or PUBLICATION NUMBER identifies the assemblies that have their own Component Maintenance Manuals. These entries are also shown in the INTRODUCTION (PGBLK 34-40-11-0) of this manual under References.
If applicable, refer to REPAIR (PGBLK 34-40-11-6000) for description of wire, sleeving, and lacing given in this DPL.
The effectivity code column. (a)
The effectivity code identifies the different configurations of the top assembly in each IPL figure.
(b)
If this column is empty, the part is used in all configurations of the top assembly for that IPL figure.
(c)
If this column has a letter code in it, the part is only used in the configuration of the top assembly that has the same letter code.
(d)
If this column has more than one letter code, the part is used in each top assembly with the same letter codes.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519
(9)
(e)
If a comma separates the column entry (A, C), the other codes do not apply. For example, a component coded “A, C” is applicable for Codes A and C only and not applicable for Code B.
(f)
If a dash separates the column entry (A-C), the other codes do apply. For example, a component coded “A-C” is applicable for Codes A, B, and C.
(g)
This column also shows “use with” and “component of” parts data. Use numbers when the effectivity code is not available or cannot be satisfactorily used to show this type of data. This code shows a relationship between parts in the same figure.
The units per assembly column. (a)
EFFECTIVITY ALL
The units per assembly column show the quantity of parts necessary in the assembly of one next higher assembly. The letters AR in this column show “as required” items and refer to bulk items or adjustable quantity items, such as shims or spacers. The letters RF are used to show an item that is shown in another area with a quantity.
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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COMPONENT MAINTENANCE MANUAL 071-01519
Figure 10001. (Sheet 1 of 1) DPL Example (GRAPHIC 34-40-11-99B-882-A01)
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10006 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519 Key for Figure 10001. (Sheet 1 of 1) 1
FIGURE/ITEM column
18
NONPROCURABLE example
2
PART NUMBER column
19
ORDER NEXT HIGHER ASSEMBLY example
3
AIRLINE STOCK NUMBER column
20
REFERENCE example
4
NOMENCLATURE column
21
ORDER PART NUMBER example
5
EFFECTIVITY (USE) CODE column
22
DELETED example
6
UNITS PER ASSEMBLY column
23
SEE FIGURE FOR BREAKDOWN example
7
OPTIONAL example
24
SEE FIGURE FOR NEXT HIGHER ASSEMBLY example
8
ALTERNATE example
25
USE WITH (ITEM or PART NUMBER) example
9
SUPERSEDED BY example
26
COMPONENT OF (ITEM or PART NUMBER) example
10
SUPERSEDES example
27
Changed or added data indicator example
11
REPLACED BY example
28
Non-illustrated indicator example
12
REPLACES example
29
Vendor code example
13
PRE SERVICE BULLETIN example
30
Honeywell specification drawing number example
14
POST SERVICE BULLETIN example
31
Effectivity and Use code example
15
PRE SPARE PARTS BULLETIN example
32
Quantity example
16
POST SPARE PARTS BULLETIN example
33
RF indicates item referenced elsewhere.
17
NONREPAIRABLE example
34
As required example
EFFECTIVITY ALL
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EFFECTIVITY ALL
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COMPONENT MAINTENANCE MANUAL 071-01519
3.
Vendor Code List NOTE:
The vendor codes and PNs that are shown in the DPL must not be construed as an authorization of the vendor, pursuant to the FAA regulations, to ship directly to the user. Neither must it be construed as a certification by Honeywell that parts shipped by vendors directly to users will conform to the type design or that such parts are airworthy or safe for installation.
Code
Vendor
00A29
PHOTO-GRAPHICS COMPANY INC, 5100 MARTHA TRUMAN RD STE C, GRANDVIEW, MO 64030-0000
02113
COILCRAFT INCORPORATED, 1102 SILVERLAKE RD, CARY, IL 60013-1658
04222
AVX CORPORATION, 801 17TH AVE S, MYRTLE BEACH, SC 29577-4245
06915
RICHCO PLASTIC CO, 5825 N TRIPP AVE, CHICAGO, IL 60646-6097
07416
NELSON NAME PLATE COMPANY, 2800 CASITAS AVE, LOS ANGELES, CA 90039-2942
08VU6
TOKO AMERICA INC, 1250 FREHANVILLE DR, MOUNT PROSPECT, IL 60056-6023
0B0T3
MARLO ELECTRONICS, 4058 NE 5TH AVE, FORT LAUDERDALE, FL 33334
0B485
PAINTED FEATHER PRECISION LLC, 8401 73RD AVE N STE 56, MINNEAPOLIS, MN 55428-1508
0GP12
RADIALL INC, 260 HATHAWAY DR, STRATFORD, CT 06497-7361
0GWP1
GENERAL INSTRUMENT CORP DEFENSE SYSTEMS GROUP, 600 W JOHN ST, HICKSVILLE, NY 11801-1040
0HAF7
EPSON AMERICA INC, 3840 KILROY AIRPORT WAY, LONG BEACH, CA 90806-2452
0JN86
NORTH AMERICAN PHILIPS CORP PHILIPS COMPONENTS SEMICONDUCTOR DIV, 3000 SCOTT BLVD, SANTA CLARA, CA 95050
0JP56
RAMTRON CORP, 1873 AUSTIA BLUFF PKY, COLORADO SPRINGS, CO 80918
0VGY3
3M COMPANY, 6801 RIVER PLACE BLVD, AUSTIN, TX 78769-2963
0WYL6
FRC COMPONENT PRODUCTS, INC, 1511 S BENJAMIN AVE, MASON CITY, IA 50401-5607
11402
HISONIC, INC, 310 N MARION ST, OLATHE, KS 66061-3107
14552
MICROSEMI CORPORATION, 2381 MORSE AVE, IRVINE, CA 92614-6233
16673
STAMPING OF MINNESOTA INC, 21980 HAMBURG AVE, LAKEVILLE, MN 55044-7246
18310
CONCORD ELECTRONICS, INC, 3300 47TH AVE, LONG ISLAND CITY, NY 11101-2430
19142
Q-E MANUFACTURING COMPANY, INC, 809 MARKET ST, NEW BERLIN, PA 17855-0000
1A839
AEROFAB INC, POMPANO BEACH, FL 33069-1400
1A942
LITTON SYSTEMS INC POTENTIOMETER DIV, WOODLAND HILLS, CA 91364
1CH66
PHILIPS SEMICONDUCTORS, 811 E ARQUES AVE, SUNNYVALE, CA 94088-3409
1DA26
WIREBENDERS, INC, 10201 N 21ST AVE STE 4, PHOENIX, AZ 85021-1827
1ES66
MAXIM INTEGRATED PRODUCTS, INC, 120 SAN GABRIEL DR, SUNNYVALE, CA 94086-5150
1MQ07
SEMICONDUCTOR COMPONENTS INDUSTRIES LLC, 5005 E MCDOWELL ROAD, PHOENIX, AZ 85008-4229
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10009 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Code
Vendor
1QYX0
P-K DIRECT INC, 501 W RAY RD STE 7, CHANDLER, AZ 85225-7284
22373
HONEYWELL INTL INC, DBA AEROSPACE ELECTRONIC SYSTEMS, 1 TECHNOLOGY CENTER, 23500 W 105TH STREET, OLATHE, KS 66061-8425
22526
FCI USA INC, 825 OLD TRAIL ROAD, ETTERS, PA 17319-9392
23540
NIAGARA PLASTICS L.L.C., 7090 EDINBORO RD, ERIE, PA 16509-4497
24687
PILOT TECHNOLOGIES CORP, 2010 FORTUNE DR 8, SAN JOSE, CA 95131-1823
27014
NATIONAL SEMICONDUCTOR CORPORATION, 2900 SEMICONDUCTOR DR, SANTA CLARA, CA 95051-0606
28198
POSITRONIC INDUSTRIES, INC, 423 N CAMPBELL AVE, SPRINGFIELD, MO 65806-1007
29309
RICHEY INC, 1219 4TH AVE S, NASHVILLE, TN 37224-0296
2M626
AFCOM, 109 COMMERCE WAY, SANFORD, FL 32771-3092
30408
BARNES GROUP INC, 434 W EDGERTON AVE, MILWAUKEE, WI 53207-6027
31433
KEMET ELECTRONICS CORPORATION, 2835 KEMET WAY, SIMPSONVILLE, SC 29681-6298
31740
LEIGHTNER ELECTRONICS, INC, 1501 S TENNESSEE ST, MC KINNEY, TX 75069-7126
33062
FERRONICS, INC, 45 OCONNOR ROAD, FAIRPORT, NY 14450
33095
SPECTRUM CONTROL, INC, 8031 AVONIA RD, FAIRVIEW, PA 16415-2829
34899
FAIR-RITE PRODUCTS CORP, 1 COMMERCIAL ROW, WALLKILL, NY 12589-0288
37942
YOSEMITE INVESTMENT INC, 1701 INDIANAPOLIS RD, GREENCASTLE, IN 46135
40080
TECHNICAL SERVICES FOR ELECTRONICS INC, 203 SHAMROCK DR, ARLINGTON, MN 55307
46384
PENN ENGINEERING AND MANUFACTURING CORP, 5190 OLD EASTON HWY, DANBORO, PA 18916-1000
50434
AVAGO TECHNOLOGIES U.S. INC, 350W TRIMBLE RD, SAN JOSE, CA 95131-1008
50558
ELECTRONIC CONCEPTS INC, 526 INDUSTRIAL WAY W, EATONTOWN, NY 07742-2212
51406
MURATA ERIE NORTH AMERICA INC HEADQUARTERS AND GEORGIA OPNS, 2200 LAKE PARK DR, SMYRNA, GA 30080
52828
REPUBLIC FASTENER MFG. CORP, 1300 RANCHO CONEJO BLVD, NEWBURY PARK, CA 91320-1405
55285
THE BERGQUIST COMPANY, 18930 W 78TH ST, CHANHASSEN, MN 55317-8728
55322
SAMTEC INC, 520 PARK E BLVD, NEW ALBANY, IN 47151-1147
55464
CENTRAL SEMICONDUCTOR CORP, 145 ADAMS AVE, HAUPPAUGE, NY 11788-3603
55680
NICHICON AMERICA CORP, 927 E STATE PKY, SCHAUMBURG, IL 60195-4526
56289
SPRAGUE ELECTRIC CO, 678 MAIN ST, SANFORD, ME 04073-7003
56501
THOMAS AND BETTS CORPORATION, 8155 T & B BLVD, MEMPHIS, TN 38125-8888
56563
PENTACON AEROSPACE GROUP, INC, 21123 NORDHOFF ST, CHATSWORTH, CA 91311
58625
LANDSDALE SEMICONDUCTOR, INC, 2412 HUNTINGTON DR, TEMPE, AZ 85282-3132
59124
KOA SPEER ELECTRONICS INC, P.O. BOX 547 BOLIVAR DR, BRADFORD, PA 16701
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10010 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Code
Vendor
59848
CERCON CASTING CORP, 201 CONSOLIDATED DR, HILLSBORO, TX 76645-0956
5X576
FINAL SPIN ENTERPRISES LLC, 181 NEWTOWN ROAD, PLAINVIEW, NY 11803-4306
62643
UNITED CHEMI-CON, INC, 9801 W HIGGINS RD STE 430, ROSEMONT, IL 60018-4725
65267
APPLIED ENGINEERING, INC, 2008 E HIGHWAY 50, YANKTON, SD 57078-6408
65590
UNIMTIC INC, 3501 RALEIGH AVE, MINNEAPOLIS, MN 55416-2625
6P860
E2V INC, 4 WESTCHESTER PLZ, ELMSFORD, NY 10523-1612
72962
HARVARD INDUSTRIES INC, LEBANON, NY 08833
7Y951
PEERLESS INSTRUMENT CO INC, 2030 COOLIDGE ST, HOLLYWOOD, FL 33020-2428
81349
MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
83826
STANLEY SPRING AND STAMPING CORP, 5050 W FOSTER AVE, CHICAGO, IL 60630-1614
8Y007
VWR SCIENTIFIC INC, 800 E FABYAN PKY, BATAVIA, IL 60510-1484
91637
VISHAY DALE ELECTRONICS, INC, 1122 23RD ST, COLUMBUS, NE 68601-3647
91929
HONEYWELL INTERNATIONAL INC, 11 WEST SPRING ST, FREEPORT, IL 61032-4316
99017
CAPLUGS LLC, 2150 ELMWOOD AVE, BUFFALO, NY 14207-1984
9H210
POSITIVE CONNECTOR CO, DERBY, CT06418
AAA42
FUSARO VITTORIO, VIA IV NOVEMBRE 14, SASSARI, ITALY 07100
AAC21
APCB (USA) INC, 2166 OLD MIDDLEFIELD WAY, MOUNTAIN VIEW, CA 94043
BAA66
AMERISTAR MFG INC, 2600 9TH AVE, MANKATO, MN 56001
BAF59
NMB CORP, 9730 INDEPENDENCE AVE, CHATSWORTH, CA 91311
BAF71
SGS-THOMSON MICROELECTRONICS INC, 1000 EAST BELL ROAD, PHOENIX, AZ 85022
BAG02
FLORIDA CROSS REFERENCE, 2100 NW 62ND STREET, FT. LAUDERDALE, FL 33309
L0375
NORANCO MANUFACTURING LTD, 1842 CLEMENTS RD, PICKERING, CANADA L1W 3R8
S5416
NEW JAPAN RADIO CO. LTD, MITSUYATORANOMON BLDG 22-14 TORANOMON 1-CHOME MINATO KU, TOKYO, JAPAN 105
S8185
PASSIVE ELECTRONICS SGP PTE LTD, 273 THOMSON ROAD 04-01 02-13 ANGMO K10 INDUSTRIAL PARK 2, SINGAPORE, SINGAPORE 307644
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10011 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10012 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
4.
Detailed Parts List
Equipment Designator Index EQUIPMENT DESIGNATOR
B1 B1 B4001 B4001 CJ4013 CJ4013 CJ4014 CJ4014 CJ4015 CJ4015 CJ4016 CJ4016 CJ4017 CJ4017 CJ4018 CJ4018 CJ4019 CJ4019 CJ5001 CJ5001 CJ5002 CJ5002 CJ5003 CJ5003 CJ5004 CJ5004 CJ5005 CJ5005 CR101 CR102 CR103 CR104 CR105 CR106 CR4001 CR4001 CR4004 CR4004 CR4005 CR4005 CR4008 CR4008 CR4009 CR4009 CR4010 CR4010 CR4015
EFFECTIVITY ALL
FIG. ITEM
7 8 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 2 2A 2 2A 2 2A 2 2A 2 2A 13 13 13 13 13 13 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3
50 50 265 265 665 665 665 665 665 665 665 665 665 665 665 665 665 665 870 870 870 870 870 870 870 870 870 870 10 10 10 10 10 55 325 325 325 355 325 325 330 330 325 325 325 325 350
GEOGRAPHIC LOCATION
5G 5G 2V 2V 2X 2X 5J 5J 4K 4K 7U 7U 5AA 5AA 6W 6W 7F 7F 6G 6G 6G 6G 6G 6G 7G 7G 3J 3K 3J 3J 3K 3K 3E 3E 4H 4H 1F 1F 4E 4E 3E 3E 4H 4H 5K
EQUIPMENT DESIGNATOR
CR4015 CR4016 CR4016 CR4017 CR4017 CR4018 CR4018 CR4021 CR4021 CR4022 CR4022 CR4025 CR4025 CR4026 CR4026 CR4030 CR4030 CR4031 CR4031 CR4034 CR4034 CR4036 CR4036 CR4037 CR4037 CR4038 CR4038 CR4039 CR4039 CR4040 CR4040 CR4041 CR4041 CR5002 CR5002 CR5003 CR5003 CR5004 CR5004 CR5005 CR5005 CR5006 CR5006 CR5007 CR5007 CR5008 CR5008
FIG. ITEM
3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
350 350 350 350 350 350 350 330 330 320 320 350 350 350 350 330 330 330 330 330 335 330 330 330 330 315 315 705 705 350 350 345 345 95 95 95 95 95 95 100 100 100 100 100 100 85 85
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
5K 4K 4K 5J 5J 6K 6K 3E 3E 6J 6J 4K 4K 4K 4K 4E 4E 6U 6U 4E 4E 4K 4K 4F 4F 4E 4E 3E 3E 4G 4G 5J 5J 6G 6G 6G 6G 6F 6F 7H 7H 7H 7H 7H 7H 7H 7H
Page 10013 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
CR5009 CR5009 CR5010 CR5010 CR5011 CR5011 CR5012 CR5012 CR5013 CR5013 CR5014 CR5014 CR5015 CR5015 CR5016 CR5016 CR5017 CR5017 CR5018 CR5018 CR5019 CR5019 CR5020 CR5020 CR5021 CR5021 CR5022 CR5022 C101 C102 C1001 C1001 C1002 C1002 C1003 C1003 C1004 C1004 C4004 C4004 C4005 C4005 C4006 C4006 C4007 C4007 C4008 C4008
EFFECTIVITY ALL
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 13 13 5 5A 5 5A 5 5A 5 5A 3 3A 3 3A 3 3A 3 3A 3 3A
100 100 100 100 95 95 100 100 90 90 95 95 790 790 105 105 80 80 80 80 95 95 80 80 95 95 95 95 20 25 30 30 35 35 20 20 25 25 540 540 560 560 525 525 515 515 555 555
GEOGRAPHIC LOCATION
7G 7G 7J 7J 6D 6D 7H 7H 7H 7H 5E 5E 6H 6H 5H 5H 5G 5G 5J 5J 6E 6E 6H 6H 6H 6H 6D 6D 4J 3H 4F 4F 5F 5F 4K 4K 4F 4F 5Y 5Y 5Y 5Y 3U 3U 4Y 4Y 5Y 5Y
EQUIPMENT DESIGNATOR
C4009 C4009 C4010 C4010 C4011 C4011 C4012 C4012 C4013 C4013 C4014 C4014 C4016 C4017 C4018 C4018 C4019 C4019 C4020 C4020 C4021 C4021 C4023 C4023 C4024 C4024 C4025 C4025 C4026 C4026 C4027 C4027 C4028 C4028 C4029 C4029 C4030 C4030 C4031 C4031 C4032 C4032 C4033 C4033 C4034 C4034 C4035 C4035
FIG. ITEM
3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3A 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A
480 480 525 525 495 495 575 575 495 495 525 525 510 450 425 425 490A 490A 525 525 510 510 525 525 525 525 525 525 525 525 525 525 525 525 525 525 480 480 515 515 525 525 460 460 445 445 500 500
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
4K 4K 3U 3U 4J 4J 2F 2F 6J 6J 4Y 4Y 4W 4X 5H 5H 2F 2F 4W 4W 5Y 5Y 4U 4U 4Z 4Z 5V 5V 4Z 4Z 5V 5V 4X 4X 5X 5X 6H 6H 6W 6W 5Z 5Z 6F 6F 4J 4J 5J 5J
Page 10014 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
C4036 C4036 C4037 C4037 C4038 C4038 C4039 C4039 C4040 C4040 C4041 C4041 C4042 C4042 C4043 C4043 C4044 C4044 C4045 C4045 C4046 C4046 C4047 C4047 C4049 C4049 C4050 C4050 C4051 C4051 C4052 C4052 C4053 C4053 C4054 C4054 C4055 C4055 C4056 C4056 C4057 C4057 C4058 C4058 C4059 C4059 C4060 C4060
EFFECTIVITY ALL
FIG. ITEM
3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A
460 460 445 445 500 500 420 420 525 525 525 525 480 480 245 515 475 475 465 465 525 525 525 525 480 480 430 455 525 525 525 525 435 435 475 475 485 485 435 435 440 440 470 470 525 525 525 525
GEOGRAPHIC LOCATION
6K 6K 5J 5J 6J 6J 3K 3K 3V 3V 3V 3V 6G 6G 6J 6J 6G 6G 5H 5H 5E 5E 5F 5F 6H 6H 3J 3J 3Z 3Z 5AA 5AA 4E 4E 6G 6G 4K 4K 4E 4E 4E 4E 3J 3J 4E 4E 5E 5E
EQUIPMENT DESIGNATOR
C4061 C4061 C4062 C4062 C4063 C4063 C4064 C4064 C4065 C4065 C4066 C4066 C4067 C4067 C4068 C4068 C4069 C4069 C4070 C4070 C4073 C4073 C4074 C4074 C4095 C4095 C4096 C4096 C4097 C4097 C4098 C4098 C4099 C4099 C4100 C4100 C4101 C4101 C4102 C4102 C4109 C4109 C4119 C4119 C4120 C4120 C4122 C4122
FIG. ITEM
3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A
525 525 525 525 355 855 355 855 470 470 525 550 525 550 525 525 525 525 525 525 430 455 430 455 500 500 500 500 535 535 535 535 535 535 535 535 570 570 570 570 525 525 525 525 525 525 500 500
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
2V 2V 5E 5E 4K 4K 4K 4K 6H 6H 5U 5U 4U 4U 6Y 6Y 5F 5F 6X 6X 6H 6H 4H 4H 6F 6F 6E 6E 6Y 6Y 6E 6E 6Y 6Y 6X 6X 5D 5D 5D 5D 2U 2U 5U 5U 2V 2V 6G 6G
Page 10015 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
C4123 C4123 C4124 C4124 C4125 C4125 C4126 C4126 C4127 C4127 C4128 C4128 C4129 C4129 C4132 C4132 C4133 C4133 C4134 C4134 C4136 C4136 C4137 C4137 C4138 C4138 C4139 C4139 C4140 C4140 C4141 C4141 C4142 C4142 C4143 C4143 C4144 C4144 C4145 C4145 C4146 C4146 C4149 C4149 C4152 C4152 C4153 C4153
EFFECTIVITY ALL
FIG. ITEM
3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A
535 535 535 535 500 500 535 535 535 535 570 570 570 570 525 525 525 525 480 480 565 565 505 505 430 430 515 515 520 520 450 450 515 515 525 525 530 530 545 545 545 545 525 525 525 525 525 525
GEOGRAPHIC LOCATION
6X 6X 6X 6X 5H 5H 6W 6W 6W 6W 5F 5F 5F 5F 5U 5U 5F 5F 3J 3J 6V 6V 4Z 4Z 6H 6H 4U 4U 4F 4F 5J 5J 6V 6V 4V 4V 3V 3V 3V 3V 2V 2V 4Y 4Y 3V 3V 6E 6E
EQUIPMENT DESIGNATOR
C4154 C4154 C4155 C4155 C4156 C4156 C4157 C4157 C5001 C5001 C5002 C5002 C5003 C5003 C5004 C5004 C5005 C5005 C5006 C5006 C5007 C5007 C5008 C5008 C5009 C5009 C5010 C5010 C5011 C5011 C5012 C5012 C5013 C5013 C5014 C5014 C5015 C5015 C5016 C5016 C5017 C5017 C5018 C5018 C5019 C5019 C5020 C5020
FIG. ITEM
3 3A 3 3A 3 3A 3 3A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
525 525 525 525 525 525 525 525 255 255 340 340 340 340 340 340 245 245 240 240 340 340 340 340 245 245 935 935 935 935 935 935 935 935 325 325 325 325 325 325 325 325 325 325 325 325 325 325
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
6X 6X 6W 6W 6X 6X 5V 5V 7D 7D 6AA 6AA 6Y 6Y 6Z 6Z 6F 6F 6F 6F 6Y 6Y 6Y 6Y 6F 6F 7AA 7AA 7AA 7AA 7AA 7AA 7AA 7AA 7Z 7Z 7Y 7Y 7Y 7Y 7Y 7Y 7Y 7Y 7Z 7Z 7Z 7Z
Page 10016 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
C5021 C5021 C5022 C5022 C5023 C5023 C5024 C5024 C5025 C5025 C5026 C5026 C5027 C5027 C5028 C5028 C5029 C5029 C5030 C5030 C5031 C5031 C5032 C5032 C5033 C5033 C5034 C5034 C5035 C5035 C5036 C5036 C5037 C5037 C5038 C5038 C5039 C5039 C5041 C5041 C5042 C5042 C5043 C5043 C5044 C5044 C5045 C5045
EFFECTIVITY ALL
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
325 325 325 325 325 325 325 325 335 335 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 250 250 250 250 330 330 335 335 250 250 330 330 260 260 345 345 250 250
GEOGRAPHIC LOCATION
7Z 7Z 7Z 7Z 7E 7E 7U 7U 1W 1W 1J 1J 3AA 3AA 3Z 3Z 3Z 3Z 2Z 2Z 2Z 2Z 3Z 3Z 3Z 3Z 4Z 4Z 7K 7K 6E 6E 6AA 6AA 2K 2K 1W 1W 5AA 5AA 7K 7K 1H 1H 6X 6X 5AA 5AA
EQUIPMENT DESIGNATOR
C5046 C5046 C5047 C5047 C5048 C5048 C5049 C5049 C5050 C5050 C5051 C5051 C5052 C5052 C5053 C5053 C5054 C5054 C5056 C5056 C5057 C5057 C5058 C5058 C5059 C5059 C5061 C5061 C5062 C5062 C5063 C5063 C5064 C5064 C5065 C5065 C5069 C5069 C5070 C5070 C5071 C5071 C5073 C5073 C5074 C5074 C5076 C5076
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
270 270 250 250 330 330 330 330 340 340 330 330 330 330 330 330 330 330 250 250 335 335 260 260 250 250 270 270 335 335 260 260 325 325 340 340 255 255 340 340 340 340 340 340 340 340 340 340
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
5E 5E 5AA 5AA 6W 6W 6L 6L 5Y 5Y 7U 7U 4W 4W 4H 4H 6W 6W 5AA 5AA 2V 2V 2K 2K 5D 5D 5E 5E 1W 1W 1H 1H 7V 7V 7W 7W 6D 6D 6E 6E 7J 7J 7W 7W 7H 7H 6H 6H
Page 10017 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
C5078 C5078 C5079 C5079 C5080 C5080 C5081 C5081 C5082 C5082 C5083 C5083 C5084 C5084 C5085 C5085 C5086 C5086 C5087 C5087 C5088 C5088 C5089 C5089 C5090 C5090 C5091 C5091 C5093 C5093 C5094 C5094 C5095 C5095 C5096 C5096 C5097 C5097 C5098 C5098 C5099 C5099 C5100 C5100 C5101 C5101 C5102 C5102
EFFECTIVITY ALL
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
340 340 340 340 340 340 340 340 340 340 340 340 340 340 250 250 340 340 340 340 340 340 340 340 260 260 340 340 335 335 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340
GEOGRAPHIC LOCATION
6W 6W 6AA 6AA 6AA 6AA 6G 6G 6AA 6AA 6AA 6AA 6X 6X 6AA 6AA 6G 6G 6X 6X 6H 6H 6W 6W 6H 6H 5W 5W 1J 1J 4Y 4Y 4Z 4Z 3Y 3Y 3Y 3Y 2Y 2Y 2Y 2Y 1X 1X 1W 1W 2W 2W
EQUIPMENT DESIGNATOR
C5103 C5103 C5104 C5104 C5105 C5105 C5106 C5106 C5107 C5107 C5108 C5108 C5109 C5109 C5110 C5110 C5111 C5111 C5112 C5112 C5113 C5113 C5114 C5114 C5115 C5115 C5116 C5116 C5117 C5117 C5118 C5118 C5119 C5119 C5120 C5120 C5121 C5121 C5122 C5122 C5123 C5123 C5124 C5124 C5125 C5125 C5126 C5126
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
3W 3W 3W 3W 4W 4W 5Y 5Y 3W 3W 2W 2W 1V 1V 3X 3X 3Y 3Y 7V 7V 5H 5H 5Y 5Y 3X 3X 7K 7K 5W 5W 5Y 5Y 5Y 5Y 4Y 4Y 6Y 6Y 5Z 5Z 4Z 4Z 4AA 4AA 4AA 4AA 7Z 7Z
Page 10018 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
C5127 C5127 C5128 C5128 C5129 C5129 C5130 C5130 C5131 C5131 C5132 C5132 C5133 C5133 C5134 C5134 C5135 C5135 C5136 C5136 C5137 C5137 C5138 C5138 C5139 C5139 C5140 C5140 C5141 C5141 C5142 C5142 C5145 C5145 C5146 C5146 C5147 C5147 C5148 C5148 C5149 C5149 C5150 C5150 C5151 C5151 C5152 C5152
EFFECTIVITY ALL
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340 340
GEOGRAPHIC LOCATION
1V 1V 5X 5X 6X 6X 3AA 3AA 4W 4W 7U 7U 3W 3W 6Y 6Y 6X 6X 6AA 6AA 6AA 6AA 6Z 6Z 5Z 5Z 4Z 4Z 4Z 4Z 5AA 5AA 4Y 4Y 5Z 5Z 6AA 6AA 5AA 5AA 5Z 5Z 7U 7U 6Y 6Y 6X 6X
EQUIPMENT DESIGNATOR
C5153 C5153 C5154 C5154 C5155 C5155 C5156 C5156 C5158 C5158 C5160 C5160 C5161 C5161 C5163 C5163 C5164 C5164 C5165 C5165 C5501 C5501 C5502 C5502 C5503 C5503 C5504 C5504 C5505 C5505 C5506 C5506 C5507 C5507 C5508 C5508 C5509 C5509 C5510 C5510 C5511 C5511 C5512 C5512 C5513 C5513 C5514 C5514
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
340 340 340 340 340 340 340 340 340 340 275 275 275 275 255 255 325 325 320 320 305 305 295 295 280 280 300 300 630 630 630 630 625 625 630 630 630 630 665 665 630 630 630 630 630 630 665 665
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
6AA 6AA 5Z 5Z 5AA 5AA 4W 4W 7U 7U 6D 6D 7G 7G 6G 6G 7U 7U 5E 5E 5K 5K 5K 5K 5K 5K 5K 5K 4K 4K 4K 4K 6J 6J 4J 4J 4J 4J 4J 4J 3K 3K 3K 3K 3J 3J 3J 3J
Page 10019 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
C5515 C5515 C5516 C5516 C5517 C5517 C5518 C5518 C5519 C5519 C5520 C5520 C5521 C5521 C5523 C5523 C5524 C5524 C5525 C5525 C5526 C5526 C5527 C5527 C5528 C5528 C5529 C5529 C5530 C5530 C5531 C5531 C5532 C5532 C5533 C5533 C5534 C5534 C5535 C5535 C5536 C5536 C5537 C5537 C5538 C5538 C5539 C5539
EFFECTIVITY ALL
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
630 630 630 630 670 670 630 630 265 265 630 630 635 635 630 630 630 630 635 635 630 630 285 285 310 310 310 310 630 630 630 630 630 630 655 655 630 630 630 630 630 630 630 630 655 655 630 630
GEOGRAPHIC LOCATION
3K 3K 3K 3K 3J 3J 3K 3K 3J 3J 2J 2J 2J 2J 6L 6L 2K 2K 2J 2J 4W 4W 6K 6K 6J 6J 5J 5J 6K 6K 6L 6L 6L 6L 6K 6K 5K 5K 5K 5K 5L 5L 5L 5L 5K 5K 4L 4L
EQUIPMENT DESIGNATOR
C5540 C5540 C5541 C5541 C5542 C5542 C5543 C5543 C5544 C5544 C5545 C5545 C5551 C5551 C5567 C5567 C5568 C5568 C5572 C5572 C5574 C5574 C5575 C5575 C5576 C5576 C5577 C5577 C5578 C5578 C5584 C5584 C5587 C5587 C5588 C5588 C5589 C5589 E1005 E1006 E4003 E4003 E4004 E4004 E4005 E4006 FL5001 FL5001
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 5A 5A 3 3A 3 3A 3 3 2 2A
630 630 630 630 290 290 310 310 645 645 630 630 630 630 630 630 650 650 630 630 625 625 625 625 315 315 640 640 640 640 660 660 630 630 630 630 630 630 45 5 360 360 360 360 360 360 150 150
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
4K 4K 4K 4K 4K 4K 5K 5K 6K 6K 6K 6K 3J 3J 5K 5K 5K 5K 5K 5K 4K 4K 5K 5K 4K 4K 3L 3L 3L 3L 6K 6K 4K 4K 6W 6W 6J 6J 5D 4D 4G 4G 4G 4G 5H 5G 5H 5H
Page 10020 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
F4001 F4001 J101 J1001 J1002 J1002 J4001 J4001 J4002 J4002 J4003 J4003 J5001 J5001 J5002 J5002 J5004 J5004 J5005 J5005 J5006 J5006 J5502 J5502 L1001 L1001 L4001 L4001 L4003 L4003 L4004 L4004 L4005 L4005 L4006 L4006 L4007 L4007 L4008 L4008 L4009 L4009 L5001 L5001 L5002 L5002 L5004 L5004
EFFECTIVITY ALL
FIG. ITEM
3 3A 13 5 5 5A 3 3A 3 3A 3 3A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 5 5A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 2 2A 2 2A 2 2A
410 410 15 5 15 15 400 400 405 405 405 405 215A 215 35 35 205 205 210 210 210 210 200 200 10 10 380 380 380 380 380 380 375 375 375 375 375 375 375 375 370 370 125 125 125 125 120 120
GEOGRAPHIC LOCATION
5J 5J 4F 4D 4E 4E 5Y 5Y 6E 6E 6F 6F 7H 7H 6F 6F 6J 6J 6E 6E 6E 6E 6K 6K 5D 5D 5K 5K 3F 3F 4E 4E 4H 4H 2H 2H 4J 4J 4H 4H 2F 2F 6J 6J 6G 6G 2K 2K
EQUIPMENT DESIGNATOR
L5005 L5005 L5006 L5006 L5008 L5008 L5014 L5014 L5016 L5016 L5017 L5017 L5018 L5018 L5019 L5019 L5501 L5501 L5502 L5502 L5504 L5504 L5505 L5505 L5506 L5506 L5507 L5507 L5523 L5523 L5524 L5524 L5525 L5525 L5526 L5526 L5527 L5527 L5534 L5534 L5536 L5536 L5537 L5537 L5538 L5538 L5539 L5539
