2. Sia a330 Etops Manual
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a330 Etops Manual...
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A330 ETOPS MANUAL AIRBUS A330-343 AIRCRAFT POWERED BY
RR TRENT 772B-60 ENGINE
Document No.
: QCD/ETOPS/A330/01
Manual Hold
:
Manual Copy No.
:
9-B AIRLINE HOUSE 25 AIRLINE ROAD SINGAPORE 819829 TEL NO: (65) 6541-5983 FAX NO: (65) 6542-4167
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DISTRIBUTION LIST Copy No.
Holder
AIRWORTHINESS AUTHORITY 1
Civil Aviation Authority of Singapore
ENGINEERING DIVISION Senior Vice President Engineering (To view via Intranet) Divisional Vice President Engineering (Services) (To view viaIntranet) 2
Senior Manager Quality Vice President Technical Services (To viewvia Intranet) Vice President Engineering Supplies (To view via Intranet) Vice President Maintenance Planning and Control (To view viaIntranet)
3
Technical Library Senior Engineering Controller, SIA OCC (To view via Intranet)
FLIGHT OPERATIONS DIVISION Chief Pilot A330 (To view via Intranet) SIA ENGINEERING COMPANY (SIAEC) Senior Vice President (Operations) (To view via ntranet) I Senior Vice President (Line Maintenance & Materials) (To viewvia Intranet) Vice President Line Maintenance (To view viaIntranet) Vice President Base Maintenance (To view viaIntranet) Vice President Quality & Safety (To view via Intranet) Vice President Productivity & Engineering Training (To view viaIntranet) Duty Engineer Line Maintenance (To view viaIntranet) AIRCRAFT COPY: One copy on each A330 aircraft (in Aircraft Documentation File) HANDLING AGENT COPY: One copy for each line station A330 handling agent (in CD-Rom) NOTE 1: The Singapore Airlines Exposition can be viewed by all staff in the SIA Group via the Intranet address:http://eng.sq.com.sg/sia_quality/manuals.html
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2
MANUAL ADMINISTRATION
2.1
The Senior Manager Quality (SMQ) is responsible for the development of this Manual and obtaining approval from the Civil Aviation Authority ofSingapore.
2.2
Manual holds, as listed in the Distribution List, are responsible for ensuring that the relevant staff in their division/department is familiar with the contents of this Manual. Changes are to be highlighted to SMQ to enable immediate review.
2.3
SMQ is responsible for ensuring that changes are incorporated into the Manual in a timely manner through revisions or amendments.
3
REVISION RECORD
STATUS
DATE OF ISSUE
DATE INSTED
SIGN
REMARKS
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LIST OF EFFECTIVE PAGES
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Appendix II
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This Singapore Airlines A330 ETOPS Manualincorporating the above listed pages isapproved by CAAS.
Signature:
Date:
11 Feb 2009
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TABLE OF CONTENTS
SECTION
SUBJECT
PAGE
1
DISTRIBUTION LIST
1
2
MANUAL ADMINISTRATION
2
3
REVISION RECORD
2
3.1
2
Back ground to Latest Issue/Revision
4
LIST OF EFFECTIVE PAGES
5
TABLE OF CONTENTS
6
INTRODUCTION
7
6.1 6.2 6.3 6.4 6.5
7 7 7 8 8
7
ETOPS APPROVAL 7.1 7.2 7.3
8
Type Certificate ETOPS Type Design Approved By Certification Authorities ETOPS Operational Approval
CONFIGURATION CONTROL 8.1 8.2
9
Purpose Regulatory Documents Responsible Individuals Associated Documents Use of Inspection Notices
Engine and Airframe Modification Procedures ETOPS Parts Control for A330 aircrafts powered by Trent 772B-60 series engines
DESPATCH CONFIGURATION AND MAINTENANCE REQUIREMENTS 9.1 9.2
Minimum Equipment List ETOPS Items in MEL
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4-6
9 9 9 10
11 11 - 12
13 13 13 - 14
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ETOPS PRE-DEPARTURE SERVICE CHECK (PDSC) 10.1 10.2 10.3 10.4
General ETOPS PDSC Requirements/Responsibilities Definition of the ETOPS PDSC Procedure for ETOPS Despatch Briefing for LAEs
15 15 15 15 - 16 16
11
ETOPS SIGNIFICANT SYSTEMS
17
12
ETOPS RELIABILITY PROGRAM
18
12.1 12.2 12.3 12.4 12.5 12.6 12.7
18 18 19 19 20 21 22
Reporting Requirements Analysis and Corrective Action Defect Resolution Plan Identification of ETOPS Tasks APU In-Flight Start Program Program Review APU In-Flight Start Form
13
PROPULSION SYSTEM MONITORING PROGRAM
23
14
OIL CONSUMPTION MONITORING PROGRAM
24
14.1 14.2
24 24
15
16
17
Oil Consumption Program Procedures/DataCollection Oil Consumption Program Despatch/CorrectiveAction Policies
ENGINE CONDITION MONITORING PROGRAM
25
15.1 15.2
25 25
ECM Program Procedures/DataCollection ECM Program - Corrective Action
ETOPS MAINTENANCE OPERATING RESTRICTIONS POLICY
26
16.1
Identical Maintenance on Similar Systems
26
RESOLUTION OF AIRCRAFT DISCREPANCIES
27
17.1 17.2 17.3
27 27 27
Verification of Maintenance Action Requirements Determination of the Need for In-Flight Verification Verification Flight Definition
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19
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AIRCRAFT DESPATCH
28
18.1 18.2 18.3
28 28 29
Procedures for Emergency Diversions Verification Flight Requirements ETOPS Verification Flight Form
ETOPS TRAINING PROGRAM
30
19.1 19.2 19.3
30 30 30
ETOPS Qualified Maintenance Personnel A330 Type Courses ETOPS Awareness Training
ETOPS AUDIT PROGRAM
31
Appendix I – Airbus Document - A330 ETOPS Part List Appendix II – A330 ETOPS Significant System List
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INTRODUCTION
6.1
Purpose
01 January 2009
The purpose of this ETOPS Manual is to identify the engineering and maintenance program requirements and organisational responsibilities for theExtended-range Two-engine Operations (ETOPS) for A330 aircraft at Singapore Airlines (SIA). It defines the practices and procedures for the ETOPS. The document explains the ETOPS engineering and maintenance program in detail, with references toother associated documents listed in paragraph 6.4 below.
6.2
Regulatory References .1 .2
6.3
Singapore Airworthiness Requirements (SAR) Chapter 4.11 EASA Acceptable Means of Compliance no. AMC 20-6
Responsible Individuals SMQ is responsible for the development of this Manual and obtaining approval from the Civil Aviation Authority of Singapore (CAAS). Direct responsibility for the implementation of the requirements identified in the Manual lies with: SIA Engineering Division .1 .2 .3 .4
Vice President Technical Services Vice President Engineering Supplies Vice President Maintenance Planning and Control Senior Manager Quality
The ongoing implementation of ETOPSrequirement is performed by: SIA Engineering Company (SIAEC) .1 .2 .3 .4
Vice President Line Maintenance Vice President Base Maintenance Vice President Quality & Safety Vice President Productivity & Engineering Training
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6.4
01 January 2009
Associated Documents The current issues/revisions of the following documents are to be used in conjunction with the ETOPS Manual. SIA Engineering Division .1 .2 .3 .4 .5 .6
Singapore Airlines Exposition Document Technical Services Department Organisation and Procedures Manual Engineering Supplies Department Organisation and Procedures Manual Maintenance Planning and Control Department Organisation and Procedures Manual Quality Department Organisation and Procedures Manual Reliability Program Manual
SIA Engineering Company (SIAEC) .7 .8 .9 .10 .11
SIA Engineering Company Exposition (CAAS) Line Maintenance Division Organisation and Procedures Manual Base Maintenance Division Organisation and Procedures Manual Quality & Safety Division Organisation and Procedures Manual Productivity & Engineering Training Division Exposition
Airbus .1 .2 .3
6.5
Configuration,Maintenance and Procedures, LR2-EASA - AMC 20-6-C-SIA-0001 A330 ETOPS Part List, AI/EA-O 418/0174/94 Iss 13 A330 ETOPS Significant System List, EAZ 418.0186/03
Use of Inspection Notices SIA receives information relating to maintenance and inspection practices through technical / maintenance publications, reports from sampling inspections & investigations and service experience. Inspection Notices serve to communicate and highlight appropriate technical, safety and maintenance issues, including ETOPS-related issues, to Licence / Authorisation Holders who performs maintenance and servicing on SIA aircraft. They may also be used to alert Licence / Authorisation Holders of changes to regulatory or company requirements which are urgent / critical in nature.
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7
ETOPS APPROVAL
7.1
Type Certificate
01 January 2009
The Type Certificate Data Sheet Note 6 indicates that production aircraft meets Type Design Approval requirements for ETOPS. Any aircraft added to the ETOPS fleet must comply with the current revision of the Configuration, Maintenance and Procedures (CMP) document and Airworthiness Directives (AD) applicable to that aircraft/engine combination. The Type Design Approval does not reflect an approval to conduct extended range operations. An Operational Approval from CAAS is required.
7.2
ETOPS Type Design Approved by Certification Authorities TABLE 1 - ETOPS TYPE DESIGN APPROVED BYCERTIFICATION AUTHORITIES Airframe / Engine Type
Certification Authority
Approval Date
A330-343 / Rolls Royce Trent 772B-60
EASA
21 October 1996
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7.3
01 January 2009
ETOPS Operational Approval SIA A330 aircraft / engine combinations that are approved for ETOPS are listed in Table 2. TABLE 2 – A330 AIRCRAFTS IN SIA FLEET
Airframe
Engine Type
A330-343
Rolls Royce Trent 772B60 Series Engines
CAAS Approval
Approved
Approved
Routes/ Times
Aircraft Registration
Diversion Time
See Note 1.
9V-STA through 9V-STS (inclusive)
180 mins
Note 1: Details of approved routes are contained in A330 Flight Operations Manual Volume 1, Chapter: Operational Policy - ETOPS Policy / Approved ETOPS Routes.
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CONFIGURATION CONTROL The aircraft listed in Table 2 are approved for ETOPS operations and comply with the ETOPS configuration standards identified in the latest revision of CMP Document No. LR2-EASA AMC 20-6-C-SIA-0001. The policies and procedures listed below, governing modifications and ETOPS parts control, assure that the aircraft will continue to comply with the applicable ETOPS configuration requirements.
8.1
Engine and Airframe Modification Procedures The Aircraft Flight Manual for the aircraft states that those airframe/engine combinations can be used for ETOPS when configured in accordance with the latest revision of the CMP document. The following paragraphs define how Service Bulletins and Airworthiness Directives will be incorporated. .1
Incorporation of ETOPS Service Bulletins Service Bulletins (SB) and Service Information Letters (SIL) identified in the current revision of the CMP document required for ETOPS operation must be incorporated in accordance with the schedule given in the CMP. TSP will review any revision of CMP on a quarterly basis and report to SIA on any changes and required actions arising. Technical Services and Quality are responsible for determining these ETOPS requirements and TSP is responsible for scheduling the affected aircraft for modification and inspection. TSP manual (Operational Process E: Planning, Maintenance Programs) refers.
.2
Incorporation of Airworthiness Directives In cases where ETOPS related SBs and SILs have been made into an Airworthiness Directive (AD), the incorporation dates in the AD will be adhered to, in accordance with the current procedure for AD control. TSP manual (Operational Process D: AD & AOT Management) refers.
8.2
ETOPS Parts Control for A330 aircrafts powered by Trent 772B-60 series engines The A330/RR Trent 772B-60 aircraft/series engine combination was designed from the onset as an ETOPS configuration. Only parts in Airbus and Rolls Royce Illustrated Parts Catalogues (IPC) shall be used on SIA A330 aircrafts powered by Trent 772B-60 series engines. .1
Purpose of Parts Control
Theused Airbus andA330 Rollsaircraft Royce and IPCsRR are approved documents for information of parts to be for the Trent 772B-60 series engines. .2
Parts Borrowing and Pooling All parts will be verified by part number and dash number as acceptable per the SIA customised IPCs for A330 aircraft and RR Trent 772 B-60 series engine. All borrowed parts shall be verified per the above before they can be used.