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
120 120 120 120 120 120 120 120 115 115 115 115 120 120 120 120 155 155 155 155 180 180 180 180 165 165 180 180 180 180 160 160 180 180 180 180 180 180 180 180 185 185 170 170 170 170 175 175
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
6L 6L 4J 4J 6J 6J 6J 6J 6J 6J 4H 4H 4J 4J 6J 6J 6G 6G 5J 5J 4J 4J 3J 3J 3J 3J 3K 3K 4L 4L 4K 4K 4K 4K 5L 5L 6K 6K 5K 5K 6K 6K 5K 5K 5K 5K 5K 5K
Page 10021 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
P2 P3 P5 P6 Q4001 Q4001 Q4002 Q4003 Q4004 Q4004 Q4007 Q4007 Q4010 Q4010 Q4015 Q4015 Q4017 Q4017 Q4018 Q4018 Q4019 Q4019 Q4020 Q4020 Q4021 Q4021 Q4022 Q4022 Q4023 Q4023 Q4026 Q4026 Q4027 Q4027 Q4028 Q4028 Q5001 Q5001 Q5002 Q5002 Q5003 Q5003 Q5004 Q5004 Q5005 Q5005 Q5006 Q5006
EFFECTIVITY ALL
FIG. ITEM
8 7 10 11 3 3A 3 3 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
10 10 45 60 270 270 340 140 270 270 310 310 340 340 340 340 290 290 305 305 285 285 295 295 280 280 340 340 290 290 285 285 300 300 340 340 145 145 65 65 145 145 65 65 145 145 65 65
GEOGRAPHIC LOCATION
3G 3G 4G 4G 3H 3H 3G 3G 4Y 4Y 4E 4E 6V 6V 7V 7V 6U 6U 5H 5H 7U 7U 4E 4E 4D 4D 4K 4K 4K 4K 4Y 4Y 7F 7F 6F 6F 7F 7F 6F 6F 7F 7F 6F 6F
EQUIPMENT DESIGNATOR
Q5007 Q5007 Q5008 Q5008 Q5009 Q5009 Q5010 Q5010 Q5011 Q5011 Q5012 Q5012 Q5013 Q5013 Q5014 Q5014 Q5015 Q5015 Q5016 Q5016 Q5017 Q5017 Q5018 Q5018 Q5019 Q5019 Q5020 Q5020 Q5021 Q5021 Q5022 Q5022 Q5023 Q5023 Q5024 Q5024 Q5501 Q5501 Q5502 Q5502 Q5503 Q5503 R101 R102 R103 R104 R105 R106
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 13 13 13 13 13 13
145 145 65 65 145 145 65 65 145 145 65 65 145 145 65 65 145 145 65 65 145 145 65 65 145 145 65 65 65 65 145 145 65 65 145 145 70 70 70 70 75 75 35 40 50 50 50 40
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
7F 7F 7F 7F 7E 7E 6E 6E 7E 7E 6E 6E 7E 7E 6E 6E 7E 7E 7E 7E 7E 7E 7E 7E 7E 7E 7E 7E 7E 7E 7E 7E 7D 7D 7D 7D 3J 3J 3J 3J 2J 2J 4K 3F 3E 3F 3F 3F
Page 10022 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
R107 R1001 R1001 R1002 R1002 R1003 R1003 R1004 R1004 R1005 R1005 R1006 R1006 R1007 R1007 R1008 R1008 R4003 R4004 R4005 R4006 R4006 R4008 R4008 R4009 R4009 R4010 R4010 R4011 R4011 R4012 R4012 R4013 R4013 R4014 R4014 R4015 R4015 R4016 R4016 R4020 R4020 R4021 R4021 R4022 R4022 R4023 R4023
EFFECTIVITY ALL
FIG. ITEM
13 5 5A 5 5A 5 5A 5 5A 5 5A 5 5A 5 5A 5 5A 3 3 3 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A
45 80 85 70 75 65 70 75 80 60 65 60 65 60 65 60 65 235 735 585 720 720 745 740 780 780 725 725 735 735 835 835 685 685 675 675 680 680 710 710 710 710 795 795 190 190 145 145
GEOGRAPHIC LOCATION
3K 4F 4F 4G 4G 4G 4G 5G 5G 5J 5J 5J 5J 5G 5G 5J 5J 4X 4X 5X 4W 4W 5Y 5Y 4Y 4Y 4W 4W 5Y 5Y 4W 4W 4G 4G 2F 2F 4H 4H 3J 3J 3J 3J 3U 3U 5X 5X 5X 5X
EQUIPMENT DESIGNATOR
R4024 R4024 R4028 R4028 R4029 R4029 R4030 R4030 R4031 R4031 R4032 R4032 R4033 R4033 R4036 R4036 R4037 R4037 R4050 R4050 R4051 R4051 R4052 R4052 R4053 R4053 R4054 R4054 R4059 R4059 R4060 R4060 R4061 R4061 R4062 R4062 R4063 R4063 R4064 R4064 R4066 R4066 R4067 R4067 R4068 R4068 R4069 R4069
FIG. ITEM
3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A
150 150 770 770 585 850 670 670 670 670 735 735 165 165 670 670 670 670 225 225 220 220 335 225 220 235 255 255 800 800 195 195 735 735 195 195 550 865 165 165 810 810 185 185 585 850 455 860
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
5X 5X 3V 3V 3V 3V 5Z 5Z 5Y 5Y 4X 4X 5Y 5Y 5Y 5Y 5Y 5Y 6W 6W 6V 6V 6V 6V 6V 6V 6V 6V 5Z 5Z 4Z 4Z 4Y 4Y 4Y 4Y 4Y 4Y 4Y 4Y 6V 6V 6V 6V 4Z 4Z 6V 6V
Page 10023 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
R4070 R4070 R4071 R4071 R4074 R4074 R4077 R4077 R4078 R4078 R4079 R4079 R4080 R4080 R4081 R4081 R4084 R4084 R4086 R4086 R4087 R4087 R4088 R4088 R4089 R4089 R4090 R4090 R4091 R4091 R4092 R4092 R4093 R4093 R4094 R4094 R4096 R4096 R4097 R4097 R4098 R4098 R4102 R4102 R4107 R4107 R4108 R4108
EFFECTIVITY ALL
FIG. ITEM
3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A
170 170 740 740 805 805 170 170 275 275 820 820 260 260 820 820 845 845 745 745 275 275 175 175 790 790 745 745 745 745 745 745 825 825 205 205 210 210 735 735 165 165 195 195 240 240 750 750
GEOGRAPHIC LOCATION
3Y 3Y 6U 6U 6W 6W 4U 4U 5V 5V 5V 5V 4V 4V 4U 4U 5F 5F 6W 6W 6G 6G 6W 6W 6W 6W 6W 6W 6W 6W 6W 6W 6G 6G 6W 6W 6V 6V 6U 6U 4Y 4Y 4Z 4Z 5X 5X 4F 4F
EQUIPMENT DESIGNATOR
R4109 R4109 R4110 R4110 R4111 R4111 R4135 R4135 R4136 R4136 R4137 R4137 R4138 R4138 R4139 R4139 R4140 R4140 R4141 R4141 R4142 R4142 R4143 R4143 R4158 R4158 R4161 R4161 R4162 R4162 R4163 R4163 R4164 R4164 R4165 R4165 R4166 R4166 R4169 R4169 R4170 R4170 R4173 R4173 R4175 R4175 R4176 R4176
FIG. ITEM
3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A
180 180 740 740 740 740 175 175 740 740 740 740 735 735 670 670 670 670 735 735 670 670 670 670 160 160 735 735 670 670 670 670 670 670 670 670 735 735 175 175 230 230 735 735 735 735 735 735
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
4F 4F 5F 5F 5F 5F 6Z 6Z 5F 5F 5Z 5Z 6Y 6Y 5Z 5Z 6Z 6Z 5D 5D 5Z 5Z 5Z 5Z 5F 5F 5F 5F 5Y 5Y 5X 5X 5Y 5Y 5Y 5Y 6X 6X 5Z 5Z 4Z 4Z 5Y 5Y 4W 3Y 2V 2V
Page 10024 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
R4178 R4178 R4179 R4180 R4180 R4181 R4181 R4182 R4182 R4183 R4183 R4185 R4185 R4186 R4186 R4187 R4187 R4188 R4188 R4189 R4189 R4190 R4190 R4191 R4191 R4192 R4192 R4195 R4195 R4196 R4196 R4197 R4197 R4198 R4198 R4199 R4199 R4200 R4200 R4201 R4201 R4202 R4202 R4203 R4203 R4204 R4204 R4205
EFFECTIVITY ALL
FIG. ITEM
3 3A 3 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3
735 735 735 735 735 735 735 735 735 735 735 700 700 785 785 200 200 745 745 815 815 165 165 160 160 755 755 690 690 735 735 735 735 155 155 735 735 695 695 260 275 840 840 740 740 165 165 735
GEOGRAPHIC LOCATION
4X 4X 5X 6X 6X 6G 6G 6T 6T 6U 6U 4J 4J 5U 5U 5U 5U 6W 6W 4Y 4Y 4Z 4Z 5U 5U 4X 4X 3J 3J 3U 3U 3U 3U 3U 3U 3U 3U 3J 3J 5V 5V 5U 5U 5V 5V 5V 5V 2V
EQUIPMENT DESIGNATOR
R4205 R4206 R4206 R4207 R4207 R4208 R4208 R4209 R4209 R4210 R4210 R4211 R4211 R4212 R4212 R4213 R4213 R4214 R4214 R4215 R4215 R4216 R4216 R4219 R4219 R4220 R4220 R4221 R4221 R4222 R4222 R4223 R4223 R4224 R4224 R4225 R4225 R4226 R4226 R4227 R4227 R4228 R4228 R4229 R4229 R4230 R4230 R4231
FIG. ITEM
3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3
735 215 215 735 735 765 765 585 850 830 830 740 740 775 775 760 760 820 155 740 740 740 740 165 165 740 740 735 735 250 250 740 740 735 735 775 775 175 175 175 245 170 170 175 175 740 740 730
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
2V 3V 3V 2V 2V 2V 2V 3U 3U 5U 5U 5V 5V 5U 5U 5V 5V 3U 3U 5E 5E 5E 5E 4Z 4Z 5E 5E 3U 3U 5U 5U 5V 5V 5V 5V 5J 5J 6U 6U 6U 6U 4Y 4Y 3V 3V 3V 3V 5V
Page 10025 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
R4231 R4232 R4233 R4235 R5001 R5001 R5002 R5002 R5003 R5003 R5006 R5006 R5007 R5007 R5008 R5008 R5009 R5009 R5010 R5010 R5011 R5011 R5012 R5012 R5013 R5013 R5014 R5014 R5015 R5015 R5016 R5016 R5017 R5017 R5018 R5018 R5019 R5019 R5020 R5020 R5021 R5021 R5022 R5022 R5023 R5023 R5024 R5024
EFFECTIVITY ALL
FIG. ITEM
3A 3A 3A 3A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
730 165 735 710 930 930 930 930 930 930 505 505 930 930 520 520 505 505 410 410 130 130 930 930 505 505 410 410 430 430 410 410 595 595 140 140 140 140 470 470 370 370 370 370 410 410 430 430
GEOGRAPHIC LOCATION
5V 4Y 6U 3H 4AA 4AA 4AA 4AA 3Z 3Z 1W 1W 3AA 3AA 4AA 4AA 3W 3W 5Z 5Z 7K 7K 2E 2E 3W 3W 6Z 6Z 6F 6F 6Y 6Y 6Y 6Y 7F 7F 7E 7E 5Z 5Z 6Y 6Y 6Y 6Y 6Y 6Y 6Y 6Y
EQUIPMENT DESIGNATOR
R5025 R5025 R5026 R5026 R5028 R5028 R5029 R5029 R5030 R5030 R5031 R5031 R5032 R5032 R5033 R5033 R5035 R5035 R5037 R5037 R5038 R5038 R5039 R5039 R5040 R5040 R5041 R5041 R5042 R5042 R5043 R5043 R5044 R5044 R5045 R5045 R5046 R5046 R5047 R5047 R5048 R5048 R5049 R5049 R5051 R5051 R5052 R5052
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
410 410 595 595 465 465 940 940 485 485 480 480 525 525 930 930 455 455 135 135 925 925 900 900 900 900 925 925 420 420 420 420 415 415 370 370 965 965 965 965 370 370 415 415 505 505 930 930
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
6F 6F 6Y 6Y 6H 6H 6W 6W 6E 6E 6F 6F 5E 5E 5F 5F 4AA 4AA 7D 7D 7AA 7AA 7AA 7AA 7AA 7AA 7AA 7AA 7Z 7Z 7Z 7Z 7Z 7Z 7Z 7Z 7Z 7Z 7E 7E 7E 7E 7Z 7Z 7Y 7Y 7Y 7Y
Page 10026 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
R5053 R5053 R5054 R5054 R5055 R5055 R5056 R5056 R5057 R5057 R5058 R5058 R5059 R5059 R5060 R5060 R5061 R5061 R5062 R5062 R5063 R5063 R5064 R5064 R5065 R5065 R5066 R5066 R5067 R5067 R5068 R5068 R5069 R5069 R5070 R5070 R5071 R5071 R5072 R5072 R5073 R5073 R5074 R5074 R5075 R5075 R5076 R5076
EFFECTIVITY ALL
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
515 515 515 515 515 515 515 515 950 950 435 435 370 370 500 500 495 495 555 555 410 410 360 360 365 365 410 390 930 930 930 930 930 930 500 500 505 505 930 930 505 505 930 930 955 955 620 620
GEOGRAPHIC LOCATION
6X 6X 6X 6X 6Y 6Y 6X 6X 6X 6X 6X 6X 6X 6X 4W 4W 7U 7U 4W 4W 7U 7U 7Y 7Y 7K 7K 7K 7K 7U 7U 7Y 7Y 7U 7U 7U 7U 3X 3X 4X 4X 3X 3X 3X 3X 4Z 4Z 6E 6E
EQUIPMENT DESIGNATOR
R5077 R5077 R5078 R5078 R5079 R5079 R5080 R5080 R5081 R5081 R5082 R5082 R5083 R5083 R5084 R5084 R5085 R5085 R5086 R5086 R5087 R5087 R5088 R5088 R5089 R5089 R5090 R5090 R5091 R5091 R5092 R5092 R5093 R5093 R5094 R5094 R5095 R5095 R5096 R5096 R5097 R5097 R5098 R5098 R5099 R5099 R5100 R5100
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
520 520 930 930 930 930 930 930 930 930 520 520 930 930 930 930 375 375 930 930 555 555 515 515 520 520 930 930 930 930 590 590 925 925 945 945 410 410 930 930 930 930 560 560 925 925 945 945
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
4X 4X 6Z 6Z 6E 6E 6Z 6Z 6Z 6Z 6Z 6Z 6E 6E 7V 7V 7U 7U 5D 5D 7U 7U 5AA 5AA 5AA 5AA 6AA 6AA 6D 6D 7U 7U 6Z 6Z 6Z 6Z 7U 7U 5Z 5Z 5E 5E 5AA 5AA 6Z 6Z 6E 6E
Page 10027 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
R5101 R5101 R5102 R5102 R5103 R5103 R5104 R5104 R5105 R5105 R5106 R5106 R5107 R5107 R5108 R5108 R5111 R5111 R5112 R5112 R5113 R5113 R5114 R5114 R5115 R5115 R5116 R5116 R5119 R5119 R5120 R5120 R5121 R5121 R5122 R5122 R5123 R5123 R5125 R5125 R5126 R5126 R5127 R5127 R5128 R5128 R5130 R5130
EFFECTIVITY ALL
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
930 930 930 930 930 930 520 520 930 930 930 930 535 535 520 520 930 930 930 930 560 560 925 925 945 945 930 930 505 505 505 505 505 505 505 505 930 930 455 455 405 405 420 420 930 930 875 875
GEOGRAPHIC LOCATION
6E 6E 5D 5D 5D 5D 5AA 5AA 5D 5D 5AA 5AA 5AA 5AA 5AA 5AA 5D 5D 5AA 5AA 6Z 6Z 6Z 6Z 6Z 6Z 6Z 6Z 5Y 5Y 5X 5X 5X 5X 5X 5X 2W 2W 4AA 4AA 6W 6W 5Y 5Y 5Y 5Y 5W 5W
EQUIPMENT DESIGNATOR
R5131 R5131 R5132 R5132 R5133 R5133 R5137 R5137 R5138 R5138 R5139 R5139 R5140 R5140 R5141 R5141 R5150 R5150 R5151 R5151 R5152 R5152 R5153 R5153 R5155 R5155 R5157 R5157 R5158 R5158 R5159 R5159 R5160 R5160 R5165 R5165 R5166 R5166 R5167 R5167 R5168 R5168 R5170 R5170 R5171 R5171 R5172 R5172
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
875 875 600 600 930 930 925 925 510 510 925 925 925 925 925 925 380 380 960 960 930 930 930 930 930 930 520 520 440 440 610 610 890 890 930 930 460 375 520 520 605 605 930 930 925 925 930 930
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
5W 5W 6Z 6Z 6Z 6Z 6W 6W 6W 6W 6W 6W 6W 6W 6W 6W 6Y 6Y 6Y 6Y 4AA 4AA 4D 4D 2X 2X 2X 2X 6W 6W 6W 6W 6W 6W 3AA 3AA 7V 7V 7U 7U 7V 7V 7U 7U 6AA 6AA 7H 7H
Page 10028 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
R5173 R5173 R5174 R5174 R5175 R5175 R5176 R5176 R5177 R5177 R5178 R5178 R5179 R5179 R5180 R5180 R5181 R5181 R5182 R5182 R5183 R5183 R5184 R5184 R5185 R5185 R5186 R5186 R5187 R5187 R5188 R5188 R5189 R5189 R5190 R5190 R5191 R5191 R5192 R5192 R5195 R5195 R5210 R5210 R5221 R5221 R5222 R5222
EFFECTIVITY ALL
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
465 465 585 585 930 930 465 465 585 585 930 930 465 465 585 585 930 930 465 465 585 585 930 930 465 465 585 585 930 930 465 465 585 585 930 930 465 465 585 585 585 585 920 920 585 585 545 545
GEOGRAPHIC LOCATION
7W 7W 6W 6W 7H 7H 7W 7W 6H 6H 7G 7G 7X 7X 6X 6X 7H 7H 7X 7X 6H 6H 7G 7G 7X 7X 6X 6X 7G 7G 7X 7X 6G 6G 7H 7H 7W 7W 6W 6W 6H 6H 6D 6D 6AA 6AA 6D 6D
EQUIPMENT DESIGNATOR
R5223 R5223 R5224 R5224 R5225 R5225 R5226 R5226 R5227 R5227 R5228 R5228 R5229 R5229 R5230 R5230 R5231 R5231 R5232 R5232 R5233 R5233 R5234 R5234 R5247 R5247 R5249 R5249 R5250 R5250 R5258 R5258 R5259 R5259 R5260 R5260 R5262 R5262 R5263 R5263 R5264 R5264 R5265 R5265 R5266 R5266 R5267 R5267
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
580 580 540 540 475 475 520 520 550 550 550 550 550 550 550 550 550 550 550 550 550 550 550 550 580 580 930 930 460 460 930 930 425 425 395 395 930 930 930 930 465 465 585 585 930 930 465 465
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
5Z 5Z 4Z 4Z 5Z 5Z 6AA 6AA 6D 6D 6AA 6AA 6D 6D 6AA 6AA 6AA 6AA 5AA 5AA 5AA 5AA 5AA 5AA 5F 5F 5Z 5Z 5Z 5Z 6D 6D 7X 7X 6AA 6AA 6AA 6AA 7H 7H 7W 7W 7H 7H 7H 7H 7W 7W
Page 10029 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
R5268 R5268 R5269 R5269 R5270 R5270 R5271 R5271 R5272 R5272 R5273 R5273 R5274 R5274 R5275 R5275 R5276 R5276 R5278 R5278 R5279 R5279 R5280 R5280 R5281 R5281 R5282 R5282 R5283 R5283 R5284 R5284 R5285 R5285 R5289 R5289 R5290 R5290 R5291 R5291 R5292 R5292 R5294 R5294 R5295 R5295 R5296 R5296
EFFECTIVITY ALL
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
585 585 930 930 465 465 585 585 930 930 465 465 585 585 490 490 505 505 505 505 505 505 930 930 930 930 445 445 930 930 940 940 385 385 930 930 505 505 505 505 505 505 925 925 400 400 930 930
GEOGRAPHIC LOCATION
7W 7W 7J 7J 7W 7W 7H 7H 7J 7J 7V 7V 7V 7V 6AA 6AA 5Z 5Z 5Z 5Z 5Y 5Y 5Z 5Z 5Z 5Z 6Y 6Y 6Y 6Y 5F 5F 5F 5F 2Z 2Z 3Y 3Y 3Y 3Y 3Z 3Z 6AA 6AA 5E 5E 2Z 2Z
EQUIPMENT DESIGNATOR
R5297 R5297 R5299 R5299 R5501 R5501 R5502 R5502 R5503 R5503 R5505 R5505 R5506 R5506 R5507 R5507 R5508 R5508 R5509 R5509 R5510 R5510 R5511 R5511 R5512 R5512 R5514 R5514 R5525 R5525 R5527 R5527 R5529 R5529 R5530 R5530 R5531 R5531 R5532 R5532 R5533 R5533 R5534 R5534 R5535 R5535 R5536 R5536
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
930 930 520 520 445 445 395 395 445 445 395 395 445 445 515 515 915 915 570 570 350 350 880 880 880 880 930 930 490 490 490 490 920 920 920 920 565 565 450 450 890 890 530 530 510 510 510 510
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
2E 2E 6AA 6AA 4J 4J 4K 4K 4J 4J 3K 3K 3J 3J 3K 3K 3J 3J 3J 3J 3J 3J 6J 6J 6K 6K 2K 2K 6L 6L 5L 5L 5K 5K 5K 5K 5L 5L 5L 5L 4K 4K 4K 4K 4K 4K 4L 4L
Page 10030 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
R5537 R5537 R5538 R5538 R5539 R5539 R5540 R5540 R5541 R5541 R5544 R5544 R5548 R5548 R5550 R5550 R5551 R5551 R5552 R5552 R5555 R5555 R5556 R5556 R5557 R5557 R5558 R5558 R5559 R5559 R5560 R5560 SK5003 SK5003 SW5001 SW5001 TP4001 TP4001 TP4002 TP4002 TP4004 TP4004 TP4005 TP4007 TP4007 TP4008 TP4008 TP4009
EFFECTIVITY ALL
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 3 3A 3 3A 3 3A 3 3 3A 3 3A 3
510 510 355 355 575 575 930 930 930 930 930 930 930 930 905 905 890 890 895 895 920 920 965 965 930 930 930 930 930 930 910 910 225 225 220 220 365 365 365 365 365 365 365 365 365 365 365 365
GEOGRAPHIC LOCATION
4L 4L 4L 4L 4K 4K 3K 3K 3K 3K 3K 3K 3K 3K 2J 2J 6K 6K 6K 6K 6K 6K 3K 3K 3L 3L 3L 3L 3L 3L 3K 3K 2B 2B 8K 8K 3E 3E 3E 3E 4G 4G 4G 6F 6F 1H 1H 6G
EQUIPMENT DESIGNATOR
TP4009 TP4010 TP4010 TP4011 TP4011 TP4014 TP4014 TP4015 TP4015 TP4016 TP4016 TP4017 TP4017 TP4020 TP4020 TP4021 TP5001 TP5001 TP5002 TP5002 TP5003 TP5003 TP5004 TP5004 TP5005 TP5005 TP5006 TP5006 TP5007 TP5007 TP5008 TP5008 TP5010 TP5010 TP5011 TP5011 TP5012 TP5012 TP5013 TP5013 TP5015 TP5015 TP5018 TP5018 TP5019 TP5019 TP5020 TP5020
FIG. ITEM
3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
365 365 365 365 365 365 365 365 365 365 365 365 365 365 365 365 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110 110
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
6G 5K 5K 5K 5K 3J 3J 5H 5H 2J 2J 2J 2J 5H 5H 5K 3E 3E 4J 4J 4D 4D 2J 2J 1G 1G 6J 6J 6J 6J 3E 3E 5D 5D 4E 4E 5D 5D 6G 6G 6H 6H 1J 1J 2G 2G 5H 5H
Page 10031 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
TP5022 TP5022 TP5023 TP5023 TP5024 TP5024 TP5025 TP5025 TP5027 TP5027 TP5031 TP5031 TP5032 TP5032 T4001 T4001 T4002 T4002 T4005 T4005 T5501 T5501 T5502 T5502 U100 U100 U101 U102 U1001 U1001 U1002 U1002 U1003 U1003 U1004 U1004 U4001 U4001 U4002 U4002 U4003 U4005 U4005 U4006 U4006 U4008 U4008 U4008U4010
EFFECTIVITY ALL
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 3 3A 3 3A 3 3A 2 2A 2 2A 10 11 13 13 5 5A 5 5A 5 5A 5 5A 3 3A 3 3A 3A 3 3A 3 3A 3 3A 3
110 110 110 110 110 110 110 110 110 110 110 110 110 110 390 390 385 385 395 395 195 195 190 190 65 70 30 30 50 55 55 60 40 40 45 50 615 615 595 595 585 620 620 620 620 655 655 661
GEOGRAPHIC LOCATION
4D 4D 1H 1H 2F 2F 1F 1F 5G 5G 3E 3E 2E 2E 3F 3F 2G 2G 5K 5K 4J 4J 3J 3J
3E 3G 6E 6E 4J 4J 4J 4J 4L 4L 4F 4F 4F 4F 4G 7W 7W 7V 7V 3E 3E 5E
EQUIPMENT DESIGNATOR
U4008U4010 U4011 U4011 U4012 U4012 U4013 U4013 U4014 U4014 U4015 U4015 U4017 U4017 U4018 U4018 U4019 U4019 U4020 U4020 U4033 U4033 U4034 U4034 U4049 U4049 U4050 U4050 U4054 U4054 U4058 U4058 U4059 U4059 U4060 U4060 U4061 U4061 U5001 U5001 U5002 U5002 U5003 U5004 U5004 U5005 U5005 U5006 U5006
FIG. ITEM
3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 3 3A 2 2A 2 2A 2A 2 2A 2 2A 2 2A
661 590 590 595 595 640 640 625 625 625 625 715 715 610 610 630 630 580 580 635 635 635 635 635 635 635 635 650 650 580 580 600 600 645 645 605 605 675 675 685 685 815 695 695 615 615 825 825
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
5E 5D 5D 5F 5F 5F 5F 4J 4J 4J 4J 6F 6F 5F 5F 6G 6G 4E 4E 7Y 7Y 7Y 7Y 7X 7X 7W 7W 4D 4D 2J 2J 2J 2J 2J 2J 5J 5J 4D 4D 3D 3D 3E 4E 4E 4E 4E 5H 5H
Page 10032 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
U5007 U5007 U5008 U5008 U5009 U5009 U5010 U5010 U5011 U5011 U5012 U5012 U5014 U5014 U5015 U5015 U5016 U5016 U5017 U5017 U5018 U5018 U5019 U5019 U5020 U5020 U5021 U5021 U5022 U5022 U5023 U5023 U5024 U5024 U5025 U5025 U5026 U5026 U5027 U5027 U5028 U5028 U5029 U5029 U5030 U5030 U5031 U5031
EFFECTIVITY ALL
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
855 855 860 860 860 860 860 860 860 860 690 690 850 850 850 850 850 850 855 855 835 835 855 855 840 840 740 740 830 830 830 830 760 760 845 845 735 735 775 775 740 740 850 850 745 745 740 740
GEOGRAPHIC LOCATION
3F 3F 2F 2F 3F 3F 3F 3F 3F 3F 4G 4G 4F 4F 4F 4F 4F 4F 5H 5H 4D 4D 4F 4F 2F 2F 6F 6F 6G 6G 6F 6F 5F 5F 7E 7E 6D 6D 7J 7J 7K 7K 2H 2H 2J 2J 6G 6G
EQUIPMENT DESIGNATOR
U5032 U5032 U5033 U5033 U5034 U5034 U5035 U5035 U5036 U5036 U5037 U5037 U5039 U5039 U5040 U5040 U5041 U5041 U5042 U5042 U5043 U5043 U5048 U5048 U5057 U5057 U5059 U5059 U5091 U5091 U5091U5038 U5091U5038 U5118 U5118 U5119 U5119 U5122 U5122 U5125 U5125 U5126 U5126 U5144 U5144 U5159 U5159 U5160 U5160
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
705 705 730 730 740 740 740 740 785 785 690 690 695 695 710 710 690 690 725 725 825 825 680 680 690 690 695 695 800 800 810A 810A 695 695 765 765 735 735 820 820 850 850 720 720 740 740 740 740
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
7K 7K 6E 6E 5E 5E 5D 5D 2H 2H 2H 2H 3G 3G 6E 6E 4G 4G 6H 6H 6H 6H 5H 5H 4G 4G 5G 5G 7F 7F 4H 4H 3H 3H 3H 3H 4H 4H 4D 4D 3G 3G 7K 7K 6D 6D 5F 5F
Page 10033 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Equipment Designator Index EQUIPMENT DESIGNATOR
U5162 U5162 U5163 U5163 U5165 U5165 U5166 U5166 U5168 U5168 U5169 U5169 U5169U5013 U5169U5013 U5171 U5171 U5501 U5501 U5502 U5502
EFFECTIVITY ALL
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 2 2A
750 750 780 780 795 795 860 860 860 860 860 860 866 866 755 755 700 700 700 700
GEOGRAPHIC LOCATION
5E 5E 5E 5E 5E 5E 5F 5F 5F 5F 5E 5E 1H 1H 6D 6D 4J 4J 3J 3J
EQUIPMENT DESIGNATOR
U5503 U5503 U5504 U5504 U5505 U5505 U5506 U5506 U5507 U5507 V5001 V5001 WG100 Y4001 Y4001 Y5001 Y5001 Y5002 Y5002
FIG. ITEM
2 2A 2 2A 2 2A 2 2A 2 2A 2 2A 9 3 3A 2 2A 2 2A
770 770 700 700 700 700 715 715 735 735 885 885 175 415 415 230 230 235 235
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
GEOGRAPHIC LOCATION
2J 2J 6K 6K 5K 5K 4K 4K 3K 3K 5H 5H 5E 5E 5D 5D 3G 3G
Page 10034 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index PART NUMBER
ADF08ST AD7226KR AQ147A101JAJMA AQ147A300JAJ AQ147A510JAJM BAS28 BCA1000FTM BCA1001FTM
BCA1002FTM BCA1004FTM
BCA1053FTM BCA1212FTM BCA1213FTM BCA1214FTM BCA1271FTM BCA1371FTM
BCA1501FTM BCA1541FTM BCA1652FTM BCA20R0FTM
BCA2002FTM
BCA2051FTM BCA2151FTM
EFFECTIVITY ALL
AIRLINE STOCK NO.
FIG. ITEM
2 2A 3 3A 2 2A 2 2A 2 2A 2 2A 3A 13 2 2A 3 3A 2 2A 3 3A 2 2A 2 2A 2 2A 3 3A 2 2A 2 2A 3A 2 2A 2 2A 2A 2 2A 3A 2 2A 3 3A 5A 3
220 220 640 640 300 300 290 290 280 280 100 100 730 40 925 925 740 740 945 945 750 750 955 955 965 965 620 620 760 760 350 350 360 360 770 370 370 380 380 390 895 895 720 410 410 780 780 70 790
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
TTL REQ
1 1 1 1 1 1 1 1 1 1 6 6 1 2 11 11 12 13 3 3 1 1 1 1 3 3 1 1 1 1 1 1 1 1 1 5 5 1 1 1 1 1 1 8 7 1 1 1 1
Page 10035 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index PART NUMBER
BCA2212FTM
BCA2431FTM BCA2432FTM
BCA2491FTM BCA2670FTM
BCA2801FTM BCA3012FTM BCA3091FTM BCA3242FTM BCA3321FTM BCA3322FTM BCA3571FTM BCA3922FTM BCA4022FTM BCA44R2FTM BCA4641FTM BCA4751FTM
BCA4991FTM
BCA5111FTM
EFFECTIVITY ALL
AIRLINE STOCK NO.
FIG. ITEM
3A 2 2A 3 3A 2 2A 3 3A 5A 3 3A 2 2A 3 3A 2 2A 2 2A 2 2A 2 2A 3 3A 3 3A 3 3A 2 2A 3 3A 2 2A 3 3A 13 2 2A 3 3A 2 2A 3 3A 2 2A
790 420 420 800 800 430 430 810 810 80 820 820 440 440 830 830 450 450 460 460 470 470 480 480 585 850 455 860 275 275 490 490 145 145 905 905 155 155 50 510 510 165 165 520 520 175 175 530 530
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
TTL REQ
1 3 3 1 1 2 2 1 1 1 3 2 1 1 1 1 1 1 2 1 1 1 1 1 4 3 1 1 2 3 3 3 1 1 1 1 1 2 3 4 4 6 7 10 10 6 5 1 1
Page 10036 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index PART NUMBER
BCA5112FTM BCA5230FTM BCA5621FTM BCA5622FTM BCA61R9FTM BCA6491FTM BCA6811FTM BCA6812FTM BCA7320FTM BCA7681FTM BCA8061FTM BCA8662FTM BCA9090FTM BLM21AF121SN1D B3LT1658 CCF55-1023F CMPD2836
CRCW120604R7J CRCW12062000F CRCW12062871F CRCW12064321F CRCW12066190F CRCW12067501F
CRCW20102R7J C0805C680J5GAC C1206C104K5RACT
EFFECTIVITY ALL
AIRLINE STOCK NO.
FIG. ITEM
3 3A 2 2A 3 3A 2 2A 2A 3 3A 2 2A 3 3A 2A 3A 3 3A 2 2A 2 2A 2 2A 9 3 3A 2 2A 3A 2 2A 2 2A 3A 2 2A 3 3A 2 2A 3A 3 3A 2 2A 3 3A
185 185 540 540 195 195 550 550 915 215 215 560 560 225 225 570 245 255 255 600 600 610 610 120 120 175 710 710 90 90 335 875 875 400 400 840 500 500 205 205 580 580 235 670 670 670 670 530 530
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
TTL REQ
1 1 1 1 3 3 8 8 1 1 1 2 2 1 2 1 1 1 1 1 1 1 1 7 7 1 2 3 1 1 1 2 2 1 1 1 2 2 1 1 2 2 1 12 12 1 1 1 1
Page 10037 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index PART NUMBER
DG441DY DG442DY DS11Q1 DS125-272K D500000V30 E526HN100318 FB110H225KP012 HDC9M30000-14 IRF9540 IST253-62 KL250
LM285D-2-5
LM2901D LM2902M LM2904M LM318M LM35DM LM358D MAX4426ESA MC33166T MC78M08BDT ML1350-5P MMBD2837LT1G MMBTA42LT1 MMBT5087LT1 MM74HCT00M
EFFECTIVITY ALL
AIRLINE STOCK NO.
FIG. ITEM
2 2A 2 2A 12 3 3A 2 2A 2 2A 3 3A 13 3 3A 6 7 1 2 2A 3 3A 5A 2 2A 3 3A 2 2A 3 3A 5A 5A 2 2A 3 3A 2 2A 2 2A 3 3A 3 3A 2 2A 3
750 750 780 780 30 700 700 15 15 155 155 430 430 15 305 305 15 35 280 40 40 630 630 50 730 730 610 610 720 720 600 600 60 40 680 680 620 620 710 710 700 700 345 345 285 285 70 70 650
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
TTL REQ
1 1 1 1 1 1 1 1 1 2 2 4 1 1 1 1 2 2 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 2 1 1 4 4 1 1 2 2 2 2 1
Page 10038 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index PART NUMBER
MS51535-4 MUR1100E MUR460G M93C56WMN6 NAS1515H04
AIRLINE STOCK NO.
FIG. ITEM
3A 8 3 3A 3A 13 3 3A
NUTTYPE1660 PMBT3906 PPLW2C04SSPA RNXW20L5059 SEP13055-03 SG615P10-000MB SLPA125-375-01
11 2 2A 1 2 2A 2 2A 2 2A 3 3A
SMCJ33A SMCJ7-0A SN74HC03D SN74LS221D SPH2R15-5PCT SP720AB SSRIF6632ZZHA3 TDL157M010M1E TLC0820AIDW TL084ID T491A474K025AH T491B335K016AH T491B475M010AH T491C106K016AH
EFFECTIVITY ALL
3 3A 2 2A 2 2A 3 3A 3 3A 2 2A 9 3 3A 2 2A 2 2A 2 2A 5A 2 2A 3
650 30 325 325 355 30 105 45 110 45 5 145 145 275 140 140 210 210 230 230 70 95 100 75 315 315 80 80 820 820 580 580 690 690 790 790 70 420 420 760 760 740 740 250 250 20 260 260 440
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
TTL REQ
1 1 5 4 1 2 1 1 1 1 1 12 12 3 2 2 2 2 1 1 2 1 1 2 1 1 3 3 1 1 2 2 1 1 1 1 2 1 1 1 1 7 7 8 8 1 4 4 1
Page 10039 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
T491C475K025AH T491D336K016AH T491D476K010AH UKL1E101KPAANA U125-0040S VK200-10-36 V82RA8 XC3042A7PQ100I
007-00065-0001 007-00065-0001 007-00179-0001
ALL
TTL REQ
3A 3 3A 13 2 2A 3 3A 11 3 3A 2 2A 2 2A 3 3A 3
440 450 450 20 240 240 490A 490A 15 375 375 885 885 690 690 590 590 140
1 1 2 1 1 1 1 1 1 4 4 1 1 4 4 1 1 1
2 2A 3 3A
65 65 340 340
12 12 5 4
SEE PMBT3906
007-00179-0001 007-00254-0001
SEE 007-00179-0001
007-00254-0001 007-00257-0001 007-00261-0003
SEE 007-00254-0001 SEE MMBTA42LT1
007-00432-0002 007-00467-0000
SEE 2N6402
007-00467-0000 007-00537-0000 007-00933-0000
SEE 007-00467-0000 SEE MMBT5087LT1
007-00933-0000 007-00937-0000 007-00961-0000 007-01033-0000 007-01033-0000 007-05241-0001 007-05241-0007 007-05245-0025
SEE 007-00933-0000 SEE IRF9540
007-05245-0025 007-06141-0005 007-06177-0000
SEE 007-05245-0025 SEE MUR1100E
EFFECTIVITY
FIG. ITEM
3 280 3A 280
1 1
3 290 3A 290
2 2
3 300 3A 300
1 1
2 75 2A 75
1 1
3 270 3A 310
2 1
3 320 3A 320
1 1
3 330
7
SEE 007-01033-0000 SEE SMCJ33A SEE SMCJ7-0A
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10040 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
007-06177-0000 007-06179-0000
SEE 007-06177-0000
007-06179-0000 007-06181-0000 007-06182-0000 007-06184-0000
SEE 007-06179-0000 SEE CMPD2836 SEE MMBD2837LT1G
007-06184-0000 007-06396-0000 007-06427-0000 007-06444-0002
SEE 007-06184-0000 SEE BAS28
007-06444-0002 007-06446-0000 007-06448-0000
SEE 007-06444-0002 SEE MUR460G
007-06448-0000 007-06452-0000 007-06452-0000 008-00008-0002
SEE 007-06448-0000
008-00008-0002 008-00065-0000 008-00073-0000 008-00073-0000 008-00096-0001
SEE 008-00008-0002 SEE 32054-0182
008-00096-0001 008-00300-0004 008-00300-0004 008-00300-0004 008-00310-0000 008-00310-0000 008-00311-0000 008-00311-0000 009-08545-0000 009-08545-0020 009-08545-0020 009-08548-0000 009-08548-0020 009-08548-0020 009-08549-0000 009-08549-0020 009-08549-0020
SEE 008-00096-0001
EFFECTIVITY ALL
FIG. ITEM
TTL REQ
3A 330
6
2 85 2A 85
1 1
2 95 2A 95
8 8
3 310 3 350 3A 350
1 7 7
13 55 2 105 2A 105
1 1 1
13 10
5
3 360 3A 360
4 2
7 30
1
SEE 007-06452-0000
SEE 008-00073-0000 2 2A 3 3A
110 110 365 365
23 23 14 14
6 10
1
5A 45
1
5A 5
1
5 85 5A 90
1 1
3 850 3A 870
1 1
2 970 2A 970
1 1
SEE MS51535-4 SEE 008-00300-0004 SEE 008-00310-0000 SEE 008-00311-0000
SEE 009-08545-0020
SEE 009-08548-0020
SEE 009-08549-0020
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10041 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
009-08705-0000 009-08705-0000 012-01316-0000
SEE 075-01563-0000
13 60
1
3 15 3A 15
6 6
012-01575-0000 012-01673-0001
SEE 012-01575-0000
1 90 9 180
1 1
SEE 012-01567-0000
013-00172-0000
ALL
TTL REQ
SEE 009-08705-0000
012-01563-0000 012-01564-0000 012-01567-0000 012-01567-0000 012-01575-0000
013-00172-0000 013-00181-0000
SEE 013-00172-0000
013-00181-0000 013-00181-0000 013-00186-0000
SEE BLM21AF121SN1D SEE 013-00181-0000
013-00186-0000 015-00207-0032
SEE 013-00186-0000
015-00207-0032 015-00238-0001 015-00238-0001 015-00239-0002 015-00248-0000
SEE 015-00207-0032
015-00248-0000 015-00249-0000 015-00250-0000 015-00250-0000 015-00313-0001 017-00251-0001
SEE 015-00248-0000 SEE RNXW20L5059
3 25 3A 25
1 1
3 3A 2 2A
1 1 2 2
20 20 115 115
5 10 5A 10
1 1
2 125 2A 125
2 2
2 130 2A 130
1 1
4 80
1
SEE 015-00238-0001 9 175A 2 135 2A 135
AR 1 1
9 165
1
2 150 2A 150
1 1
2 160 2A 160
1 1
SEE 015-00250-0000 SEE B3LT1658
017-00251-0001 019-02314-0090 019-02314-0091
SEE 017-00251-0001 SEE E526HN100318
019-02314-0091 019-02331-0000
SEE 019-02314-0091
EFFECTIVITY
FIG. ITEM
3 370 370A 370B 370C 370D 370E
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
1 1 1 1 1 1
Page 10042 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
019-02331-0000 019-02331-0002
SEE 019-02331-0000
019-02331-0002 019-02331-0005
SEE 019-02331-0002
019-02331-0005 019-02331-0006
SEE 019-02331-0005
019-02331-0006 019-02331-0008
SEE 019-02331-0006
019-02331-0008 019-02331-0010
SEE 019-02331-0008
019-02331-0010 019-02331-0011
SEE 019-02331-0010
019-02331-0011 019-02331-0012
SEE 019-02331-0011
019-02331-0012 019-02332-0000 019-02368-0000
SEE 019-02331-0012 SEE VK200-10-36
019-02368-0000 019-02660-0013 019-02660-0015
SEE 019-02368-0000 SEE 1008CS101XKB
019-02660-0015 019-02660-0017 019-02660-0040
SEE 019-02660-0015 SEE 1008CS221XJLC
019-02660-0040 019-02660-0050 019-06133-0000
SEE 019-02660-0040 SEE 1008CS820XK
019-06133-0000 019-07255-0000
SEE 019-06133-0000
EFFECTIVITY ALL
FIG. ITEM
TTL REQ
370F 370G 3A 370 370A 370B 370C 370D 370E 370F 370G
1 1 1 1 1 1 1 1 1 1
3 370A 3A 370A
1 1
3 370B 3A 370B
1 1
3 370C 3A 370C
1 1
3 370D 3A 370D
1 1
3 370E 3A 370E
1 1
3 370F 3A 370F
1 1
3 370G 3A 370G
1 1
3 380 3A 380
3 3
2 170 2A 170
2 2
2 180 2A 180
8 8
3 385 3A 385
1 1
3 390
1
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10043 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
019-07255-0000 019-07257-0000
SEE 019-07255-0000
019-07257-0000 019-08265-0001
SEE 019-07257-0000
019-08265-0001 019-08265-0002
SEE 019-08265-0001
019-08265-0002 021-00127-0001 029-00766-0002 029-00766-0002 029-00767-0001 029-00767-0001 029-00768-0001 029-00768-0001 030-00444-0001
SEE 019-08265-0002
030-00464-0000 030-00464-0000 030-01058-0001 030-01444-0000 030-01444-0000 030-01444-0000 030-01453-0000
ALL
TTL REQ
3A 390
1
3 395 3A 395
1 1
2 190 2A 190
1 1
2 195 2A 195
1 1
6 20 9 110
1 1
9 15
1
9 60
1
2 200 5 5 2A 200
1 1 1
10 50
5
10 11 7 8
1 1 1 1
SEE 029-00766-0002 SEE 029-00767-0001 SEE 029-00768-0001
SEE 030-00464-0000 SEE 65307-001 SEE 030-01444-0000 SEE 77138-101LF
030-02204-0002 030-02204-0002 030-02205-0005 030-02346-0012 030-02352-0000 030-02352-0007 030-02520-0003 030-02832-0003
SEE SEE SEE SEE SEE SEE
030-02832-0003 030-03170-0003 030-03170-0003 030-03170-0003 030-03171-0003
SEE 030-02832-0003
030-03171-0003 030-03209-0003 030-03252-0001
SEE 030-03171-0003 SEE SEP13055-03
EFFECTIVITY
FIG. ITEM
40 55 10 10
030-02204-0002 47745-000 HDC9M30000-14 4541-10-0-7 D500000V30 65823-183 3 405 3A 405
2 2
10 45
1
2 2A 5 5A
205 205 15 15
1 1 1 1
2 215
1
SEE 030-03170-0003 SEE 69307-006LF
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10044 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
030-03252-0008 030-03252-0008 031-00756-0006 033-00224-0003
SEE 030-03252-0008 SEE ADF08ST
033-00224-0003 035-01540-0018 035-01540-0018 036-00057-0010 0410-5
SEE 033-00224-0003
SEE SG615P10-000MB
044-00309-0005 044-00309-0006
SEE 044-00309-0005
044-00309-0006 047-05201-0001
SEE 044-00309-0006
047-05201-0001 047-09643-0001 047-09643-0001 047-09644-0002 047-09644-0002 047-09947-0001 047-09947-0001 047-09951-0001 047-09951-0001 047-09953-0001 047-09953-0001 047-09968-0001 047-09968-0001 047-10012-0001
SEE 047-05201-0001
ALL
1 1
2 225 2A 225
1 1
1 295
1
3 265 3A 265
1 1
3 415 3A 415
1 1
2 235 2A 235
1 1
2 25 2A 25
2 2
12 20
1
12 50
1
9 75
1
1 185
1
4 5
1
1 35
1
SEE 047-09644-0002 SEE 047-09947-0001 SEE 047-09951-0001 SEE 047-09953-0001 SEE 047-09968-0001 2 2A 2 2A 2 2A 11
047-10014-0001
EFFECTIVITY
2 215A 2A 215
SEE 047-09643-0001
047-10013-0001
047-10162-0002
TTL REQ
SEE 035-01540-0018 SEE 251005
044-00309-0003 044-00309-0005
047-10018-0002 047-10018-0002 047-10021-0001 047-10021-0001 047-10124-0001 047-10162-0002
FIG. ITEM
45 45 50 50 55 55 35
1 1 1 1 1 1 1
1 85
1
SEE 047-10018-0002 SEE 047-10021-0001 1 10 7 8
270 55 25 25
1 1 1 1
SEE 047-10162-0002
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10045 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
047-10500-0001 047-10500-0001 047-10501-0001 047-10501-0001 047-10549-0001 047-10549-0001 047-10675-0001
ALL
1
11 50
1
1 260
1
SEE 047-10549-0001 3 3A 3 3A
130 135 55 55
1 1 1 1
9 125
1
1 190
1
SEE 047-10676-0001 SEE 047-10683-0001 SEE 047-10880-0001
SEE 057-01540-0000
057-03231-0004 057-03231-0004 057-03511-0001 057-05287-0109 057-05335-0009 057-05335-0011 057-05335-0011 057-05587-0000 057-05587-0001 057-05656-1001 057-05656-1003 057-05716-0000 057-05716-0000 057-05728-0000 057-05734-0000 057-06159-0001 06562-047
SEE 057-03231-0004 SEE 26147-0004 SEE 8051399-0001
EFFECTIVITY
10 30
SEE 047-10501-0001
057-01540-0000 057-02834-0000 057-03231-0004
071-00097-0100 071-01519-0101 073-00925-0002 073-00925-0002 073-00936-0002 073-00936-0002 073-00946-0002 073-00946-0002 073-00968-0003
TTL REQ
SEE 047-10500-0001
047-10676-0001 047-10676-0001 047-10683-0001 047-10683-0001 047-10880-0001 047-10880-0001 057-01540-0000
FIG. ITEM
1 5 3 5 3A 5
1 1 1
12 10 3 10 3A 10
1 1 1
1 110 1 120 1 125
1 1 1
SEE 057-05335-0011 12 12 1 1 1
15 5 30 25 50
1 1 1 1 1
1 1 1 2 2A 12 1 1
215 20 15 800 800 1 1 290
1 1 1 1 1 RF RF 1
SEE 057-05716-0000
SEE 073-00925-0002 1 210
1
4 55
1
10 25
1
SEE 073-00936-0002 SEE 073-00946-0002
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10046 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
073-00968-0003 073-00969-0001 073-05176-0003 073-05176-0003 073-05178-0003 075-01563-0000 076-02277-0000 076-02277-0000 076-02278-0001 076-02278-0001 076-02817-0001 076-02817-0001 076-02821-0001 076-02821-0001 076-02823-0000
SEE 073-00968-0003
076-02823-0000 076-02825-0000 076-02825-0000 076-02825-0001 076-02825-0001 076-02868-0000 076-02868-0000 076-02868-0001 076-02868-0001 076-02876-0001 076-02876-0001 076-02890-0001 076-02890-0001 076-02894-0001
SEE 076-02823-0000
078-02101-0000 078-02101-0000 088-03123-0001 088-03123-0001 088-03137-0000 088-03137-0000 088-03143-0000 088-03143-0000 088-03147-0000 088-03148-0000 088-03148-0000 088-03158-0000 088-03158-0000 088-03164-0000 089-02136-0000 089-02136-0000 089-02136-0000 089-02140-0000
EFFECTIVITY ALL
FIG. ITEM
TTL REQ
9 25 10 70
1 1
11 75 1 80 9 80
1 1 2
SEE 073-05176-0003
SEE 076-02277-0000 1 145
2
4 75
4
6 5
2
7 45 8 45
1 1
4 35
1
4 40
1
1 75
2
1 70
2
1 150
2
SEE 076-02278-0001 SEE 076-02817-0001 SEE 076-02821-0001
SEE 076-02825-0000 SEE 076-02825-0001 SEE 076-02868-0000 SEE 076-02868-0001 SEE 076-02876-0001 10 60
1
2 60 2A 60 11 30
9 9 1
SEE 076-02890-0001
SEE 078-02101-0000 9 115
1
SEE 088-03123-0001 11 40
1
9 5
1
11 25 9 135
1 1
1 195
2
1 155 10 5
2 1
3 80
1
SEE 088-03137-0000 SEE 088-03143-0000
SEE 088-03148-0000 SEE 088-03158-0000
SEE NUTTYPE1660 SEE 089-02136-0000
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10047 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
FIG. ITEM
3A 85 089-02140-0000 089-02162-0055 089-02162-0055 089-05857-0006
SEE 089-02140-0000
089-05857-0006 089-05874-0003 089-05874-0004
SEE 089-05857-0006
089-05874-0004 089-05874-0004 089-05878-0004
SEE PPLW2C04SSPA SEE 089-05874-0004
089-05878-0004 089-05878-0005 089-05878-0005 089-05878-0006 089-05878-0006 089-05878-0010 089-05899-0008 089-05903-0003
SEE 089-05878-0004
ALL
1
1 160
2
7 40 8 40 9 160 90
1 1 1 1
4 15 4 10 60
2 1 2
1 180 205 255 265 65 2 20 2A 20
1 4 3 1 2 2 2
9 55
4
9 40
4
SEE 089-02162-0055
SEE 089-05878-0005 SEE 089-05878-0006 12 4 3 3A 2 2A
089-05903-0004 089-05903-0004 089-05903-0004 089-05903-0005 089-05903-0005 089-05903-0006 089-05903-0022 089-05907-0003 089-05907-0006
SEE 089-05903-0004 SEE 6332-0404
089-05907-0006 089-06004-0003 089-06008-0004 089-06008-0007 089-06008-0007 089-06119-0002 089-06119-0002 089-06491-0004
SEE 089-05907-0006 SEE 6732-0203 SEE 6732-0404
EFFECTIVITY
TTL REQ
35 30 135 140 30 30
2 1 6 6 2 2
3A 65
2
1 9 3 3A
2 1 2 2
SEE 089-05903-0005 SEE 6332-0406 100 30 30 30
1 45
9
12 25
2
11 45
1
SEE 089-06008-0007 SEE 089-06119-0002
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10048 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
089-06491-0004 089-06492-0005 089-06492-0005 089-06493-0007 089-06494-0005 089-06494-0005 089-06494-0005 089-06494-0007 089-06494-0028 089-08001-0034 089-08001-0034 089-08076-0030 089-08076-0030 089-08093-0030 089-08110-0034 089-08110-0034 089-08111-0034 089-08158-0011 089-08335-0000 089-08335-0000 089-08335-0000 089-08339-0000 089-08339-0000 089-08600-0000
089-08600-0000 089-08600-0002 089-08600-0004 089-08600-0007 090-00019-0002 090-00559-0003 090-00559-0003 090-00973-0003 090-00973-0005
ALL
TTL REQ
SEE 089-06491-0004 9 20
4
9 145
4
1 165 240 9 120 4 45
4 4 4 2
SEE 089-06492-0005 SEE 46068-0607S SEE 089-06494-0005 SEE 46068-0805S
SEE 089-08001-0034 10 20 11 20
1 1
10 10 11 10 9 95
1 1 2
1 175 250 10 15
3 4 1
9 65
1
9 105 105A 105B 105C
1 1 1 1
9 105A 9 105B 9 105C
1 1 1
SEE 089-08076-0030
SEE 089-08110-0034 SEE 36037-3406
SEE U125-0040S SEE 089-08335-0000 SEE 089-08339-0000
SEE 089-08600-0000
SEE 36008-025C 13 5
2
3 40 3A 40
1 1
1 55
1
2 10 2A 10
2 2
SEE 090-00559-0003 SEE SLPA125-375-01
090-00973-0005 090-00988-0000 090-00990-0001 090-00990-0010 090-00990-0010 090-01019-0020
SEE 090-00973-0005 SEE KL250 SEE DS11Q1
090-01019-0020
SEE 090-01019-0020
EFFECTIVITY
FIG. ITEM
SEE 090-00990-0010
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10049 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
091-00054-0003
091-00054-0003 091-00109-0000
SEE 091-00054-0003
091-00109-0000 091-00109-0003
SEE 091-00109-0000
091-00109-0003 091-00286-0000 091-00286-0002
SEE 091-00109-0003
091-00286-0002 091-00286-0020 091-00480-0071
SEE 091-00286-0002 SEE 3223-07FR52
091-00480-0071 091-00602-0000 092-05003-0018
SEE 091-00480-0071 SEE NAS1515H04
096-01082-0025 096-01082-0028 096-01082-0052 096-01082-0052 096-01082-0055 096-01082-0065
SEE TDL157M010M1E
ALL
TTL REQ
3 100 50 3A 105 50
1 2 1 2
1 285 7 20 8 20
2 2 2
9 10 130 150
2 1 4
3 65 3 115 85 3A 120 90
1 1 1 1 1
3 125 90 3A 130 95
1 1 1 1
3 110 3A 115
2 2
3 425 3A 425
1 1
3 3A 3 3A
490 490 435 435
1 1 2 2
2 245 2A 245
2 2
5 20
1
3 445 3A 445
2 2
SEE 096-01082-0052 SEE FB110H225KP012
096-01186-0011 096-01186-0011 096-01186-0011 096-01186-0012
SEE T491D476K010AH SEE 096-01186-0011
096-01186-0012 096-01186-0013 096-01186-0013 096-01186-0014 096-01186-0015 096-01186-0018
SEE 096-01186-0012
096-01186-0018
SEE 096-01186-0018
EFFECTIVITY
FIG. ITEM
SEE T491B335K016AH SEE T491C106K016AH SEE T491D336K016AH
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10050 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
096-01186-0020 096-01186-0022 096-01186-0027
SEE T491A474K025AH SEE T491C475K025AH
096-01186-0027 096-01186-0059 096-01186-0064
SEE 096-01186-0027 SEE T491B475M010AH
096-01186-0064 097-00104-0038 097-00104-0038 097-00217-0008 097-00217-0009
SEE 096-01186-0064
097-00217-0009 097-00217-0013 097-00218-0003
SEE 097-00217-0009 SEE 94SA227X0010F
097-00218-0003 097-00218-0004
SEE 097-00218-0003
097-00218-0004 097-00218-0005
SEE 097-00218-0004
097-00218-0005 097-00238-0093 1008CS101XKB
SEE 097-00218-0005 SEE UKL1E101KPAANA
1008CS820XK 105-00169-0000
ALL
TTL REQ
2 255 2A 255
3 3
2 265 2A 265
1 1
3A 455
3
3 465 3A 465
1 1
3 475 3A 475
2 2
3 480 3A 480
5 5
3 485 3A 485
1 1
2 2A 2 2A 2 2A 3 3A
165 165 175 175 185 185 495 495
1 1 1 1 1 1 2 2
2 2A 3 3A
270 270 500 500
2 2 6 6
2 2A 3 3A
275 275 355 855
2 2 2 2
2 285 2A 285
1 1
SEE 097-00104-0038 SEE 20SA68M
1008CS221XJLC
105-00169-0000 106-00122-0000
SEE 105-00169-0000
106-00122-0000 106-00124-0000
SEE 106-00122-0000
106-00124-0000 106-00126-0003 106-00126-0004
SEE 106-00124-0000 SEE AQ147A510JAJM
106-00126-0004
SEE 106-00126-0004
EFFECTIVITY
FIG. ITEM
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10051 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
106-00126-0005 106-00126-0007
SEE AQ147A300JAJ
106-00126-0007 106-00126-0010 106-00126-0012
SEE 106-00126-0007 SEE AQ147A101JAJMA
106-00126-0012 106-00129-0000 106-00133-0001
SEE 106-00126-0012
106-00133-0001 106-00133-0005
SEE 106-00133-0001
106-00133-0005 106-04100-0016
SEE 106-00133-0005
106-04100-0016 106-04101-0026
SEE 106-04100-0016
106-04101-0026 106-04102-0026
SEE 106-04101-0026
106-04102-0026 106-04102-0046
SEE 106-04102-0026
106-04102-0046 106-04103-0046
SEE 106-04102-0046
106-04103-0046 106-04103-0047
SEE 106-04103-0046
106-04103-0047 106-04104-0046
SEE 106-04103-0047
106-04104-0046 106-04104-0047 106-04153-0046
SEE 106-04104-0046 SEE C1206C104K5RACT
EFFECTIVITY ALL
FIG. ITEM
TTL REQ
2 295 2A 295
1 1
2 305 2A 305
1 1
3 245 2 310 2A 310
1 3 3
2 315 2A 315
1 1
2 320 2A 320
1 1
2 325 2A 325
13 13
3 505 3A 505
1 1
2 2A 3 3A 5 5A
330 330 510 510 25 25
8 8 1 2 1 1
13 2 2A 3 3A
25 335 335 515 515
1 5 5 4 5
3 520 3A 520
1 1
2 2A 3 3A 5 5A
96 96 40 38 1 1
340 340 525 525 30 30
3 535
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
8
Page 10052 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
106-04153-0046 106-04153-0047
SEE 106-04153-0046
106-04153-0047 106-04180-0026
SEE 106-04153-0047
106-04180-0026 106-04221-0014
SEE 106-04180-0026
106-04221-0014 106-04222-0016 106-04224-0047 106-04272-0016
SEE 106-04221-0014
106-04272-0016 106-04330-0026
SEE 106-04272-0016
106-04330-0026 106-04332-0046 106-04332-0046 106-04471-0026
SEE 106-04330-0026
ALL
TTL REQ
3A 535
8
3 540 3A 540
1 1
2 345 2A 345
1 1
3 545 3A 545
2 2
3 555
1
SEE 1206B224K500N 5 35 5A 35
1 1
2 935 2A 935
4 4
3A 555
1
3 560 3A 560
1 1
3 565 3A 565
1 1
3 570 3A 570
4 4
2 625 2A 625
3 3
2 630 2A 630
31 31
2 635 2A 635
2 2
2 640 2A 640
2 2
2 645 2A 645
1 1
2 650 2A 650
1 1
2 655
2
SEE 106-04332-0046
106-04471-0026 106-04751-0016
SEE 106-04471-0026
106-04751-0016 106-04821-0016
SEE 106-04751-0016
106-04821-0016 106-05101-0016
SEE 106-04821-0016
106-05101-0016 106-05102-0016
SEE 106-05101-0016
106-05102-0016 106-05103-0046
SEE 106-05102-0016
106-05103-0046 106-05104-0037
SEE 106-05103-0046
106-05104-0037 106-05121-0016
SEE 106-05104-0037
106-05121-0016 106-05200-0016
SEE 106-05121-0016
106-05200-0016 106-05270-0016
SEE 106-05200-0016
EFFECTIVITY
FIG. ITEM
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10053 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
106-05270-0016 106-05271-0016
SEE 106-05270-0016
106-05271-0016 106-05470-0016
SEE 106-05271-0016
106-05470-0016 106-05680-0016 118-00082-0000
SEE 106-05470-0016 SEE C0805C680J5GAC
118-00082-0000 120-00108-0002 120-02213-0002
SEE 118-00082-0000 SEE SN74LS221D
120-02213-0002 120-02233-0003 120-02233-0003 120-02233-0003 120-02420-0003 120-02452-0000
SEE 120-02213-0002
ALL
TTL REQ
2A 655
2
2 660 2A 660
1 1
2 665 2A 665
2 2
3 575 3A 575
1 1
2 675 2A 675
1 1
3A 585
1
2 685 2A 685
1 1
2 615 2 695 2A 695
1 4 4
2 705 2A 705
1 1
2 715 2A 715
1 1
5 40
1
2 725 2A 725
1 1
3 595 3A 595
2 2
2 735 2A 735
3 3
SEE MAX4426ESA SEE 120-02233-0003 SEE M93C56WMN6
120-02452-0000 120-02469-0001 120-02494-0000 120-02981-0112
SEE 120-02452-0000 SEE XC3042A7PQ100I
120-02981-0112 120-03020-0001 120-03026-0080
SEE 120-02981-0112 SEE ML1350-5P
120-03026-0080 120-03026-0082 120-03027-0004
SEE 120-03026-0080 SEE MC78M08BDT
120-03027-0004 120-03053-0009 120-03053-0009 120-03053-0010 120-03126-0005
SEE 120-03027-0004
120-03126-0005 120-03163-0001
SEE 120-03126-0005
120-03163-0001 120-03163-0001 120-03167-0004 120-03174-0013
SEE LM2901D SEE 120-03163-0001 SEE LM318M
EFFECTIVITY
FIG. ITEM
SEE LM358D SEE LM2904M
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10054 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
120-03174-0013 120-03174-0014
SEE 120-03174-0013
120-03174-0014 120-03174-0014 120-03196-0000 120-03285-0002
SEE TL084ID SEE 120-03174-0014 SEE LM2902M
120-03393-0002 120-03400-0001
SEE DG441DY
120-03400-0001 120-03430-0000
SEE 120-03400-0001
120-03430-0000 120-03475-0003 120-03488-0000
SEE 120-03430-0000 SEE TLC0820AIDW
120-03488-0000 120-03501-0000
SEE 120-03488-0000
120-03501-0000 120-03510-0000 120-03520-0000
SEE 120-03501-0000 SEE MC33166T
120-03520-0000 120-03544-0000 120-03544-0000 120-03569-0000
SEE 120-03520-0000
120-03569-0000 120-03581-0000
SEE 120-03569-0000
120-03581-0000 120-03584-0000
SEE 120-03581-0000
120-03584-0000 120-03592-0000
SEE 120-03584-0000
120-03592-0000 120-03592-0000 120-03593-0000
SEE AD7226KR SEE 120-03592-0000
120-03593-0000 120-03593-0000 120-03598-0000
SEE DG442DY SEE 120-03593-0000
120-03599-0000 120-06065-0002
SEE SP720AB
EFFECTIVITY ALL
FIG. ITEM
TTL REQ
3 605 3A 605
1 1
2 745 2A 745
1 1
2 755 2A 755
1 1
3 615 3A 615
1 1
2 765 2A 765
1 1
2 770 2A 770
1 1
3 625 3A 625
2 2
5 45
1
3 635 3A 635
4 4
5 50 5A 55
1 1
10 65 11 70
1 1
2 775 2A 775
1 1
3 645 3A 645
1 1
2 785 2A 785
1 1
2 795
1
SEE LM285D-2-5
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10055 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
120-06065-0002 120-08030-0010 1206B224K500N 122-01338-0109
122-30048-0003 122-30049-0004 122-30064-0000 123-00003-0003 123-00573-0003
SEE SN74HC03D
123-00573-0003 123-04351-0003 124-00000-0003 124-00008-0003
SEE 123-00573-0003 SEE 74HC4351D SEE MM74HCT00M
124-00008-0003 124-00074-0003
SEE 124-00008-0003
124-00074-0003 124-00139-1003 124-00157-0003
SEE 124-00074-0003 SEE 74ACT139SC
124-00157-0003 124-00245-0002 124-00573-0003
SEE 124-00157-0003 SEE 74HCT245D
124-00573-0003 124-00574-0003 125-00751-0109 126-00047-0004
SEE 124-00573-0003 SEE 74HCT574D
126-00059-0003 126-00074-0000 126-00089-0003 130-05000-0035
EFFECTIVITY ALL
TTL REQ
2A 795
1
3A 1 2A 2 2A 2 2A 2 2A 3 3A
2 1 RF 1 1 1 1 1 1 1 1
SEE 120-06065-0002 SEE 06562-047
122-30048-0002
130-05000-0035 130-05027-0043 130-05047-0033
FIG. ITEM
550 131 815 810 810 810A 810A 866 866 661 661
2 825 2A 825
2 2
2 835 2A 835
1 1
3 655 3A 655
1 1
2 845 2A 845
1 1
2 855 2A 855
3 3
1 2 2A 2A 3 3A 2 2 2A 3 3A
1 1 1 1 1 1 1 5 5 7 7
130 865 865 805 660 660 805 870 870 665 665
SEE 130-05000-0035 SEE CRCW20102R7J SEE CRCW120604R7J
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10056 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
130-05101-0043 130-05101-0043 130-05561-0043
ALL
TTL REQ
13 35
1
2 880 2A 880
2 2
3 675 3A 675
1 1
3 680 3A 680
1 1
3A 685
1
3 685
1
3 695 3A 695
1 1
3 705 3A 705
1 1
2 3 3A 5
495 715 715 55
1 1 1 1
2 890 2A 890
3 3
3 720
1
3 725 3A 725
1 1
2 900 2A 900
2 2
2 910 2A 910
1 1
2 915 2 920 2A 920
1 4 4
SEE 130-05101-0043
130-05561-0043 131-00100-0033
SEE 130-05561-0043
131-00100-0033 131-00101-0033
SEE 131-00100-0033
131-00101-0033 132-00102-0017 132-00102-0017 132-00135-0000 132-05051-0000 133-00562-2103 133-00562-2202 133-00562-2202 134-01015-0031 134-01026-0006
SEE 131-00101-0033 SEE 132-00102-0017 SEE SPH2R15-5PCT
SEE 133-00562-2202 SEE DS125-272K
134-02001-0000 136-01023-0072 136-01023-0072 136-04222-0062 137-00034-0000
SEE V82RA8 SEE CCF55-1023F SEE 134-01026-0006
137-00034-0000 137-00034-0000 139-00100-0000
SEE LM35DM SEE 137-00034-0000
139-00100-0000 139-00150-0000 139-00200-0000 139-00221-0000
SEE 139-00100-0000
139-00221-0000 139-00309-0000
SEE 139-00221-0000
139-00309-0000 139-00442-0000 139-00499-0000
SEE 139-00309-0000 SEE BCA44R2FTM
139-00499-0000 139-00619-0000 139-00750-0000 139-01000-0000
SEE 139-00499-0000 SEE BCA61R9FTM
EFFECTIVITY
FIG. ITEM
SEE BCA20R0FTM
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10057 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
139-01000-0000 139-01000-0000 139-01001-0000
SEE BCA1000FTM SEE 139-01000-0000
139-01001-0000 139-01001-0000 139-01002-0000
SEE BCA1001FTM SEE 139-01001-0000
139-01002-0000 139-01002-0000 139-01003-0000
SEE BCA1002FTM SEE 139-01002-0000
139-01003-0000 139-01004-0000 139-01021-0000
SEE 139-01003-0000 SEE BCA1004FTM
139-01021-0000 139-01023-0000
SEE 139-01021-0000
139-01023-0000 139-01053-0000 139-01071-0000
SEE 139-01023-0000 SEE BCA1053FTM
139-01071-0000 139-01212-0000 139-01213-0000 139-01241-0000 139-01271-0000 139-01302-0000
SEE SEE SEE SEE SEE
139-01302-0000 139-01332-0000
SEE 139-01302-0000
139-01332-0000 139-01371-0000 139-01372-0000
SEE 139-01332-0000 SEE BCA1371FTM
139-01372-0000 139-01501-0000 139-01502-0000
SEE 139-01372-0000 SEE BCA1501FTM
139-01502-0000 139-01541-0000
SEE 139-01502-0000 SEE BCA1541FTM
EFFECTIVITY ALL
FIG. ITEM
TTL REQ
3 735 3A 735
25 24
13 45 2 930 2A 930
1 67 67
2 2A 3 3A 5 5A
940 940 745 745 60 65
2 2 6 5 4 4
3 755 3A 755
1 1
2 950 2A 950
1 1
2 960 2A 960
1 1
3 765 3A 765
1 1
2 355 2A 355
1 1
2 365 2A 365
1 1
2 375 2A 375 3 335
1 2 1
139-01071-0000 BCA1212FTM BCA1213FTM BCA1214FTM BCA1271FTM
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10058 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
139-01622-0000 139-01622-0000 139-01652-0000 139-01822-0000
SEE 139-01622-0000 SEE BCA1652FTM
139-01822-0000 139-01911-0000 139-02000-0000 139-02001-0000
SEE 139-01822-0000
ALL
TTL REQ
2 385 2A 385
1 1
2 395 2A 395
3 3
3 770
1
SEE CRCW12062000F 2 2A 3 3A
139-02001-0000 139-02002-0000 139-02051-0000 139-02051-0000 139-02102-0000
SEE 139-02001-0000 SEE BCA2002FTM
139-02102-0000 139-02151-0000 139-02210-0000 139-02211-0000
SEE 139-02102-0000 SEE BCA2151FTM
139-02211-0000 139-02212-0000 139-02213-0000
SEE 139-02211-0000 SEE BCA2212FTM
139-02213-0000 139-02372-0000
SEE 139-02213-0000
139-02372-0000 139-02431-0000 139-02432-0000 139-02432-0000 139-02433-0000
SEE 139-02372-0000 SEE BCA2431FTM
139-02433-0000 139-02491-0000 139-02493-0000
SEE 139-02433-0000 SEE BCA2491FTM
139-02493-0000 139-02553-0000
SEE 139-02493-0000
139-02553-0000
SEE 139-02553-0000
EFFECTIVITY
FIG. ITEM
405 405 775 775
1 1 1 1
5 65
1
3 785 3A 785
1 1
3 2 2A 3 3A 5 5A
730 415 415 795 795 70 75
1 2 2 1 1 1 1
3 805 3A 805
1 1
2 425 2A 425
1 1
5 75
1
3 815 3A 815
1 1
3 825 3A 825
1 1
2 435 2A 435
1 1
SEE BCA2051FTM
SEE BCA2432FTM
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10059 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
139-02670-0000 139-02742-0000
SEE BCA2670FTM
139-02742-0000 139-02801-0000 139-02871-0000 139-03010-0000
SEE 139-02742-0000 SEE BCA2801FTM SEE CRCW12062871F
139-03010-0000 139-03012-0000 139-03013-0000
SEE 139-03010-0000 SEE BCA3012FTM
139-03013-0000 139-03091-0000 139-03241-0000
SEE 139-03013-0000 SEE BCA3091FTM
139-03241-0000 139-03242-0000 139-03321-0000 139-03322-0000 139-03323-0000
SEE SEE SEE SEE
139-03323-0000 139-03402-0000
SEE 139-03323-0000
139-03402-0000 139-03480-0000 139-03571-0000 139-03922-0000 139-04021-0000 139-04022-0000 139-04222-0000 139-04222-0000 139-04321-0000 139-04322-0000
SEE 139-03402-0000
139-04322-0000 139-04641-0000 139-04750-0000
SEE 139-04322-0000 SEE BCA4641FTM
139-04750-0000 139-04751-0000 139-04752-0000
SEE 139-04750-0000 SEE BCA4751FTM
EFFECTIVITY ALL
FIG. ITEM
2 2A 3 3A
TTL REQ
445 445 835 835
4 4 1 1
2 455 2A 455
2 2
2 2A 3 3A
12 12 1 1
465 465 845 845
2 475 2A 475
1 1
2 485 2A 485
1 1
3 550 3A 865
1 1
3 250
1
3 840
1
2A 495
1
3 150 3A 150
1 1
2 2A 3 3A
16 16 2 2
139-03241-0000 BCA3242FTM BCA3321FTM BCA3322FTM
SEE BCA3571FTM SEE BCA3922FTM SEE BCA4022FTM SEE 139-04222-0000 SEE CRCW12064321F
505 505 160 160
2 515
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
6
Page 10060 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
139-04752-0000 139-04991-0000 139-04992-0000
SEE 139-04752-0000 SEE BCA4991FTM
139-04992-0000 139-05111-0000
SEE 139-04992-0000
139-05111-0000 139-05111-0000 139-05112-0000
SEE BCA5111FTM SEE 139-05111-0000
139-05112-0000 139-05112-0000 139-05113-0000
SEE BCA5112FTM SEE 139-05112-0000
139-05113-0000 139-05230-0000 139-05621-0000
SEE 139-05113-0000 SEE BCA5230FTM
139-05621-0000 139-05621-0000 139-05622-0000 139-05761-0000
SEE BCA5621FTM SEE 139-05621-0000 SEE BCA5622FTM
139-05761-0000 139-06190-0000 139-06191-0000
SEE 139-05761-0000 SEE CRCW12066190F
139-06191-0000 139-06491-0000
SEE 139-06191-0000
139-06491-0000 139-06491-0000 139-06811-0000
SEE BCA6491FTM SEE 139-06491-0000
139-06811-0000 139-06811-0000 139-06812-0000 139-07151-0000
SEE BCA6811FTM SEE 139-06811-0000 SEE BCA6812FTM
139-07151-0000 139-07320-0000 139-07321-0000
SEE 139-07151-0000 SEE BCA7320FTM
EFFECTIVITY ALL
FIG. ITEM
TTL REQ
2A 515 3 170 3A 170
6 3 3
2 525 2A 525
1 1
3 180 3A 180
1 1
2 535 2A 535
1 1
3 190 3A 190
1 1
2 545 2A 545
1 1
2 2A 3 3A
555 555 200 200
2 2 1 1
3 210 3A 210
1 1
5 80 5A 85
1 1
3 220 3A 220
2 1
2 565 2A 565
1 1
3 230 3A 230
1 1
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10061 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
139-07321-0000 139-07500-0000
SEE 139-07321-0000
139-07500-0000 139-07501-0000 139-07502-0000
SEE 139-07500-0000 SEE CRCW12067501F
139-07502-0000 139-07681-0000 139-07682-0000
SEE 139-07502-0000 SEE BCA7681FTM
139-07682-0000 139-07870-0000 139-08060-0000 139-08060-0000 139-08061-0000
SEE 139-07682-0000
139-08061-0000 139-08061-0000 139-08661-0000 139-08662-0000 139-08871-0000 139-08871-0000 139-08872-0000
SEE BCA8061FTM SEE 139-08061-0000
139-08872-0000 139-09090-0000 139-09091-0000 147-05169-0010 147-05169-0012 147-05169-0012 148-05182-0003
SEE 139-08872-0000 SEE BCA9090FTM
ALL
TTL REQ
2 575 2A 575
1 1
2 2A 3 3A
13 13 1 1
585 585 240 240
2 590 2A 590
1 1
2 570 3A 250
1 1
2 595 2A 595
2 2
3 260
2
3A 260
1
2 605 2A 605
1 1
3 235
1
9 35
2
7 50 8 50
1 1
8 35
2
4 70
1
2 35 2A 35
1 1
4 20
1
4 65
1
SEE 139-08060-0000
SEE BCA8662FTM SEE 139-08871-0000
SEE SSRIF6632ZZHA3 SEE 147-05169-0012
148-05182-0003 148-05186-0000 150-00072-0000 150-00072-0000 150-00072-0000 155-02744-0001 155-02744-0001 155-02745-0000
SEE 148-05182-0003 SEE 0410-5
155-02745-0000 187-01813-0000 187-01813-0000 187-01814-0000 187-01814-0000
SEE 155-02745-0000
EFFECTIVITY
FIG. ITEM
SEE IST253-62 SEE 150-00072-0000 SEE 155-02744-0001
SEE 187-01813-0000 SEE 187-01814-0000
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10062 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
187-01869-0001 187-01869-0001 2N6402 20SA68M 200-05173-0000 200-05173-0010 200-05174-0000 200-05175-0020 200-05310-0000 200-05313-0000 200-05553-0001 200-05554-0000 200-08545-0000 200-08545-0020 200-08548-0000 200-08548-0020 200-08549-0000 200-08549-0020 200-08549-0099 200-08705-0000 205-00717-1109 206-00246-0109 251005 26147-0004 32054-0182 3223-07FR52 36008-025C 36037-3406
4541-10-0-7
EFFECTIVITY ALL
FIG. ITEM
4 50
TTL REQ
1
SEE 187-01869-0001 3 3A 3 3A 9 7 9 1 8 1 9 6 9 1 11 4 9 10 9 4 5 4 5A 1 3 1 3A 1 2 1 2A 2 12 13 1 1 3 3A 2 2A 9 3A 9 1
295 295 460 460 50 1 50A 200 1 230 1 1 155 235 1 1 140 1 170 25 1 25A 1 140 1 140A 1 135 1 135A 1 3 45 1 115 105 410 410 5 5 45 70 100 170 225 245 12 40
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
1 1 2 2 1 RF 1 1 RF 1 RF RF 1 1 RF RF 1 RF 1 1 RF 1 RF 1 RF 1 RF 1 RF 1 RF 1 1 RF 1 1 1 1 1 1 1 2 2 4 1 4 2
Page 10063 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Numerical Index AIRLINE STOCK NO.