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.3
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Non-Approved ETOPS Parts for A330 aircrafts powered by Trent 772B-60 series engines Information towards the control of ETOPS partsare provided in the A330 ETOPSPart nd List, reference no: AI/EA-O 418/0174/94 / Issue 13, issued on 2 May 2007. A copy of the document is provided in Appendix I to this manual. This document, used in conjunction with the Configuration, Maintenance and Procedures (CMP) document and the Illustrated Parts Catalogues (IPC) defines all ETOPS compliant that can be used in the A330 / RR Trent 772B-60 engine type.
.4
ETOPS Parts for A330-343 Aircraft Due to the availability of different configurations for the Cargo Fire Suppression System on the A330 aircraft variants, the following table shows the ETOPS parts which are approved for SIA A330-343 aircraft. No
Component
Part Number Approved for A330-343
Part Number NOT Approved for A330-343
472625-1
Refer to Page 26.1 of
472931-2
the A330 ETOPS Part List document stated in Section 8.2.3
ATA 26 – FIRE PROTECTION Cargo Fire Extinguishers 1 Walter Kidde Inc. (1600 cu. In) Cargo Fire Extinguishers 2 Walter Kidde Inc. (2170 cu. In)
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DESPATCH CONFIGURATION AND MAINTENANCE REQUIREMENTS
9.1
Minimum Equipment List
01 January 2009
The SIA A330 Minimum Equipment List (MEL) has been developed from the JAA Master MEL for A330 aircraft.
9.2
ETOPS Items in MEL Information provided below is extracted from SIA's A330 MEL, as amended. For items which will affect aircraft despatch for ETOPS flights, a Deferred Defect Log (DDL) entry should be raised and annotated:“ETOPS IMPACTED”. Maintenance Control Centre (MCC) or Maintrol has to be informed accordingly. CAUTION: The latest copy of the MEL must be used to determine applicability of MEL for despatch of aircraft. MEL items affecting ETOPS flights are clearly ident ified within the publication. These items are marked thus, “[ER]”. A list of all the ETOPS affected items are listed below:
ITEM
SYSTEM
DESCRIPTION
1.
21-31-01
Automatic Cabin Pressure Control System (CPC, out ow valve AUTO channels)
2.
21-31-02
Manual Cabin Pressure Control System (Outflow valve MAN channel, MAN V/S CTL Sel)
3.
22-10-01
Autopilot (AP)* [P] [CAT II/III]
4.
22-10-05
AP Disengagement Warning*
5.
22-72-01
Lateral Navigation
6.
22-73-02
Fuel/Time Prediction
7.
22-82-01A
Multipurpose Control and Display Unit (MCDU) − MCDU*
8.
22-82-01B
Multipurpose Control and Display Unit (MCDU) − FM Selection on MCDU MENU*
9.
22-83-01
Flight Management Guidance (FMGEC)
10.
22-83-02A
FMA Indications on PFD − AP/FD Related Indications
11.
23-11-01
HF System [P]
12.
23-12-01
VHF System [P]
13.
24-22-02
IDG Oil Circuit
fl
and
Envelope
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ITEM
SYSTEM
DESCRIPTION
14.
24-25-01B
AC ESS FEED Control — Manual Transfer to AC BUS 2 (ALTN Function)*
15.
27-44-01
Stabilizer Actuator Electrical Motor [CATII/III] [P]
16.
27-93-01A
PRIM − PRIM 1* [CAT II/III] [P]
17.
28-21-01A
Inner Tank Pump
18.
28-23-01
Crossfeed Valve*
19.
30-21-01
Engine Anti-Ice Valve* [P]
20.
30-31-04
Angle of Attack Probes Heating
21.
31-63-01
Display Unit (DU)* [P] [CAT II/III]
22.
32-31-03
Landing Gear Retracting System* [P]*
23.
32-33-01
Landing Gear Gravity Extension System* [P]*
24.
33-42-01
Landing Light*
25.
34-10-01A
ADIRS − IR [CAT II/III] [P]
26.
34-10-01B
ADIRS − ADR [CAT II/III] [P]
27.
34-14-01A
Indications on PFD and ND − Attitude Display [CAT II/III] [P]
28.
34-36-01
ILS* [P] [CAT II/III]
29.
34-41-01
Weather Radar System
30.
34-51-01
DME* [P]
31.
34-52-01
ATC − Transponder*
32.
34-53-01
ADF [P]
33.
34-55-01
VOR/MARKER* [P]
34.
36-11-01
Bleed Air Supply System*
35.
73-25-01C
FADEC − EPR Control Mode [P]*
36.
73-25-01D
FADEC — A/C 115VAC Power Supply Channel A
37.
74-11-01
Ignition Emergency Power Supply System
38.
79-21-01
Air/Oil Heat Exchanger Valve
−
Main* [P]
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ETOPS PRE-DEPARTURE SERVICE CHECK (PDSC)
10.1
General ETOPS PDSC Requirements/Responsibilities
01 January 2009
Prior to departure of an A330 aircraft on an ETOPS flight, an ETOPS PDSC is required. For SIA A330 aircraft, the ETOPS PDSC is included in the common Transit Check, Pre-Departure Check and Daily Check lists. All departures from Singapore and line stations are treated like ETOPS flights unless otherwise stated that the aircraft has been downgraded for non-ETOPS operation. Responsibility for compliance with PDSC procedures and conducting the checks lies with the Line Maintenance’s or Technical Handling Agent’s Licensed Aircraft Engines (LAE) performing transit or departure check.
10.2
Definition of the ETOPS PDSC The ETOPS PDSC will be integrated within the common Transit Check, Pre-Departure Check and Daily Check lists contained in the CAAS approved A330 Maintenance Schedule.
10.3
Procedure for ETOPS Despatch In addition to the normal despatch procedure, the following points should be noted for an ETOPS flight: .1
ETOPS FLIGHT ROUTING The information on the ETOPS routes by city pairs can be found in the relevant chapters of the Flight Operations Manual covering ETOPS policies.
.2
ETOPS MEL ITEMS The MEL will dictate whether an item or a defect affects flight despatch. Where despatch is not allowed, Flight Despatch will be informed for alternate non-ETOPS route planning. No Despatch Authorisations for ETOPS MEL ite ms are permitted to be granted.
.3
OIL CONSUMPTION CHECK Prior to an ETOPS flight, if the engine or APU oil uplift exceeds the limits for maximum oil consumption, the oil uplifts from the previous sectors will be noted and the average oil consumption per flight hour computed. If the rate exceeds the acceptable limit, Line Maintenance’s Duty Engineer (for Singapore) and Maintenance Control Centre (for line stations) will be consulted for advice on problem resolution and disposition.
.4
PARTS UPLIFT FROM From time to time, loan LINE partsSTATIONS may be necessary for fitment to SIA A330 aircraft with RR Trent 772B-60 series engine at line stations. These replacement parts must be acceptable for an ETOPS aircraft, and the LAE in-charge of despatching the ETOPS flight will ensure that only approved parts are installed. The Airbus and Rolls Royce IPCs are the approved documents for the information of parts to be used on SIA A330 aircraft with RR Trent 772B-60 series engines.
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A330-343 ETOPS CONFIRMATION CHECKSHEET The ETOPS Confirmation Process is introduced for the A330-343 fleet. It is to confirm the accomplishment of the ETOPS pre-departure service check (PDSC), which is part of the normal Transit Check, Pre-Departure Check and Daily Checks. This Confirmation Process is to be performed during .1 .2 .3
10.4
Pre-Departure Checks (to be accomplished before the first flight after the Daily Check); Transit Checks in SIN for selected flights specified in Maintenance Process Sheet (MPS) Form no. INS/A330/3020; and Transit Checks at designated line stations as specified in the MPS form no. INS/A330/3020.
Briefing For LAEs LAEs assigned to depart an aircraft on an ETOPS flight shall be trained on the ETOPS PDSC requirements and responsibilities.
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ETOPS SIGNIFICANT SYSTEMS ETOPS Significant Systems are categorized into 3Categories: Category 1 Systems, Category 2 and Category 3 Systems. The definitions and the content of these system items areprovided in the Airbus document referenced, EAZ 418.0186/03. A current matrix of this document is provided on Appendix II of this manual.
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01 January 2009
ETOPS RELIABILITY PROGRAM SIA ETOPS Reliability Program is an event-oriented program, where each ETOPSrelated event is reported and investigated. The ETOPS Reliability Program is included in the Reliability Program currently in place for all SIA aircraft. ETOPS-related issues are discussed during the monthly Reliability Control Board (RCB) meetings. CAAS participates in the meeting.
12.1
Reporting Requirements Under the existing Reliability Program, data of the aircraft systems defects, unscheduled component removals and engine removal events are collected, collated and published each month. Also, the Mandatory Defect Report system will highlight significant and airworthiness related problems, including ETOPS events, to CAAS. If there exists any adverse trend that requires additional attention or investigation, arrangem ents will be made for SIA and aircraft / engine manufacturers to discuss these operational issues with the CAAS. The CAAS will be briefed on these issues and the corrective actions. The reliability program, technical incident and AOC meetings with CAAS and Mandatory Defect Report System will be extended to cover the A330 aircraft with RR Trent 772B-60 series engine to adequately meet the requirements of CAASSAR Chapter 4.11.
12.2
Analysis and Corrective Action The data that are provided on published reports as discussed in para. 12.1 are used for monthly Recurring Defect Committee (RDC) and monthly Reliability meetings, which review trending aircraft, engine or component defects. Additionally, the technical incidents and AOC meetings with CAAS will review engine in-flight shut down (IFSD) events, air-turn-backs (ATB) and diversions. Each significant ETOPS event will be reviewed by Line / BaseMaintenance, Technical Services, and Quality to determine the cause of the problem. If corrective action is required, Special Inspection or Modification will be issued to ha ve the necessary work performed. Maintenance Planning and Control will schedule the work to be accomplished. Line / Base Maintenance will carry out the corrective action. Following completion of the work, Technical Services and Quality will monitor the item to ensure that corrective action has been effective. Further analysis and corrective action willbe conducted, if required.
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Defect Resolution Plan Short Term The existing daily operations review meeting is extended to cover A330 aircraft / RR Trent 772B-60 series engine defects / problems. The meeting, with relevant represen tation from Line Maintenance, Technical Services, Quality, Airbus and Rolls Royce will review technical delays, cancellations, diversions, ATBs, engine IFSD events and significant defects. Causes will be discussed, corrective action decided, and plansto normalise the situation established. Long Term The existing Reliability Meetings, Aircraft / Engine / APU Delay Meetings are extended to cover A330 aircraft / RR Trent 772B-60 series engine defects / problems. The meeting, with relevant representation from Line Maintenance, Base Maintenance, Workshops, Technical Services, Quality, Engineering Supplies, Maintenance Planning and Control, Airbus and Rolls Royce will review all and long term concerns together with the required rectification, modification, reliability / product improvement and other necessary follow up action through bi-monthly AOC meetings with CAAS. In addition, Technical Services has an established program to identify, regularly discuss and resolve aircraft / engine problem withaircraft / engine manufacturers including A330 aircraft RR / Trent 772B-60 series engine.
12.4
Identification of ETOPS Tasks The maintenance program is set up by Fleet Management Department based on the Maintenance Planning Document (MPD), which includes allETOPS maintenance tasks as basic requirements. ETOPS tasks are identified by Quality Department and Fleet Management Department. Such tasks must be highlighted on the task cards. ETOPS related tasks that have accomplishment interval different from the planned maintenance check intervals will be controlled separately through the use of Special Inspection (SI).
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01 January 2009
APU In-flight Start Program The APU In-flight Start Program for SIA A330 aircraft is to monitor the APU start and run reliability in order to ensure adequate reliability for ETOPS. In order to demonstrate the reliability of the APU in SIA aircraft, the following program has been implemented. The Program is based on the successful APU start at three (3) attempts or less for the same flight. An APU In-flight Start shall be conducted on each aircraft once every three (3) months. The Flight Crew shall do the following: .1
Attempt to start the APU sometime during the one-hour period prior to the top of descent, or at such time to ensure atwo-hour cold soak at altitude. Multiple start attempts may be performed within the limits stated in the Aircraft Flight Manual.