PART NUMBER
46068-0607S 46068-0805S 47745-000
9 1 7 8 3A
53001970-2 53001970-2 53002736-1 53002736-1 6332-0404
85 220 15 15 270
2 1 5 5 2
2A 615
1
1 60 95 3 120 35 60 3A 125 35 60 3 75 3A 80 7 5 8 5 3 400 3A 400 10 35 1 40 11 60 2 840 2A 840 2 850 2A 850 2 860 2A 860 2 830 2A 830 11 65 1 10 3 470 3A 470
1 5 1 1 3 1 1 1 1 1 1 1 1 1 2 2 1 1 1 5 5 7 7 2 2 5 1 2 2
SEE 53002736-1
65307-001 65823-183 6732-0203 6732-0404 69307-006LF 74ACT139SC 74HCT245D 74HCT574D 74HC4351D 77138-101LF 8051399-0001 94SA227X0010F
ALL
TTL REQ
SEE 53001970-2
6332-0406
EFFECTIVITY
FIG. ITEM
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10064 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10065 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 1. (Sheet 1 of 1) ART 2000 Final Assembly
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10066 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
1 -
1
071-01519-0101
FINAL ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ART 2000 (ESDS)
RF
5
057-01540-0000
.TAG
1
10
8051399-0001
.DECAL
15
057-06159-0001
.PATENT LABEL
20
057-05734-0000
25
......................................... WARNING HV (V00A29) (CSD: 057-01540-0000 V22373) ...................................... CAUTION (VBAG02) (CSD: 057-03511-0001 V22373)
1
................................
1
.LABEL
....................................... RF RAD WARN
1
057-05656-1003
.TAG
......................................... PART NUMBER
1
30
057-05656-1001
.TAG
......................................... SERIAL NUMBER
1
35
047-09968-0001
.COVER
40
6732-0404
.SCREW
2
45
089-06008-0007
.SCREW
9
50
057-05716-0000
.DECAL
...................................... W/ FINISH (VBAA66) (CSD: 047-09968-0001 V22373) (ATTACHING PARTS) ...................................... FHP (4-40 X 1/4) (VBAG02) (CSD: 089-06008-0004 V22373) ...................................... FHP (4-40 X 7/16) (VBAG02) (CSD: 089-06008-0007 V22373) ---*--...................................... BD REMOVAL (V07416) (CSD: 057-05716-0000 V22373)
1
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10067 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
1 55
090-00990-0010
.CAP
60
6332-0404
.SCREW
1
65
089-05878-0004
.SCREW
2
70
076-02868-0001
.SPACER
2
75
076-02868-0000
.SPACER
2
80
075-01563-0000
.COVER
1
85
047-10021-0001
.COVER
1
90
012-01564-0000
.COVER
1
95
6332-0404
.SCREW
5
100
089-05903-0022
.SCREW
2
......................................... PROTECTIVE, SUB-D (50 P) (V99017) (CSD: 090-00990-0010 V22373) ...................................... PHP (4-40 X 1/4) (VBAG02) (CSD: 089-05903-0004 V22373) ...................................... PHP (4-40 X 1/4) (V56563) (CSD: 089-05878-0004 V22373) ..................................... (4-40, 0.605) (V65590) (CSD: 076-02868-0001 V22373) ..................................... (4-40, 0.250) (V65590) (CSD: 076-02868-0000 V22373) ...................................... INSUL I/F (VAAA42) (CSD: 012-01563-0000 V22373) ...................................... FENCE I/F (V24687) (CSD: 047-10021-0001 V22373) ...................................... INSUL I/F ...................................... PHP (4-40 X 1/4) (VBAG02) (CSD: 089-05903-0004 V22373) ...................................... PHP (4-40 X 1 3/8)
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10068 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
EFFECT (USE) CODE
NOMENCLATURE
UNITS PER ASSY
1 -
105
206-00246-0109
.SOFTWARE SET
...............................
1
........................................ SFTW ID
1
(ESDS)
-
110
057-05287-0109
..TAG
115
205-00717-1109
..LOGIC SET
..................................
1
..................................... DASH 09
(ESDS) -
120
057-05335-0009
...DECAL
1
-
125
057-05335-0011
...DECAL
1
-
130
125-00751-0109
...LOGIC BOARD SW
-
131
122-01338-0109
....INTEGRATED CIRCUIT
1
135
200-08549-0000
...LOGIC BOARD
1
135A
200-08549-0020
...LOGIC BOARD
1
140
200-08548-0000
..POWER SUPPLY/MODULATOR BOARD
-
..................................... DASH 11 (V00A29) (CSD: 057-05335-0011 V22373) ............................
........................ (ESDS) (SEE IPL FIGURE 2A ITEM 815 FOR LOCATION)
............................... (ESDS) (REPL BY ITEM: 135A) (PRE SB ART 2000-3) (SEE 2 FOR DETAILS) ............................... (ESDS) (REPL ITEM: 135) (POST SB ART 2000-3) (SEE 2A FOR DETAILS)
1
............
1
............
1
......................................... PVT, AZIM W/FINISH (V65590) (CSD: 076-02278-0001 V22373)
2
(ESDS) (REPL BY ITEM: 140A) (PRE SB ART 2000-3) (SEE 3 FOR DETAILS) -
140A
200-08548-0020
..POWER SUPPLY/MODULATOR BOARD (ESDS) (REPL ITEM: 140) (POST SB ART 2000-3) (SEE 3A FOR DETAILS)
145
076-02278-0001
.PIN
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10069 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
1 150
076-02876-0001
.WASHER
2
155
088-03164-0000
.WASHER
..................................... LOAD
2
160
089-02162-0055
.NUT
......................................... LOCK (10-32) (V52828) (CSD: 089-02162-0055 V22373)
2
165
089-06494-0007
.SCREW
4
170
36037-3406
.WASHER
4
175
089-08158-0011
.WASHER
3
180
089-05878-0004
.SCREW
1
185
047-09951-0001
.PLATE
1
190
047-10880-0001
.SPRING
1
195
088-03158-0000
.GEAR
2
200
200-05174-0000
.AZIMUTH MOTOR ASSEMBLY
1
..................................... THRUST (V19142) (CSD: 076-02876-0001 V22373)
...................................... SHC (8-32 X 7/16) ..................................... SPLT (LK #8) (VBAG02) (CSD: 089-08111-0034 V22373) ..................................... FLAT (#8) ...................................... PHP (4-40 X 1/4) (V56563) (CSD: 089-05878-0004 V22373) ....................................... STOP (VBAA66) (CSD: 047-09951-0001 V22373) ...................................... GND, W/FINISH (VL0375) (CSD: 047-10880-0001 V22373) ....................................... BUMPER SCAN (V65590) (CSD: 088-03158-0000 V22373) .................... (SEE IPL FIGURE 8 FOR DETAILS)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10070 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
1 (ATTACHING PARTS) ...................................... PHP (4-40 X 1/4) (V56563) (CSD: 089-05878-0004 V22373)
205
089-05878-0004
.SCREW
210
073-00936-0002
.BRACKET
1
215
057-05728-0000
.COVER
1
220
46068-0805S
.SCREW
1
225
36037-3406
.WASHER
1
230
200-05175-0020
.GIMBAL ASSEMBLY
1
235
200-05313-0000
.SCAN SENSOR ASSEMBLY
1
240
089-06494-0007
.SCREW
245
36037-3406
.WASHER
250
089-08158-0011
.WASHER
---*--.................................... PVT BOT W/FINISH (V59848) (CSD: 073-00936-0002 V22373) ...................................... WAVEGUIDE
...................................... SHC (8-32 X 1 1/8) (VBAG02) (CSD: 089-06494-0005 V22373) ..................................... SPLT (LK #8) (VBAG02) (CSD: 089-08111-0034 V22373) ............................ (SEE IPL FIGURE 9 FOR DETAILS) ...................... (SEE IPL FIGURE 11 FOR DETAILS)
(ATTACHING PARTS) ...................................... SHC (8-32 X 7/16) ---*--..................................... SPLT (LK #8) (VBAG02) (CSD: 089-08111-0034 V22373) (ATTACHING PARTS) ..................................... FLAT (#8)
4
4
4
4
---*---
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10071 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
1 255
089-05878-0004
.SCREW
3
260
047-10549-0001
.COVER
1
265
089-05878-0004
.SCREW
270
047-10124-0001
.CLAMP
275
PPLW2C04SSPA
.SCREW
-
280
KL250
.CABLE CLIP
1
-
285
091-00109-0000
.CABLE TIE
2
290
073-00925-0002
.BASE
1
295
035-01540-0018
.BAG STATIC
1
-
...................................... PHP (4-40 X 1/4) (V56563) (CSD: 089-05878-0004 V22373) ...................................... DIP SW, W/FINISH (V16673) (CSD: 047-10549-0001 V22373) (ATTACHING PARTS) ...................................... PHP (4-40 X 1/4) (V56563) (CSD: 089-05878-0004 V22373) ---*--...................................... WIRE TB W/FINISH (ATTACHING PARTS) ...................................... PHP (2-56 X 1/4) (V56563) (CSD: 089-05874-0004 V22373) ---*--.................................. TWIST LOK (V06915) (TRUE PN IS KL-250) (CSD: 090-00988-0000 V22373) ................................... (V56501) (TRUE PN IS TY523M OR TY23M(BULK)) (CSD: 091-00109-0000 V22373) ........................................ W/FINISH (V65267) (CSD: 073-00925-0002 V22373) .................................. (NONPROCURABLE) (18 X 18) (V8Y007) (CSD: 035-01540-0018 V22373)
1
1
3
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10072 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 2. (Sheet 1 of 3) Logic Board (-0000)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10073/10074 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 2. (Sheet 2 of 3) Logic Board (-0000)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10075/10076 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 2. (Sheet 3 of 3) Logic Board (-0000)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10077/10078 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 -
1
200-08549-0000
LOGIC BOARD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (ESDS) (SEE IPL FIGURE 1 ITEM 135 FOR NHA)
RF
-
3
200-08549-0099
.LOGIC BOARD
................................
1
5
26147-0004
..BDX
........................................ (VBAG02) (CSD: 057-03231-0004 V22373)
1
10
090-01019-0020
..FINGER STOCK
2
15
D500000V30
..LOCKING TAB
1
20
089-05878-0004
..SCREW
25
047-05201-0001
..BRACKET . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
............................... (V5X576) (CSD: 090-01019-0020 V22373) ................................ (V28198) (CSD: 030-02352-0007 V22373) (SUPPLIED AS A PAIR) (ATTACHING PARTS) ..................................... PHP (4-40 X 1/4) (V56563) (CSD: 089-05878-0004 V22373)
2
---*--2
W/FINISH (VBAA66) (CSD: 047-05201-0001 V22373) (ATTACHING PARTS) ..................................... PHP (4-40 X 1/4) (VBAG02) (CSD: 089-05903-0004 V22373)
30
089-05903-0004
..SCREW
35
155-02745-0000
..CABLE RIBBON
---*--...............................
2
1
(40 P) (V0VGY3) (CSD: 155-02745-0000 V22373) J5002 40
..CABLE CLIP
KL250
.................................. TWIST LOK (V06915) (CSD: 090-00988-0000 V22373)
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10079 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 45
047-10012-0001
..FENCE
......................................
1
......................................
1
...................................... I/F, W/FINISH
I/F 50
047-10013-0001
..FENCE I/F
55
047-10014-0001
..FENCE
1
60
076-02894-0001
..SPACER
9
65
007-00179-0001
..TRANSISTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
12
..................................... (0.12)
SOT23 (ESDS) (V66958) (CSD: 007-00179-0001 V22373) Q5002, Q5004, Q5006, Q5008, Q5010, Q5012, Q5014, Q5016, Q5018, Q5020, Q5021, Q5023 70
MMBT5087LT1
..TRANSISTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2
PNP (ESDS) (V1MQ07) (CSD: 007-00537-0000 V22373) Q5501, Q5502 75
007-00933-0000
..TRANSISTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
(ESDS) (V55464) (CSD: 007-00933-0000 V22373) Q5503 80
SMCJ7-0A
..TRANSORBER
3
85
007-06179-0000
..DIODE
1
................................ (1500 W, 7 V) (ESDS) (V14552) (TRUE PN IS SMCJ7.0A) (CSD: 007-05241-0007 V22373) CR5017, CR5018, CR5020 ...................................... SI (ESDS) (V50434) (CSD: 007-06179-0000 V22373) CR5008
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10080 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 90
CMPD2836
..DIODE
1
95
007-06184-0000
..DIODE
8
100
BAS28
..DIODE
6
105
007-06448-0000
..DIODE
1
110
008-00096-0001
..TERMINAL TEST POINT
23
115
013-00172-0000
..FERRITE BEAD
2
120
BLM21AF121SN1D
..FERRITE CHIP
7
...................................... DUAL (ESDS) (V55464) (CSD: 007-06181-0000 V22373) CR5013 ...................................... DUAL SWITCHING (ESDS) (V1MQ07) (CSD: 007-06184-0000 V22373) CR5002 thru CR5004, CR5011, CR5014, CR5019, CR5021, CR5022 ...................................... SW DUAL (ESDS) (V26769) (CSD: 007-06396-0000 V22373) CR5005 thru CR5007, CR5009, CR5010, CR5012 ...................................... SCHTKY (1 A, 30 V) (ESDS) (V1MQ07) (CSD: 007-06448-0000 V22373) CR5016 ........................ (V79963) (TRUE PN IS 6069-14 (REEL) OR 1069-14 (LOOSE)) (CSD: 008-00096-0001 V22373) TP5001 thru TP5008, TP5010 thru TP5013, TP5015, TP5018 thru TP5020, TP5022 thru TP5025, TP5027, TP5031, TP5032 ............................... (V34899) (CSD: 013-00172-0000 V22373) L5016, L5017 ................................ IND (V51406) (CSD: 013-00181-0000 V22373) L5004 thru L5006, L5008, L5014, L5018, L5019
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10081 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 125
013-00186-0000
..FERRITE CHOKE
2
130
015-00207-0032
..RESISTOR
................................... OCTAL (10,000 EW) (V91637) (TRUE PN IS SOMC 1603 103G-S399) (CSD: 015-00207-0032 V22373) R5011
1
135
015-00248-0000
..RESISTOR NETWORK . . . . . . . . . . . . . . . . . . . . . . . . . .
1
.............................. Z-MAX (V33062) (CSD: 013-00186-0000 V22373) L5001, L5002
(V59124) (CSD: 015-00248-0000 V22373) R5037 140
RNXW20L5059
..RESISTOR NETWORK . . . . . . . . . . . . . . . . . . . . . . . . . .
2
(V59124) (TRUE PN IS RNXW20 L___5059) (CSD: 015-00249-0000 V22373) R5018, R5019 145
PMBT3906
..TRANSISTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
12
SOT-23 (ESDS) (VBAE55) (CSD: 007-00065-0001 V22373) Q5001, Q5003, Q5005, Q5007, Q5009, Q5011, Q5013, Q5015, Q5017, Q5019, Q5022, Q5024 150
017-00251-0001
..RFI/EMI SUPP FIL
1
155
E526HN100318
..IDCTR
2
160
019-02314-0091
..IDCTR
1
............................. (V51406) (CSD: 017-00251-0001 V22373) FL5001 ...................................... W/O CAN (V 4.5 T) (V08VU6) (TRUE PN IS E526HN-100318) (CSD: 019-02314-0090 V22373) L5501, L5502 ...................................... W/ CAN (V 4.5 T) (V08VU6) (CSD: 019-02314-0091 V22373) L5524
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10082 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 165
1008CS101XKB
..INDUCTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
SM (100 V, 10%) (V02113) (TRUE PN IS 1008CS-101XKB_) (CSD: 019-02660-0013 V22373) L5506 170
019-02660-0015
..INDUCTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2
SM (150 V, 10%) (V02113) (CSD: 019-02660-0015 V22373) L5537, L5538 175
1008CS221XJLC
..INDUCTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
SM (220 V, 5% OR 10%) (V02113) (TRUE PN IS 1008CS-221XJLC) (CSD: 019-02660-0017 V22373) L5539 180
019-02660-0040
..INDUCTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8
SM (10,000 V, 10%) (V02113) (CSD: 019-02660-0040 V22373) L5504, L5505, L5507, L5523, L5525 thru L5527, L5534 185
1008CS820XK
..INDUCTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
SM (82 V, 10%) (V02113) (TRUE PN IS 1008CS-820XK_) (CSD: 019-02660-0050 V22373) L5536 190
019-08265-0001
..TRANSFORMER
.............................. IF (63 MHZ) (V1DA26) (CSD: 019-08265-0001 V22373) T5502
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10083 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 195
019-08265-0002
..TRANSFORMER
.............................. IF (63 MHZ) (V1DA26) (CSD: 019-08265-0002 V22373) T5501
1
200
030-00444-0001
..CONNECTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
SM COAX J5502 205
030-03171-0003
..CONNECTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
HEADER (6 P) (V0VGY3) (CSD: 030-03171-0003 V22373) J5004 210
SEP13055-03
..CONNECTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2
HEADER (V55322) (TRUE PN IS SEP-13055-03) (CSD: 030-03209-0003 V22373) J5005, J5006 215
030-03252-0001
..CONNECTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
FLTR (50 PIN) (PRE SB ART 2000-7) -
215A
030-03252-0008
..CONNECTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
FLTR (50 PIN) (POST SB ART 2000-7) J5001 220
ADF08ST
..SWITCH
1
225
033-00224-0003
..SKT PLCC
1
..................................... DIP (8 POS) (V56501) (CSD: 031-00756-0006 V22373) SW5001 ................................... SM (32 PIN) (V26742) (CSD: 033-00224-0003 V22373) SK5003
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10084 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 230
SG615P10-000MB
..OSCILLATOR
1
235
044-00309-0006
..OSCILLATOR
1
240
T491D476K010AH
..CAPACITOR
1
245
096-01186-0012
..CAPACITOR
2
250
T491A474K025AH
..CAPACITOR
8
255
096-01186-0027
..CAPACITOR
3
260
T491B475M010AH
..CAPACITOR
4
265
096-01186-0064
..CAPACITOR
1
................................. (10 MHZ) (V0HAF7) (TRUE PN IS SG-615P 10.000MB) (CSD: 044-00309-0003 V22373) Y5001 ................................. (41.4 MHZ) (V61722) (CSD: 044-00309-0006 V22373) Y5002 .................................. (47 UF, 10 V, 10%) (V31433) (CSD: 096-01186-0011 V22373) C5006 .................................. (1 UF, 16 V, 10%) (V31433) (CSD: 096-01186-0012 V22373) C5005, C5009 .................................. (0.47 UF, 25 V, 10%) (V31433) (CSD: 096-01186-0020 V22373) C5036, C5037, C5041, C5045, C5047, C5056, C5059, C5085 .................................. (0.33 UF, 35 V, 10%) (V31433) (CSD: 096-01186-0027 V22373) C5001, C5069, C5163 .................................. (4.7 UF, 10 V, 20%) (V31433) (CSD: 096-01186-0059 V22373) C5043, C5058, C5063, C5090
.................................. (10 UF, 16 V, 20%) (V31433) (CSD: 096-01186-0064 V22373) C5519
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10085 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 270
106-00122-0000
..CAPACITOR CHIP
2
275
106-00124-0000
..CAPACITOR CHIP
2
280
AQ147A510JAJM
..CH MCRWV NPO
1
285
106-00126-0004
..CH MCRWV NPO
1
290
AQ147A300JAJ
..CH MCRWV NPO
1
295
106-00126-0007
..CH MCRWV NPO
1
300
AQ147A101JAJMA
..CH MCRWV NPO
1
305
106-00126-0012
..CH MCRWV NPO
1
............................. CER (0.33 UF, 50 V, 10%) (V51406) (TRUE PN IS GRM43-2X7R334K050B_) (CSD: 106-00122-0000 V22373) C5046, C5061 ............................. (0.15 UF, 500 V) (V95275) (CSD: 106-00124-0000 V22373) C5160, C5161 .............................. (51 PF) (V04222) (TRUE PN IS AQ147A510JAJM_) (CSD: 106-00126-0003 V22373) C5503 .............................. (1000 PF) (V04222) (CSD: 106-00126-0004 V22373) C5527
.............................. (30 PF) (V04222) (TRUE PN IS AQ147A300JAJ_) (CSD: 106-00126-0005 V22373) C5542 .............................. (0.8 PF) (V04222) (CSD: 106-00126-0007 V22373) C5502 .............................. (100 PF) (V04222) (CSD: 106-00126-0010 V22373) C5504 .............................. (24 PF) (V51406) (CSD: 106-00126-0012 V22373) C5501
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10086 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 310
106-00133-0001
..CAPACITOR CHIP
3
315
106-00133-0005
..CAPACITOR CHIP
1
320
106-04100-0016
..CAPACITOR CHIP
1
325
106-04101-0026
..CAPACITOR CHIP
13
330
106-04102-0046
..CAPACITOR CHIP
8
335
106-04103-0046
..CAPACITOR CHIP
5
340
106-04104-0046
..CAPACITOR CHIP
96
............................. (33 PF) (V51406) (TRUE PN IS GRM42-6S2H330J050__) (CSD: 106-00133-0001 V22373) C5528, C5529, C5543 ............................. (33 PF) (V51406) (CSD: 106-00133-0005 V22373) C5576
............................. (10 PF, 50 V) (V51406) (TRUE PN IS GRM42-CC0G100J050B) (CSD: 106-04100-0016 V22373) C5165 ............................. (100 PF, 100 V) (V51406) (CSD: 106-04101-0026 V22373) C5014 thru C5024, C5064, C5164 ............................. (1000 PF, 50 V, 5%) (V51406) (TRUE PN IS GRM42-6X7R102J050B) (CSD: 106-04102-0046 V22373) C5038, C5042, C5048, C5049, C5051 thru C5054
............................. (10,000 PF, 50 V) (V51406) (CSD: 106-04103-0046 V22373) C5025, C5039, C5057, C5062, C5093 ............................. (0.1 UF, 50 V) (V51406) (TRUE PN IS GRM42-6X7R104J050B) (CSD: 106-04104-0046 V22373) C5002 thru C5004, C5007, C5008, C5026 thru C5035, C5050, C5065, C5070, C5071, C5073, C5074, C5076, C5078 thru C5084, C5086 thru C5089, C5091, C5094 thru C5142, C5145 thru C5156, C5158
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10087 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 345
106-04180-0026
..CAPACITOR CHIP
1
350
BCA1271FTM
..RESISTOR CHIP
1
355
139-01332-0000
..RESISTOR CHIP
1
360
BCA1371FTM
..RESISTOR CHIP
1
365
139-01372-0000
..RESISTOR
1
370
BCA1501FTM
..RESISTOR CHIP
5
375
139-01502-0000
..RESISTOR CHIP
1
380
BCA1541FTM
..RESISTOR CHIP
1
385
139-01622-0000
..RESISTOR CHIP
1
............................. (18 PF, 100 V) (V51406) (CSD: 106-04180-0026 V22373) C5044 .............................. (1270 EW, 1%) (VS8185) (CSD: 139-01271-0000 V22373) R5510 .............................. (13,300 EW, 1%) (VS8185) (CSD: 139-01332-0000 V22373) R5538 .............................. (1370 EW, 1%) (VS8185) (CSD: 139-01371-0000 V22373) R5064 ................................... (13,700 EW, 1%) (VS8185) (CSD: 139-01372-0000 V22373) R5065
.............................. (1500 EW, 1%) (VS8185) (CSD: 139-01501-0000 V22373) R5021, R5022, R5045, R5048, R5059 .............................. (15,000 EW, 1%) (VS8185) (CSD: 139-01502-0000 V22373) R5085 .............................. (1540 EW, 1%) (VS8185) (CSD: 139-01541-0000 V22373) R5150 .............................. (16,200 EW, 1%) (VS8185) (CSD: 139-01622-0000 V22373) R5285
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10088 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 395
139-01822-0000
..RESISTOR CHIP
3
400
CRCW12062000F
..RESISTOR CHIP
1
405
139-02001-0000
..RESISTOR CHIP
1
410
BCA2002FTM
..RESISTOR CHIP
8
415
139-02211-0000
..RESISTOR CHIP
2
420
BCA2212FTM
..RESISTOR CHIP
3
425
139-02372-0000
..RESISTOR
1
430
BCA2431FTM
..RESISTOR CHIP
2
.............................. (18,200 EW, 1%) (VS8185) (CSD: 139-01822-0000 V22373) R5260, R5502, R5505 .............................. (200 EW, 1%) (V91637) (TRUE PN IS CRCW12062000F___) (CSD: 139-02000-0000 V22373) R5295 .............................. (2000 EW, 1%) (VS8185) (CSD: 139-02001-0000 V22373) R5126 .............................. (20,000 EW, 1%) (VS8185) (CSD: 139-02002-0000 V22373) R5010, R5014, R5016, R5023, R5025, R5063, R5066, R5095 .............................. (2210 EW, 1%) (VS8185) (CSD: 139-02211-0000 V22373) R5044, R5049 .............................. (22,100 EW, 1%) (VS8185) (CSD: 139-02212-0000 V22373) R5042, R5043, R5127 ................................... (23,700 EW, 1%) (VS8185) (CSD: 139-02372-0000 V22373) R5259
.............................. (2430 EW, 1%) (VS8185) (CSD: 139-02431-0000 V22373) R5015, R5024
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10089 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 435
139-02553-0000
..RESISTOR CHIP
1
440
BCA2670FTM
..RESISTOR
1
445
139-02742-0000
..RESISTOR CHIP
4
450
BCA2801FTM
..RESISTOR CHIP
1
455
139-03010-0000
..RESISTOR CHIP
2
460
BCA3012FTM
..RESISTOR CHIP
2
465
139-03013-0000
..RESISTOR CHIP
12
470
BCA3091FTM
..RESISTOR CHIP
1
.............................. (255,000 EW, 1%) (VS8185) (CSD: 139-02553-0000 V22373) R5058 ................................... (267 EW, 1%) (VS8185) (CSD: 139-02670-0000 V22373) R5158 .............................. (27,400 EW, 1%) (VS8185) (CSD: 139-02742-0000 V22373) R5282, R5501, R5503, R5506 .............................. (2800 EW, 1%) (VS8185) (CSD: 139-02801-0000 V22373) R5532 .............................. (301 EW, 1%) (V91637) (CSD: 139-03010-0000 V22373) R5035, R5125 .............................. (30,100 EW, 1%) (VS8185) (CSD: 139-03012-0000 V22373) R5166, R5250 .............................. (301,000 EW, 1%) (VS8185) (CSD: 139-03013-0000 V22373) R5028, R5173, R5176, R5179, R5182, R5185, R5188, R5191, R5264, R5267, R5270, R5273 .............................. (3090 EW, 1%) (VS8185) (CSD: 139-03091-0000 V22373) R5020
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10090 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 475
139-03241-0000
..RESISTOR CHIP
1
480
BCA3242FTM
..RESISTOR CHIP
1
485
139-03323-0000
..RESISTOR CHIP
1
490
BCA3922FTM
..RESISTOR CHIP
3
495
136-04222-0062
..RESISTOR CHIP
1
500
CRCW12064321F
..RESISTOR CHIP
2
505
139-04750-0000
..RESISTOR CHIP
16
510
BCA4751FTM
..RESISTOR CHIP
4
.............................. (3240 EW, 1%) (VS8185) (CSD: 139-03241-0000 V22373) R5225 .............................. (32,400 EW, 1%) (VS8185) (CSD: 139-03242-0000 V22373) R5031 .............................. (332,000 EW, 1%) (VS8185) (CSD: 139-03323-0000 V22373) R5030 .............................. (39,200 EW, 1%) (VS8185) (CSD: 139-03922-0000 V22373) R5275, R5525, R5527 .............................. (42,200 EW, 1%) R5061 .............................. (4320 EW, 1%) (V91637) (TRUE PN IS CRCW12064321F___) (CSD: 139-04321-0000 V22373) R5060, R5070
.............................. (475 EW, 1%) (VS8185) (CSD: 139-04750-0000 V22373) R5006, R5009, R5013, R5051, R5071, R5073, R5119 thru R5122, R5276, R5278, R5279, R5290 thru R5292 .............................. (4750 EW, 1%) (VS8185) (CSD: 139-04751-0000 V22373) R5138, R5535 thru R5537
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10091 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 515
139-04752-0000
..RESISTOR CHIP
6
520
BCA4991FTM
..RESISTOR CHIP
10
525
139-04992-0000
..RESISTOR CHIP
1
530
BCA5111FTM
..RESISTOR CHIP
1
535
139-05112-0000
..RESISTOR CHIP
1
540
BCA5230FTM
..RESISTOR CHIP
1
545
139-05621-0000
..RESISTOR CHIP
1
550
BCA5622FTM
..RESISTOR CHIP
8
.............................. (47,500 EW, 1%) (VS8185) (CSD: 139-04752-0000 V22373) R5053 thru R5056, R5088, R5507 .............................. (4990 EW, 1%) (VS8185) (CSD: 139-04991-0000 V22373) R5008, R5077, R5082, R5089, R5104, R5108, R5157, R5167, R5226, R5299 .............................. (49,900 EW, 1%) (VS8185) (CSD: 139-04992-0000 V22373) R5032 .............................. (5110 EW, 1%) (VS8185) (CSD: 139-05111-0000 V22373) R5534 .............................. (51,100 EW, 1%) (VS8185) (CSD: 139-05112-0000 V22373) R5107 .............................. (523 EW, 1%) (VS8185) (CSD: 139-05230-0000 V22373) R5224 .............................. (5620 EW, 1%) (VS8185) (CSD: 139-05621-0000 V22373) R5222 .............................. (56,200 EW, 1%) (VS8185) (CSD: 139-05622-0000 V22373) R5227 thru R5234
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10092 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 555
139-05761-0000
..RESISTOR CHIP
2
560
BCA6811FTM
..RESISTOR CHIP
2
565
139-07151-0000
..RESISTOR CHIP
1
570
139-07870-0000
..RESISTOR CHIP
1
575
139-07500-0000
..RESISTOR CHIP
1
580
CRCW12067501F
..RESISTOR CHIP
2
585
139-07502-0000
..RESISTOR CHIP
13
590
139-07682-0000
..RESISTOR CHIP
1
.............................. (5760 EW, 1%) (VS8185) (CSD: 139-05761-0000 V22373) R5062, R5087 .............................. (6810 EW, 1%) (VS8185) (CSD: 139-06811-0000 V22373) R5098, R5113 .............................. (7150 EW, 1%) (VS8185) (CSD: 139-07151-0000 V22373) R5531 .............................. (787 EW, 1%) R5509 .............................. (750 EW, 1%) (VS8185) (CSD: 139-07500-0000 V22373) R5539 .............................. (7500 EW, 1%) (V91637) (TRUE PN IS CRCW12067501F___) (CSD: 139-07501-0000 V22373) R5223, R5247 .............................. (75,000 EW, 1%) (VS8185) (CSD: 139-07502-0000 V22373) R5174, R5177, R5180, R5183, R5186, R5189, R5192, R5195, R5221, R5265, R5268, R5271, R5274 .............................. (76,800 EW, 1%) (VS8185) (CSD: 139-07682-0000 V22373) R5092
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10093 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 595
139-08061-0000
..RESISTOR CHIP
2
600
BCA8662FTM
..RESISTOR CHIP
1
605
139-08872-0000
..RESISTOR CHIP
1
610
BCA9090FTM
..RESISTOR CHIP
1
615
120-02494-0000
..INTEGRATED CIRCUIT
.............................. (8060 EW, 1%) (VS8185) (CSD: 139-08061-0000 V22373) R5017, R5026 .............................. (86,600 EW, 1%) (VS8185) (CSD: 139-08662-0000 V22373) R5132 .............................. (88,700 EW, 1%) (VS8185) (CSD: 139-08872-0000 V22373) R5168 .............................. (909 EW, 1%) (VS8185) (CSD: 139-09090-0000 V22373) R5159 .........................
1
.............................. (121,000 EW, 1%) (VS8185) (CSD: 139-01213-0000 V22373) R5076
NOVRAM PLCC (X20C16) (ESDS) U5005 620
BCA1213FTM
..RESISTOR CHIP
1
625
106-05101-0016
..CAPACITOR CHIP
3
630
106-05102-0016
..CAPACITOR CHIP
31
............................. (100 PF, 50 V) (V51406) (CSD: 106-05101-0016 V22373) C5507, C5574, C5575 ............................. (1000 PF, 50 V) (V51406) (TRUE PN IS GRM40C0G102J050B) (CSD: 106-05102-0016 V22373) C5505, C5506, C5508, C5509, C5511 thru C5513, C5515, C5516, C5518, C5520, C5523, C5524, C5526, C5530 thru C5532, C5534 thru C5537, C5539 thru C5541, C5545, C5551, C5567, C5572, C5587 thru C5589
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10094 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 635
106-05103-0046
..CAPACITOR CHIP
2
640
106-05104-0037
..CAPACITOR CHIP
2
645
106-05121-0016
..CAPACITOR CHIP
1
650
106-05200-0016
..CAPACITOR CHIP
1
655
106-05270-0016
..CAPACITOR CHIP
2
660
106-05271-0016
..CAPACITOR CHIP
1
665
106-05470-0016
..CAPACITOR CHIP
2
670
C0805C680J5GAC
..CAPACITOR CHIP
1
............................. (10,000 PF, 50 V) (V51406) (CSD: 106-05103-0046 V22373) C5521, C5525 ............................. (100,000 PF, 25 V) (V51406) (TRUE PN IS GRM40X7R104K025B) (CSD: 106-05104-0037 V22373) C5577, C5578
............................. (120 PF, 50 V) (V51406) (CSD: 106-05121-0016 V22373) C5544 ............................. (20 PF, 50 V) (V51406) (TRUE PN IS GRM40C0G200J050B) (CSD: 106-05200-0016 V22373) C5568 ............................. (27 PF, 50 V) (V51406) (CSD: 106-05270-0016 V22373) C5533, C5538 ............................. (270 PF, 50 V) (V51406) (TRUE PN IS GRM40C0G271J050B) (CSD: 106-05271-0016 V22373) C5584 ............................. (47 PF, 50 V) (V51406) (CSD: 106-05470-0016 V22373) C5510, C5514 ............................. (68 PF, 50 V) (V31433) (CSD: 106-05680-0016 V22373) C5517
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10095 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 675
120-02213-0002
..INTEGRATED CIRCUIT
1
680
MAX4426ESA
..INTEGRATED CIRCUIT
1
685
120-02452-0000
..INTEGRATED CIRCUIT
1
690
XC3042A7PQ100I
..INTEGRATED CIRCUIT
4
695
120-02981-0112
..INTEGRATED CIRCUIT
4
700
ML1350-5P
..INTEGRATED CIRCUIT
4
705
120-03026-0080
..INTEGRATED CIRCUIT
1
......................... Z80 PLCC (10 MHZ) (ESDS) (V56708) (CSD: 120-02213-0002 V22373) U5001 ......................... DUAL DRIVER (ESDS) (V1ES66) (CSD: 120-02233-0003 V22373) U5048 ......................... RESET/WTCHDG CNTL (ESDS) (V1ES66) (CSD: 120-02452-0000 V22373) U5002
......................... 3042 GATE ARRAY (ESDS) (V68994) (TRUE PN IS XC3042A-7PQ100I) (CSD: 120-02469-0001 V22373) U5012, U5037, U5041, U5057 ......................... SOJ (32K X 8, 28 PIN) (ESDS) (V65786) (CSD: 120-02981-0112 V22373) U5004, U5039, U5059, U5118
......................... IF AMP SO (ESDS) (V58625) (CSD: 120-03020-0001 V22373) U5501, U5502, U5504, U5505 ......................... 78M05 DPAK VLT REG (ESDS) (V1MQ07) (CSD: 120-03026-0080 V22373) U5032
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10096 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 710
MC78M08BDT
..INTEGRATED CIRCUIT
1
715
120-03027-0004
..INTEGRATED CIRCUIT
1
720
LM2904M
..INTEGRATED CIRCUIT
1
725
120-03126-0005
..INTEGRATED CIRCUIT
1
730
LM2901D
..INTEGRATED CIRCUIT
1
735
120-03174-0013
..INTEGRATED CIRCUIT
3
740
TL084ID
..INTEGRATED CIRCUIT
7
......................... 78M08 DPAK VLT REG (ESDS) (V1MQ07) (CSD: 120-03026-0082 V22373) U5040 ......................... BALANCED MOD/DEMOD (ESDS) (V1MQ07) (CSD: 120-03027-0004 V22373) U5506 ......................... SO PKG (ESDS) (V27014) (CSD: 120-03053-0010 V22373) U5144 ......................... (ESDS) (V27014) (CSD: 120-03126-0005 V22373) U5042 ......................... SO-14 COMP (ESDS) (V66958) (CSD: 120-03163-0001 V22373) U5033 ......................... OP AMP BI FET SO (ESDS) (V82647) (CSD: 120-03174-0013 V22373) U5026, U5122, U5507 ......................... OP AMP BI FET SO (ESDS) (V82647) (CSD: 120-03174-0014 V22373) U5021, U5028, U5031, U5034, U5035, U5159, U5160
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10097 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 745
120-03285-0002
..INTEGRATED CIRCUIT
1
750
DG441DY
..INTEGRATED CIRCUIT
1
755
120-03400-0001
..INTEGRATED CIRCUIT
1
760
TLC0820AIDW
..INTEGRATED CIRCUIT
1
765
120-03488-0000
..INTEGRATED CIRCUIT
1
770
120-03501-0000
..INTEGRATED CIRCUIT
1
775
120-03592-0000
..INTEGRATED CIRCUIT
1
......................... A/D CONVERT CA3306 (ESDS) U5030 ......................... QUAD SWITCH (ESDS) (V17856) (CSD: 120-03393-0002 V22373) U5162 ......................... REF-02 PREC V REG (ESDS) (V1ES66) (CSD: 120-03400-0001 V22373) U5171 ......................... 8-BIT A/D SO (ESDS) (V82647) (CSD: 120-03475-0003 V22373) U5024 ......................... PM7224FS DAC (ESDS) (V24355) (CSD: 120-03488-0000 V22373) U5119 ......................... HIGH SPEED DP-AMP (ESDS) (V24355) (TRUE PN IS AD847AR (EXCLUDING 9942 DATE CODE)) (CSD: 120-03501-0000 V22373) U5503 ......................... CMOS QUAD 8-BIT DAC (ESDS) (V24355) (CSD: 120-03592-0000 V22373) U5027
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10098 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 780
DG442DY
..INTEGRATED CIRCUIT
785
120-03598-0000
..INTEGRATED CIRCUIT
......................... QUAD SW (ESDS) (V17856) (CSD: 120-03593-0000 V22373) U5163
1
.........................
1
.................................. (VS6019) (CSD: 120-03599-0000 V22373) CR5015
HI5700 8-BIT A/D (ESDS) U5036
-
790
SP720AB
..ESD ARRAY
1
795
120-06065-0002
..INTEGRATED CIRCUIT
1
800
06562-047
..INTEGRATED CIRCUIT
1
805
126-00089-0003
..WX COMP ROM
1
......................... 10-BIT SO (0.10%) (ESDS) (V24355) (CSD: 120-06065-0002 V22373) U5165 ......................... 429 ARINC LSI, 28 PIN PLCC (ESDS) (V31471) (CSD: 120-08030-0010 V22373) U5091 ...............................
(ESDS)
-
810
122-30048-0002
...INTEGRATED CIRCUIT
1
810A
122-30048-0003
...INTEGRATED CIRCUIT
1
820
SN74HC03D
..INTEGRATED CIRCUIT
1
......................... (ESDS) (PRE SB ART 2000-6)
......................... (ESDS) (POST SB ART 2000-6) U5038 ......................... SO (ESDS) (V82647) (CSD: 123-00003-0003 V22373) U5125
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10099 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 825
123-00573-0003
..INTEGRATED CIRCUIT
2
830
74HC4351D
..INTEGRATED CIRCUIT
2
835
124-00008-0003
..INTEGRATED CIRCUIT
1
840
74ACT139SC
..INTEGRATED CIRCUIT
1
845
124-00157-0003
..INTEGRATED CIRCUIT
1
850
74HCT245D
..INTEGRATED CIRCUIT
5
855
124-00573-0003
..INTEGRATED CIRCUIT
3
......................... SO (ESDS) (V7D893) (CSD: 123-00573-0003 V22373) U5006, U5043 ......................... MUXIDEMUX (ESDS) (V1CH66) (CSD: 123-04351-0003 V22373) U5022, U5023 ......................... SO PKG (ESDS) (V7D893) (CSD: 124-00008-0003 V22373) U5018 ......................... (ESDS) (V7D893) (CSD: 124-00139-1003 V22373) U5020 ......................... SO PKG (ESDS) (V1CH66) (CSD: 124-00157-0003 V22373) U5025 ......................... SO PKG (ESDS) (V1CH66) (CSD: 124-00245-0002 V22373) U5014 thru U5016, U5029, U5126 ......................... SO (ESDS) (V1CH66) (CSD: 124-00573-0003 V22373) U5007, U5017, U5019
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10100 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2
-
860
74HCT574D
..INTEGRATED CIRCUIT
7
865
126-00047-0004
..FPGA ROM
1
......................... (ESDS) (V0JN86) (CSD: 124-00574-0003 V22373) U5008 thru U5011, U5166, U5168, U5169 ..................................
(ESDS) 866
122-30049-0004
...INTEGRATED CIRCUIT
.........................
1
.............................. (0 QW) (V91637) (CSD: 130-05000-0035 V22373) CJ5001 thru CJ5005
(ESDS) U5013 870
130-05000-0035
..RESISTOR CHIP
5
875
CRCW120604R7J
..RESISTOR CHIP
2
880
130-05561-0043
..RESISTOR CHIP
2
885
V82RA8
..VARISTOR
1
890
139-00100-0000
..RESISTOR CHIP
3
895
BCA20R0FTM
..RESISTOR CHIP
1
.............................. (4.7 QW, 5%) (V91637) (TRUE PN IS CRCW120604R7J___) (CSD: 130-05047-0033 V22373) R5130, R5131 .............................. (560 HW, 5%) (V91637) (CSD: 130-05561-0043 V22373) R5511, R5512 ................................... (82 V) (V75915) (CSD: 134-02001-0000 V22373) V5001 .............................. (10 EW, 1%) (VS8185) (CSD: 139-00100-0000 V22373) R5160, R5533, R5551 .............................. (20 EW, 1%) (VS8185) (CSD: 139-00200-0000 V22373) R5552
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10101 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 900
139-00309-0000
..RESISTOR CHIP
2
905
BCA44R2FTM
..RESISTOR CHIP
1
910
139-00499-0000
..RESISTOR CHIP
1
915
139-00750-0000
..RESISTOR CHIP
.............................. (30.9 EW, 1%) (VS8185) (CSD: 139-00309-0000 V22373) R5039, R5040 .............................. (44.2 EW, 1%) (VS8185) (CSD: 139-00442-0000 V22373) R5550 .............................. (49.9 EW, 1%) (VS8185) (CSD: 139-00499-0000 V22373) R5560 ..............................
1
.............................. (100 EW, 1%) (VS8185) (CSD: 139-01000-0000 V22373) R5210, R5529, R5530, R5555
(75 EW, 1%) R5508 920
139-01000-0000
..RESISTOR CHIP
4
925
BCA1001FTM
..RESISTOR CHIP
11
930
139-01002-0000
..RESISTOR CHIP
67
.............................. (1000 EW, 1%) (VS8185) (CSD: 139-01001-0000 V22373) R5038, R5041, R5093, R5099, R5114, R5137, R5139 thru R5141, R5171, R5294 .............................. (10,000 EW, 1%) (VS8185) (CSD: 139-01002-0000 V22373) R5001 thru R5003, R5007, R5012, R5033, R5052, R5067 thru R5069, R5072, R5074, R5078 thru R5081, R5083, R5084, R5086, R5090, R5091, R5096, R5097, R5101 thru R5103, R5105, R5106, R5111, R5112, R5116, R5123, R5128, R5133, R5152, R5153, R5155, R5165, R5170, R5172, R5175, R5178, R5181, R5184, R5187, R5190, R5249, R5258, R5262, R5263, R5266, R5269, R5272, R5280, R5281, R5283, R5289, R5296, R5297, R5514, R5540, R5541, R5544, R5548, R5557 thru R5559
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10102 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2 935
106-04330-0026
..CAPACITOR CHIP
4
940
139-01003-0000
..RESISTOR CHIP
2
945
BCA1004FTM
..RESISTOR CHIP
3
950
139-01023-0000
..RESISTOR CHIP
1
955
BCA1053FTM
..RESISTOR CHIP
1
960
139-01071-0000
..RESISTOR CHIP
1
965
BCA1212FTM
..RESISTOR CHIP
3
970
009-08549-0000
..PC BOARD
1
............................. (33 PF, 100 V) (V51406) (TRUE PN IS GRM42-6C0G330J100B) (CSD: 106-04330-0026 V22373) C5010 thru C5013 .............................. (100,000 EW, 1%) (VS8185) (CSD: 139-01003-0000 V22373) R5029, R5284 .............................. (1M EW, 1%) (VS8185) (CSD: 139-01004-0000 V22373) R5094, R5100, R5115 .............................. (105,000 EW, 1%) (VS8185) (CSD: 139-01023-0000 V22373) R5057 .............................. (105,000 EW, 1%) (VS8185) (CSD: 139-01053-0000 V22373) R5075 .............................. (1070 EW, 1%) (VS8185) (CSD: 139-01071-0000 V22373) R5151 .............................. (12,100 EW, 1%) (VS8185) (CSD: 139-01212-0000 V22373) R5046, R5047, R5556 ...................................
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10103 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10104 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 2A. (Sheet 1 of 3) Logic Board (-0020)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10105/10106 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 2A. (Sheet 2 of 3) Logic Board (-0020)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10107/10108 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 2A. (Sheet 3 of 3) Logic Board (-0020)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10109/10110 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A -
1
200-08549-0020
LOGIC BOARD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (ESDS) (SEE IPL FIGURE 1 ITEM 135A FOR NHA)
RF
5
26147-0004
.BDX
1
10
090-01019-0020
.FINGER STOCK
2
15
D500000V30
.LOCKING TAB
1
20
089-05878-0004
.SCREW
25
047-05201-0001
.BRACKET
30
089-05903-0004
.SCREW
35
155-02745-0000
.CABLE RIBBON
......................................... (VBAG02) (CSD: 057-03231-0004 V22373) ............................... (V5X576) (CSD: 090-01019-0020 V22373) ................................. (V28198) (CSD: 030-02352-0007 V22373) (SUPPLIED AS A PAIR) (ATTACHING PARTS) ...................................... PHP (4-40 X 1/4) (V56563) (CSD: 089-05878-0004 V22373) ---*--.................................... W/FINISH (VBAA66) (CSD: 047-05201-0001 V22373) (ATTACHING PARTS) ...................................... PHP (4-40 X 1/4) (VBAG02) (CSD: 089-05903-0004 V22373) ---*--...............................
2
2
2
1
(40 P) (V0VGY3) (CSD: 155-02745-0000 V22373) J5002 40
KL250
.CABLE CLIP
1
45
047-10012-0001
.FENCE
1
.................................. TWIST LOK (V06915) (CSD: 090-00988-0000 V22373) ......................................
I/F
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10111 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 50
047-10013-0001
.FENCE
......................................
1
...................................... I/F, W/FINISH
I/F 55
047-10014-0001
.FENCE
1
60
076-02894-0001
.SPACER
9
65
007-00179-0001
.TRANSISTOR
12
70
MMBT5087LT1
.TRANSISTOR
2
75
007-00933-0000
.TRANSISTOR
1
80
SMCJ7-0A
.TRANSORBER
3
85
007-06179-0000
.DIODE
1
90
CMPD2836
.DIODE
1
..................................... (0.12) ................................. SOT23 (ESDS) (V66958) (CSD: 007-00179-0001 V22373) Q5002, Q5004, Q5006, Q5008, Q5010, Q5012, Q5014, Q5016, Q5018, Q5020, Q5021, Q5023
................................. PNP (ESDS) (V1MQ07) (CSD: 007-00537-0000 V22373) Q5501, Q5502 ................................. (ESDS) (V55464) (CSD: 007-00933-0000 V22373) Q5503 ................................ (1500 W, 7 V) (ESDS) (V14552) (TRUE PN IS SMCJ7.0A) (CSD: 007-05241-0007 V22373) CR5017, CR5018, CR5020 ....................................... SI (ESDS) (V50434) (CSD: 007-06179-0000 V22373) CR5008 ....................................... DUAL (ESDS) (V55464) (CSD: 007-06181-0000 V22373) CR5013
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10112 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 95
007-06184-0000
.DIODE
8
100
BAS28
.DIODE
6
105
007-06448-0000
.DIODE
1
110
008-00096-0001
.TERMINAL TEST POINT
23
115
013-00172-0000
.FERRITE BEAD
2
120
BLM21AF121SN1D
.FERRITE CHIP
7
125
013-00186-0000
.FERRITE CHOKE
2
....................................... DUAL SWITCHING (ESDS) (V1MQ07) (CSD: 007-06184-0000 V22373) CR5002 thru CR5004, CR5011, CR5014, CR5019, CR5021, CR5022 ....................................... SW DUAL (ESDS) (V26769) (CSD: 007-06396-0000 V22373) CR5005 thru CR5007, CR5009, CR5010, CR5012
....................................... SCHTKY (1 A, 30 V) (ESDS) (V1MQ07) (CSD: 007-06448-0000 V22373) CR5016 ......................... (V79963) (TRUE PN IS 6069-14 (REEL) OR 1069-14 (LOOSE)) (CSD: 008-00096-0001 V22373) TP5001 thru TP5008, TP5010 thru TP5013, TP5015, TP5018 thru TP5020, TP5022 thru TP5025, TP5027, TP5031, TP5032 ................................ (V34899) (CSD: 013-00172-0000 V22373) L5016, L5017 ................................ IND (V51406) (CSD: 013-00181-0000 V22373) L5004 thru L5006, L5008, L5014, L5018, L5019 .............................. Z-MAX (V33062) (CSD: 013-00186-0000 V22373) L5001, L5002
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10113 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 130
015-00207-0032
.RESISTOR
1
135
015-00248-0000
.RESISTOR NETWORK
1
140
RNXW20L5059
.RESISTOR NETWORK
2
145
PMBT3906
.TRANSISTOR
12
150
017-00251-0001
.RFI/EMI SUPP FIL
1
155
E526HN100318
.IDCTR
2
160
019-02314-0091
.IDCTR
1
................................... OCTAL (10,000 EW) (V91637) (TRUE PN IS SOMC 1603 103G-S399) (CSD: 015-00207-0032 V22373) R5011 .......................... (V59124) (CSD: 015-00248-0000 V22373) R5037 .......................... (V59124) (TRUE PN IS RNXW20 L___5059) (CSD: 015-00249-0000 V22373) R5018, R5019 ................................. SOT-23 (ESDS) (VBAE55) (CSD: 007-00065-0001 V22373) Q5001, Q5003, Q5005, Q5007, Q5009, Q5011, Q5013, Q5015, Q5017, Q5019, Q5022, Q5024 .............................. (V51406) (CSD: 017-00251-0001 V22373) FL5001 ....................................... W/O CAN (V 4.5 T) (V08VU6) (TRUE PN IS E526HN-100318) (CSD: 019-02314-0090 V22373) L5501, L5502 ....................................... W/ CAN (V 4.5 T) (V08VU6) (CSD: 019-02314-0091 V22373) L5524
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10114 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 165
1008CS101XKB
.INDUCTOR
1
170
019-02660-0015
.INDUCTOR
2
175
1008CS221XJLC
.INDUCTOR
1
180
019-02660-0040
.INDUCTOR
8
185
1008CS820XK
.INDUCTOR
1
190
019-08265-0001
.TRANSFORMER
1
................................... SM (100 V, 10%) (V02113) (TRUE PN IS 1008CS-101XKB_) (CSD: 019-02660-0013 V22373) L5506 ................................... SM (150 V, 10%) (V02113) (CSD: 019-02660-0015 V22373) L5537, L5538
................................... SM (220 V, 5% OR 10%) (V02113) (TRUE PN IS 1008CS-221XJLC) (CSD: 019-02660-0017 V22373) L5539
................................... SM (10,000 V, 10%) (V02113) (CSD: 019-02660-0040 V22373) L5504, L5505, L5507, L5523, L5525 thru L5527, L5534 ................................... SM (82 V, 10%) (V02113) (TRUE PN IS 1008CS-820XK_) (CSD: 019-02660-0050 V22373) L5536 ............................... IF (63 MHZ) (V1DA26) (CSD: 019-08265-0001 V22373) T5502
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10115 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 195
019-08265-0002
.TRANSFORMER
1
200
030-00464-0000
.CONNECTOR
1
205
030-03171-0003
.CONNECTOR
1
210
SEP13055-03
.CONNECTOR
2
215
030-03252-0008
.CONNECTOR
1
220
ADF08ST
.SWITCH
1
225
033-00224-0003
.SKT PLCC
1
............................... IF (63 MHZ) (V1DA26) (CSD: 019-08265-0002 V22373) T5501 ................................. RF, RECPT (V0GP12) (CSD: 030-00464-0000 V22373) J5502 ................................. HEADER (6 P) (V0VGY3) (CSD: 030-03171-0003 V22373) J5004 ................................. HEADER (V55322) (TRUE PN IS SEP-13055-03) (CSD: 030-03209-0003 V22373) J5005, J5006 ................................. PLG, D-SUB (V33095) (CSD: 030-03252-0008 V22373) (SEL FR PN: V) J5001 ..................................... DIP (8 POS) (V56501) (CSD: 031-00756-0006 V22373) SW5001
.................................... SM (32 PIN) (V26742) (CSD: 033-00224-0003 V22373) SK5003
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10116 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 230
SG615P10-000MB
.OSCILLATOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
(10 MHZ) (V0HAF7) (TRUE PN IS SG-615P 10.000MB) (CSD: 044-00309-0003 V22373) Y5001 235
044-00309-0006
.OSCILLATOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
(41.4 MHZ) (V61722) (CSD: 044-00309-0006 V22373) Y5002 240
T491D476K010AH
.CAPACITOR
1
245
096-01186-0012
.CAPACITOR
2
250
T491A474K025AH
.CAPACITOR
8
255
096-01186-0027
.CAPACITOR
3
260
T491B475M010AH
.CAPACITOR
4
265
096-01186-0064
.CAPACITOR
1
.................................. (47 UF, 10 V, 10%) (V31433) (CSD: 096-01186-0011 V22373) C5006 .................................. (1 UF, 16 V, 10%) (V31433) (CSD: 096-01186-0012 V22373) C5005, C5009
.................................. (0.47 UF, 25 V, 10%) (V31433) (CSD: 096-01186-0020 V22373) C5036, C5037, C5041, C5045, C5047, C5056, C5059, C5085 .................................. (0.33 UF, 35 V, 10%) (V31433) (CSD: 096-01186-0027 V22373) C5001, C5069, C5163 .................................. (4.7 UF, 10 V, 20%) (V31433) (CSD: 096-01186-0059 V22373) C5043, C5058, C5063, C5090
.................................. (10 UF, 16 V, 20%) (V31433) (CSD: 096-01186-0064 V22373) C5519
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10117 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 270
106-00122-0000
.CAPACITOR CHIP
2
275
106-00124-0000
.CAPACITOR CHIP
2
280
AQ147A510JAJM
.CH MCRWV NPO
1
285
106-00126-0004
.CH MCRWV NPO
1
290
AQ147A300JAJ
.CH MCRWV NPO
1
295
106-00126-0007
.CH MCRWV NPO
1
300
AQ147A101JAJMA
.CH MCRWV NPO
1
305
106-00126-0012
.CH MCRWV NPO
1
.............................. CER (0.33 UF, 50 V, 10%) (V51406) (TRUE PN IS GRM43-2X7R334K050B_) (CSD: 106-00122-0000 V22373) C5046, C5061 .............................. (0.15 UF, 500 V) (V95275) (CSD: 106-00124-0000 V22373) C5160, C5161 .............................. (51 PF) (V04222) (TRUE PN IS AQ147A510JAJM_) (CSD: 106-00126-0003 V22373) C5503 .............................. (1000 PF) (V04222) (CSD: 106-00126-0004 V22373) C5527
.............................. (30 PF) (V04222) (TRUE PN IS AQ147A300JAJ_) (CSD: 106-00126-0005 V22373) C5542 .............................. (0.8 PF) (V04222) (CSD: 106-00126-0007 V22373) C5502 .............................. (100 PF) (V04222) (CSD: 106-00126-0010 V22373) C5504 .............................. (24 PF) (V51406) (CSD: 106-00126-0012 V22373) C5501
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10118 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 310
106-00133-0001
.CAPACITOR CHIP
3
315
106-00133-0005
.CAPACITOR CHIP
1
320
106-04100-0016
.CAPACITOR CHIP
1
325
106-04101-0026
.CAPACITOR CHIP
13
330
106-04102-0046
.CAPACITOR CHIP
8
335
106-04103-0046
.CAPACITOR CHIP
5
340
106-04104-0046
.CAPACITOR CHIP
96
.............................. (33 PF) (V51406) (TRUE PN IS GRM42-6S2H330J050__) (CSD: 106-00133-0001 V22373) C5528, C5529, C5543 .............................. (33 PF) (V51406) (CSD: 106-00133-0005 V22373) C5576 .............................. (10 PF, 50 V) (V51406) (TRUE PN IS GRM42-CC0G100J050B) (CSD: 106-04100-0016 V22373) C5165
.............................. (100 PF, 100 V) (V51406) (CSD: 106-04101-0026 V22373) C5014 thru C5024, C5064, C5164 .............................. (1000 PF, 50 V, 5%) (V51406) (TRUE PN IS GRM42-6X7R102J050B) (CSD: 106-04102-0046 V22373) C5038, C5042, C5048, C5049, C5051 thru C5054
.............................. (10,000 PF, 50 V) (V51406) (CSD: 106-04103-0046 V22373) C5025, C5039, C5057, C5062, C5093 .............................. (0.1 UF, 50 V) (V51406) (TRUE PN IS GRM42-6X7R104J050B) (CSD: 106-04104-0046 V22373) C5002 thru C5004, C5007, C5008, C5026 thru C5035, C5050, C5065, C5070, C5071, C5073, C5074, C5076, C5078 thru C5084, C5086 thru C5089, C5091, C5094 thru C5142, C5145 thru C5156, C5158
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10119 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 345
106-04180-0026
.CAPACITOR CHIP
1
350
BCA1271FTM
.RESISTOR CHIP
1
355
139-01332-0000
.RESISTOR CHIP
1
360
BCA1371FTM
.RESISTOR CHIP
1
365
139-01372-0000
.RESISTOR
1
370
BCA1501FTM
.RESISTOR CHIP
5
375
139-01502-0000
.RESISTOR CHIP
2
380
BCA1541FTM
.RESISTOR CHIP
1
385
139-01622-0000
.RESISTOR CHIP
1
.............................. (18 PF, 100 V) (V51406) (CSD: 106-04180-0026 V22373) C5044 ............................... (1270 EW, 1%) (VS8185) (CSD: 139-01271-0000 V22373) R5510 ............................... (13,300 EW, 1%) (VS8185) (CSD: 139-01332-0000 V22373) R5538 ............................... (1370 EW, 1%) (VS8185) (CSD: 139-01371-0000 V22373) R5064 ................................... (13,700 EW, 1%) (VS8185) (CSD: 139-01372-0000 V22373) R5065
............................... (1500 EW, 1%) (VS8185) (CSD: 139-01501-0000 V22373) R5021, R5022, R5045, R5048, R5059 ............................... (15,000 EW, 1%) (VS8185) (CSD: 139-01502-0000 V22373) R5085, R5166 ............................... (1540 EW, 1%) (VS8185) (CSD: 139-01541-0000 V22373) R5150 ............................... (16,200 EW, 1%) (VS8185) (CSD: 139-01622-0000 V22373) R5285
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10120 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 390
BCA1652FTM
.RESISTOR CHIP
1
395
139-01822-0000
.RESISTOR CHIP
3
400
CRCW12062000F
.RESISTOR CHIP
1
405
139-02001-0000
.RESISTOR CHIP
1
410
BCA2002FTM
.RESISTOR CHIP
7
415
139-02211-0000
.RESISTOR CHIP
2
420
BCA2212FTM
.RESISTOR CHIP
3
425
139-02372-0000
.RESISTOR
1
............................... (16,500 EW, 1%) (VS8185) (CSD: 139-01652-0000 V22373) R5066 ............................... (18,200 EW, 1%) (VS8185) (CSD: 139-01822-0000 V22373) R5260, R5502, R5505
............................... (200 EW, 1%) (V91637) (TRUE PN IS CRCW12062000F___) (CSD: 139-02000-0000 V22373) R5295 ............................... (2000 EW, 1%) (VS8185) (CSD: 139-02001-0000 V22373) R5126 ............................... (20,000 EW, 1%) (VS8185) (CSD: 139-02002-0000 V22373) R5010, R5014, R5016, R5023, R5025, R5063, R5095
............................... (2210 EW, 1%) (VS8185) (CSD: 139-02211-0000 V22373) R5044, R5049 ............................... (22,100 EW, 1%) (VS8185) (CSD: 139-02212-0000 V22373) R5042, R5043, R5127 ................................... (23,700 EW, 1%) (VS8185) (CSD: 139-02372-0000 V22373) R5259
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10121 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 430
BCA2431FTM
.RESISTOR CHIP
2
435
139-02553-0000
.RESISTOR CHIP
1
440
BCA2670FTM
.RESISTOR
1
445
139-02742-0000
.RESISTOR CHIP
4
450
BCA2801FTM
.RESISTOR CHIP
1
455
139-03010-0000
.RESISTOR CHIP
2
460
BCA3012FTM
.RESISTOR CHIP
1
465
139-03013-0000
.RESISTOR CHIP
12
............................... (2430 EW, 1%) (VS8185) (CSD: 139-02431-0000 V22373) R5015, R5024 ............................... (255,000 EW, 1%) (VS8185) (CSD: 139-02553-0000 V22373) R5058 ................................... (267 EW, 1%) (VS8185) (CSD: 139-02670-0000 V22373) R5158 ............................... (27,400 EW, 1%) (VS8185) (CSD: 139-02742-0000 V22373) R5282, R5501, R5503, R5506 ............................... (2800 EW, 1%) (VS8185) (CSD: 139-02801-0000 V22373) R5532
............................... (301 EW, 1%) (V91637) (CSD: 139-03010-0000 V22373) R5035, R5125 ............................... (30,100 EW, 1%) (VS8185) (CSD: 139-03012-0000 V22373) R5250 ............................... (301,000 EW, 1%) (VS8185) (CSD: 139-03013-0000 V22373) R5028, R5173, R5176, R5179, R5182, R5185, R5188, R5191, R5264, R5267, R5270, R5273
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10122 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 470
BCA3091FTM
.RESISTOR CHIP
1
475
139-03241-0000
.RESISTOR CHIP
1
480
BCA3242FTM
.RESISTOR CHIP
1
485
139-03323-0000
.RESISTOR CHIP
1
490
BCA3922FTM
.RESISTOR CHIP
3
495
139-04222-0000
.RESISTOR CHIP
1
500
CRCW12064321F
.RESISTOR CHIP
2
505
139-04750-0000
.RESISTOR CHIP
16
............................... (3090 EW, 1%) (VS8185) (CSD: 139-03091-0000 V22373) R5020 ............................... (3240 EW, 1%) (VS8185) (CSD: 139-03241-0000 V22373) R5225 ............................... (32,400 EW, 1%) (VS8185) (CSD: 139-03242-0000 V22373) R5031
............................... (332,000 EW, 1%) (VS8185) (CSD: 139-03323-0000 V22373) R5030 ............................... (39,200 EW, 1%) (VS8185) (CSD: 139-03922-0000 V22373) R5275, R5525, R5527 ............................... (42,200 EW, 1%) (V91637) (CSD: 139-04222-0000 V22373) R5061
............................... (4320 EW, 1%) (V91637) (TRUE PN IS CRCW12064321F___) (CSD: 139-04321-0000 V22373) R5060, R5070 ............................... (475 EW, 1%) (VS8185) (CSD: 139-04750-0000 V22373) R5006, R5009, R5013, R5051, R5071, R5073, R5119 thru R5122, R5276, R5278, R5279, R5290 thru R5292
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10123 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 510
BCA4751FTM
.RESISTOR CHIP
4
515
139-04752-0000
.RESISTOR CHIP
6
520
BCA4991FTM
.RESISTOR CHIP
10
525
139-04992-0000
.RESISTOR CHIP
1
530
BCA5111FTM
.RESISTOR CHIP
1
535
139-05112-0000
.RESISTOR CHIP
1
540
BCA5230FTM
.RESISTOR CHIP
1
545
139-05621-0000
.RESISTOR CHIP
1
............................... (4750 EW, 1%) (VS8185) (CSD: 139-04751-0000 V22373) R5138, R5535 thru R5537 ............................... (47,500 EW, 1%) (VS8185) (CSD: 139-04752-0000 V22373) R5053 thru R5056, R5088, R5507 ............................... (4990 EW, 1%) (VS8185) (CSD: 139-04991-0000 V22373) R5008, R5077, R5082, R5089, R5104, R5108, R5157, R5167, R5226, R5299 ............................... (49,900 EW, 1%) (VS8185) (CSD: 139-04992-0000 V22373) R5032 ............................... (5110 EW, 1%) (VS8185) (CSD: 139-05111-0000 V22373) R5534 ............................... (51,100 EW, 1%) (VS8185) (CSD: 139-05112-0000 V22373) R5107 ............................... (523 EW, 1%) (VS8185) (CSD: 139-05230-0000 V22373) R5224 ............................... (5620 EW, 1%) (VS8185) (CSD: 139-05621-0000 V22373) R5222
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10124 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 550
BCA5622FTM
.RESISTOR CHIP
8
555
139-05761-0000
.RESISTOR CHIP
2
560
BCA6811FTM
.RESISTOR CHIP
2
565
139-07151-0000
.RESISTOR CHIP
1
570
BCA7320FTM
.RESISTOR CHIP
1
575
139-07500-0000
.RESISTOR CHIP
1
580
CRCW12067501F
.RESISTOR CHIP
2
585
139-07502-0000
.RESISTOR CHIP
13
............................... (56,200 EW, 1%) (VS8185) (CSD: 139-05622-0000 V22373) R5227 thru R5234
............................... (5760 EW, 1%) (VS8185) (CSD: 139-05761-0000 V22373) R5062, R5087 ............................... (6810 EW, 1%) (VS8185) (CSD: 139-06811-0000 V22373) R5098, R5113 ............................... (7150 EW, 1%) (VS8185) (CSD: 139-07151-0000 V22373) R5531 ............................... (732 EW, 1%) (VS8185) (CSD: 139-07320-0000 V22373) R5509
............................... (750 EW, 1%) (VS8185) (CSD: 139-07500-0000 V22373) R5539 ............................... (7500 EW, 1%) (V91637) (TRUE PN IS CRCW12067501F___) (CSD: 139-07501-0000 V22373) R5223, R5247 ............................... (75,000 EW, 1%) (VS8185) (CSD: 139-07502-0000 V22373) R5174, R5177, R5180, R5183, R5186, R5189, R5192, R5195, R5221, R5265, R5268, R5271, R5274
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10125 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 590
139-07682-0000
.RESISTOR CHIP
1
595
139-08061-0000
.RESISTOR CHIP
2
600
BCA8662FTM
.RESISTOR CHIP
1
605
139-08872-0000
.RESISTOR CHIP
1
610
BCA9090FTM
.RESISTOR CHIP
1
615
53002736-1
.INTEGRATED CIRCUIT
1
620
BCA1213FTM
.RESISTOR CHIP
1
625
106-05101-0016
.CAPACITOR CHIP
3
............................... (76,800 EW, 1%) (VS8185) (CSD: 139-07682-0000 V22373) R5092 ............................... (8060 EW, 1%) (VS8185) (CSD: 139-08061-0000 V22373) R5017, R5026 ............................... (86,600 EW, 1%) (VS8185) (CSD: 139-08662-0000 V22373) R5132 ............................... (88,700 EW, 1%) (VS8185) (CSD: 139-08872-0000 V22373) R5168 ............................... (909 EW, 1%) (VS8185) (CSD: 139-09090-0000 V22373) R5159 .......................... FRAM MEMORY (64 KB) (ESDS) (V0JP56) (CSD: 53002736-1 V22373) U5005
............................... (121,000 EW, 1%) (VS8185) (CSD: 139-01213-0000 V22373) R5076 .............................. (100 PF, 50 V) (V51406) (CSD: 106-05101-0016 V22373) C5507, C5574, C5575
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10126 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 630
106-05102-0016
.CAPACITOR CHIP
31
635
106-05103-0046
.CAPACITOR CHIP
2
640
106-05104-0037
.CAPACITOR CHIP
2
645
106-05121-0016
.CAPACITOR CHIP
1
650
106-05200-0016
.CAPACITOR CHIP
1
655
106-05270-0016
.CAPACITOR CHIP
2
660
106-05271-0016
.CAPACITOR CHIP
1
.............................. (1000 PF, 50 V) (V51406) (TRUE PN IS GRM40C0G102J050B) (CSD: 106-05102-0016 V22373) C5505, C5506, C5508, C5509, C5511 thru C5513, C5515, C5516, C5518, C5520, C5523, C5524, C5526, C5530 thru C5532, C5534 thru C5537, C5539 thru C5541, C5545, C5551, C5567, C5572, C5587 thru C5589 .............................. (10,000 PF, 50 V) (V51406) (CSD: 106-05103-0046 V22373) C5521, C5525
.............................. (100,000 PF, 25 V) (V51406) (TRUE PN IS GRM40X7R104K025B) (CSD: 106-05104-0037 V22373) C5577, C5578 .............................. (120 PF, 50 V) (V51406) (CSD: 106-05121-0016 V22373) C5544 .............................. (20 PF, 50 V) (V51406) (TRUE PN IS GRM40C0G200J050B) (CSD: 106-05200-0016 V22373) C5568
.............................. (27 PF, 50 V) (V51406) (CSD: 106-05270-0016 V22373) C5533, C5538 .............................. (270 PF, 50 V) (V51406) (TRUE PN IS GRM40C0G271J050B) (CSD: 106-05271-0016 V22373) C5584
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10127 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 665
106-05470-0016
.CAPACITOR CHIP
2
670
C0805C680J5GAC
.CAPACITOR CHIP
1
675
120-02213-0002
.INTEGRATED CIRCUIT
1
680
MAX4426ESA
.INTEGRATED CIRCUIT
1
685
120-02452-0000
.INTEGRATED CIRCUIT
1
690
XC3042A7PQ100I
.INTEGRATED CIRCUIT
4
695
120-02981-0112
.INTEGRATED CIRCUIT
4
.............................. (47 PF, 50 V) (V51406) (CSD: 106-05470-0016 V22373) C5510, C5514 .............................. (68 PF, 50 V) (V31433) (CSD: 106-05680-0016 V22373) C5517 .......................... Z80 PLCC (10 MHZ) (ESDS) (V56708) (CSD: 120-02213-0002 V22373) U5001 .......................... DUAL DRIVER (ESDS) (V1ES66) (CSD: 120-02233-0003 V22373) U5048 .......................... RESET/WTCHDG CNTL (ESDS) (V1ES66) (CSD: 120-02452-0000 V22373) U5002
.......................... 3042 GATE ARRAY (ESDS) (V68994) (TRUE PN IS XC3042A-7PQ100I) (CSD: 120-02469-0001 V22373) U5012, U5037, U5041, U5057 .......................... SOJ (32K X 8, 28 PIN) (ESDS) (V65786) (CSD: 120-02981-0112 V22373) U5004, U5039, U5059, U5118
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10128 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 700
ML1350-5P
.INTEGRATED CIRCUIT
4
705
120-03026-0080
.INTEGRATED CIRCUIT
1
710
MC78M08BDT
.INTEGRATED CIRCUIT
1
715
120-03027-0004
.INTEGRATED CIRCUIT
1
720
LM2904M
.INTEGRATED CIRCUIT
1
725
120-03126-0005
.INTEGRATED CIRCUIT
1
730
LM2901D
.INTEGRATED CIRCUIT
1
.......................... IF AMP SO (ESDS) (V58625) (CSD: 120-03020-0001 V22373) U5501, U5502, U5504, U5505 .......................... 78M05 DPAK VLT REG (ESDS) (V1MQ07) (CSD: 120-03026-0080 V22373) U5032 .......................... 78M08 DPAK VLT REG (ESDS) (V1MQ07) (CSD: 120-03026-0082 V22373) U5040 .......................... BALANCED MOD/DEMOD (ESDS) (V1MQ07) (CSD: 120-03027-0004 V22373) U5506 .......................... SO PKG (ESDS) (V27014) (CSD: 120-03053-0010 V22373) U5144
.......................... (ESDS) (V27014) (CSD: 120-03126-0005 V22373) U5042 .......................... SO-14 COMP (ESDS) (V66958) (CSD: 120-03163-0001 V22373) U5033
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10129 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 735
120-03174-0013
.INTEGRATED CIRCUIT
3
740
TL084ID
.INTEGRATED CIRCUIT
7
745
120-03285-0002
.INTEGRATED CIRCUIT
1
750
DG441DY
.INTEGRATED CIRCUIT
1
755
120-03400-0001
.INTEGRATED CIRCUIT
1
760
TLC0820AIDW
.INTEGRATED CIRCUIT
1
765
120-03488-0000
.INTEGRATED CIRCUIT
1
.......................... OP AMP BI FET SO (ESDS) (V82647) (CSD: 120-03174-0013 V22373) U5026, U5122, U5507 .......................... OP AMP BI FET SO (ESDS) (V82647) (CSD: 120-03174-0014 V22373) U5021, U5028, U5031, U5034, U5035, U5159, U5160 .......................... A/D CONVERT CA3306 (ESDS) U5030 .......................... QUAD SWITCH (ESDS) (V17856) (CSD: 120-03393-0002 V22373) U5162 .......................... REF-02 PREC V REG (ESDS) (V1ES66) (CSD: 120-03400-0001 V22373) U5171 .......................... 8-BIT A/D SO (ESDS) (V82647) (CSD: 120-03475-0003 V22373) U5024 .......................... PM7224FS DAC (ESDS) (V24355) (CSD: 120-03488-0000 V22373) U5119
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10130 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 770
120-03501-0000
.INTEGRATED CIRCUIT
1
775
120-03592-0000
.INTEGRATED CIRCUIT
1
780
DG442DY
.INTEGRATED CIRCUIT
1
785
120-03598-0000
.INTEGRATED CIRCUIT
.......................... HIGH SPEED DP-AMP (ESDS) (V24355) (TRUE PN IS AD847AR (EXCLUDING 9942 DATE CODE)) (CSD: 120-03501-0000 V22373) U5503 .......................... CMOS QUAD 8-BIT DAC (ESDS) (V24355) (CSD: 120-03592-0000 V22373) U5027 .......................... QUAD SW (ESDS) (V17856) (CSD: 120-03593-0000 V22373) U5163 ..........................