.2
The Flight Crew will make an entry in the Aircraft Technical Log and APU In-flight Start Form (Form No: SIA/MPS/004) shown on the next page, for each flight during which an APU in-flight start is attempted. The entry will include the following information: 1 2 3 4 5
Altitude of each attempt Statement that attempt was or was not successful Outside Air Temperature (OAT) Indicate if APU shut down after reaching 95% Indicate if APU failed to start on ground
If an APU is not capable of in-flight start, an entry shall be made in the Deferred Defect Log (DDL) to inform the Flight Crew that APU is not available for ETOPS flights more than 180 minutes. The subject DDL entry should be closed upon rectification and the successful completion of another APU in-flight start. Technical Services and Quality will periodically review the data to monitor the APU in-flight start reliability and identify procedural design problem if necessary. Other than the APU Controller, which senses, monitor and control the start and operation of the APU, there are other components which, when replaced, may affect the APU in-flight start capability. When any of these components are replaced, apart from performing the usual functional check on ground, an APU in-flight start will need to be performed on the next flight to verify that the in-flight start capability and the opera tion of the APU is not affected. The result of the in-flight start will be lodged within the Aircraft Technical Log. The components affected are listed below: No. .1 .2
ATA: System 49-16: Air Intake
Component Affected Air Intake Flap Actuator
49–23: Load Compressor
•
•
• •
.3
49-30: Engine Fuel and Control
• • •
Inlet Temperature Sensor Outlet Temperature Sensor Inlet Pressure Transducer Fuel Temperature Sensor Primary / Secondary Fuel Atomizer Fuel Control Unit
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No.
ATA: System
Component Affected Flow Divider Fuel Low Pressure Switch
• •
.4
49-40: Ignition & Starting
• • • • • •
.5
49-50: Air
Main / Backup Start Contactor
•
Total Air Pressure Sensor Bleed Flow Sensor Bleed Valve Surge Control Valve
• • •
.6
49-60: Engine Controls
•
Electronic Control Box
.7
49-72: Temperature Indicating
•
EGT Thermocouple Rake
.8
49-90: Oil
• • • • • •
12.6
Ignition Exciter Igniter Plug Ignition Lead Starter Start Clutch Module
Low Oil Temperature Sensor Oil Pump Module Low Quantity Switch Low Pressure Switch High Oil Temperature Sensor Oil Heater
Program Review The ETOPS Reliability Program, including related procedures, will be reviewed regularly to ensure effectiveness of the program.
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12.7
01 January 2009
APU In-flight Start Form (Form No: SIA/MPS/004) Note: To refer to latest issue
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13
01 January 2009
PROPULSION SYSTEM MONITORING PROGRAM Quality is responsible for monitoring all engine IFSD events and calculating the IFSD rate. The tracking function is subcontracted by TSP to be performed by SIAEC Reliability Section. The IFSD rate, based on 1000 engine hours, is computed on a monthly basis. The IFSD rate data, together with the 12-month moving average, will beincluded in the monthly Reliability Report. A copy of the monthly Reliability Report is provided to the CAAS, and the IFSD rate data is reviewed during the monthly Reliability meetings chaired by SIAQuality. Technical Services and Quality will carry out investigation of every IFSD, exceedence and unsatisfactory trends. CAAS will be informed of each IFSD thro ugh Mandatory Defect Report (MDR). If the IFSD rate exceeds 0.03/1000 engine hours for 180-minute operation, a fact finding and evaluation team lead by Technical Services and Quality will be initiated and a recovery plan developed as follows: .1
IFSD events during the preceding 12-month period will be audited to verify the cause and validity of the corrective action taken.
.2
Engine and airframe manufacturers will be contacted to evaluate the 12-month analysis and participate in the development of arecovery plan.
.3
The recovery plan will be implemented.
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14
01 January 2009
OIL CONSUMPTION MONITORING PROGRAM The engine and APU oil consumption will be monitored on a flight-by-flight basis to identify exceedence of limits. Aircraft exhibiting questionable characteristics will be restricted from ETOPS until the fault has been corrected for limits of oil consumption rate. Refer to A330 AMM.
14.1
Oil Consumption Program Procedures/DataCollection Engine and APU oil quantity will be checked and serviced to the FULL level prior to despatch on an ETOPS flight. Engine oil quantity will be physically checked using the oil sight gauge, whereas APU oil quantity may be checked using the ECAM readout. Engine and APU oil will be checked within 5 to 30 minutes of engine shutdown after each flight segment. The information will be entered into the Fuel and Oil Record log book. There is one column for each engine and APU in the Fuel and Oil Recor d log book. If the engine or APU oil uplift exceeds the limits for maximum oil consumption per Maintenance Manual, the oil uplifts from the previous sectors shall be noted and the average oil consumption per flight hour computed. If the rate exceeds the acceptable limit, Line Maintenance‘s Duty Engineer (for despatch from SIN) or Senior Maintenance Controller (SMC), SIA Operation Control Centre, (SIAOCC) (for despatch from line stations), will be consulted for advice on problem resolution and disposition. The technical handling agent at the respective line station is responsible for notifying SMC, SIAOCC of abnormal oil quantity uplifts. If the oil consumption rates are acceptable, or when a detected problem has been corrected, the aircraft can be released forETOPS, providing other restraints have been cleared. Engine and APU oil uplifted for each flight are updated byTechnical Services Department using the Fuel and Oil Records as well as correspondences from overseas line stations. Technical Services Department will monitor the oilconsumption rate and rectify any abnormal oil uplifts.
14.2
Oil Consumption Program Despatch/CorrectiveAction Policies Oil consumption will be determined prior to despatch of the aircraft into ETOPS service. Aircraft exhibiting questionable characteristics will be restricted from ETOPS service until the fault has been corrected. NOTE: If Duty Engineer, SMC, SIAOCC or Technical Ser vices can positively determine that apparent exceedence is due to a one-time, identifiable anomaly, or to calculation tolerances resulting from short flight segments, the aircraft may be despatched into ETOPS service. On short flight segments, computed consumption may appear to exceed limits dueamounts to the accumulation indicating system and the off of fractional of oil addedofduring servicin g. tolerances In such instance s, rounding the oil computed consumption rate should be computed over more sectors prior to further troubleshooting.
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15
01 January 2009
ENGINE CONDITION MONITORING PROGRAM The purpose of the Engine Condition Monitoring (ECM) program is to continuously monitor engine performance and to initiate timely corrective action when necessary. This program will ensure that engine limit margins aremaintained so that a prolonged single-engine diversion may be conducted without exceeding approved engine limits, e.g. rotor speeds (N1, N2, N3), exhaust gas temperatures, (EGT).
15.1
ECM Program Procedures/DataCollection The ECM program utilises the ECM computer software provided by the engine manufacturer to provide trending reports on the applicable engine parameters. Monitored parameters (depending on engine type and manufacturer) include parameters such as EGT, N1, N2, N3, Fuel Flow, AVM, Oil Temperature, and Oil Pressure. SIA has contracted Data System+Services (DS+S) to monitor the health of the engines under the SIA engine management programme. This contracted organisation (established by the engine manufacturer), continuously monitors the performance of allthe operating engines in the aircraft fleet during flight and will notify Technical Services Power Plant Section whenever any anomalies are noticed.
15.2
ECM Program - Corrective Action Whenever an engine trending becomes of concern, SIATechnical Services Power Plant Section will investigate the problem to determine the cause. Appropriate action will be recommended during the daily Maintenance Review meeting. After corrective action has been implemented, verification of the maintenance willbe performed in accordance with Section 17.
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16
ETOPS MAINTENANCE OPERATING RESTRICTIONS POLICY
16.1
Identical Maintenance On Similar Systems
01 January 2009
Special consideration will be given to maintenance carried out on identical units in ETOPS Significant Systems listed in Section 11, particularly on both the engines at the same time. Identical maintenance action on multiple, similar systems is defined as the same task, such as servicing, removal/installation, disassembly or repairs, being performed on more than one engine or similar systems or components during the same maintenance visit. Examples would include, but not limited to: .1
Removal of both engine oil filters or both chip detectors.
.2
Replacement of both Integrated Drive Generators (IDG).
k cap removed is not an “Identical Maintenance NOTE: Engine oil servicing or oil check with tan Task”. For identical maintenance on ETOPS Category 2 Significant Systems as listed in Appendix II, different sets of crew (LAEs and technicians) arerequired to perform the maintenance. Scheduled maintenance on multiple, similar systems should be scheduled as much as possible such that tasks will be performed during different check packages or different phases of phased checks. Routine line checks should also be staggered to prevent maintenance action from being performed on both systems at the same time. If, through some non-routine or tight inspection interval causes, multiple actions do occur, the following will apply: .1
Different LAEs and Technicians will perform the maintenance on similar systems; or
.2
All other tasks on ETOPS Category 2 and 3 Significant Systems performed by different technicians and inspected by a Licence/Authorisation hold shall have to be cleared by VPQ-SIA/SMQ-SIA, who will determine the additional maintenance requirements to be carried out.
Technical Services / Quality may be consulted to determine the necessity for a verification flight per Section 17 or any other additional checks based upon the systems involved and the maintenance performed. Detailed information on the above, which is relevant to maintenance personnel, is contained in the latest revisions of Inspection Notices reference nos: SIA/00-001, SIA/00-025 & SIA/00-026. Regular sampling checks will be conducted to ensure compliance to ETOPS Maintenance Operating Restrictions Policy.
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17
01 January 2009
RESOLUTION OF AIRCRAFT DISCREPANCIES Positive verification that the corrective action taken to resolve problems significant to ETOPS has to be effective and is required prior to subsequent ETOPS flights. Positive verification of effective maintenance is also required for situations identified in Section 16. Verification may be accomplished by Built-In Test Equipment (BITE), ground checks per the Trouble Shooting Manual (TSM) or the Maintenance Manual (MM). Under certain circumstances, it may be necessary to verify success of themaintenance action during an actual flight.
17.1
Verification of Maintenance Action Requirements Verification of maintenance will be required inthe following circumstances: .1 .2 .3 .4 .5 .6
After an engine in-flight shut-down (IFSD) on a previous flight; After primary airframe system failure on a previous flight; After replacement of an engine; After failure of an engine power control system or significant adverse trends in engine performance; After any major maintenance work on the aircraft, such as Zonal / Heavy Maintenance Visit (HMV). After failure of any ETOPS Category 2 and 3 Significant Systems.
Technical Services / Quality may determine any other maintenance action or conditions which will require verification on acase-by-case basis.
17.2
Determination of the Need for In-Flight Verification In the event that maintenance action cannot be verified by normal ground tests, or the problem or fault cannot be duplicated on the ground, an in-flight verification will be required. Technical Services / Quality may be consulted to determine the necessity for a verification flight. A verification flight should be usedONLY in the following circumstances: .1 .2 .3
.5 .6
The is no effective ground check; No check exists in the MM; BITE checks do not adequately verify system operation or effectiveness of the corrective action; The system can only be finally "confirmed fixed" during actual operation in the air, i.e., fault cannot be duplicated on ground; After an engine in-flight shut-down (IFSD) on a previous flight; After replacement of an engine; or
.7
After(HMV). any major maintenance work on the aircraft, such as Zonal / Heavy Maintenance Visit
.4
17.3
Verification Flight Definition A verification flight may be a non-revenue functional check flight or non-ETOPS revenue flight during which the flight crew is requested to assist Maintenance in determining that an ETOPS Significant System is confirmed to be operating normally, or that an ETOPS significant problem has been resolved. This shall be reflected in the aircraft technical log.
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18
01 January 2009
AIRCRAFT DESPATCH SIA shall ensure that all A330 aircraft are precluded from being despatch for ETOPS unless all problems significant to ETOPS are positivelyresolved per Section 17.
18.1
Procedures for Emergency Diversions Such procedures are written in Engineering Procedures for Aircraft Crisis Manual. The procedures will focus on aircraft recovery after passengers have been evacuated from the aircraft.
18.2
Verification Flight Requirements A Verification Flight is compulsoryfor the following: .1 .2 .3 .4
After an engine in-flight shut-down (IFSD) on a previous flight; After replacement of an engine; or After any major maintenance work on the aircraft, such as Zonal / Heavy Maintenance Visit (HMV). If corrective maintenance action cannot be positively verified.