1
.................................. (VS6019) (CSD: 120-03599-0000 V22373) CR5015
HI5700 8-BIT A/D (ESDS) U5036
-
790
SP720AB
.ESD ARRAY
1
795
120-06065-0002
.INTEGRATED CIRCUIT
1
800
06562-047
.INTEGRATED CIRCUIT
1
805
126-00059-0003
.WX COMP ROM
1
.......................... 10-BIT SO (0.10%) (ESDS) (V24355) (CSD: 120-06065-0002 V22373) U5165 .......................... 429 ARINC LSI, 28 PIN PLCC (ESDS) (V31471) (CSD: 120-08030-0010 V22373) U5091 ...............................
(ESDS)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10131 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A
-
810
122-30048-0002
..INTEGRATED CIRCUIT
1
810A
122-30048-0003
..INTEGRATED CIRCUIT
1
815
122-01338-0109
.INTEGRATED CIRCUIT
RF
820
SN74HC03D
.INTEGRATED CIRCUIT
1
825
123-00573-0003
.INTEGRATED CIRCUIT
2
830
74HC4351D
.INTEGRATED CIRCUIT
2
835
124-00008-0003
.INTEGRATED CIRCUIT
1
840
74ACT139SC
.INTEGRATED CIRCUIT
1
......................... (ESDS) (PRE SB ART 2000-6) ......................... (ESDS) (POST SB ART 2000-6) U5038 .......................... (ESDS) (POST SWB ART 2000-SW5) (SEE IPL FIGURE 1 ITEM 131 FOR LOCATION) U5003 .......................... SO (ESDS) (V82647) (CSD: 123-00003-0003 V22373) U5125 .......................... SO (ESDS) (V7D893) (CSD: 123-00573-0003 V22373) U5006, U5043 .......................... MUXIDEMUX (ESDS) (V1CH66) (CSD: 123-04351-0003 V22373) U5022, U5023 .......................... SO PKG (ESDS) (V7D893) (CSD: 124-00008-0003 V22373) U5018 .......................... (ESDS) (V7D893) (CSD: 124-00139-1003 V22373) U5020
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10132 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A
-
845
124-00157-0003
.INTEGRATED CIRCUIT
1
850
74HCT245D
.INTEGRATED CIRCUIT
5
855
124-00573-0003
.INTEGRATED CIRCUIT
3
860
74HCT574D
.INTEGRATED CIRCUIT
7
865
126-00047-0004
.FPGA ROM
1
866
122-30049-0004
..INTEGRATED CIRCUIT
.......................... SO PKG (ESDS) (V1CH66) (CSD: 124-00157-0003 V22373) U5025 .......................... SO PKG (ESDS) (V1CH66) (CSD: 124-00245-0002 V22373) U5014 thru U5016, U5029, U5126 .......................... SO (ESDS) (V1CH66) (CSD: 124-00573-0003 V22373) U5007, U5017, U5019 .......................... (ESDS) (V0JN86) (CSD: 124-00574-0003 V22373) U5008 thru U5011, U5166, U5168, U5169
................................... (ESDS) .........................
1
............................... (0 QW) (V91637) (CSD: 130-05000-0035 V22373) CJ5001 thru CJ5005
(ESDS) U5013 870
130-05000-0035
.RESISTOR CHIP
5
875
CRCW120604R7J
.RESISTOR CHIP
2
880
130-05561-0043
.RESISTOR CHIP
2
............................... (4.7 QW, 5%) (V91637) (TRUE PN IS CRCW120604R7J___) (CSD: 130-05047-0033 V22373) R5130, R5131
............................... (560 HW, 5%) (V91637) (CSD: 130-05561-0043 V22373) R5511, R5512
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10133 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 885
V82RA8
.VARISTOR
1
890
139-00100-0000
.RESISTOR CHIP
3
895
BCA20R0FTM
.RESISTOR CHIP
1
900
139-00309-0000
.RESISTOR CHIP
2
905
BCA44R2FTM
.RESISTOR CHIP
1
910
139-00499-0000
.RESISTOR CHIP
1
915
BCA61R9FTM
.RESISTOR CHIP
1
920
139-01000-0000
.RESISTOR CHIP
4
.................................... (82 V) (V75915) (CSD: 134-02001-0000 V22373) V5001 ............................... (10 EW, 1%) (VS8185) (CSD: 139-00100-0000 V22373) R5160, R5533, R5551 ............................... (20 EW, 1%) (VS8185) (CSD: 139-00200-0000 V22373) R5552 ............................... (30.9 EW, 1%) (VS8185) (CSD: 139-00309-0000 V22373) R5039, R5040 ............................... (44.2 EW, 1%) (VS8185) (CSD: 139-00442-0000 V22373) R5550
............................... (49.9 EW, 1%) (VS8185) (CSD: 139-00499-0000 V22373) R5560 ............................... (61.9 EW, 1%) (VS8185) (CSD: 139-00619-0000 V22373) R5508 ............................... (100 EW, 1%) (VS8185) (CSD: 139-01000-0000 V22373) R5210, R5529, R5530, R5555
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10134 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 925
BCA1001FTM
.RESISTOR CHIP
11
930
139-01002-0000
.RESISTOR CHIP
67
935
106-04330-0026
.CAPACITOR CHIP
4
940
139-01003-0000
.RESISTOR CHIP
2
945
BCA1004FTM
.RESISTOR CHIP
3
950
139-01023-0000
.RESISTOR CHIP
1
............................... (1000 EW, 1%) (VS8185) (CSD: 139-01001-0000 V22373) R5038, R5041, R5093, R5099, R5114, R5137, R5139 thru R5141, R5171, R5294 ............................... (10,000 EW, 1%) (VS8185) (CSD: 139-01002-0000 V22373) R5001 thru R5003, R5007, R5012, R5033, R5052, R5067 thru R5069, R5072, R5074, R5078 thru R5081, R5083, R5084, R5086, R5090, R5091, R5096, R5097, R5101 thru R5103, R5105, R5106, R5111, R5112, R5116, R5123, R5128, R5133, R5152, R5153, R5155, R5165, R5170, R5172, R5175, R5178, R5181, R5184, R5187, R5190, R5249, R5258, R5262, R5263, R5266, R5269, R5272, R5280, R5281, R5283, R5289, R5296, R5297, R5514, R5540, R5541, R5544, R5548, R5557 thru R5559 .............................. (33 PF, 100 V) (V51406) (TRUE PN IS GRM42-6C0G330J100B) (CSD: 106-04330-0026 V22373) C5010 thru C5013
............................... (100,000 EW, 1%) (VS8185) (CSD: 139-01003-0000 V22373) R5029, R5284 ............................... (1M EW, 1%) (VS8185) (CSD: 139-01004-0000 V22373) R5094, R5100, R5115
............................... (105,000 EW, 1%) (VS8185) (CSD: 139-01023-0000 V22373) R5057
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10135 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
2A 955
BCA1053FTM
.RESISTOR CHIP
1
960
139-01071-0000
.RESISTOR CHIP
1
965
BCA1212FTM
.RESISTOR CHIP
3
970
009-08549-0020
.PC BOARD
1
............................... (105,000 EW, 1%) (VS8185) (CSD: 139-01053-0000 V22373) R5075 ............................... (1070 EW, 1%) (VS8185) (CSD: 139-01071-0000 V22373) R5151 ............................... (12,100 EW, 1%) (VS8185) (CSD: 139-01212-0000 V22373) R5046, R5047, R5556 ................................... (VL2665) (CSD: 009-08549-0020 V22373)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10136 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 3. (Sheet 1 of 3) Power Supply/Modulator Board (-0000)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10137/10138 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 3. (Sheet 2 of 3) Power Supply/Modulator Board (-0000)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10139/10140 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 3. (Sheet 3 of 3) Power Supply/Modulator Board (-0000)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10141/10142 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 -
1
200-08548-0000
POWER SUPPLY/MODULATOR BOARD . . . . . . . . . . . . . (ESDS) (SEE IPL FIGURE 1 ITEM 140 FOR NHA)
RF
5
057-01540-0000
.TAG
......................................... WARNING HV (V00A29) (CSD: 057-01540-0000 V22373)
1
10
057-03231-0004
.BDX
......................................... (VBAG02) (CSD: 057-03231-0004 V22373)
1
15
012-01316-0000
.INSULATOR
6
20
012-01673-0001
.INSULATOR
1
25
012-01575-0000
.INSULATOR
1
30
089-05907-0006
.SCREW
2
35
6332-0404
.SCREW
...................................... PHP (4-40 X 1/4) (VBAG02) (CSD: 089-05903-0004 V22373)
1
40
090-00973-0005
.PIN
......................................... SNAP LOCK (0.625) (V06915) (CSD: 090-00973-0005 V22373)
1
45
NAS1515H04
.WASHER
1
50
091-00054-0003
.WASHER
2
................................... POLY FOAM ................................... (POST SA ART 2000-102) ................................... PS BD (VAAD11) (CSD: 012-01575-0000 V22373) ...................................... PHP (6-32 X 3/8) (VBAG02) (CSD: 089-05907-0006 V22373)
..................................... INSUL (V86928) (CSD: 091-00602-0000 V22373) ..................................... INSUL (0.500 DIA) (VAAA42) (CSD: 091-00054-0003 V22373)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10143 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 55
047-10676-0001
.HEATSINK
60
6332-0404
.SCREW
65
091-00286-0000
.INSULATOR
.................................... W/FINISH (VBAE38) (CSD: 047-10676-0001 V22373) (ATTACHING PARTS) ...................................... PHP (4-40 X 1/4) (VBAG02) (CSD: 089-05903-0004 V22373) ---*--...................................
1
3
1
XSTR (0.437) 70
SLPA125-375-01
.PIN
75
6332-0406
.SCREW
...................................... PHP (4-40 X 3/8) (VBAG02) (CSD: 089-05903-0006 V22373)
1
80
089-02140-0000
.NUT
......................................... LOCK (4-40) (V2M626) (CSD: 089-02140-0000 V22373)
1
85
091-00286-0002
.INSULATOR
1
90
091-00480-0071
.BUSHING
1
......................................... SNAP LOCK (0.375) (V06915) (CSD: 090-00973-0003 V22373)
................................... XSTR (0.687) (V55285) (CSD: 091-00286-0002 V22373) .................................... FLG (0.116) (VBAG02) (CSD: 091-00480-0071 V22373)
2
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10144 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 95
SLPA125-375-01
.PIN
100
091-00054-0003
.WASHER
1
105
NAS1515H04
.WASHER
1
110
092-05003-0018
.EYE ROLL
2
115
091-00286-0002
.INSULATOR
1
120
6332-0404
.SCREW
1
125
091-00480-0071
.BUSHING
1
130
047-10675-0001
.HEATSINK
1
135
089-05903-0003
.SCREW
140
007-00065-0001
.TRANSISTOR
......................................... SNAP LOCK (0.375) (V06915) (CSD: 090-00973-0003 V22373) ..................................... INSUL (0.500 DIA) (VAAA42) (CSD: 091-00054-0003 V22373) ..................................... INSUL (V86928) (CSD: 091-00602-0000 V22373) .................................... (0.125 X 0.250) ................................... XSTR (0.687) (V55285) (CSD: 091-00286-0002 V22373)
...................................... PHP (4-40 X 1/4) (VBAG02) (CSD: 089-05903-0004 V22373) .................................... FLG (0.116) (VBAG02) (CSD: 091-00480-0071 V22373) .................................... MOTOR W/FINISH
(ATTACHING PARTS) ...................................... PHP (4-40 X 3/16) ---*--................................. 2N3906 (SOT-23) (ESDS) Q4003
1
6
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10145 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 145
BCA4022FTM
.RESISTOR CHIP
1
150
139-04322-0000
.RESISTOR CHIP
1
155
BCA4641FTM
.RESISTOR CHIP
1
160
139-04750-0000
.RESISTOR CHIP
2
165
BCA4751FTM
.RESISTOR CHIP
6
170
139-04752-0000
.RESISTOR CHIP
3
175
BCA4991FTM
.RESISTOR CHIP
6
180
139-05111-0000
.RESISTOR CHIP
1
185
BCA5112FTM
.RESISTOR CHIP
1
............................... (40,200 EW, 1%) (VS8185) (CSD: 139-04022-0000 V22373) R4023 ............................... (43,2000 EW, 1%) (V91637) (CSD: 139-04322-0000 V22373) R4024 ............................... (4640 EW, 1%) (VS8185) (CSD: 139-04641-0000 V22373) R4198 ............................... (475 EW, 1%) (VS8185) (CSD: 139-04750-0000 V22373) R4158, R4191 ............................... (4750 EW, 1%) (VS8185) (CSD: 139-04751-0000 V22373) R4033, R4064, R4098, R4190, R4204, R4219 ............................... (47,500 EW, 1%) (VS8185) (CSD: 139-04752-0000 V22373) R4070, R4077, R4228 ............................... (4990 EW, 1%) (VS8185) (CSD: 139-04991-0000 V22373) R4088, R4135, R4169, R4226, R4227, R4229 ............................... (5110 EW, 1%) (VS8185) (CSD: 139-05111-0000 V22373) R4109 ............................... (51,100 EW, 1%) (VS8185) (CSD: 139-05112-0000 V22373) R4067
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10146 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 190
139-05113-0000
.RESISTOR CHIP
1
195
BCA5621FTM
.RESISTOR CHIP
3
200
139-05761-0000
.RESISTOR CHIP
1
205
CRCW12066190F
.RESISTOR CHIP
1
210
139-06191-0000
.RESISTOR CHIP
1
215
BCA6491FTM
.RESISTOR CHIP
1
220
139-06811-0000
.RESISTOR CHIP
2
225
BCA6812FTM
.RESISTOR CHIP
1
............................... (511,000 EW, 1%) (VS8185) (CSD: 139-05113-0000 V22373) R4022 ............................... (5620 EW, 1%) (VS8185) (CSD: 139-05621-0000 V22373) R4060, R4062, R4102 ............................... (5760 EW, 1%) (VS8185) (CSD: 139-05761-0000 V22373) R4187 ............................... (619 EW, 1%) (V91637) (TRUE PN IS CRCW12066190F___) (CSD: 139-06190-0000 V22373) R4094 ............................... (6190 EW, 1%) (VS8185) (CSD: 139-06191-0000 V22373) R4096 ............................... (6490 EW, 1%) (VS8185) (CSD: 139-06491-0000 V22373) R4206 ............................... (6810 EW, 1%) (VS8185) (CSD: 139-06811-0000 V22373) R4051, R4053 ............................... (68,100 EW, 1%) (VS8185) (CSD: 139-06812-0000 V22373) R4050
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10147 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 230
139-07321-0000
.RESISTOR CHIP
1
235
139-09091-0000
.RESISTOR CHIP
1
240
139-07502-0000
.RESISTOR CHIP
1
245
106-00129-0000
.CAPACITOR CHIP
1
250
139-03480-0000
.RESISTOR CHIP
1
255
BCA8061FTM
.RESISTOR CHIP
1
260
139-08661-0000
.RESISTOR CHIP
............................... (8660 EW, 1%) R4080, R4201
2
265
0410-5
.FAN
......................................... BRUSHLESS (VS8507) (CSD: 148-05186-0000 V22373) B4001
1
270
007-00961-0000
.TRANSISTOR POWER
2
275
BCA3571FTM
.RESISTOR CHIP
2
............................... (7320 EW, 1%) (VS8185) (CSD: 139-07321-0000 V22373) R4170 ............................... (9090 EW, 1%) R4003 ............................... (75,000 EW, 1%) (VS8185) (CSD: 139-07502-0000 V22373) R4107 .............................. (1 UF X7R/50 V) C4043 ............................... (3486 EW, 1%) R4222 ............................... (8060 EW, 1%) (VS8185) (CSD: 139-08061-0000 V22373) R4054
.......................... MOSFET, N-CHANNEL (ESDS) Q4001, Q4004 ............................... (3570 EW, 1%) (VS8185) (CSD: 139-03571-0000 V22373) R4078, R4087
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10148 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 280
007-00254-0001
.TRANSISTOR
1
285
MMBTA42LT1
.TRANSISTOR
2
290
007-00261-0003
.TRANSISTOR
2
295
2N6402
.THYRISTOR
1
300
007-00467-0000
.TRANSISTOR
1
305
IRF9540
.TRANSISTOR
1
310
007-06427-0000
.TRANSISTOR
................................. S PNP SOT-23 (ESDS) (V1MQ07) (CSD: 007-00254-0001 V22373) Q4021 ................................. SO PKG (ESDS) (V1MQ07) (CSD: 007-00257-0001 V22373) Q4019, Q4026 ................................. SOT (ESDS) Q4017, Q4023
.................................. (ESDS) (V1MQ07) (CSD: 007-00432-0002 V22373) Q4020 ................................. S NPN (ESDS) (V55464) (CSD: 007-00467-0000 V22373) Q4027
................................. P-CHAN HEXFET (ESDS) (V59993) (CSD: 007-00937-0000 V22373) Q4018 .................................
1
..................................... (1500 W, 33 V) (ESDS) (V14552) (CSD: 007-05241-0001 V22373) CR4038
1
SCR (4 A) (ESDS) Q4007 315
SMCJ33A
.TRNSRB
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10149 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 320
007-05245-0025
.DIODE
1
325
MUR1100E
.DIODE
5
330
007-06177-0000
.DIODE
7
335
139-01502-0000
.RESISTOR CHIP
1
340
007-00179-0001
.TRANSISTOR
5
345
MMBD2837LT1G
.DIODE
1
350
007-06444-0002
.DIODE
7
....................................... (36 V) (ESDS) (V1MQ07) (CSD: 007-05245-0025 V22373) CR4022 ....................................... (1000 V) (ESDS) (VBAE40) (CSD: 007-06141-0005 V22373) CR4001, CR4004, CR4005, CR4009, CR4010 ....................................... SMD, SI (ESDS) (V0GWP1) (CSD: 007-06177-0000 V22373) CR4008, CR4021, CR4030, CR4031, CR4034, CR4036, CR4037 ............................... (15,000 EW, 1%) R4052 ................................. SOT23 (ESDS) (V66958) (CSD: 007-00179-0001 V22373) Q4002, Q4010, Q4015, Q4022, Q4028
....................................... DUAL (ESDS) (V1MQ07) (CSD: 007-06182-0000 V22373) CR4041 ....................................... (1 A, 150 V) (ESDS) (V1MQ07) (CSD: 007-06444-0002 V22373) CR4015 thru CR4018, CR4025, CR4026, CR4040
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10150 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 355
106-00124-0000
.CAPACITOR CHIP
2
360
008-00008-0002
.TERM SPLIT
4
365
008-00096-0001
.TERMINAL TEST POINT
14
370
019-02331-0000
.INDUCTOR
1
-
370A
019-02331-0002
.INDUCTOR
1
-
370B
019-02331-0005
.INDUCTOR
1
-
370C
019-02331-0006
.INDUCTOR
1
.............................. CR (0.15 UF, 500 V) (V95275) (CSD: 106-00124-0000 V22373) C4063, C4064 .................................. TURR (V81312) (CSD: 008-00008-0002 V22373) E4003 thru E4006 ......................... (V79963) (TRUE PN IS 6069-14 (REEL) OR 1069-14 (LOOSE)) (CSD: 008-00096-0001 V22373) TP4001, TP4002, TP4004, TP4005, TP4007 thru TP4011, TP4014 thru TP4017, TP4020 ................................... FIL (0.180-0.230) (V1DA26) (CSD: 019-02331-0000 V22373) L4009 ................................... FIL (0.300-0.355) (V1DA26) (CSD: 019-02331-0002 V22373) (OPT MFR: 019-02331-0000 V1DA26) ................................... FIL (0.455-0.500) (V1DA26) (CSD: 019-02331-0005 V22373) (OPT MFR: 019-02331-0000 V1DA26) ................................... FIL (0.630-0.685) (V1DA26) (CSD: 019-02331-0006 V22373) (OPT MFR: 019-02331-0000 V1DA26)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10151 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 -
370D
019-02331-0008
.INDUCTOR
1
-
370E
019-02331-0010
.INDUCTOR
1
-
370F
019-02331-0011
.INDUCTOR
1
-
370G
019-02331-0012
.INDUCTOR
1
375
VK200-10-36
.CHOKE PARASITIC
4
380
019-02368-0000
.TOROID CHOKE
3
385
019-06133-0000
.TRANSFORMER
1
................................... FIL (0.980-1.10) (V1DA26) (CSD: 019-02331-0008 V22373) (OPT MFR: 019-02331-0000 V1DA26) ................................... FIL (1.50-1.70) (V1DA26) (CSD: 019-02331-0010 V22373) (OPT MFR: 019-02331-0000 V1DA26) ................................... FIL (1.70-1.90) (V1DA26) (CSD: 019-02331-0011 V22373) (OPT MFR: 019-02331-0000 V1DA26) ................................... FIL (2.50-2.80) (V1DA26) (CSD: 019-02331-0012 V22373) (OPT MFR: 019-02331-0000 V1DA26) ............................. (V9V250) (TRUE PN IS VK 200 10/36) (CSD: 019-02332-0000 V22373) L4005 thru L4008 ............................... (V11402) (CSD: 019-02368-0000 V22373) L4001, L4003, L4004 ............................... PULSE (ESDS) (V31740) (CSD: 019-06133-0000 V22373) T4002
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10152 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 390
019-07255-0000
.TRANSFORMER
1
395
019-07257-0000
.TRANSFORMER
1
400
65823-183
.CONNECTOR
1
405
030-02832-0003
.TERMINAL PC HEADER
2
410
251005
.FUSE
........................................ (5 A, 125 V) (ESDS) (V75915) (CSD: 036-00057-0010 V22373) F4001
1
415
044-00309-0005
.OSCILLATOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
............................... FLYBACK (ESDS) (V1QYX0) (CSD: 019-07255-0000 V22373) T4001 ............................... POWER (ESDS) (V11402) (CSD: 019-07257-0000 V22373) T4005 ................................. RT ANG HDR 40 (V22526) (CSD: 030-02520-0003 V22373) J4001 ......................... (V22526) (CSD: 030-02832-0003 V22373) J4002, J4003
(1.025 MHZ) (ESDS) (V0HAF7) (CSD: 044-00309-0005 V22373) Y4001 420
TDL157M010M1E
.CAPACITOR
1
425
096-01082-0028
.CAPACITOR
1
.................................. TN (150 UF, 10 V) (V37942) (CSD: 096-01082-0025 V22373) C4039 .................................. TN (47 UF, 20V) C4018
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10153 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 430
FB110H225KP012
.CAPACITOR
4
435
096-01186-0011
.CAPACITOR
2
440
T491C106K016AH
.CAPACITOR
1
445
096-01186-0018
.CAPACITOR
2
450
T491C475K025AH
.CAPACITOR
1
455
BCA3322FTM
.RESISTOR CHIP
1
460
20SA68M
.CAPACITOR
2
465
097-00217-0009
.CAPACITOR
1
.................................. TN (22 UF, 50 V) (V66958) (TRUE PN IS FB110H22K P-012) (CSD: 096-01082-0055 V22373) C4050, C4073, C4074, C4138 .................................. (47 UF, 10 V, 10%) (V31433) (CSD: 096-01186-0011 V22373) C4053, C4056 .................................. (10 UF, 16 V, 10%) (V31433) (CSD: 096-01186-0014 V22373) C4057 .................................. (6.8 UF, 20 V, 10%) (V31433) (CSD: 096-01186-0018 V22373) C4034, C4037 .................................. (4.7 UF, 25 V, 10%) (V31433) (CSD: 096-01186-0022 V22373) C4141 ............................... (33,200 EW, 1%) (VS8185) (CSD: 139-03322-0000 V22373) R4069 .................................. AL/O (68 UF, 20 V) (VS4915) (CSD: 097-00217-0008 V22373) C4033, C4036 .................................. EL (100 UF, 16 V) (VS4915) (CSD: 097-00217-0009 V22373) C4045
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10154 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3
-
470
94SA227X0010F
.CAPACITOR
2
475
097-00218-0003
.CAPACITOR
2
480
097-00218-0004
.CAPACITOR
5
485
097-00218-0005
.CAPACITOR
1
490
096-01082-0065
.CAPACITOR
1
490A
UKL1E101KPAANA
.CAPACITOR
1
495
105-00169-0000
.CAPACITOR
2
.................................. EL (220 UF, 10 V) (V56289) (CSD: 097-00217-0013 V22373) C4058, C4065 .................................. EL (470 UF, 25 V) (V62643) (CSD: 097-00218-0003 V22373) C4044, C4054 .................................. EL (330 UF, 50 V) (V62643) (TRUE PN IS EKMG630ELL331MJ20S) (CSD: 097-00218-0004 V22373) C4009, C4030, C4042, C4049, C4134
.................................. EL (22 UF, 100 V) (V29309) (CSD: 097-00218-0005 V22373) C4055 .................................. AL, LOW LEAKAGE CURRENT (100 UF, 20 V) (PRE SB ART 2000-9)
.................................. AL, LOW LEAKAGE CURRENT (100 UF, 25 V) (V55680) (CSD: 097-00238-0093 V22373) (POST SB ART 2000-9) C4019 .................................. MYLAR (5 VFD) (V50558) (CSD: 105-00169-0000 V22373) C4011, C4013
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10155 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 500
106-00122-0000
.CAPACITOR CHIP
6
505
106-04102-0026
.CAPACITOR CHIP
1
510
106-04102-0046
.CAPACITOR CHIP
1
515
106-04103-0046
.CAPACITOR CHIP
4
520
106-04103-0047
.CAPACITOR CHIP
1
525
106-04104-0046
.CAPACITOR CHIP
40
530
C1206C104K5RACT
.CAPACITOR CHIP
1
.............................. CER SMT 1812 (0.33 UF, 50 V, 10%) (V51406) (TRUE PN IS GRM43-2X7R334K050B_) (CSD: 106-00122-0000 V22373) C4035, C4038, C4095, C4096, C4122, C4125 .............................. (1000 PF, 100 V) (V56699) (CSD: 106-04102-0026 V22373) C4137 .............................. (1000 PF, 50 V, 5%) (V51406) (TRUE PN IS GRM42-6X7R102J050B) (CSD: 106-04102-0046 V22373) C4021 .............................. (10,000 PF, 50 V) (V51406) (CSD: 106-04103-0046 V22373) C4007, C4031, C4139, C4142
.............................. (10,000 PF, 50 V) (V51406) (TRUE PN IS GRM42-6X7R103K050B) (CSD: 106-04103-0047 V22373) C4140 .............................. (0.1 UF, 50 V) (V51406) (CSD: 106-04104-0046 V22373) C4006, C4010, C4014, C4020, C4023 thru C4029, C4032, C4040, C4041, C4046, C4047, C4051, C4052, C4059 thru C4062, C4066 thru C4070, C4109, C4119, C4120, C4132, C4133, C4143, C4149, C4152 thru C4157 .............................. (100,000 PF, 50 V) (V31433) (TRUE PN IS C1206C104K5RACT_) (CSD: 106-04104-0047 V22373) C4144
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10156 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 535
106-04153-0046
.CAPACITOR CHIP
8
540
106-04153-0047
.CAPACITOR CHIP
1
545
106-04221-0014
.CAPACITOR CHIP
2
550
139-03402-0000
.RESISTOR CHIP
1
555
106-04222-0016
.CAPACITOR CHIP
1
560
106-04471-0026
.CAPACITOR CHIP
1
565
106-04751-0016
.CAPACITOR CHIP
1
570
106-04821-0016
.CAPACITOR CHIP
4
.............................. (15,000 PF, 50 V) (V51406) (CSD: 106-04153-0046 V22373) C4097 thru C4100, C4123, C4124, C4126, C4127 .............................. (15,000 PF, 50 V) (V51406) (TRUE PN IS GRM42-6X7R153K050B) (CSD: 106-04153-0047 V22373) C4004 .............................. (220 PF, 2%) (V31433) (CSD: 106-04221-0014 V22373) C4145, C4146
............................... (34,000 EW, 1%) (VS8185) (CSD: 139-03402-0000 V22373) R4063 .............................. (2200 PF, NPO/ 50 V) C4008 .............................. (470 PF, 100 V) (V51406) (TRUE PN IS GRM42-6C0G471J100B) (CSD: 106-04471-0026 V22373) C4005
.............................. (750 PF, 50 V) (V51406) (CSD: 106-04751-0016 V22373) C4136 .............................. (820 PF, 50 V) (V51406) (TRUE PN IS GRM42-6C0G821J050B) (CSD: 106-04821-0016 V22373) C4101, C4102, C4128, C4129
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10157 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 575
118-00082-0000
.CAPACITOR
1
580
SN74LS221D
.INTEGRATED CIRCUIT
2
585
BCA3321FTM
.RESISTOR CHIP
4
590
XC3042A7PQ100I
.INTEGRATED CIRCUIT
1
595
120-03163-0001
.INTEGRATED CIRCUIT
2
600
LM318M
.INTEGRATED CIRCUIT
1
605
120-03174-0014
.INTEGRATED CIRCUIT
1
610
LM2902M
.INTEGRATED CIRCUIT
1
.................................. (0.005 UF, 1000 V) (V59660) (CSD: 118-00082-0000 V22373) C4012 .......................... (ESDS) (V82647) (CSD: 120-00108-0002 V22373) U4020, U4058
............................... (3320 EW) (VS8185) (CSD: 139-03321-0000 V22373) R4005, R4029, R4068, R4209 .......................... GATE ARRAY (ESDS) (V68994) (TRUE PN IS XC3042A-7PQ100I) (CSD: 120-02469-0001 V22373) U4011 .......................... SO-14 COMP (ESDS) (V66958) (CSD: 120-03163-0001 V22373) U4002, U4012 .......................... (ESDS) (V27014) (CSD: 120-03167-0004 V22373) U4059
.......................... OP AMP BI FET SO (ESDS) (V82647) (CSD: 120-03174-0014 V22373) U4061 .......................... (ESDS) (V27014) (CSD: 120-03196-0000 V22373) U4018
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10158 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 615
120-03430-0000
.INTEGRATED CIRCUIT
1
620
MC33166T
.INTEGRATED CIRCUIT
2
625
120-03520-0000
.INTEGRATED CIRCUIT
2
630
LM285D-2-5
.INTEGRATED CIRCUIT
1
635
120-03569-0000
.INTEGRATED CIRCUIT
4
640
AD7226KR
.INTEGRATED CIRCUIT
1
645
120-03593-0000
.INTEGRATED CIRCUIT
1
.......................... (ESDS) (V34333) (CSD: 120-03430-0000 V22373) U4001 .......................... PWR SWTCHG REGULTR (ESDS) (V1MQ07) (CSD: 120-03510-0000 V22373) U4005, U4006 .......................... OVER VOLTAGE SENSE (ESDS) (V1MQ07) (CSD: 120-03520-0000 V22373) U4014, U4015 .......................... VOLT REF (ESDS) (V1MQ07) (TRUE PN IS LM285D-2.5) (CSD: 120-03544-0000 V22373) U4019 .......................... DMOS F-B DVR (ESDS) (V66958) (CSD: 120-03569-0000 V22373) U4033, U4034, U4049, U4050 .......................... CMOS QUAD 8-BIT DAC (ESDS) (V24355) (CSD: 120-03592-0000 V22373) U4013 .......................... QUAD SW (ESDS) (V17856) (CSD: 120-03593-0000 V22373) U4060
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10159 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3
-
650
MM74HCT00M
.INTEGRATED CIRCUIT
1
655
124-00074-0003
.INTEGRATED CIRCUIT
1
660
126-00074-0000
.MICROSTEPING ROM
.......................... SO PKG (ESDS) (V7D893) (CSD: 124-00000-0003 V22373) U4054 .......................... SO PKG (ESDS) (V0JN86) (CSD: 124-00074-0003 V22373) U4008 ..........................
1
.........................
1
............................... (0 QW) (V91637) (CSD: 130-05000-0035 V22373) CJ4013 thru CJ4019
(ESDS) 661
122-30064-0000
..INTEGRATED CIRCUIT (ESDS) U4010
665
130-05000-0035
.RESISTOR CHIP
7
670
CRCW20102R7J
.RESISTOR CHIP
12
675
131-00100-0033
.RESISTOR
1
680
131-00101-0033
.RESISTOR
1
............................... (2.7 HW, 5%) (V91637) (TRUE PN IS CRCW20102R7J___) (CSD: 130-05027-0043 V22373) R4030, R4031, R4036, R4037, R4139, R4140, R4142, R4143, R4162 thru R4165 ................................... CF (10 HW, 5%) (VBAD71) (CSD: 131-00100-0033 V22373) R4014 ................................... CF (100 HW, 5%) (VBAD71) (TRUE PN IS CF1/2 5% 100 OHM) (CSD: 131-00101-0033 V22373) R4015
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10160 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 685
132-00135-0000
.RESISTOR
1
690
SPH2R15-5PCT
.RESISTOR
1
695
133-00562-2103
.RESISTOR
1
700
DS125-272K
.RESISTOR
1
705
134-01026-0006
.VRSTR
1
710
CCF55-1023F
.RESISTOR
2
715
137-00034-0000
.TEMP SENSOR
1
720
139-00150-0000
.RESISTOR CHIP
1
................................... WW (0.18 OHM, 1 W, 5%) R4013
................................... WW (0.15 OHM, 2 W, 5%) (V11502) (TRUE PN IS SPH-2 R15 5%) (CSD: 132-05051-0000 V22373) R4195 ................................... VAR 12-15T (10,000 OHMS) R4200
................................... THMS (2700 OHMS, 10%) (V15454) (TRUE PN IS DS125 272K) (CSD: 134-01015-0031 V22373) R4185 ...................................... VI00ZA15 (81 V) (V75915) (CSD: 136-01023-0072 V22373) CR4039
................................... PF (102,000 QW, 1%) (V91637) (TRUE PN IS CCF-55 1023 F) (CSD: 136-01023-0072 V22373) R4016, R4020 ................................ (ESDS) (V27014) (CSD: 137-00034-0000 V22373) U4017 ............................... (15 EW, 1%) R4006
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10161 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 725
139-00221-0000
.RESISTOR CHIP
1
730
139-02210-0000
.RESISTOR CHIP
1
735
139-01001-0000
.RESISTOR CHIP
25
740
BCA1002FTM
.RESISTOR CHIP
12
745
139-01003-0000
.RESISTOR CHIP
6
750
BCA1004FTM
.RESISTOR CHIP
1
755
139-01021-0000
.RESISTOR CHIP
1
760
BCA1214FTM
.RESISTOR CHIP
1
............................... (22.1 EW, 1%) (VS8185) (CSD: 139-00221-0000 V22373) R4010 ............................... (100 EW, 1%) R4231 ............................... (1000 EW, 1%) (VS8185) (CSD: 139-01001-0000 V22373) R4004, R4011, R4032, R4061, R4097, R4138, R4141, R4161, R4166, R4173, R4175, R4176, R4178 thru R4183, R4196, R4197, R4199, R4205, R4207, R4221, R4224 ............................... (10,000 EW, 1%) (VS8185) (CSD: 139-01002-0000 V22373) R4071, R4110, R4111, R4136, R4137, R4203, R4211, R4215, R4216, R4220, R4223, R4230 ............................... (100,000 EW, 1%) (VS8185) (CSD: 139-01003-0000 V22373) R4008, R4086, R4090 thru R4092, R4188 ............................... (1M EW, 1%) (VS8185) (CSD: 139-01004-0000 V22373) R4108 ............................... (1020 EW, 1%) (VS8185) (CSD: 139-01021-0000 V22373) R4192 ............................... (1240 EW, 1%) (VS8185) (CSD: 139-01241-0000 V22373) R4213
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10162 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 765
139-01302-0000
.RESISTOR CHIP
1
770
139-01911-0000
.RESISTOR CHIP
1
775
139-02001-0000
.RESISTOR CHIP
1
780
BCA2002FTM
.RESISTOR CHIP
1
785
139-02102-0000
.RESISTOR CHIP
1
790
BCA2151FTM
.RESISTOR CHIP
1
795
139-02211-0000
.RESISTOR CHIP
1
800
BCA2212FTM
.RESISTOR CHIP
1
805
139-02213-0000
.RESISTOR CHIP
1
............................... (13,000 EW, 1%) (VS8185) (CSD: 139-01302-0000 V22373) R4208 ............................... (1910 EW, 1%) R4028 ............................... (2000 EW, 1%) (VS8185) (CSD: 139-02001-0000 V22373) R4212, R4225 ............................... (20,000 EW, 1%) (VS8185) (CSD: 139-02002-0000 V22373) R4009 ............................... (21,000 EW, 1%) (VS8185) (CSD: 139-02102-0000 V22373) R4186
............................... (2150 EW, 1%) (VS8185) (CSD: 139-02151-0000 V22373) R4089 ............................... (2210 EW, 1%) (VS8185) (CSD: 139-02211-0000 V22373) R4021 ............................... (22,100 EW, 1%) (VS8185) (CSD: 139-02212-0000 V22373) R4059
............................... (221,000 EW, 1%) (V91637) (CSD: 139-02213-0000 V22373) R4074
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10163 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3 810
BCA2432FTM
.RESISTOR CHIP
1
815
139-02433-0000
.RESISTOR CHIP
1
820
BCA2491FTM
.RESISTOR CHIP
3
825
139-02493-0000
.RESISTOR CHIP
1
830
BCA2670FTM
.RESISTOR
1
835
139-02742-0000
.RESISTOR CHIP
1
840
139-04021-0000
.RESISTOR CHIP
1
845
139-03013-0000
.RESISTOR CHIP
1
850
009-08548-0000
.PC BOARD
1
............................... (24,300 EW, 1%) (VS8185) (CSD: 139-02432-0000 V22373) R4066 ............................... (243,000 EW, 1%) (VS8185) (CSD: 139-02433-0000 V22373) R4189 ............................... (2490 EW, 1%) (VS8185) (CSD: 139-02491-0000 V22373) R4079, R4081, R4214 ............................... (249,000 EW, 1%) (VS8185) (CSD: 139-02493-0000 V22373) R4093 ................................... (267 EW, 1%) (VS8185) (CSD: 139-02670-0000 V22373) R4210 ............................... (27,400 EW, 1%) (VS8185) (CSD: 139-02742-0000 V22373) R4012 ............................... (4020 EW, 1%) R4202 ............................... (301,000 EW, 1%) (VS8185) (CSD: 139-03013-0000 V22373) R4084 ...................................
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10164 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 3A. (Sheet 1 of 3) Power Supply/Modulator Board (-0020)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10165/10166 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 3A. (Sheet 2 of 3) Power Supply/Modulator Board (-0020)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10167/10168 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 3A. (Sheet 3 of 3) Power Supply/Modulator Board (-0020)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10169/10170 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A -
1
200-08548-0020
POWER SUPPLY/MODULATOR BOARD . . . . . . . . . . . . . (ESDS) (SEE IPL FIGURE 1 ITEM 140A FOR NHA)
RF
5
057-01540-0000
.TAG
......................................... WARNING HV (V00A29) (CSD: 057-01540-0000 V22373)
1
10
057-03231-0004
.BDX
......................................... (VBAG02) (CSD: 057-03231-0004 V22373)
1
15
012-01316-0000
.INSULATOR
6
20
012-01673-0001
.INSULATOR
1
25
012-01575-0000
.INSULATOR
1
30
089-05907-0006
.SCREW
2
35
6332-0404
.SCREW
...................................... PHP (4-40 X 1/4) (VBAG02) (CSD: 089-05903-0004 V22373)
1
40
090-00973-0005
.PIN
......................................... SNAP LOCK (0.625) (V06915) (CSD: 090-00973-0005 V22373)
1
45
NAS1515H04
.WASHER
1
50
091-00054-0003
.WASHER
2
................................... POLY FOAM ................................... (POST SA ART 2000-102) ................................... PS BD (VAAD11) (CSD: 012-01575-0000 V22373) ...................................... PHP (6-32 X 3/8) (VBAG02) (CSD: 089-05907-0006 V22373)
..................................... INSUL (V86928) (CSD: 091-00602-0000 V22373) ..................................... INSUL (0.500 DIA) (VAAA42) (CSD: 091-00054-0003 V22373)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10171 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 55
047-10676-0001
.HEATSINK
60
6332-0404
.SCREW
1
65
089-05903-0005
.SCREW
2
70
3223-07FR52
.INSULATOR
.................................... W/FINISH (VBAE38) (CSD: 047-10676-0001 V22373) (ATTACHING PARTS) ...................................... PHP (4-40 X 1/4) (VBAG02) (CSD: 089-05903-0004 V22373) ...................................... PHP (4-40 X 5/16) (VBAG02) (CSD: 089-05903-0005 V22373) ---*--...................................
1
2
XSTR (0.855) (V55285) (TRUE PN IS 3223-07FR-52) (CSD: 091-00286-0020 V22373) 75
SLPA125-375-01
.PIN
80
6332-0406
.SCREW
...................................... PHP (4-40 X 3/8) (VBAG02) (CSD: 089-05903-0006 V22373)
1
85
089-02140-0000
.NUT
......................................... LOCK (4-40) (V2M626) (CSD: 089-02140-0000 V22373)
1
90
091-00286-0002
.INSULATOR
......................................... SNAP LOCK (0.375) (V06915) (CSD: 090-00973-0003 V22373)
................................... XSTR (0.687) (V55285) (CSD: 091-00286-0002 V22373)
2
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10172 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 95
091-00480-0071
.BUSHING
.................................... FLG (0.116) (VBAG02) (CSD: 091-00480-0071 V22373)
1
100
SLPA125-375-01
.PIN
......................................... SNAP LOCK (0.375) (V06915) (CSD: 090-00973-0003 V22373)
1
105
091-00054-0003
.WASHER
1
110
NAS1515H04
.WASHER
1
115
092-05003-0018
.EYE ROLL
2
120
091-00286-0002
.INSULATOR
1
125
6332-0404
.SCREW
1
130
091-00480-0071
.BUSHING
1
135
047-10675-0001
.HEATSINK
1
..................................... INSUL (0.500 DIA) (VAAA42) (CSD: 091-00054-0003 V22373) ..................................... INSUL (V86928) (CSD: 091-00602-0000 V22373) .................................... (0.125 X 0.250) ................................... XSTR (0.687) (V55285) (CSD: 091-00286-0002 V22373)
...................................... PHP (4-40 X 1/4) (VBAG02) (CSD: 089-05903-0004 V22373) .................................... FLG (0.116) (VBAG02) (CSD: 091-00480-0071 V22373) .................................... MOTOR W/FINISH
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10173 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A (ATTACHING PARTS) ...................................... PHP (4-40 X 3/16)
140
089-05903-0003
.SCREW
145
BCA4022FTM
.RESISTOR CHIP
1
150
139-04322-0000
.RESISTOR CHIP
1
155
BCA4641FTM
.RESISTOR CHIP
2
160
139-04750-0000
.RESISTOR CHIP
2
165
BCA4751FTM
.RESISTOR CHIP
7
170
139-04752-0000
.RESISTOR CHIP
3
175
BCA4991FTM
.RESISTOR CHIP
5
---*--............................... (40,200 EW, 1%) (VS8185) (CSD: 139-04022-0000 V22373) R4023 ............................... (43,2000 EW, 1%) (V91637) (CSD: 139-04322-0000 V22373) R4024 ............................... (4640 EW, 1%) (VS8185) (CSD: 139-04641-0000 V22373) R4198, R4214 ............................... (475 EW, 1%) (VS8185) (CSD: 139-04750-0000 V22373) R4158, R4191 ............................... (4750 EW, 1%) (VS8185) (CSD: 139-04751-0000 V22373) R4033, R4064, R4098, R4190, R4204, R4219, R4232 ............................... (47,500 EW, 1%) (VS8185) (CSD: 139-04752-0000 V22373) R4070, R4077, R4228
............................... (4990 EW, 1%) (VS8185) (CSD: 139-04991-0000 V22373) R4088, R4135, R4169, R4226, R4229
6
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10174 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 180
139-05111-0000
.RESISTOR CHIP
1
185
BCA5112FTM
.RESISTOR CHIP
1
190
139-05113-0000
.RESISTOR CHIP
1
195
BCA5621FTM
.RESISTOR CHIP
3
200
139-05761-0000
.RESISTOR CHIP
1
205
CRCW12066190F
.RESISTOR CHIP
1
210
139-06191-0000
.RESISTOR CHIP
1
215
BCA6491FTM
.RESISTOR CHIP
1
............................... (5110 EW, 1%) (VS8185) (CSD: 139-05111-0000 V22373) R4109 ............................... (51,100 EW, 1%) (VS8185) (CSD: 139-05112-0000 V22373) R4067
............................... (511,000 EW, 1%) (VS8185) (CSD: 139-05113-0000 V22373) R4022 ............................... (5620 EW, 1%) (VS8185) (CSD: 139-05621-0000 V22373) R4060, R4062, R4102 ............................... (5760 EW, 1%) (VS8185) (CSD: 139-05761-0000 V22373) R4187 ............................... (619 EW, 1%) (V91637) (TRUE PN IS CRCW12066190F___) (CSD: 139-06190-0000 V22373) R4094 ............................... (6190 EW, 1%) (VS8185) (CSD: 139-06191-0000 V22373) R4096 ............................... (6490 EW, 1%) (VS8185) (CSD: 139-06491-0000 V22373) R4206
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10175 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 220
139-06811-0000
.RESISTOR CHIP
1
225
BCA6812FTM
.RESISTOR CHIP
2
230
139-07321-0000
.RESISTOR CHIP
1
235
CRCW12067501F
.RESISTOR CHIP
1
240
139-07502-0000
.RESISTOR CHIP
1
245
BCA7681FTM
.RESISTOR CHIP
1
250
139-08060-0000
.RESISTOR CHIP
1
255
BCA8061FTM
.RESISTOR CHIP
1
............................... (6810 EW, 1%) (VS8185) (CSD: 139-06811-0000 V22373) R4051 ............................... (68,100 EW, 1%) (VS8185) (CSD: 139-06812-0000 V22373) R4050, R4052 ............................... (7320 EW, 1%) (VS8185) (CSD: 139-07321-0000 V22373) R4170 ............................... (7500 EW, 1%) (V91637) (TRUE PN IS CRCW12067501F___) (CSD: 139-07501-0000 V22373) R4053 ............................... (75,000 EW, 1%) (VS8185) (CSD: 139-07502-0000 V22373) R4107 ............................... (7680 EW, 1%) (VS8185) (CSD: 139-07681-0000 V22373) R4227 ............................... (806 EW, 1%) (VS8185) (CSD: 139-08060-0000 V22373) R4222 ............................... (8060 EW, 1%) (VS8185) (CSD: 139-08061-0000 V22373) R4054
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10176 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 260
139-08871-0000
.RESISTOR CHIP
............................... (8870 EW, 1%) (VS8185) (CSD: 139-08871-0000 V22373) R4080
1
265
0410-5
.FAN
......................................... BRUSHLESS (VS8507) (CSD: 148-05186-0000 V22373) B4001
1
270
53001970-2
.TRANSISTOR POWER
2
275
BCA3571FTM
.RESISTOR CHIP
3
280
007-00254-0001
.TRANSISTOR
1
285
MMBTA42LT1
.TRANSISTOR
2
290
007-00261-0003
.TRANSISTOR
2
295
2N6402
.THYRISTOR
1
.......................... MOSFET, N-CHANNEL (ESDS) (V66958) (CSD: 53001970-2 V22373) Q4001, Q4004
............................... (3570 EW, 1%) (VS8185) (CSD: 139-03571-0000 V22373) R4078, R4087, R4201
................................. S PNP SOT-23 (ESDS) (V1MQ07) (CSD: 007-00254-0001 V22373) Q4021 ................................. SO PKG (ESDS) (V1MQ07) (CSD: 007-00257-0001 V22373) Q4019, Q4026 ................................. SOT (ESDS) Q4017, Q4023
.................................. (ESDS) (V1MQ07) (CSD: 007-00432-0002 V22373) Q4020
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10177 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 300
007-00467-0000
.TRANSISTOR
1
305
IRF9540
.TRANSISTOR
1
310
007-01033-0000
.TRANSISTOR
1
315
SMCJ33A
.TRNSRB
1
320
007-05245-0025
.DIODE
1
325
MUR1100E
.DIODE
4
330
007-06177-0000
.DIODE
6
................................. S NPN (ESDS) (V55464) (CSD: 007-00467-0000 V22373) Q4027 ................................. P-CHAN HEXFET (ESDS) (V59993) (CSD: 007-00937-0000 V22373) Q4018 ................................. SCR (600 V) (ESDS) (V55464) (CSD: 007-01033-0000 V22373) Q4007 ..................................... (1500 W, 33 V) (ESDS) (V14552) (CSD: 007-05241-0001 V22373) CR4038 ....................................... (36 V) (ESDS) (V1MQ07) (CSD: 007-05245-0025 V22373) CR4022 ....................................... (1000 V) (ESDS) (VBAE40) (CSD: 007-06141-0005 V22373) CR4001, CR4005, CR4009, CR4010 ....................................... SMD, SI (ESDS) (V0GWP1) (CSD: 007-06177-0000 V22373) CR4008, CR4021, CR4030, CR4031, CR4036, CR4037
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10178 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 335
CMPD2836
.DIODE
1
340
007-00179-0001
.TRANSISTOR
4
345
MMBD2837LT1G
.DIODE
1
350
007-06444-0002
.DIODE
7
355
MUR460G
.DIODE
1
360
008-00008-0002
.TERM SPLIT
2
365
008-00096-0001
.TERMINAL TEST POINT
14
....................................... DUAL (ESDS) (V55464) (CSD: 007-06181-0000 V22373) CR4034 ................................. SOT23 (ESDS) (V66958) (CSD: 007-00179-0001 V22373) Q4010, Q4015, Q4022, Q4028 ....................................... DUAL (ESDS) (V1MQ07) (CSD: 007-06182-0000 V22373) CR4041
....................................... (1 A, 150 V) (ESDS) (V1MQ07) (CSD: 007-06444-0002 V22373) CR4015 thru CR4018, CR4025, CR4026, CR4040 ....................................... ULTRAFAST (ESDS) (V1MQ07) (CSD: 007-06446-0000 V22373) CR4004 .................................. TURR (V81312) (CSD: 008-00008-0002 V22373) E4003, E4004 ......................... (V79963) (TRUE PN IS 6069-14 (REEL) OR 1069-14 (LOOSE)) (CSD: 008-00096-0001 V22373) TP4001, TP4002, TP4004, TP4007 thru TP4011, TP4014 thru TP4017, TP4020, TP4021
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10179 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 370
019-02331-0000
.INDUCTOR
1
-
370A
019-02331-0002
.INDUCTOR
1
-
370B
019-02331-0005
.INDUCTOR
1
-
370C
019-02331-0006
.INDUCTOR
1
-
370D
019-02331-0008
.INDUCTOR
1
-
370E
019-02331-0010
.INDUCTOR
1
-
370F
019-02331-0011
.INDUCTOR
1
................................... FIL (0.180-0.230) (V1DA26) (CSD: 019-02331-0000 V22373) L4009 ................................... FIL (0.300-0.355) (V1DA26) (CSD: 019-02331-0002 V22373) (OPT MFR: 019-02331-0000 V1DA26) ................................... FIL (0.455-0.500) (V1DA26) (CSD: 019-02331-0005 V22373) (OPT MFR: 019-02331-0000 V1DA26) ................................... FIL (0.630-0.685) (V1DA26) (CSD: 019-02331-0006 V22373) (OPT MFR: 019-02331-0000 V1DA26) ................................... FIL (0.980-1.10) (V1DA26) (CSD: 019-02331-0008 V22373) (OPT MFR: 019-02331-0000 V1DA26)
................................... FIL (1.50-1.70) (V1DA26) (CSD: 019-02331-0010 V22373) (OPT MFR: 019-02331-0000 V1DA26) ................................... FIL (1.70-1.90) (V1DA26) (CSD: 019-02331-0011 V22373) (OPT MFR: 019-02331-0000 V1DA26)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10180 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A -
370G
019-02331-0012
.INDUCTOR
1
375
VK200-10-36
.CHOKE PARASITIC
4
380
019-02368-0000
.TOROID CHOKE
3
385
019-06133-0000
.TRANSFORMER
1
390
019-07255-0000
.TRANSFORMER
1
395
019-07257-0000
.TRANSFORMER
1
400
65823-183
.CONNECTOR
1
405
030-02832-0003
.TERMINAL PC HEADER
2
................................... FIL (2.50-2.80) (V1DA26) (CSD: 019-02331-0012 V22373) (OPT MFR: 019-02331-0000 V1DA26) ............................. (V9V250) (TRUE PN IS VK 200 10/36) (CSD: 019-02332-0000 V22373) L4005 thru L4008
............................... (V11402) (CSD: 019-02368-0000 V22373) L4001, L4003, L4004 ............................... PULSE (ESDS) (V31740) (CSD: 019-06133-0000 V22373) T4002 ............................... FLYBACK (ESDS) (V1QYX0) (CSD: 019-07255-0000 V22373) T4001
............................... POWER (ESDS) (V11402) (CSD: 019-07257-0000 V22373) T4005 ................................. RT ANG HDR 40 (V22526) (CSD: 030-02520-0003 V22373) J4001 ......................... (V22526) (CSD: 030-02832-0003 V22373) J4002, J4003
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10181 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 410
251005
.FUSE
........................................ (5 A, 125 V) (ESDS) (V75915) (CSD: 036-00057-0010 V22373) F4001
1
415
044-00309-0005
.OSCILLATOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
(1.025 MHZ) (ESDS) (V0HAF7) (CSD: 044-00309-0005 V22373) Y4001 420
TDL157M010M1E
.CAPACITOR
1
425
096-01082-0052
.CAPACITOR
1
430
FB110H225KP012
.CAPACITOR
1
435
096-01186-0011
.CAPACITOR
2
440
T491C106K016AH
.CAPACITOR
1
.................................. TN (150 UF, 10 V) (V37942) (CSD: 096-01082-0025 V22373) C4039 .................................. TN (47 UF, 35 V) (V04222) (CSD: 096-01082-0052 V22373) C4018 .................................. TN (22 UF, 50 V) (V66958) (TRUE PN IS FB110H22K P-012) (CSD: 096-01082-0055 V22373) C4138 .................................. (47 UF, 10 V, 10%) (V31433) (CSD: 096-01186-0011 V22373) C4053, C4056 .................................. (10 UF, 16 V, 10%) (V31433) (CSD: 096-01186-0014 V22373) C4057
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10182 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 445
096-01186-0018
.CAPACITOR
2
450
T491C475K025AH
.CAPACITOR
2
455
097-00104-0038
.CAPACITOR
3
460
20SA68M
.CAPACITOR
2
465
097-00217-0009
.CAPACITOR
1
470
94SA227X0010F
.CAPACITOR
2
475
097-00218-0003
.CAPACITOR
2
.................................. (6.8 UF, 20 V, 10%) (V31433) (CSD: 096-01186-0018 V22373) C4034, C4037 .................................. (4.7 UF, 25 V, 10%) (V31433) (CSD: 096-01186-0022 V22373) C4017, C4141 .................................. AL (47 UF, 50 V) (VBAF69) (CSD: 097-00104-0038 V22373) C4050, C4073, C4074 .................................. AL/O (68 UF, 20 V) (VS4915) (CSD: 097-00217-0008 V22373) C4033, C4036
.................................. EL (100 UF, 16 V) (VS4915) (CSD: 097-00217-0009 V22373) C4045 .................................. EL (220 UF, 10 V) (V56289) (CSD: 097-00217-0013 V22373) C4058, C4065
.................................. EL (470 UF, 25 V) (V62643) (CSD: 097-00218-0003 V22373) C4044, C4054
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10183 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A
-
480
097-00218-0004
.CAPACITOR
5
485
097-00218-0005
.CAPACITOR
1
490
096-01082-0065
.CAPACITOR
1
490A
UKL1E101KPAANA
.CAPACITOR
1
495
105-00169-0000
.CAPACITOR
2
500
106-00122-0000
.CAPACITOR CHIP
6
505
106-04102-0026
.CAPACITOR CHIP
1
.................................. EL (330 UF, 50 V) (V62643) (TRUE PN IS EKMG630ELL331MJ20S) (CSD: 097-00218-0004 V22373) C4009, C4030, C4042, C4049, C4134 .................................. EL (22 UF, 100 V) (V29309) (CSD: 097-00218-0005 V22373) C4055 .................................. AL, LOW LEAKAGE CURRENT (PRE SB ART 2000-9) .................................. AL, LOW LEAKAGE CURRENT (100 UF, 25 V) (V55680) (CSD: 097-00238-0093 V22373) (POST SB ART 2000-9) C4019 .................................. MYLAR (5 VFD) (V50558) (CSD: 105-00169-0000 V22373) C4011, C4013 .............................. CER SMT 1812 (0.33 UF, 50 V, 10%) (V51406) (TRUE PN IS GRM43-2X7R334K050B_) (CSD: 106-00122-0000 V22373) C4035, C4038, C4095, C4096, C4122, C4125 .............................. (1000 PF, 100 V) (V56699) (CSD: 106-04102-0026 V22373) C4137
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10184 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 510
106-04102-0046
.CAPACITOR CHIP
2
515
106-04103-0046
.CAPACITOR CHIP
5
520
106-04103-0047
.CAPACITOR CHIP
1
525
106-04104-0046
.CAPACITOR CHIP
38
530
C1206C104K5RACT
.CAPACITOR CHIP
1
535
106-04153-0046
.CAPACITOR CHIP
8
540
106-04153-0047
.CAPACITOR CHIP
1
.............................. (1000 PF, 50 V, 5%) (V51406) (TRUE PN IS GRM42-6X7R102J050B) (CSD: 106-04102-0046 V22373) C4016, C4021
.............................. (10,000 PF, 50 V) (V51406) (CSD: 106-04103-0046 V22373) C4007, C4031, C4043, C4139, C4142 .............................. (10,000 PF, 50 V) (V51406) (TRUE PN IS GRM42-6X7R103K050B) (CSD: 106-04103-0047 V22373) C4140
.............................. (0.1 UF, 50 V) (V51406) (CSD: 106-04104-0046 V22373) C4006, C4010, C4014, C4020, C4023 thru C4029, C4032, C4040, C4041, C4046, C4047, C4051, C4052, C4059 thru C4062, C4068 thru C4070, C4109, C4119, C4120, C4132, C4133, C4143, C4149, C4152 thru C4157 .............................. (100,000 PF, 50 V) (V31433) (TRUE PN IS C1206C104K5RACT_) (CSD: 106-04104-0047 V22373) C4144
.............................. (15,000 PF, 50 V) (V51406) (CSD: 106-04153-0046 V22373) C4097 thru C4100, C4123, C4124, C4126, C4127 .............................. (15,000 PF, 50 V) (V51406) (TRUE PN IS GRM42-6X7R153K050B) (CSD: 106-04153-0047 V22373) C4004
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10185 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 545
106-04221-0014
.CAPACITOR CHIP
2
550
1206B224K500N
.CAPACITOR CHIP
2
555
106-04332-0046
.CAPACITOR CHIP
1
560
106-04471-0026
.CAPACITOR CHIP
1
565
106-04751-0016
.CAPACITOR CHIP
1
570
106-04821-0016
.CAPACITOR CHIP
4
575
118-00082-0000
.CAPACITOR
1
580
SN74LS221D
.INTEGRATED CIRCUIT
2
.............................. (220 PF, 2%) (V31433) (CSD: 106-04221-0014 V22373) C4145, C4146 .............................. (0.22 UF, 50 V, +/-10%) (V65238) (TRUE PN IS 1206B224K500N_) (CSD: 106-04224-0047 V22373) C4066, C4067 .............................. (3300 PF, 50 V) (V31433) (CSD: 106-04332-0046 V22373) C4008
.............................. (470 PF, 100 V) (V51406) (TRUE PN IS GRM42-6C0G471J100B) (CSD: 106-04471-0026 V22373) C4005 .............................. (750 PF, 50 V) (V51406) (CSD: 106-04751-0016 V22373) C4136
.............................. (820 PF, 50 V) (V51406) (TRUE PN IS GRM42-6C0G821J050B) (CSD: 106-04821-0016 V22373) C4101, C4102, C4128, C4129 .................................. (0.005 UF, 1000 V) (V59660) (CSD: 118-00082-0000 V22373) C4012 .......................... (ESDS) (V82647) (CSD: 120-00108-0002 V22373) U4020, U4058
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10186 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 585
120-02233-0003
.INTEGRATED CIRCUIT
1
590
XC3042A7PQ100I
.INTEGRATED CIRCUIT
1
595
120-03163-0001
.INTEGRATED CIRCUIT
2
600
LM318M
.INTEGRATED CIRCUIT
1
605
120-03174-0014
.INTEGRATED CIRCUIT
1
610
LM2902M
.INTEGRATED CIRCUIT
1
615
120-03430-0000
.INTEGRATED CIRCUIT
1
.......................... DUAL DRIVER (ESDS) (V1ES66) (CSD: 120-02233-0003 V22373) U4003 .......................... GATE ARRAY (ESDS) (V68994) (TRUE PN IS XC3042A-7PQ100I) (CSD: 120-02469-0001 V22373) U4011 .......................... SO-14 COMP (ESDS) (V66958) (CSD: 120-03163-0001 V22373) U4002, U4012 .......................... (ESDS) (V27014) (CSD: 120-03167-0004 V22373) U4059 .......................... OP AMP BI FET SO (ESDS) (V82647) (CSD: 120-03174-0014 V22373) U4061
.......................... (ESDS) (V27014) (CSD: 120-03196-0000 V22373) U4018 .......................... (ESDS) (V34333) (CSD: 120-03430-0000 V22373) U4001
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10187 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 620
MC33166T
.INTEGRATED CIRCUIT
2
625
120-03520-0000
.INTEGRATED CIRCUIT
2
630
LM285D-2-5
.INTEGRATED CIRCUIT
1
635
120-03569-0000
.INTEGRATED CIRCUIT
4
640
AD7226KR
.INTEGRATED CIRCUIT
1
645
120-03593-0000
.INTEGRATED CIRCUIT
1
650
MM74HCT00M
.INTEGRATED CIRCUIT
1
.......................... PWR SWTCHG REGULTR (ESDS) (V1MQ07) (CSD: 120-03510-0000 V22373) U4005, U4006 .......................... OVER VOLTAGE SENSE (ESDS) (V1MQ07) (CSD: 120-03520-0000 V22373) U4014, U4015 .......................... VOLT REF (ESDS) (V1MQ07) (TRUE PN IS LM285D-2.5) (CSD: 120-03544-0000 V22373) U4019 .......................... DMOS F-B DVR (ESDS) (V66958) (CSD: 120-03569-0000 V22373) U4033, U4034, U4049, U4050
.......................... CMOS QUAD 8-BIT DAC (ESDS) (V24355) (CSD: 120-03592-0000 V22373) U4013 .......................... QUAD SW (ESDS) (V17856) (CSD: 120-03593-0000 V22373) U4060 .......................... SO PKG (ESDS) (V7D893) (CSD: 124-00000-0003 V22373) U4054
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10188 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A
-
655
124-00074-0003
.INTEGRATED CIRCUIT
660
126-00074-0000
.MICROSTEPING ROM
.......................... SO PKG (ESDS) (V0JN86) (CSD: 124-00074-0003 V22373) U4008
1
..........................