An ETOPS Verification Flight Form (Form No: SIA/MPS/012) shown on the next page has been introduced to ensure that a verification flight is duly conducted and annotated in the Technical Log. This form is kept in the Aircraft Documentation File onboard every A330 aircraft. A verification flight shall be conducted successfully before the aircraft is released for ETOPS operations.
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18.3
01 January 2009
ETOPS Verification Flight Form (Form No: SIA/MPS/012) Note: To refer to latest issue
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01 January 2009
ETOPS TRAINING PROGRAM The ETOPS Training Program is included in the normal maintenance training program. The goal of the ETOPS Training Program is to ensure that all personnel involved in ETOPS are provided with the necessary training to emphasise the special nature of ETOPS maintenance requirements and to assure that ETOPS programs are properly accomplished. Human factors training is also covered in the normal maintenance program as well as the recurrent training.
19.1
ETOPS Qualified Maintenance Personnel ETOPS training is covered in all "ETOPS-capable" aircraft type courses conducted by SIAEC Engineering Training Department (ETD). All ETOPS training materials are jointly reviewed by ETD and SIA Quality to ensure applicability and appropriateness. Training records of ETOPS qualified maintenance personnel are kept by SIAEC training department for a minimum period of 7 years and all ETOPS personnel are required to undergo a recurring training every 2 years. There is no additional need for a separate ETOPS Training Program to specifically qualify maintenance personnel for certification of ETOPS maintenance tasks. Other airlines' and contracted technical handling agents’ maintenance personnel trained on the A330 aircraft, and whose training includes SIA aircraft differences and ETOPS training will be eligible for qualification. Additional briefings will be conducted for those who have no experience despatching A330 aircraft on ETOPS routes. This is to ensure that they are aware of the special nature of ETOPS.
19.2
A330 Type Courses The following courses conducted by SIAEC Engineering Training Department are approved by CAAS, and have ETOPS training incorporated in thesyllabus:
19.3
.1
A340/A330 / RR Trent 772B-60, Airframe and Engine Conversion
.2
A340/A330 Electrical and Instrument Conversion
.3
A330 Radio
ETOPS Awareness Training Non-authorisation holders including Technical Services Engineers, Quality Engineers, Planning Engineers fromtraining SIAEDconducted and SIAECby who deal Engineering with ETOPS issues/matters are to undergo familiarization SIAEC Training Department. Regular ETOPS updates on latest ETOPS developments are available in he t Quality Department website.
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20
01 January 2009
ETOPS AUDIT PROGRAM The purpose of the ETOPS Audit Program is to verify that ETOPS maintenance requirements and practices are being adhered to. ETOPS audits are conducted e r gularly by the TSP (Total Services Programme) group personnel. SIA Quality Department will maintain oversight over these activities. The scope of the ETOPS audit may includes: .1 Minimum Equipment List .2 ETOPS parts control .3 ETOPS Critical/Significantsystems including air-conditioningpacks .4 Identical maintenance on similar systems .5 Oil consumption check .6 Verification of corrective maintenance action .7 Verification flight .8 Fuel/Oil system maintenance .9 Engine maintenance During the audit, interviews are also conducted with the maintenance personnel involved to ensure that they are aware ofthe ETOPS maintenance requirements.
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n ts d E e PL date C irem M S A e U p a ft IP e q u T N ot B ircr rts R ~ E A a M N ~ P l o U il r t of C w AIRBUS DO tent refe tion n e a Appendix I Co l e a s fo r m P In A330 ETOPS PARTS orrect C r
LIST
This issue of ETOPS PARTS LIST corresponds to A330 CMP Document Revision 18 dated 16 Feb. 2007 (Applicable to all A330 models) - CMP Data Reference: "LR2/EASA : AMC 20-6/CMP" -
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n ts d E e PL date C irem M A U p t IP e q u 1. Purpose: S e raf R T N t B ircusage To identify Epartsowhose on ETOPS aircraft and to further categorize them into rts is restricted a M N those authorized and Anot P authorized on an aircraft dispatched for ETOPS operation. l o C U t w i l fe r t o f O n 2. DContents: ten se re atio n a listformcorresponds to Airbus A330 ETOPS Configuration, Maintenance and Procedures The Coparts Document Ple I(CMP), n CMP Data Reference: “LR2/EASA : AMC 20-6/CMP”, and a revision number, for A330 aircraft. The list relates the CMP item name, its associated modification number and service bulletin (SB) ct number, Airbus and/or vendor, to a parts listing which may or may not be used on an orreflying aircraft ETOPS. It also traces the history of each part group, through use of pre- and postC numbers. The part's list reference number, issue date and corresponding CMP reference r ofmodification are marked on each page. 3. Method used to create the parts list: The parts list is created after the referenced CMP is issued. The modification number and/or service bulletin number is used as the starting point to identify the old andthe new part numbers. Once identified, a part number search is performed using Airbus parts data base, the service bulletin and the modification dossier, to establish the part's family tree. The parts are then classified NOT APPROVED FOR ETOPS or MINIMUM STANDARD APPROVED FOR ETOPS. Those parts NOT APPROVED are all those which are the pre-modification standard or earlier. The parts APPROVED are all those which are the post modification standard or more advanced. An item which is the direct responsibility of a vendor (noted VIPC) or the engine manufacturer may not be listed or if it is listed, may not have a complete family tree due to the unavailability of the information at Airbus. Only part numbers of major components are identified. Support items for this component, i.e. brackets, washers, nuts, etc., are not listed. If an entire configuration was changed a major component in the system change is identified. If no major component exists, no part numbers are identified and the user must assure that the correct page in the IPC (noted by the major modification number) is used. 4. Cautions (list short falls): The family trees identified are as complete as possible and may give part numbers, especially in the not approved listing, which are obsolete. On the other hand, the list may not state all of theapproved ETOPS parts due to an evolution in the product's standard. It is up to each user to customize this list to its operation by using its customized IPC. This list also does not contain compatibility requirements. For instance, if a certain computer invalidates the usage of another computer, the second computer is not listed. It is up to the individual user to make this liaison using IPC codes. Part numbers authorized via accomplishment of a service bulletin, but not available as a spare, may not appear on this list. As long as it can be shown that the component is post-modification standard, the part is authorized; vice-versa, a pre-modification standard is not approved. This list does not identify all amendment numbers or other similar markings which differentiates the application of lower level SBs. This information is identified if it is available and if it is needed to differentiate between an ETOPS and non-ETOPS configuration. If no note is mentioned and a second level of identifications exists, all parts within the parent numerical value are effected. This list does not track changes to higher assembly part numbers.
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n ts d E e PL date C irem M SA e Up aft IP equ T 5. Liability Statement: N ot B ircr rts R E A Pato provide an aide in controlling ETOPS configurations. It may not be full This list isMcreated U ll N r by to Airbus fthis list inan ETOPS operation, eachcompany should verify this information proof!CPriorwito adopting oIPC. e O t f against its customized corrections and/or comments to improve the contents of this list n D n re tioto Airbus'Any shouldtebe provided ETOPS department. a e n Co leas form P In 6. Users Guide By Column: orrect 6.1CColumn 1 - AI Mod No.: fo r *Component/configuration name:
states the name of the component or configuration effected; name close to or identical to that in the CMP
* mod numbers: modification numbers that are called out in the CMP * CMP Eff: :
states which aircraft models have this item in their CMP. Note that this item may not be in a CMP, but may be basic to the aircraft, by default validating the usage of parts in the approved for ETOPS column.
* or: choice of one of the modifications * and: both modifications mustbe embodied * ------AND : the modification(s) above and belowdotted lines must beincorporated ------* ------OR : the modification(s) above or belowdotted lines must beincorporated ------* ( xxxxx ) : extra information to define scope of modification effectivity
* Note - "**The configuration(s) prior to this standard is (are) not flagged ("Not approved for ETOPS ") in the IPC.**":Signals that an entire configuration and not a component was effected and that once the IPC contains ETOPS notes the modification numbers will not be identified as ETOPS or non-ETOPS.
6.2 Column 2 - AI or vendor SB: * Mod xxxxx: relates to the modification number to the service bulletin number * A330-xx-xxxx: Airbus Service Bulletin number. Same SB numberappears in the CMP. * vendor name and SB number: listed when available * or: choice of one of the modifications
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n ts d E e PL date C irem M * and: both modifications A Up must IPbeeembodied qu S t f e a T R B r EN Not Airc arts * ------M ANDU : the to of P above and belowdotted lines must beincorporated ill modification(s) C ------r w e DO tent ref tion * ------se modification(s) on e:athe ma above or below dotted lines must be incorporated OR C------lP nfor I * ( xxxxx rrect) : extra information to define scope of modification effectivity o C non-priority, * (... fonor later than DD MM YY): states that all SBs and or modifications listed above this message must be incorporated on ETOPS aircraft by the day (DD) month (MM) year (YY) given. Until that time, the aircraft can fly ETOPS without this item being embodied. If more than one note like this appears, all text above the first set of parentheses is concerned and all text after the first set of parentheses and above the second set of parentheses is governed by the note in the second parentheses. * ------Superseded by : -------
mods/SBs above the top dotted line are superseded by the mods/SBs below the bottom dotted line
6.3 Column 3 - P/Ns NOT ETOPS Approved: *
Lists all part numbers of that referenced component/equipment which are not allowed to be used on aircraft flying ETOPS.
* Pre-mod xxxxx / Pre-SB xx-xxxx:
provides a reference to part numbers which were introduced prior to the ETOPS mod or SB, Mod xxxxx / SB xx-xxxx.
.Part numbers listed directly underneath this heading:The part numbers listed directly underneath this pre-mod or pre-SB heading are the part numbers which have been invalidated for use on ETOPS aircraft due to the fact that Mod xxxxx becomes the minimum configuration standard. Caution : Higher assemblies part numbers are not listed. * (mod xxxxx): appears after a part number listed underneath the heading "more advanced standards" and identifies the modification number which introduces this part. * Equipment / component name:
this is the equipment or component which is effected. If more than one component's name is listed underneath a modification number or SB number, then all components are effected by this mod orSB. If the modification number orSB number is situated underneath the component or equipment name, then the mod or SB only effects this immediate equipment.
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n ts d E e PL date C irem M Up ft IPhasequ This phrase appears when an entire configuration has * Phrase "If the a/c SA inequestion T mod xxxxx, then IPC been changed and there is no individual equipment or N ot Bareipages cra not sR r reflecting E this mod not rt component effected. The only identification feature is A a M N authorized the design feature itself which is controlled by a modification U for to o f P ill use.": C standard. r w e nt ref tion DO teDD the date which all of the part numbers (entire column) above this date * (after a Signals eMM mYY): n s o are not allowed to be used on ETOPS aircraft. Until that time, these part a r C le fo numbers can be installed on ETOPS aircraft. If more than one note like this P In appears, all text above the first set of parentheses is concerned and all text after the first set of parentheses and above the second set of parentheses is ro rect governed by the note in the second parentheses. If this note does not appear C in a column, that means the item is priority for ETOPS and all part numbers in r the column cannot be mounted on an aircraft flying an ETOPS route. fo * -------: separates equipment or modification part numbers * (VIPC):
indicates that this part number is found in the vendor IPC and is not a part sold by Airbus. The part's family tree may be incomplete due to limited information available. The respective vendor should be contacted in case of questions.
* See ( Engine manufacturer's name) IPC:
indicates that the referenced engine manufacturer is responsible for this part and that it is found in its documentation. The part's family tree should be obtained from the engine manufacturer, if not given.
* ------OR : -------
the part number(s) above the dotted line apply to one configuration and the part number(s) below the dotted line apply to another configuration. The configuration is mentioned inbold at the top each part number group.
6.4 Column 4 - MINIMUM STANDARD P/N ETOPS APPROVED: *
Lists the part number of that referenced component/equipment which is the minimum standard allowed to be used on aircraft flying ETOPS. More advanced standards and the allowed interchangeability are listed in t he IPC.
* Mod xxxxx / SB xx-xxxx:
relates to the modification number or to the service bulletin number which caused the part number to be changed.
.Part numbers listed directly underneath this heading: The part number(s) listed directly underneath this mod number or SB number is (are) the part number(s) introduced by the mentioned change. Caution, : Higher assembly part numbers are not listed. * more advanced standards: part numbers introduced after the minimum ETOPS standard and allowed for used on ETOPS aircraft are found in the IPC; hence the note consult the IPC.
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n ts d E e PL date C irem M qu * Phrase "P/Ns shown SA e Uonp IPC t IPpages e f a T R reflecting mod xxxxx This phrase appears when an entire configuration has been r B standard": EN Not Airc arts changed and there is no individual equipment or component M effected. The only identification feature is the design feature P l o U l t i f C itself which is controlled by a modification standard. r o w e O nt ef on D i r * Equipment name: this is the equipment or component whichis effected. If more than at nte ase / component o m one component's name is listed underneath a modification r C le fo number or SB number, then all components are effected by P In this mod or SB. If the modification number or SBnumber is situated underneath the component or equipment name, ro rect then the mod or SB only effects this immediate equipment. C r fo* -------: separates equipment ormodification part numbers * (VIPC):
indicates that this part number is found in the vendor IPC and is not a part sold by Airbus. The part's family tree may be incomplete due to limited information available. The respective vendor should be contacted in case of questions.
* See (Engine manufacturer's name) IPC:
* ------OR -------
:
indicates that the referenced engine manufacturer is responsible for this part and that it is found in its documentation. The part's family tree should be obtained from the engine manufacturer, if not given.
the part number(s) above the dotted line apply to one configuration and the part number(s) below the dotted line apply to another configuration. The configuration is mentioned inbold at the top each part number group.
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fo
n ts d E e PL date C irem M IP equ ETOPS AIRCRAFT MODELS UpOFft APPROVED SA LIST e a T (EASA) N ot B ircr rts R E A a M N U ill r to of P C w DO tent refe tion n e a Co leas form Series Engine A330 Model P In A330-301 rrect o GE A330-302 rC A330-303 A330-321 A330-300
PW
A330-322 A330-323 A330-341
RR
A330-342 A330-343 A330-201
GE
A330-202 A330-203
PW
A330-223
RR
A330-243
A330-200
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n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 21 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to AIof orPaVendor SB C Approved w e DO tent ref tion n as e m a Pack r Co lController Mod 42309: Pre-mod 42309: P e In fo none 977A0000-03 977A0000-02 ro rect 977A0000-01 C 42309 r fo NOT
MINIMUM
STANDARD P/N ETOPS APPROVED
Mod 42309:
CMP Eff:-301,-321,-322 -341,-342 CMP Item: 21-1-0000-001
977A0000-04 more advanced stds: 977A0000-05 Consult IPC
Packs and Temperature Sensors CMP Eff:-301,-321,-322 - 341,-342 CMP Item: 21-1-0000-002
42628 and 42629
Mod 42628: A330-21-3010 / Liebherr SBs 956A-21-01 Mod 42629 : A330-21-3010/ Liebherr SB 9105A-21-1
Pre-mod 42628: 956A0000-02 956A0000-01 Pre-mod 42629 : 9105A0001-01
Mod 42628: 956A0000-03 more advanced stds: Consult IPC Mod 42629 : 9105A0005-01 more advanced standards : Consult IPC
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
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n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 22 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to AIof orPaVendor SB C Approved w e DO tent ref tion n se ma Standard L-5 FMGEC r Co leaFM Mod 42792: Pre-mod 42792: P In fo A330-22-3002/ B490BAM0103 Sextant r e c t r Avionique SB 42792 Co B490BAM-22-001 of r_____ _____ _____ NOT
MINIMUM
STANDARD P/N ETOPS APPROVED
Mod 43724:
CMP Eff: -301
B490BAM0106
CMP Item: 22-1-0000-001
AND
43724 CMP Item: 22-1-0000-003
FMGEC FM
more advanced stds: B490BAM0307 (Mod 45328)
AND Standard L-6 B3 Mod 43724: A330-22-3011
Pre-mod 43724: B490BAM0105
Standard L-5 Mod 42931: none
Pre-mod 42931: B490CAM0101 B490DAM0101
_____ AND Standard L-6 C3 Mod 44661: A330-22-3009
_____
more advanced stds: B490CAM0305
Pre-mod 44661: B490CAM0102 B490CAM0103
(Mod 45239)
Pre-mod 41815: N/A
Mod 44662: B490DAM0104
_____
more advanced stds: Consult IPC
Mod 44661: B490CAM0104
CMP Eff: -321, -322 CMP Item: 22-1-0000-002
42931 _____ AND 44661 CMP Item: 22-1-0000-003
FMGEC FM
Standard L-5 Mod 41815: none
CMP Eff : -341,-342 CMP Item: 22-1-0000-002
41815 _____ AND 44662
_____ AND Standard L-6 D3 Mod 44662: A330-22-3010
Pre-mod 44662: B490DAM0101 B490DAM0102
CMP Item: 22-1-0000-003
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 24 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion on ease Services Additional ma r C o l Configuration preon CSMG Power Mod 41462: P In f SB A330-24-3018 mods and are prohibited. 4278341462 ro rect and Use of IPCs not C showing this configuration is Mod 42783: for41462 NOT
CMP Eff: -301,-321,-322 -341,-342 CMP Item: 24-1-0000-001
and 42783
SB A330-24-3004
prohibited.
Mod 40121: none
Configuration premods 40121 are prohibited. Use of IPCs not showing this
MINIMUM
STANDARD P/N ETOPS APPROVED
P/Ns shown on IPC pages reflecting P/Ns mod 41462 standard. shown on IPC pages reflecting mod 42783 standard.
** The configuration(s) prior to this standard is (are) not flagged ("Not approved for ETOPS") in the IPC.**
Electrical Feeder Gauge in Engine Pylons CMP Eff: -301 CMP Item: 24-1-0000-002
P/Ns shown on IPC pages reflecting mod 40121 standard.
configuration prohibited. is
40121 Electrical Feeder Gauge in Engine Pylons
Mod 40209: none
CMP Eff: -321,-322 CMP Item: 24-1-0000-002
40209 Electrical Feeder Gauge in Engine Pylons
Mod 40210: none
CMP Eff: -341,-342 CMP Item: 24-1-0000-002
Configuration premods 40209 are prohibited. Use of IPCs not showing this configuration is prohibited.
P/Ns shown on IPC pages reflecting mod 40209 standard.
Configuration premods 40210 are prohibited. Use of IPCs not showing this
P/Ns shown on IPC pages reflecting mod 40210 standard.
configuration is prohibited.
40210
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 24 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion n as e m a APU r Co Gen Ple Info Mod 42952: Pre-mod A330-24-3005/ 5909129 42952: ro rect Sundstrand 5909012 C 42952 Aerospace 5908508 r SB 90EGS07AG-24-1 fo NOT
MINIMUM
STANDARD P/N ETOPS APPROVED
CMP Eff: -301,-321,-322 -341,-342 CMP Item: 24-1-0000-003
Mod 42952: 5910139 more advanced stds: Consult IPC
GCU of CSM/G CMP Eff: -301,-321,-322 -341,-342 CMP Item: 24-1-0000-004
42957
Mod 42957: A330-24-3006/ Vickers SB 920395-24-01
Pre-mod 42957: 920395
Mod 42957: 928005
Mod 43286:
Pre-mod 43286:
Mod 43286:
752168
752168A
more advanced stds: Consult IPC
IDG CMP Eff: -301 CMP Item: 24-1-0000-005
43286
A330-24-3008/ Sundstrand SB 115EGS01I-24-1
more advanced stds: Consult IPC
IDG Mod 43285: CMP Eff: -321, -322 CMP Item: 24-1-0000-005
43285
A330-24-3008/ Sundstrand SB 115EGS01I-24-1
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
Pre-mod 43285: 755017
Mod 43285: 755017A more advanced stds: Consult IPC
This issue corresponds to AI/EA5000 Rev 18
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 26 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of Pa AI or vendor SB C Approved w e DO tent ref tion e maFire onmineasCargo 160 r C l Extinguishing Pre-mod BASIC: P Info System Mod BASIC: (Bottles)-Walter Kiddie none not applicable ro rect C fo r NOT
CMP Eff: -301, -321,-322 -341,-342,-323,-343
MINIMUM
STANDARD P/N ETOPS APPROVED
Mod BASIC: Bottle 1: 472931-2 (2140 cu. inch bottle)
BASIC
!! Configuration acceptable for ETOPS operations not exceeding 145 min diversion time !!
Bottle 2: 472930-2 (800 cu. inch bottle) 472930-1 (800 cu. inch bottle) (minimum standard P/N for bottle 2, ETOPS approved for diversion time up to 145 mins)
more advanced stds: 285 min Cargo Fire Extinguishing System (Bottles)-Walter Kiddie CMP Eff: -301, -302, -303, -321,-322, -323, -341, -342, -343 -201, -202, -203, -223, -243
Consult IPC Mod 40314 or Mod 45435 (for A330-200)
Pre-mod 40314: Or Pre-mod 45435 (for A330-200):
Mod 40314: or Mod 45435 (for A330200)
none
Bottle 1: none
Bottle 1: 472931-2 (2140 cu. inch
40314 or 45435 (for A330-200)
bottle)
* Option to 40487*
Bottle 2 :
!! Modification mandatory if operating 180 min ETOPS; Configuration acceptable for ETOPS
472930-2 (800 cu. inch bottle) 472930-1 (800 cu. inch bottle)
operations not exceeding 270min diversion time !!
diversion time > 145 mins)
Bottle 2: 472625-1 (1600 cu. inch bottle)
(NOT ETOPS approved for
more advanced stds: Consult IPC
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 26 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of Pa AI or vendor SB C Approved w e DO tent ref tion se rma on eFire Cargo Mod 42451: Pre-mod 42451: a C l Extinguisher F2627007000400 P Info Discharge A330-26-3002 Flexible Hose F2627007000200 Assembly ro rect C fo r NOT
CMP Eff: -301,-321,-322 -341,-342 CMP Item: 26-1-0000-001
MINIMUM
STANDARD P/N ETOPS APPROVED
Mod 42451: F2627007200200 F2627007200000 more advanced stds: Consult IPC
42451 SDCU (Smoke Detection Control Unit) CMP Eff: -301,-321,-322 -341,-342 CMP Item: 26-1-0000-002
Mod 42148: A330-26-3003/ Sextant Avionique SB RAI 2810-26-001
Pre-mod 42148: RAI2810M0202 RAI2810M0101
Mod 40487
Pre-mod 40487:
Mod 40487 (and Mod
(and Mod 45435 for A330-200 only):
(and Pre-mod 45435 for A330-200 only):
45435 for A330-200 only):
none
none; new standard
Bottle 1: 34900008-1
Mod 42148: RAI2810M0303 more advanced stds: Consult IPC
42148 285 min HTL Fire Extinguishing System (Bottles) CMP Eff: -301, -302, -303, -321,-322,341,-342, -201, -202, -203,-223,-243, 323, -343
40487 (and 45435 for A330-200 only) * Option to 40314* !! Modification mandatory if operating 180 min ETOPS; Configuration acceptable for ETOPS operations not exceeding 270 min diversion time !!
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
(2170 cu. inch bottle)
Bottle 2: 35200003-1 (1600 cu. inch bottle)
more advanced stds: Consult IPC
This issue corresponds to AI/EA5000 Rev 18
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 27 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PAIa or vendor SB C Approved w e DO tent ref tion on ease (Pedal, PTLU/RTLU ma r C o l Rudder Travel Mod 42707: P In f Limitation Unit) A330-27-3010/ Pre-mod 42707: Sarma SB 341400M01 ro rect 341400-27-001 341400M00 C fo r NOT
MINIMUM
STANDARD P/N ETOPS APPROVED
Mod 42707: 341400M02
CMP Eff: -301,-321,-322 -341,-342 CMP Item: 27-1-0000-001
42707 FCSC2 (Provide second electrical power supply)
Mod 44047: A330-27-3039
CMP Eff: -301,-321,-322 -341,-342 CMP Item: 27-1-0000-002
44047
more advanced stds: Consult IPC
If the a/c in question has mod 44047, then IPC pages not reflecting this mod are not authorized for use.
P/Ns shown on IPC pages reflecting mod 44047 standard.