1
.........................
1
............................... (0 QW) (V91637) (CSD: 130-05000-0035 V22373) CJ4013 thru CJ4019
(ESDS) 661
122-30064-0000
..INTEGRATED CIRCUIT (ESDS) U4010
665
130-05000-0035
.RESISTOR CHIP
7
670
CRCW20102R7J
.RESISTOR CHIP
12
675
131-00100-0033
.RESISTOR
1
680
131-00101-0033
.RESISTOR
1
685
132-00102-0017
.RESISTOR
1
............................... (2.7 HW, 5%) (V91637) (TRUE PN IS CRCW20102R7J___) (CSD: 130-05027-0043 V22373) R4030, R4031, R4036, R4037, R4139, R4140, R4142, R4143, R4162 thru R4165
................................... CF (10 HW, 5%) (VBAD71) (CSD: 131-00100-0033 V22373) R4014 ................................... CF (100 HW, 5%) (VBAD71) (TRUE PN IS CF1/2 5% 100 OHM) (CSD: 131-00101-0033 V22373) R4015 ................................... WW (0.24 OHM, 1 W, 5%) (V24546) (CSD: 132-00102-0017 V22373) R4013
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10189 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 690
SPH2R15-5PCT
.RESISTOR
1
695
133-00562-2202
.RESISTOR
1
700
DS125-272K
.RESISTOR
1
705
134-01026-0006
.VRSTR
1
710
CCF55-1023F
.RESISTOR
3
715
137-00034-0000
.TEMP SENSOR
1
720
BCA20R0FTM
.RESISTOR CHIP
1
................................... WW (0.15 OHM, 2 W, 5%) (V11502) (TRUE PN IS SPH-2 R15 5%) (CSD: 132-05051-0000 V22373) R4195 ................................... VAR 12-15T (2000 OHMS) (V32997) (CSD: 133-00562-2202 V22373) R4200 ................................... THMS (2700 OHMS, 10%) (V15454) (TRUE PN IS DS125 272K) (CSD: 134-01015-0031 V22373) R4185
...................................... VI00ZA15 (81 V) (V75915) (CSD: 136-01023-0072 V22373) CR4039 ................................... PF (102,000 QW, 1%) (V91637) (TRUE PN IS CCF-55 1023 F) (CSD: 136-01023-0072 V22373) R4016, R4020, R4235 ................................ (ESDS) (V27014) (CSD: 137-00034-0000 V22373) U4017 ............................... (20 EW, 1%) (VS8185) (CSD: 139-00200-0000 V22373) R4006
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10190 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 725
139-00221-0000
.RESISTOR CHIP
1
730
BCA1000FTM
.RESISTOR CHIP
1
735
139-01001-0000
.RESISTOR CHIP
24
740
BCA1002FTM
.RESISTOR CHIP
13
745
139-01003-0000
.RESISTOR CHIP
5
750
BCA1004FTM
.RESISTOR CHIP
1
755
139-01021-0000
.RESISTOR CHIP
1
760
BCA1214FTM
.RESISTOR CHIP
1
............................... (22.1 EW, 1%) (VS8185) (CSD: 139-00221-0000 V22373) R4010 ............................... (100 EW, 1%) (VS8185) (CSD: 139-01000-0000 V22373) R4231 ............................... (1000 EW, 1%) (VS8185) (CSD: 139-01001-0000 V22373) R4011, R4032, R4061, R4097, R4138, R4141, R4161, R4166, R4173, R4175, R4176, R4178, R4180 thru R4183, R4196, R4197, R4199, R4205, R4207, R4221, R4224, R4233 ............................... (10,000 EW, 1%) (VS8185) (CSD: 139-01002-0000 V22373) R4008, R4071, R4110, R4111, R4136, R4137, R4203, R4211, R4215, R4216, R4220, R4223, R4230
............................... (100,000 EW, 1%) (VS8185) (CSD: 139-01003-0000 V22373) R4086, R4090 thru R4092, R4188 ............................... (1M EW, 1%) (VS8185) (CSD: 139-01004-0000 V22373) R4108 ............................... (1020 EW, 1%) (VS8185) (CSD: 139-01021-0000 V22373) R4192 ............................... (1240 EW, 1%) (VS8185) (CSD: 139-01241-0000 V22373) R4213
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10191 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 765
139-01302-0000
.RESISTOR CHIP
1
770
BCA1371FTM
.RESISTOR CHIP
1
775
139-02001-0000
.RESISTOR CHIP
1
780
BCA2002FTM
.RESISTOR CHIP
1
785
139-02102-0000
.RESISTOR CHIP
1
790
BCA2151FTM
.RESISTOR CHIP
1
795
139-02211-0000
.RESISTOR CHIP
1
800
BCA2212FTM
.RESISTOR CHIP
1
805
139-02213-0000
.RESISTOR CHIP
1
............................... (13,000 EW, 1%) (VS8185) (CSD: 139-01302-0000 V22373) R4208 ............................... (1370 EW, 1%) (VS8185) (CSD: 139-01371-0000 V22373) R4028 ............................... (2000 EW, 1%) (VS8185) (CSD: 139-02001-0000 V22373) R4212, R4225 ............................... (20,000 EW, 1%) (VS8185) (CSD: 139-02002-0000 V22373) R4009 ............................... (21,000 EW, 1%) (VS8185) (CSD: 139-02102-0000 V22373) R4186
............................... (2150 EW, 1%) (VS8185) (CSD: 139-02151-0000 V22373) R4089 ............................... (2210 EW, 1%) (VS8185) (CSD: 139-02211-0000 V22373) R4021 ............................... (22,100 EW, 1%) (VS8185) (CSD: 139-02212-0000 V22373) R4059 ............................... (221,000 EW, 1%) (V91637) (CSD: 139-02213-0000 V22373) R4074
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10192 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 810
BCA2432FTM
.RESISTOR CHIP
1
815
139-02433-0000
.RESISTOR CHIP
1
820
BCA2491FTM
.RESISTOR CHIP
2
825
139-02493-0000
.RESISTOR CHIP
1
830
BCA2670FTM
.RESISTOR
1
835
139-02742-0000
.RESISTOR CHIP
1
840
CRCW12062871F
.RESISTOR CHIP
1
845
139-03013-0000
.RESISTOR CHIP
1
............................... (24,300 EW, 1%) (VS8185) (CSD: 139-02432-0000 V22373) R4066
............................... (243,000 EW, 1%) (VS8185) (CSD: 139-02433-0000 V22373) R4189 ............................... (2490 EW, 1%) (VS8185) (CSD: 139-02491-0000 V22373) R4079, R4081 ............................... (249,000 EW, 1%) (VS8185) (CSD: 139-02493-0000 V22373) R4093 ................................... (267 EW, 1%) (VS8185) (CSD: 139-02670-0000 V22373) R4210 ............................... (27,400 EW, 1%) (VS8185) (CSD: 139-02742-0000 V22373) R4012
............................... (2870 EW, 1%) (V91637) (TRUE PN IS CRCW12062871F___) (CSD: 139-02871-0000 V22373) R4202 ............................... (301,000 EW, 1%) (VS8185) (CSD: 139-03013-0000 V22373) R4084
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10193 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
3A 850
BCA3321FTM
.RESISTOR CHIP
3
855
106-00124-0000
.CAPACITOR CHIP
2
860
BCA3322FTM
.RESISTOR CHIP
1
865
139-03402-0000
.RESISTOR CHIP
1
870
009-08548-0020
.PC BOARD
1
............................... (3320 EW) (VS8185) (CSD: 139-03321-0000 V22373) R4029, R4068, R4209 .............................. CR (0.15 UF, 500 V) (V95275) (CSD: 106-00124-0000 V22373) C4063, C4064 ............................... (33,200 EW, 1%) (VS8185) (CSD: 139-03322-0000 V22373) R4069 ............................... (34,000 EW, 1%) (VS8185) (CSD: 139-03402-0000 V22373) R4063 ................................... (VAAC40) (CSD: 009-08548-0020 V22373)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10194 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 4. (Sheet 1 of 1) Receiver Assembly
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10195/10196 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
4 -
1
200-05553-0001
RECEIVER ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . . . (ESDS) (SEE IPL FIGURE 9 ITEM 140 FOR NHA)
RF
5
047-09953-0001
.COVER
1
10
089-05874-0004
.SCREW
1
15
089-05874-0003
.SCREW
2
20
187-01813-0000
.GASKET
...................................... PREAMP W/FINISH (VBAA66) (CSD: 047-09953-0001 V22373) (ATTACHING PARTS) ...................................... PHP (2-56 X 1/4) (V56563) (CSD: 089-05874-0004 V22373) ...................................... PHP (2-56 X 3/16) ---*--.....................................
1
EMI (VAAA42) (CSD: 187-01813-0000 V22373) 25
200-08545-0000
.PREAMP BOARD ASSEMBLY
.....................
1
.....................
1
SRX24 (ESDS) (REPL BY ITEM: 25A) (PRE SB ART 2000-3) (SEE 5 FOR DETAILS) -
25A
200-08545-0020
.PREAMP BOARD ASSEMBLY SRX24 (ESDS) (REPL ITEM: 25) (POST SB ART 2000-3) (SEE 5A FOR DETAILS)
(ATTACHING PARTS) ...................................... PHP (2-56 X 1/2)
30
089-05899-0008
.SCREW
35
076-02825-0000
.SPACER
---*--..................................... THREADED (V65590) (CSD: 076-02825-0000 V22373)
1
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10197 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
4 40
076-02825-0001
.SPACER
45
089-08001-0034
.WASHER
50
187-01869-0001
.ABSORBER
1
55
073-00946-0002
.HOUSING
1
60
089-05874-0004
.SCREW
65
187-01814-0000
.GASKET
..................................... THREADED (V65590) (CSD: 076-02825-0001 V22373) (ATTACHING PARTS) ..................................... SPLIT (LK #2) (VBAG02) (CSD: 089-08001-0034 V22373) ---*--................................... MICROWAVE (V1A839) (CSD: 187-01869-0001 V22373) .................................... PRE-AMP (V59848) (CSD: 073-00946-0002 V22373) (ATTACHING PARTS) ...................................... PHP (2-56 X 1/4) (V56563) (CSD: 089-05874-0004 V22373) ---*--.....................................
1
2
2
1
EMI (VAAA42) (CSD: 187-01814-0000 V22373) 70
155-02744-0001
.CABLE ASSEMBLY
1
75
076-02817-0001
.INSERT
4
80
015-00238-0001
.X-BAND RADAR
1
............................. PRE-AMP (V40080) (CSD: 155-02744-0001 V22373) ...................................... METRIC/UNC (V65590) (CSD: 076-02817-0001 V22373) ............................... FR END (VS5416) (TRUE PN IS NJT 1946AN) (CSD: 015-00238-0001 V22373)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10198 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 5. (Sheet 1 of 1) Preamp Board Assembly (-0000)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10199/10200 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
5 -
1
200-08545-0000
PREAMP BOARD ASSEMBLY . . . . . . . . . . . . . . . . . . . . . SRX24 (ESDS) (SEE IPL FIGURE 4 ITEM 25 FOR NHA)
RF
5
030-00444-0001
.CONNECTOR
1
10
013-00181-0000
.FERRITE CHIP
................................. SM COAX J1001 ................................
1
................................. HDR RTANG J1002
IND L1001 15
030-03171-0003
.CONNECTOR
1
20
096-01186-0013
.CAPACITOR CHIP
1
25
106-04102-0046
.CAPACITOR CHIP
1
30
106-04104-0046
.CAPACITOR CHIP
1
35
106-04272-0016
.CAPACITOR CHIP
.............................. (0.0027 UF, NPO, 50 V) C1002
1
40
120-03053-0009
.OP AMP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
.............................. (3.3 UF, 16 V) C1003 .............................. (1000 UF, 50 V, 5%) C1004 .............................. (0.1 UF, X7R, 50 V) C1001
DUAL (ESDS) U1003 45
120-03544-0000
.VOLT REF
1
50
120-03581-0000
.MMIC
1
55
137-00034-0000
.TEMP SENSOR
.................................... (ESDS) U1004 ........................................ INA02184 (ESDS) U1001 ................................
1
(ESDS) U1002 60
139-01003-0000
.RESISTOR CHIP
............................... (100,000 EW, 1%) R1005 thru R1008
4
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10201 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
5 65
139-02051-0000
.RESISTOR CHIP
1
70
139-02211-0000
.RESISTOR CHIP
1
75
139-02432-0000
.RESISTOR CHIP
1
80
139-06491-0000
.RESISTOR CHIP
1
85
009-08545-0000
.PC BOARD
1
............................... (2050 EW, 1%) R1003 ............................... (2210 EW, 1%) R1002 ............................... (24,300 EW, 1%) R1004 ............................... (6490 EW, 1%) R1001 ...................................
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10202 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 5A. (Sheet 1 of 1) Preamp Board Assembly (-0020)
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10203/10204 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
5A -
1
200-08545-0020
PREAMP BOARD ASSEMBLY . . . . . . . . . . . . . . . . . . . . . SRX24 (ESDS) (SEE IPL FIGURE 4 ITEM 25A FOR NHA)
RF
5
008-00311-0000
.TERMINAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
BIFURCATE (ESDS) (V18310) (CSD: 008-00311-0000 V22373) E1006 10
013-00181-0000
.FERRITE CHIP
1
15
030-03171-0003
.CONNECTOR
1
20
T491B335K016AH
.CAPACITOR CHIP
1
25
106-04102-0046
.CAPACITOR CHIP
1
30
106-04104-0046
.CAPACITOR CHIP
1
35
106-04272-0016
.CAPACITOR CHIP
1
................................ IND (V51406) (CSD: 013-00181-0000 V22373) L1001 ................................. HDR RTANG (6P) (V0VGY3) (CSD: 030-03171-0003 V22373) J1002 .............................. (3.3 UF, 16 V) (V31433) (CSD: 096-01186-0013 V22373) C1003 .............................. (1000 UF, 50 V, 5%) (V51406) (CSD: 106-04102-0046 V22373) C1004
.............................. (0.1 UF, X7R, 50 V) (V51406) (TRUE PN IS GRM42-6X7R104J050B) (CSD: 106-04104-0046 V22373) C1001 .............................. (0.0027 UF, NPO, 50 V) (V31433) (CSD: 106-04272-0016 V22373) C1002
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10205 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
5A 40
.OP AMP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
LM358D
1
DUAL (ESDS) (V1MQ07) (CSD: 120-03053-0009 V22373) U1003 45
008-00310-0000
.TERMINAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
BIFURCATE (ESDS) (V1A942) (CSD: 008-00310-0000 V22373) E1005 50
LM285D-2-5
.VOLT REF
1
55
120-03581-0000
.MMIC
1
60
LM35DM
.TEMP SENSOR
1
65
139-01003-0000
.RESISTOR CHIP
4
70
BCA2051FTM
.RESISTOR CHIP
1
75
139-02211-0000
.RESISTOR CHIP
1
.................................... (ESDS) (V1MQ07) (TRUE PN IS LM285D-2.5) (CSD: 120-03544-0000 V22373) U1004 ........................................ INA02184 (ESDS) (CSD: 120-03581-0000 V22373) U1001 ................................ (ESDS) (V27014) (CSD: 137-00034-0000 V22373) U1002 ............................... (100,000 EW, 1%) (VS8185) (CSD: 139-01003-0000 V22373) R1005 thru R1008 ............................... (2050 EW, 1%) (VS8185) (CSD: 139-02051-0000 V22373) R1003
............................... (2210 EW, 1%) (VS8185) (CSD: 139-02211-0000 V22373) R1002
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10206 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
5A 80
BCA2432FTM
.RESISTOR CHIP
1
85
139-06491-0000
.RESISTOR CHIP
1
90
009-08545-0020
.PC BOARD
1
............................... (24,300 EW, 1%) (VS8185) (CSD: 139-02432-0000 V22373) R1004
............................... (6490 EW, 1%) (VS8185) (CSD: 139-06491-0000 V22373) R1001 ................................... (VAAC21) (CSD: 009-08545-0020 V22373)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10207 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10208 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 6. (Sheet 1 of 1) Magnetron Assembly
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10209/10210 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
6 -
1
200-05310-0000
MAGNETRON ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . (SEE IPL FIGURE 9 ITEM 155 FOR NHA)
RF
5
076-02821-0001
.TUBE WIRE
2
10
008-00300-0004
.TERMINAL LUG
............................... (V81349) (CSD: 008-00300-0004 V22373)
1
15
IST253-62
.SLEEVE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2
................................... W/ FINISH (V65590) (CSD: 076-02821-0001 V22373)
SOLDER (0.62) (V0VGY3) (TRUE PN IS IST-253-62) (CSD: 150-00072-0000 V22373) 20
021-00127-0001
.MAGNETRON
................................. (X-BAND)
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10211 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10212 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 7. (Sheet 1 of 1) Pitch Motor Assembly
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10213/10214 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
7 -
1
200-05173-0010
PITCH MOTOR ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . FLEX WIRE (SEE IPL FIGURE 9 ITEM 50 FOR NHA)
RF
5
65307-001
.CONNECTOR
1
10
030-02204-0002
.CONNECTOR
................................. HSG (6 CAV) (V22526) (CSD: 030-02204-0002 V22373) P3
1
15
47745-000
.TERMINAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5
................................. PLUG, KEYING (V22526) (CSD: 030-01058-0001 V22373)
(22-26) (V22526) (CSD: 030-02205-0005 V22373) 20
091-00109-0000
.CABLE TIE
2
25
047-10162-0002
.FEEDTHRU
................................... W/FERRULE (V16673) (CSD: 047-10162-0002 V22373)
1
30
008-00073-0000
.TERMINAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
................................... (V56501) (TRUE PN IS TY523M OR TY23M(BULK)) (CSD: 091-00109-0000 V22373)
RING (V9H210) (CSD: 008-00073-0000 V22373) 35
IST253-62
.SLEEVE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2
SOLDER (V0VGY3) (TRUE PN IS IST-253-62) (CSD: 150-00072-0000 V22373) 40
089-05857-0006
.SCREW
1
45
076-02823-0000
.DAMPER
1
...................................... SET (4-40 X 3/16) (VBAG02) (CSD: 089-05857-0006 V22373) ..................................... (V65590) (CSD: 076-02823-0000 V22373)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10215 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
7 50
148-05182-0003
.GEAR ASSEMBLY
.............................. MOTOR, ROBOTIC WIRES (V7Y951) (CSD: 148-05182-0003 V22373) B1
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10216 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 8. (Sheet 1 of 1) Azimuth Motor Assembly
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10217/10218 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
8 -
1
200-05174-0000
AZIMUTH MOTOR ASSEMBLY . . . . . . . . . . . . . . . . . . . . . (SEE IPL FIGURE 1 ITEM 200 FOR NHA)
RF
5
65307-001
.CONNECTOR
1
10
030-02204-0002
.CONNECTOR
................................. HSG (6 CAV) (V22526) (CSD: 030-02204-0002 V22373) P2
1
15
47745-000
.TERMINAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5
................................. PLUG, KEYING (V22526) (CSD: 030-01058-0001 V22373)
(22-26) (V22526) (CSD: 030-02205-0005 V22373) 20
091-00109-0000
.CABLE TIE
2
25
047-10162-0002
.FEEDTHRU
................................... W/FERRULE (V16673) (CSD: 047-10162-0002 V22373)
1
30
MS51535-4
.TERMINAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
................................... (V56501) (CSD: 091-00109-0000 V22373)
RING (V81349) (CSD: 008-00300-0004 V22373) 35
150-00072-0000
.SLEEVE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2
SOLDER (V0VGY3) (CSD: 150-00072-0000 V22373) 40
089-05857-0006
.SCREW
1
45
076-02823-0000
.DAMPER
1
...................................... SET (4-40 X 3/16) (VBAG02) (CSD: 089-05857-0006 V22373) ..................................... (V65590) (CSD: 076-02823-0000 V22373)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10219 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
8 50
148-05182-0003
.GEAR ASSEMBLY
.............................. MOTOR, ROBOTIC WIRES (V7Y951) (CSD: 148-05182-0003 V22373) B1
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10220 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10221 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 9. (Sheet 1 of 2) Gimbal Assembly
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10222 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 9. (Sheet 2 of 2) Gimbal Assembly
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10223/10224 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
9 -
1
200-05175-0020
GIMBAL ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (ESDS) (SEE IPL FIGURE 1 ITEM 230 FOR NHA)
RF
5
088-03143-0000
.GUIDE CABLE
1
10
091-00109-0003
.CABLE TIE
2
15
029-00767-0001
.GEAR SCAN
1
20
089-06492-0005
.SCREW
25
073-00969-0001
.CAM POS FDBK
30
089-05907-0003
.SCREW
35
147-05169-0012
.BEARING
2
40
089-05878-0006
.SCREW
...................................... PHP (4-40 X 3/8) (V56563) (CSD: 089-05878-0006 V22373)
4
45
32054-0182
.LUG
......................................... SLDR (VBAG02) (CSD: 008-00065-0000 V22373)
1
................................. (V0WYL6) (CSD: 088-03143-0000 V22373)
................................... (V56501) (CSD: 091-00109-0003 V22373) .................................. W/ FINISH (V7Y951) (CSD: 029-00767-0001 V22373) (ATTACHING PARTS) ...................................... SHC (4-40 X 5/16) (VBAG02) (CSD: 089-06492-0005 V22373) ---*--............................... W/ FINISH (ATTACHING PARTS) ...................................... PHP (6-32 X 3/16) ---*--.................................... FLNGD SHLD (VBAF59) (CSD: 147-05169-0012 V22373)
4
1
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10225 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
9
-
50
200-05173-0000
.PITCH MOTOR ASSEMBLY
1
50A
200-05173-0010
.PITCH MOTOR ASSEMBLY
1
55
089-05878-0005
.SCREW
60
029-00768-0001
.CLUSTER GEAR
1
65
089-08339-0000
.WASHER
1
70
SSRIF6632ZZHA3
.BEARING
2
75
047-09947-0001
.MOUNTING PLATE
............................. TILT MOTOR (V0B485) (CSD: 047-09947-0001 V22373)
1
80
076-02277-0000
.PIN
......................................... PIVOT (V19142) (CSD: 076-02277-0000 V22373)
2
85
46068-0607S
.SCREW
....................... FLEX WIRE (REPL BY ITEM: 50A) (PRE SB ART 2000-11)
....................... FLEX WIRE (REPL ITEM: 50) (POST SB ART 2000-11) (SEE IPL FIGURE 7 FOR DETAILS) (ATTACHING PARTS) ...................................... PHP (4-40 X 5/16) (V56563) (CSD: 089-05878-0005 V22373) ---*--............................... W/ FINISH (V7Y951) (CSD: 029-00768-0001 V22373) ..................................... CURVED SPRG (V56563) (CSD: 089-08339-0000 V22373) .................................... FLNGD SHLD (VBAF59) (TRUE PN IS SSRIF-6632ZZHA3) (CSD: 147-05169-0010 V22373)
...................................... SHC (6-32 X 7/16) (VBAG02) (CSD: 089-06493-0007 V22373)
4
2
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10226 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
9 90
089-05857-0006
.SCREW SET
1
95
089-08110-0034
.WASHER
2
100
36008-025C
.RING RETAINER
............................... (0.25) (VBAG02) (CSD: 090-00019-0002 V22373)
2
105
089-08600-0000
.SHIM
........................................ (0.002 IN. THK) (V56563) (CSD: 089-08600-0000 V22373)
1
-
105A
089-08600-0002
.SHIM
........................................ (0.006 IN. THK) (OPT MFR: 089-08600-0000 V56563)
1
-
105B
089-08600-0004
.SHIM
........................................ (0.010 IN. THK) (OPT MFR: 089-08600-0000 V56563)
1
-
105C
089-08600-0007
.SHIM
........................................ (0.016 IN. THK) (OPT MFR: 089-08600-0000 V56563)
1
110
029-00766-0002
.GEAR TILT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
.................................. (4-40 X 3/16) (VBAG02) (CSD: 089-05857-0006 V22373) ..................................... SPLIT (LK #6) (VBAG02) (CSD: 089-08110-0034 V22373)
(48 PTCH) (V7Y951) (CSD: 029-00766-0002 V22373) 115
088-03123-0001
.CABLE GUARD
120
089-06494-0028
.SCREW
125
047-10683-0001
.CLIP CABLE
................................ W/ BRACKET (V0WYL6) (CSD: 088-03123-0001 V22373) (ATTACHING PARTS) ...................................... SHC (8-32 X 1-3/4) ---*--.................................. W/ FINISH (V16673) (CSD: 047-10683-0001 V22373)
1
4
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10227 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
9 130
091-00109-0003
.CABLE TIE
1
135
088-03148-0000
.SHROUD CABLE
1
140
200-05553-0001
.RECEIVER ASSEMBLY
1
145
089-06494-0005
.SCREW
4
150
091-00109-0003
.CABLE TIE
................................... (V56501) (CSD: 091-00109-0003 V22373)
4
155
200-05310-0000
.MAGNETRON ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . .
1
................................... (V56501) (CSD: 091-00109-0003 V22373) ............................... (V0WYL6) (CSD: 088-03148-0000 V22373) .......................... (ESDS) (SEE IPL FIGURE 4 FOR DETAILS) ...................................... SHC (8-32 X 5/16) (VBAG02) (CSD: 089-06494-0005 V22373)
(SEE IPL FIGURE 6 FOR DETAILS) 160
089-05857-0006
.SCREW SET
1
165
015-00250-0000
.RF NETWORK
................................. (V6P860) (CSD: 015-00250-0000 V22373)
1
170
200-05554-0000
.TILT SENSOR ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . .
1
.................................. (4-40 X 3/16) (VBAG02) (CSD: 089-05857-0006 V22373)
(SEE IPL FIGURE 10 FOR DETAILS)
-
175
B3LT1658
.X-BAND LIMITER
1
175A
015-00239-0002
.X-BAND LIMITER
AR
180
012-01567-0000
.LINER
1
.............................. (V6P860) (CSD: 015-00313-0001 V22373) (SELECT FROM THIS OR THE FOLLOWING) WG100 .............................. (POST SA ART 2000-107) ....................................... TEFLON (VAAA42) (CSD: 012-01567-0000 V22373)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10228 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 10. (Sheet 1 of 1) Tilt Sensor Assembly
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10229/10230 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
10 -
1
200-05554-0000
TILT SENSOR ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . (SEE IPL FIGURE 9 ITEM 170 FOR NHA)
RF
5
089-02136-0000
.NUT
1
10
089-08093-0030
.WASHER
1
15
089-08335-0000
.WASHER
1
20
089-08076-0030
.WASHER
1
25
073-00968-0003
.FOLL TILT
1
30
047-10500-0001
.COVER
1
35
6732-0203
.SCREW
40
030-01453-0000
.POLARIZING PLUG . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
......................................... LOCK (2-56) (V72962) (CSD: 089-02136-0000 V22373) ..................................... FLAT (STD 0.094) ..................................... CURVED SPRING (V30408) (CSD: 089-08335-0000 V22373) ..................................... FLAT (STD 0.130) (V5X576) (CSD: 089-08076-0030 V22373) .................................... W/HDWR (V7Y951) (CSD: 073-00968-0003 V22373) ...................................... W/F (VBAA66) (CSD: 047-10500-0001 V22373) (ATTACHING PARTS) ...................................... FHP (2-56 X 3/16) (VBAG02) (CSD: 089-06004-0003 V22373)
2
---*--1
HEADER (2MM) 45
030-03170-0003
.CONNECTOR
................................. HSG (2 ROW, 6 POSITION) (V22526) (CSD: 030-03170-0003 V22373) P5
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10231 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
10 50
030-01444-0000
.CONTACT
5
55
047-10162-0002
.FEEDTHRU
1
60
076-02890-0001
.FERRULE
1
65
120-03584-0000
.LINEAR HALL EFFECT
1
70
073-05176-0003
.GIMBAL
1
.................................... (V22526) (CSD: 030-01444-0000 V22373) ................................... W/FERRULE (V16673) (CSD: 047-10162-0002 V22373) .................................... (V65590) (CSD: 076-02890-0001 V22373) .......................... (V91929) (CSD: 120-03584-0000 V22373) U100 ...................................... W/HDW (V65267) (CSD: 073-05176-0003 V22373)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10232 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 11. (Sheet 1 of 1) Scan Sensor Assembly
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10233/10234 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
11 -
1
200-05313-0000
SCAN SENSOR ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . (SEE IPL FIGURE 1 ITEM 235 FOR NHA)
RF
5
NUTTYPE1660
.NUT
1
10
089-08093-0030
.WASHER
1
15
U125-0040S
.WASHER
1
20
089-08076-0030
.WASHER
..................................... FLAT (STD 0.130) (V5X576) (CSD: 089-08076-0030 V22373)
1
25
088-03147-0000
.SLEEVE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
30
078-02101-0000
.SPRING TORSION
1
35
047-10018-0002
.FOLLOWER SCAN AXIS
1
40
088-03137-0000
.CABLE BUMPER
1
45
089-06491-0004
.SCREW
50
047-10501-0001
.COVER
......................................... LOCK (2-56) (V72962) (TRUE PN IS NUT TYPE 1660) (CSD: 089-02136-0000 V22373) ..................................... FLAT (STD 0.094) ..................................... CURVED SPRING (V30408) (TRUE PN IS U125-0040-S) (CSD: 089-08335-0000 V22373)
............................. (V83826) (CSD: 078-02101-0000 V22373) ......................... (V16673) (CSD: 047-10018-0002 V22373) ............................... (V0WYL6) (CSD: 088-03137-0000 V22373) (ATTACHING PARTS) ...................................... SHC (2-56 X 1/4) (V56563) (CSD: 089-06491-0004 V22373) ---*--...................................... W/F (VBAA66) (CSD: 047-10501-0001 V22373)
1
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10235 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
11 55
030-01453-0000
.POLARIZING PLUG . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
HEADER (2MM) 60
69307-006LF
.CONNECTOR
1
65
77138-101LF
.CONTACT
5
70
120-03584-0000
.LINEAR HALL EFFECT
1
75
073-05178-0003
.BRACKET
1
................................. HSG (2 ROW, 6 POSITION) (V22526) (CSD: 030-03170-0003 V22373) P6 .................................... (V22526) (CSD: 030-01444-0000 V22373) .......................... (V91929) (CSD: 120-03584-0000 V22373) U100 .................................... PIVOT, TOP
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10236 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 12. (Sheet 1 of 1) Configuration Module Assembly
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10237/10238 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
EFFECT (USE) CODE
NOMENCLATURE
UNITS PER ASSY
12 -
1
071-00097-0100
CONFIGURATION MODULE ASSEMBLY . . . . . . . . . . . . . CM2000 (ESDS)
RF
5
057-05587-0001
.TAG
......................................... SERIAL NUMBER
1
10
057-02834-0000
.TAG
......................................... ESD
1
15
057-05587-0000
.TAG
......................................... SERIAL NUMBER
1
20
047-09643-0001
.CASE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
(VBAA66) (CSD: 047-09643-0001 V22373) (ATTACHING PARTS) ...................................... PHP (2-56 X 1/8) (V56563) (CSD: 089-06119-0002 V22373)
25
089-06119-0002
.SCREW
30
DS11Q1
.CAP
35
089-05878-0010
.SCREW
2
40
4541-10-0-7
.LOCK TAB
2
45
200-08705-0000
.CONFIGURATION MODULE BOARD ASSEMBLY
---*--......................................... PROTECTIVE, SUB-D (9P) (V23540) (CSD: 090-00990-0001 V22373) ...................................... PHP (4-40 X 5/8) .................................... (V28198) (CSD: 030-02352-0000 V22373)
2
1
.....
1
........................................ (VL0375) (CSD: 047-09644-0002 V22373)
1
(ESDS) (SEE IPL FIGURE 13 FOR DETAILS) 50
047-09644-0002
.BASE
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10239 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
Blank Page
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10240 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
IPL Figure 13. (Sheet 1 of 1) Configuration Module Board Assembly
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Pages 10241/10242 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
13 -
1
200-08705-0000
CONFIGURATION MODULE BOARD ASSEMBLY . . . . . . (ESDS) (SEE IPL FIGURE 12 ITEM 45 FOR NHA)
RF
5
090-00559-0003
.STANDOFF
2
10
007-06452-0000
.DIODE
5
15
HDC9M30000-14
.CONNECTOR
1
20
T491D336K016AH
.CAPACITOR
1
25
106-04103-0046
.CAPACITOR CHIP
1
30
M93C56WMN6
.SERIAL EEPROM
2
35
130-05101-0043
.RESISTOR CHIP
1
................................... (0.116) (V46384) (CSD: 090-00559-0003 V22373) ....................................... SIGNAL (0.2 A, 85 V) (ESDS) (V55464) (CSD: 007-06452-0000 V22373) CR101 thru CR105 ................................. SUB-MINIATURE (9P) (V28198) (CSD: 030-02346-0012 V22373) J101 .................................. (33 UF, 16V, 10%) (V31433) (CSD: 096-01186-0015 V22373) C101 .............................. (10,000 UF, X7R/50V) (V51406) (CSD: 106-04103-0046 V22373) C102 .............................. SO-8 (ESDS) (VBAF71) (TRUE PN IS M93C56-WMN6) (CSD: 120-02420-0003 V22373) U101, U102
............................... (100 HW) (V91637) (CSD: 130-05101-0043 V22373) R101
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10243 3 Jan 2012
COMPONENT MAINTENANCE MANUAL 071-01519
FIG. ITEM
PART NUMBER
AIRLINE STOCK NO. 1234567
NOMENCLATURE
EFFECT (USE) CODE
UNITS PER ASSY
13 40
BCA1001FTM
.RESISTOR CHIP
2
45
139-01002-0000
.RESISTOR CHIP
1
50
BCA4751FTM
.RESISTOR CHIP
3
55
007-06448-0000
.DIODE
1
60
009-08705-0000
.PC BOARD
1
............................... (1000 EW, 1%) (VS8185) (CSD: 139-01001-0000 V22373) R102, R106 ............................... (10,000 EW, 1%) (VS8185) (CSD: 139-01002-0000 V22373) R107 ............................... (4750 EW, 1%) (VS8185) (CSD: 139-04751-0000 V22373) R103 thru R105 ....................................... SCHTKY (1 A, 30 V) (ESDS) (V1MQ07) (CSD: 007-06448-0000 V22373) CR106 ................................... (V0B0T3) (CSD: 009-08705-0000 V22373)
- ITEM NOT ILLUSTRATED
EFFECTIVITY ALL
34-40-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10244 3 Jan 2012
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