Pre-mod 44441: B492AAM0405 B492AAM0406 B492AAM0407 B492AAM0304
Mod 44441: B492AAM0408
**The configuration(s) prior to this standard is (are) not flagged ("Not approved for ETOPS") in the IPC.** FCSC M10 Standard CMP Eff: -301,-321,-322 -341,-342 CMP Item: 27-1-0000-003
Mod 44441: A330-27-3041
44441
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
more advanced stds: Consult IPC
This issue corresponds to AI/EA5000 Rev 18
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 28 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion se rma onAireaSeparator Fuel Drain Valve : C o l and Drain Valve Mod 42890: f P In A330-28-3014 Pre-mod 42890: none - new part ro rect introduced via mod C 42890 fo r NOT
CMP Eff: -301,-321,-322 -341,-342 CMP Item: 28-1-0000-001
42890
Air Separator : Pre-mod 42890: F2827001100600 F2827001100000
MINIMUM
STANDARD P/N ETOPS APPROVED
Drain Valve : Mod 42890: 4127360 more advanced stds: Consult IPC Air Separator : Mod 42890: F2827001101000 more advanced stds: Consult IPC
Fuel Air Separator Drainage and Access Hatch CMP Eff: -301,-321,-322 -341,-342 CMP Item: 28-1-0000-002
Mod 42921 Or Mod 43169 A330-53-3016
Access Hatch:
Access Hatch:
If the a/c in question has mod 42921 or 43169, then IPC pages not reflecting this mod are not authorized for use.
P/Ns shown on IPC pages reflecting mod 42921 or 43169 standards.
42921 or 43169 **The configuration(s) prior to this standard is (are) not fl agged ("Not approved for ETOPS") in the IPC.**
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
28.1
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 28 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion seTransfer on Tank Fuel ma a r C e o l If the a/c in question Valves Electrical Mod 42636: P In f Wiring to CSM/G A330-28-3011 has mod 42636 IPC pages not , then Power ro rect reflecting this mod are C not authorized for use. fo r NOT
MINIMUM
STANDARD P/N ETOPS APPROVED
P/Ns shown on IPC pages standard. mod 42636 reflecting
CMP Eff: -301,-321,-322 -341,-342 CMP Item: 28-1-0000-003
42636 **The configuration(s) prior to this standard is (are) not flagged ("Not approved for ETOPS") in the IPC.**
Inner Wing Tank Refuel Pipe Restrictor
Mod 41871: none
CMP Eff: -301,-321,-322 -341,-342
If the a/c in question has mod 41871, then IPC pages not
P/Ns shown on IPC pages reflecting mod 41871 standard.
reflecting this mod are not authorized for use.
CMP Item: 28-1-0000-004
41871 Collector Cell Water Scavenge System
Mod 42708: A330-28-3009
CMP Eff: -301,-321,-322 -341,-342 CMP Item: 28-1-0000-005
If the a/c in question has mod 42708, then IPC pages not reflecting this mod are not authorized for use.
P/Ns shown on IPC pages reflecting mod 42708 standard.
42708 **The configuration(s) prior to this standard is (are) not flagged ("Not approved for ETOPS") in the IPC.**
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
28.2
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 28 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion se Tank on Inner Wing Wiring: ma a r C e o l Wiring Mod 42014: f P In A330-28-3003 Pre-mod If the a/c in42014: question ro rect has mod 42014, then C IPC pages not reflecting this mod are for42014 NOT
CMP Eff: -301,-321,-322 -341,-342 CMP Item: 28-1-0000-006
MINIMUM
STANDARD P/N ETOPS APPROVED
Wiring: Mod P/Ns 42014: shown on IPC pages reflecting mod 42014 standard.
not authorized for use.
Wing Inner Tank FQI Harnesses
Mods 42243: A330-28-3003
CMP Eff: -301,-321,-322 -341,-342 CMP Item: 28-1-0000-007
41282 and 42243 Note: Mod 42243 supersedes Mod 41282.
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
Harnesses:
Harnesses:
Pre-mod 42243:
Mod 42243:
103QT: 50150-0312 (Mod 42158) 50150-0212 (Mod 41282) 50150-0112 104QT: 50150-0309 (Mod 41282)
103QT: 50150-0412 104QT: 50150-0409 118QT: 50150-0413
50150-0209 50150-0109 118QT: 50150-0313 50150-0213 50150-0113 119QT: 50150-0214 50150-0114 50150-0111
119QT: 50150-0314 (Mod 42158) (Mod 41282)
more advanced stds (all harnesses): Consult IPC
(Mod 41282)
This issue corresponds to AI/EA5000 Rev 18
28.3
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 28 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion se Tank on Inner Wing Probes: Probes: ma a r C e o l Probes f P In Mod 42242: Pre-mod 42242: A330-28-3003 ro rect 120QT: C 20130-0118 r 121QT: fo42242 NOT
CMP Eff: -301,-321,-322 -341,-342 CMP Item: 28-1-0000-006
none 122QT: none 123QT: none 124QT: none
MINIMUM
STANDARD P/N ETOPS APPROVED
Probes: Mod 42242: 120QT: 20130-0218 121QT: 20130-0111 122QT: 20130-0113 123QT: 20130-0112 124QT: 20130-0113 more advanced stds (all probes): Consult IPC
Fuel Temperature Sensor and Densitometer Relocation
Mods 42278 and 42787: A330-28-3003
CMP Eff: -301,-321,-322 -341,-342 CMP Item: 28-1-0000-08
42278 and 42787
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
Sensor and Densitometer Relocation:
Sensor and Densitometer Relocation:
Pre-mod 42278: If the a/c in question has mod 42278, then IPC pages not reflecting this mod are not authorized for use. ------Harness: Pre-mod 42787: 50150-0506 50150-0406 50150-0306 50150-0206 50150-0106
Mod 42278: P/Ns shown on IPC pages reflecting mod 42278 standard.
------Harness: Mod 42787: 50150-0606 more advanced stds: Consult IPC
This issue corresponds to AI/EA5000 Rev 18
28.4
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 28 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion se Control on e(Fuel FCMC Stage 7.1 Pre-mod 44575: ma a r C o l B494AAM0611 and Monitoring Mod 44575: f P In Computer) A330-28-3037 B494AAM0610 B494AAM0609 ro rect B494AAM0608 C B494AAM0507 r B494AAM0506 fo44575 NOT
CMP Eff: -301,-321,-322 -341,-342
CMP Item: 28-1-0000-016
B494AAM0405 B494AAM0404 B494AAM0303 B494AAM0202 B494AAM0101
(compliance with CMP item 28-1-0000-020 i.e. incorporation of FCMC STD-9) (MOD 47930) supersedes the requirement of CMP item 28-1-0000-016)
MINIMUM
STANDARD P/N ETOPS APPROVED
MOD 47930 B494AAM0614 B494AAM0615 further advanced standards: Consult IPC
Mod 44575: B494AAM0612 (see CMP item 28-10000-20) (NOT ETOPS approved after 31/12/2006)
more advanced stds:B494AAM0613 (see CMP item 28-10000-20) (NOT ETOPS approved after 31/12/2006)
Outer Tank Inlet Valve CMP Eff :
-301,-321,-322 -341,-342 CMP Item: 28-1-0000-011
Mod 43035 : A330-28-3016 or Mod 43122 : A330-28-3017
43035 or 43122
Pre-mods 43035 and 43122 :
Mod 43035 : B97H63-602
B97H38-602 B97H38-601
Mod 43122 : B97H38-603 more advanced stds : Consult IPC
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
28.5
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 28 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion se rFault on System Fuel Mod 43227: Pre-mod 43227: ma a C e o l A330-33-3005 If the a/c in question Indication f P In has mod 43227 IPC pages not , then ro rect reflecting this mod are C not authorized for use. fo r NOT
CMP Eff: -301,-321,-322, -341,-342 CMP Item: 28-1-0000-013
43227
MINIMUM
STANDARD P/N ETOPS APPROVED
Mod 43227: P/Ns shown on IPC pages 43227 reflecting standard mod more advanced stds: Consult IPC
** The configuration(s) prior to this standard is (are) not flagged ("Not Approved for ETOPS") in the IPC**
Larger Mesh-Aft Fuel Pump Grills
Mods 43115 and 43117: A330-28-3020
CMP Eff : -301,-321,-322 -341,-342 CMP Item: 28-1-0000-012
43115 and 43117
Automatic Pre-Flight Check of APU Aft Pump
Mod 43689: A330-28-3026
CMP Eff : -301,-321,-322 -341,-342 CMP Item: 28-1-0000-014
Pre-mods 43115 and 43117 : If the a/c in question has mod 43115 and mod 43117, then IPC
Mods 43115 and 43117 : P/Ns shown on IPC pages reflecting mod 43115 and mod 43117
pages not reflecting these mods are not authorized for use
standard
Pre-mod 43689: If the a/c in question has mod 43689, then IPC pages not reflecting this mod is not authorized for use
Mod 43689: P/Ns shown on IPC pages reflecting mod 43689 standard
more advanced stds: Consult IPC
more advanced stds: Consult IPC
43689
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
28.6
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 28 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion a e mfuel on easAPU Modified Mod 44603: r C o l A330-28-3041 If the a/c in question Pump electrical f P In supply has mod 44603 IPC pages not , then ro rect reflecting this mod are C not authorized for use. fo r NOT
MINIMUM
STANDARD P/N ETOPS APPROVED
P/Ns shown on IPC pages standard. mod 44603 reflecting
CMP Eff : -301,-321,-322 -341,-342 CMP Item: 28-1-0000-015
44603 New APU Aft Pump
Mod 44725: A330-28-3040
CMP Eff : -301,-321,-322 -341,-342 CMP Item: 28-1-0000-017
Pre-mods 44725 : P93A19-202
Mod 44725 : P93A19-203 more advanced stds : Consult IPC
44725 Add latching device and time delay circuit
Mod 45049: A330-28-3048
in fuel trim transfer system. CMP Eff : -301,-321,-322 -341,-342 CMP Item: 28-1-0000-018
If the a/c in question
P/Ns shown on IPC
has mod 45049, then IPC pages not reflecting this mod is not authorized for use
pages reflecting mod 45049 standard more advanced stds: Consult IPC
45049
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
28.7
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 28 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion e maof on easwiring Modified Mod 46825: Pre-mod 46825: r C o l A330-28-3062 trim tank transfer f P In system none ro rect C fo r NOT
CMP Eff : -201, -202,-203,-223,-243 CMP Item: 28-1-0000-019
MINIMUM
STANDARD P/N ETOPS APPROVED
Mod 46825: Relay time delay: E0217XXU006A Relay 4-pole: E0671D28A0
---OR ----
46825 ---OR ----
FCMC (Fuel Control and Monitoring Computer)
Mod 47930: A330-28-3067 / Sextant SB B494AAM-28-015
CMP Eff : -201, -202,-203,-223,-243
Pre-mod 47930: B494AAM0613 B494AAM0612 (NOT ETOPS approved after 31/12/2006)
CMP Item: 28-1-0000-19 (refer also to CMP item 28-1-0000-020)
47930 Note: compliance with CMP item 28-1-0000-20 entails compliance with CMP item 28-1-0000-19
Mod 47930: B494AAM0614 B494AAM0615 more advanced stds: Consult IPC
B494AAM0611 B494AAM0610 B494AAM0609 B494AAM0608 B494AAM0507 B494AAM0506 B494AAM0405 B494AAM0404 B494AAM0303 B494AAM0202 B494AAM0101 (Not ETOPS approved)
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
28.8
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 28 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion se rma on FU/FOB “Fuel Mod 49800: Pre-mod 49800: a C e o l A330-28-3080 discrepancy” crew f P In alert _____ orrect C AND r fo NOT
no dedicated P/N information neither for FCMC without FU/FOB discrepancy alert, nor for FCMC P/N with PIN programming for alert deactivation (Mod 49801)
CMP Eff : All
CMP Item : 28-1-0000-020
49800
MINIMUM
STANDARD P/N ETOPS APPROVED
Mod 49800: no dedicated P/N information: FCMC P/N is not changed by PIN programming for activation of FU/FOB discrepancy alert
FWC:
_____ AND
FWC:
FWC (Flight Warning Computer) 47420
Mod 47420: A330-31-3042 / Aerospatiale SB LA2E0-31-016 or Mod 49193
or 49193 (incorporation of FWC std K5 or above supersedes the requirement of CMP item 31-1-0000-001)
_____ AND
FWC:
Pre-mod 47420: LA2E0060AK40000 LA2E0060A3K0000 LA2E0060AK30000 LA2E006091K0000 LA2E00609K10000 LA2E00609920000 LA2E00609910000 LA2E00609620000 LA2E00609610000 LA2E00609330000
FCMC (Fuel Control and Monitoring Computer) Std 14 47930 (incorporation of FCMC std –14 supersedes the requirements of CMP items 28-1-0000-010, 28-1-0000016 and 28-1-0000-19)
FCMC: Mod 47930: A330-28-3067 / SEXTANT SB B494AAM-28-015
more advanced stds: LA2E0060BK60000 LA2E20101K70000 standard K8: P/N’s LA2E20101K800000 & LA2E0060BK800000
LA2E00607320000 (NOT ETOPS approved after 31/12/2006)
LA2E00607310000
_____ AND
Mod 47420: LA2E0060BK50000
FCMC: Pre-mod 47930: B494AAM0613 B494AAM0612 (NOT ETOPS approved after 31/12/2006)
further advanced standards: Consult IPC FCMC: Mod 47930: B494AAM0614 B494AAM0615 more advanced stds: Consult IPC
B494AAM0611 B494AAM0610 B494AAM0609 B494AAM0608 B494AAM0507 B494AAM0506 B494AAM0405 B494AAM0404 B494AAM0303 B494AAM0202 B494AAM0101
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
28.9
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 29 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PAIa or vendor SB C Approved w e DO tent ref tion a se rmPlugs on Locked Wire a C Mod 42036: Pre-mod 42036: e o l on Manifolds P In f A330-29-3003 AN814-10D AN814-10 AN814-12D ro rect AN814-12 C AN814-16D of r42036 NOT
CMP Eff: -301,-321,-322 -341,-342,-202 CMP Item: 29-1-0000-001
Note: SB applicable only for A330 MSNs 030 and 037. All other A330's have MSN 42036 as part of their basic delivery configuration.
** The part numbers herewith are not flagged in the IPC due to their use in more than one location on the a/c.** EDP
Mod 43458: A330-29-3009
CMP Eff: -301,-321, -322,-202,-203 CMP Item: 29-1-0000-003
AN814-16 AN814-6
MINIMUM
STANDARD P/N ETOPS APPROVED
Mod 42036: AN814-10DL AN814-10L AN814-12DL AN814-12L AN814-16DL AN814-16L AN814-6L AN814-8L
**Consult SB for effected areas. **
**Consult SB for effected areas. **
Pre-mod 43458: 848354 848194 518547
Mod 43458: 971844
43458
More advanced Stds: 972630 (Mod 44176)
Consult IPC for further stds Modified Hose in Yellow Hydraulic Circuit
Mod 43696: A330-29-3013
CMP Eff:
-301,-321, -322, -341, 342,-202,-203 CMP Item: 29-1-0000-004
Pre-mod 43696: F0003160007900
Mod 43696: F0003160010700 more advanced stds: Consult IPC
43696
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 29 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PAIa or vendor SB C Approved w e DO tent ref tion on ease ofrma Installation If the a/c in question Mod 43547: C o damper A330-29-3071/ has the concerned Pl toInfreduce hydraulic engine SB PW4G-100-A72modification proposal, hose pressure pulse. 125 addressed by mod ro rect 43547, then IPC C pages not reflecting r this MP are not fo NOT
CMP Eff: -321, -322, -223, -323 CMP Item: 72-1-0204-007
MINIMUM
STANDARD P/N ETOPS APPROVED
P/Ns shown on IPC pages reflecting the concerned modification proposal, which is addressed by mod 43547 standard.
authorized for use.
43547
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 30 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion e ma on easCircuitry: Modified r C l If the a/c in question Wing Anti-Icing Mod 42288: P In fo Operation A330-30-3003 has mod 42288 IPC pages not , then ro rect reflecting this mod are C not authorized for use. fo r NOT
MINIMUM
STANDARD P/N ETOPS APPROVED
P/Ns shown on IPC pages standard. mod 42288 reflecting
CMP Eff:-301,-321,-322 -341,-342 CMP Item: 30-1-0000-001
42288 **The configuration(s) prior to this standard is (are) not fl agged ("Not approved for ETOPS") in the IPC.**
Wing Anti-ice Valve CMP Eff:-301,-321,-322 -341,-342 CMP Item: 30-1-0000-002
Mod 42531: Grimes SB 38E 93-30-01
Pre-mod 42531: 38E93-4 38E93-3 38E93-1
Mod 42531: 38E93-5
more advanced stds: Consult IPC
42531 HYMATIC Valves
(cannot be fitted on A330 at all): HC1750 HC1751 HC1752 HC1756 HC1758 HC1755 HC1757 SAS911-002A SAS912-002A
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 31 e NT ot B ircra rts R E A AI Mod ETOPS UMNo.ill N r to oAIf Pora vendor SB P/Ns C Approved w e DO tent ref tion se rma on (Flight FWC a C e l Warning fo Mod 42673: Pre-mod 42673: P In Computer) A330-31-3005/ LA2E00607310000 Aerospatiale SB ro rect LA2E0-31-003 Mod 42673: C LA2E00607320000 r (M3.2 std) fo42673 NOT
CMP Eff: -301,-202,-203 CMP Item: 31-1-0000-001
(compliance with CMP item 28-1-0000-020 i.e. incorporation of FWC std K5 or above (CMP Eff: all) supersedes the requirement of CMP item 31-1-0000001)
(see CMP item 28-10000-20) (NOT ETOPS approved after 31/12/2006)
more advanced stds: LA2E00609330000 LA2E00609K10000 LA2E006091K0000 LA2E0060AK30000 LA2E0060A3K0000 LA2E0060AK40000 (see CMP item 28-10000-20)
MINIMUM
STANDARD P/N ETOPS APPROVED
std K5 or above LA2E0060BK50000 LA2E0060BK60000 LA2E20101K70000 standard K8: P/N’s LA2E20101K800000 & LA2E0060BK800000
further advanced stds: Consult IPC
(NOT ETOPS approved after 31/12/2006)
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 31 e NT ot B ircra rts R E A AI Mod ETOPS UMNo.ill N r to oAIf Pora vendor SB P/Ns C Approved w e DO tent ref tion se rma on (Flight FWC a C e l Warning fo Mod 42880: Pre-mod 42880: P In Computer) none not applicable ro rect Mod 42880: C LA2E00609610000 r (N3.0 std) fo42880 NOT
CMP Eff: -321,-322
CMP Item: 31-1-0000-002
(compliance with CMP item 28-1-0000-020 i.e. incorporation of FWC std K5 or above (CMP Eff: all) supersedes the requirement of CMP item 31-1-0000002)
(see CMP item 28-10000-20) (NOT ETOPS approved after 31/12/2006)
more advanced stds: LA2E00609620000 LA2E00609K10000 LA2E006091K0000 LA2E0060AK30000 LA2E0060A3K0000 LA2E0060AK40000 (see CMP item 28-10000-20)
MINIMUM
STANDARD P/N ETOPS APPROVED
std K5 or above
LA2E0060BK5000 0 LA2E0060BK60000 LA2E20101K70000 standard K8: P/N’s LA2E20101K800000 & LA2E0060BK800000
further advanced stds: Consult IPC
(NOT ETOPS approved after 31/12/2006)
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 31 e NT ot B ircra rts R E A AI Mod ETOPS UMNo.ill N r to oAIf Pora vendor SB P/Ns C Approved w e DO tent ref tion se rma on (Flight FWC a C e l Warning fo Mod 43578: Pre-mod 43578: P In Computer) none Not applicable ro rect Mod 43578: C LA2E00609920000 r (see CMP item 28-1fo43578 NOT
CMP Eff: -341,-342
CMP Item: 31-1-0000-003
0000-20) (NOT ETOPS approved after 31/12/2006)
(compliance with CMP item 28-1-0000-020 i.e. incorporation of FWC std K5 or above (CMP Eff: all) supersedes the requirement of CMP item 31-1-0000003)
more advanced stds: LA2E00609K10000 LA2E006091K0000 LA2E0060AK30000 LA2E0060A3K0000 LA2E0060AK40000 (see CMP item 28-10000-20)
MINIMUM
STANDARD P/N ETOPS APPROVED
std K5 or above LA2E0060BK50000 LA2E0060BK60000 LA2E20101K70000 standard K8: P/N’s LA2E20101K800000 & LA2E0060BK800000
further advanced stds: Consult IPC
(NOT ETOPS approved after 31/12/2006)
Push button (P/B) Dimming Electrical Configuration
Mod 42664: none
CMP Eff: -301,-321,-322 -341,-342,-202,-203 CMP Item: 31-1-0000-004
If the a/c in question has mod 42664, then IPC pages not reflecting this mod are not authorized for use.
P/Ns shown on IPC pages reflecting mod 42664 standard.
42664 **The configuration(s) prior to this standard is (are) not flagged ("Not approved for ETOPS") in the IPC.**
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 34 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PAIa or vendor SB C Approved w e DO tent ref tion e ma sData on (Air ADM a r C e l If the a/c in question Module) Thermal Mod 42885: P In fo Insulation A330-34-3008 has 42885 IPC mod pages not , then ro rect reflecting this mod are C not authorized for use. fo r NOT
MINIMUM
STANDARD P/N ETOPS APPROVED
P/Ns shown on IPC pages standard. mod 42885 reflecting
CMP Eff: Honeywell & Litton ADIRU -301,-321,-322 CMP Item: 34-1-0000-001
42885
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 36 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PAIa or vendor SB C Approved w e DO tent ref tion a n se m(FAV) Fan r Co AirleaValve o Mod 42570: Pre-mod 42570: P In f A330-36-3002 / ABG 6733A020000 Semca SB 6733A010000 ro rect 6733-36-01 C 42570 fo r NOT
MINIMUM
STANDARD P/N ETOPS APPROVED
Mod 42570:
CMP Eff: -301,-321,-322 -341,-342 CMP Item: 36-1-0000-001
BMC (Bleed Monitoring Computer) CMP Eff: -301,-321,-322 -341,-342 CMP Item: 36-1-0000-002
Mod 42943: A330-36-3003 / Intertechnique SB 706-36-157
Pre-mod 42943: 785-840-1 785-840
6733A030000 more advanced stds: Consult IPC
Mod 42943: 785-840-2 more advanced stds: 785-840-3 (Mod 43468)
42943
Consult IPC
APU Check Valve CMP Eff : -301,-321,-322 -341,-342
Mod 43190: A330-36-3006
Pre-mod 43190: 4063-18202-1 4063-18202
CMP Item: 36-1-0000-003
43190
High Pressure Valve (HPV) CMP Eff : -301 CMP Item: 36-1-0000-004
Mod 43190: 4063-18202-2 more advanced stds: Consult IPC
Mod 43197 : A330-36-3007/ ABG Semca SB 6763-36-01
Pre-mod 43197: 6763C040000 6763C020000 6763A010000
Mod 43197 : 6763C050000
Mod 43198: none
Pre-mod 43198: 6763D040000 6763D020000
Mod 43198: 6763D050000
more advanced stds: Consult IPC
43197
High Pressure Valve (HPV) CMP Eff : -321,-322,-341,-342 CMP Item: 36-1-0000-004
more advanced stds: Consult IPC
43198
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
36.1 THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 49 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion on ease rma APU C GTCPl 331-350-C Mod 42406: Pre-mod 42406: P In fo Allied Signal 3800454-2 SBs GTCP 331-493800454-1 ro rect 6842 and 3881000C 49-6844 ---forDash 3: NOT
CMP Eff: All CMP item: 49-1-2003-02
42406
OR ----
---OR ----
ETOPS APPROVED
Mod 42406: 3800454-3 (approved until 30/06/2008 only – see CMP item 49-1-2003-16)
or Mod 43440: 3800454-4 (approved until 30/06/2008 only – see CMP item 49-1-2003-16)
Mod 43440: Allied Signal
Dash 4: 43440
MINIMUM
STANDARD P/N
SB GTCP 331-49-7073
more advanced stds: 3800454-5 (approved until 30/06/2008 only – see CMP item 49-12003-16)
3800454-4A 3800454-6 further advanced stds: Consult IPC ECB Aircraft Wiring, Lightning Protection CMP Eff: All CMP item: 49-1-2003-004
Mod 42186 or Mod 42272: none
42186 or 42272 **The configuration(s) prior to this standard is (are) not flagged ("Not approved for ETOPS") in the IPC.**
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
If the a/c in question has mod 42186 or 42272, then IPC pages not reflecting this mod are not authorized for use. (Modification in the aircraft type definition.)
P/Ns shown on IPC pages reflecting mod 42186 or 42272 standard.
This issue corresponds to AI/EA5000 Rev 18
49.1
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 49 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion Pre-SBs 49-7092, 49on easePump FCU/Lube ma r SB 49-4012 C 7093, 49-7094 o l Assembly f SB 49-3008 P In FCU: ---3883240-5 ro rect 3883240-3 OR 43730 C ---of r NOT
MINIMUM
STANDARD P/N ETOPS APPROVED
SBs 49-7092, 497093, 49-7094:
CMP Eff: All
CMP item: 49-1-2003-14
Lube Pump Assy:
or
Wiring Harness (De-Oil Solenoid connector)
3881000-5 3881000-4 3881000-2 3881000-1
none
De-Oil Connector:
GTCP 331-49-7094
FCU: 3883240-6 Lube Pump Assy: 3881000-6
De-Oil Connector: 3888297-2
3888297-1
more advanced stds: Consult IPC
De-oiling System Mini-Harness CMP Eff: All CMP item: 49-1-2003-008
Mod 42918: A330-49-3004/ Allied Signal SB GTCP 331-49-6874
Pre-mod 42918: none - new part
Mod 42918: 3888346-1 3888347-1 more advanced stds: none
Dash-3 only 42918
Oil Type CMP Eff: All CMP item: 49-1-2003-007
Mod 42918: A330-49-3004/ Allied Signal SB GTCP 331-49-6937
Pre-Mod 42918: Type II oil
Mod 42918: Type I oil, MIL-L7808 Note : After initial servicing with Type I oil, subsequent servicing with up to one quart of Type II oil during occasional maintenance checks is permitted. If this is done, the oil system should be drained and re-serviced with Type I oil at the next maintenance opportunity.
Dash-3 Only 42918
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
49.2
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 49 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion n as e m a Fuel None : Pre-SB 49-7085: Co Nozzles lP e nfor Allied Signal SB I GTCP 331-49-7085 Fuel Nozzles : 3883264-1 r e c t r 3883264-3 None Co of r NOT
MINIMUM
STANDARD P/N ETOPS APPROVED
SB 49-7085:
CMP Eff: All
CMP item: 49-1-2003-009
Fuel Nozzle: 3883839-2 Fuel Nozzle Assy : 3883890-1 more advanced stds: Consult IPC
Cooling Fan CMP Eff: All CMP item: 49-1-2003-010
None
None : Allied Signal SB GTCP 331-49-7120 or GTCP 331-49-7121
Pre-SB 49-7120 or 49-7121 : 3614163-2 3614163-4 3614163-1
SB 49-7120 or 49-7121 : 3614163-5
more advanced stds: Consult IPC
Gearbox Assembly/ Starter Clutch CMP Eff: All CMP item: 49-1-2003-011
None : Allied Signal SB 3805028-49-7109 or GTCP 331-49-7108
Pre-SB 49-7109 or 49-7108: 3805028-1 (VIPC) 3805028-3 (VIPC) 3805028-4 (VIPC)
SB 49-7109 or 49-7108: 3805028-5 (VIPC) more advanced stds: Consult VIPC
None : Allied Signal SB 3804007-49-6977
Pre-SB 49-6977: A64982-2
SB 49-6977: A64982-3
None IGV Actuator CMP Eff: All CMP item: 49-1-2003-012
more advanced stds: Consult IPC
None
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
49.3
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 49 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion se rma on Compressor Load a C e l (L/C) Module P In fo orrect C fo r NOT
MINIMUM
STANDARD P/N ETOPS APPROVED
CMP Eff : All
Load Compressor with improved IGV (Vespel Bushing): CMP item: 49-1-2003-016
(priority, to be incorporated prior to ETOPS)
Mod: none Allied Signal SB 3804007-49-7123 or GTCP 331-49-7127
Mod: none
Pre-SB 49-7123 or 49-7127: 3804007-4 3804007-5 3804007-6 3804007-7 Post-SB 49-7123 or 49-7127: 3804007-8
Mod 46768: 3804007-11
(NOT ETOPS approved after 30/06/2006)
Load Compressor
Mod 46768:
Dash 4676811:
Allied Signal SB GTCP 380400749-7429 or Allied Signal SB GTCP 331-49-7430
CMP item: 49-12003-016
Pre-mod 46768: 3804007-10 3804007-9 3804007-8
more advanced stds: Consult IPC
(NOT ETOPS approved after 30/06/2006)
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
49.4
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 49 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion n e a ECB Co leas form P In 43765: Pre-mod 43765: Dash-9 orrecort VECB dash – Mod GTCP SB 331-49-7087 304486-8 C 010100 r Rev. 1 304486-7 fo NOT
MINIMUM
STANDARD P/N ETOPS APPROVED
CMP Eff: All
CMP item: 49-1-2003-013
(priority, to be incorporated or prior to ETOPS)
Mod 45332: A330-49-3018/GTCP SB 331-49-7368
43765 or 45332
Dash-10 or VECB dash – 210101 CMP item: 49-1-2003-16
Mod 46255: A330-49-3019 / GTCP SB 331-49-7420 or Allied Signal BGT SB 304486-49-7423
304486-6
Mod 43765: 304486-9 (NOT ETOPS approved after 30/06/2006)
Mod 45332: 3888394-010100 (NOT ETOPS approved after 30/06/2006)
Mod 46255: 304486-10 (until 30/06/2007)
Mod 47454: 3888394-210101 (until 30/06/2007)
46255 or 47454 (Mod 46255 or Mod 47454 supersedes Mod 43765 and Mod 45332)
or Mod 47454: A330-49-3021 / GTCP SB 331-49-7549 or Allied Signal BGT SB 3888394-49-7548
Dash-11 or VECB dash210102
Mod 50295: A330-49-3023 / (to be incorporated no later HONEYWELL SB 304486-49-7705 or than 30/06/2007) HONEYWELL SB 50295 GTCP331-49-7706 or or 50245 CMP item: 49-1-2003-018
(Mod 50295 or Mod 50245 supersedes Mod 46255 and Mod 47454)
Mod 50245: A330-49-3024 / HONEYWELL SB 304486-49-7701 or HONEYWELL SB GTCP331-49-7702
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
Pre-mod 46255: 304486-9 (NOT ETOPS approved after 30/06/2006)
Pre-mod 47454: 3888394-010100 (NOT ETOPS approved after 30/06/2006)
Mod 50295: 304486-11
Mod 50245: 3888394-210102 more advanced stds: Consult IPC
Pre-mod 50295: 304486-10 (NOT ETOPS approved after 30/06/2007)
Pre-mod 50245: 3888394-210101 issue approved corresponds to AI/EA5000 Rev 18 (NOTThis ETOPS after 30/06/2007)
49.5
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f ATA 49 e NT ot B ircra rts R E A AI Mod P/Ns ETOPS UMNo.ill N r to of PaAI or vendor SB C Approved w e DO tent ref tion a se rmValve on eControl Surge a C Mod 45953: Pre-mod 45953: o l (SCV) P In f GTCP SB 331-493290476-3 7369 or Allied Signal Aerospace SB (NOT ETOPS orrect 3290476-49-7018 C approved after r 30/06/2006) fo NOT
CMP Eff: All
MINIMUM
STANDARD P/N ETOPS APPROVED
Mod 45953: 3290476-5 3290476-4
CMP item: 49-1-2003-16
45953
more advanced stds: Consult IPC
APU GTCP 331-350-C with modified Bumper Quill Shaft CMP Eff: All
Mod 50179: SB A330-49-3022 / HONEYWELL SB GTCP331-49-7704 or HONEYWELL SB GTCP331-49-7738
Pre-mod 50179: 3800454-5 3800454-4 (NOT ETOPS approved after 30/06/2008)
Mod 50179: 3800454-6 3800454-4A
CMP item: 49-1-2003-017
(to be incorporated no later than 30/06/2008)
more advanced stds: Consult IPC
50179 Note: compliance with CMP item 49-1-2003-017 entails compliance with CMP item 49-1-2003-017
Ref: AI/EA-O 418/0174/94 Iss 13 Issue date: 02 May 2007
This issue corresponds to AI/EA5000 Rev 18
49.6
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
fo
n ts d E e PL date C irem M u ETOPS PARTS LIST A Up t IP eqA330 S f e NT ot B ircra rts R E A UM ill N r to of Pa C w DO tent refe tion n e a Co leas form P In orrect C r
AIRBUS 1 Rond Point Maurice Bellonte 31707 Blagnac Cedex FRANCE Telephone (33) 61 93 33 33 © Airbus All Rights Reserved
Printed in France
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
Appendix II - A330 ETOPS SIGNIFICANT SYSTEM LIST The following list defines the A330 systems / functions which are ETOPS significant, as per the following criteria: o o o
Category 1 - Systems to be tracked as "ETOPS Significant" in the Reliability Program Category 2 - Systems to be treated as "ETOPS Parallel critical systems" for maintenance Category 3 - Systems involved in ETOPS Significant event to be reported
ATA Chapter
21 - Air Conditioning
22 - Auto Flight
" ETOPS Signi fi cant" System
ATA Sect.
Category 1
3
Significant System category Ad di ti on al i nfor matio n f or Categor y 3 i tem
Avionics Equipment Ventilation Pressure Control & Monitoring Air Conditioning (Packs)
21-26 21-31 21-52
X
X
X
X
Complete loss of avionics cooling Complete loss of pressurisation Uncontained failure of high speed rotating
Pack Control and Indicating
21-53
X
X
component (air cycle machine turbofan .... )
Autopilot
22-10
X
Flight Management (FM) - Navigation / Lateral Functions
22-72
Flight Management (FM) - Performance / 22-73 Vertical Functions Flight Management, Guidance& Envelope 22-83 Computer (FMGEC) Flight Control Unit (FCU) 22-15
X
X
X
X X
X
Dual loss of system / function
X
X
X X
Complete loss of communication in flight (HF) Non recoverable total loss of communication in flight (HF)
X
Complete loss of one or more electrical power gen. system
HF System
23-11
X X
24 - Electrical Power
Integrated Drive Generator System (lDG 24-21 and GCU) APU Generator and APU GCU 24-23 AC Emergency Generation (CSM/G) 24-24 AC Essential Generation Switching (GLC, 24-25 BTC) Transformer Rectifier (TR) 24-32
X
X
23 - Communication
26 - Fire Protection
2
X
X
Loss of AC + DC electrical power distribution
X X
X
X
X
Smoke Detector Control Unit (SDCU)
26-16
X
X
Lower Deck Cargo Compartment Fire Extinguishing
26-23
X
X
system Loss of 2 or 3 TR Fire warning
X
lavatories) protection with or without warning (usually findings from maintenance)
Page 1 of THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
Appendi x II - A 330 ETOPS SIGNIFICANT SYS
ATA Chapter
27 - Flight Controls
" ETOPS Signi fi cant" System
ATA Sect.
Category 1
2
Flight Control Primary Computer (FCPC)
27-93
X
Flight Control Secondary Computer (FCSC)
27-94
X
Flight Control Data Concentrator (FCDC)
27-95
X
Distribution
28-20
Main Fuel Pump System APU Fuel Pump System
28-21 28-22
X X
Cross-feed System
28-23
X
Indicating
28-40
X
Fuel Control and Monitoring Computer (FCMC)
28-51
X
X
Engine Driven Pumps (G)
29-11
X
X
Engine Driven Pump (B)
29-12
X
X
Engine Driven Pump (Y) Hydraulic reservoir Pressurizing System FSOV Wing Ice Protection & Valves
29-13 29-14 29-15 30-11
X
X
Engine Air Intake Ice Protection & Valves
Protection
31 - Indicating & Recording Systems
28 - Fuel
29 - Hydraulic Power
30 - Ice & Rain
34 - Navigation
3
X X
Significant System category Ad di ti on al i nfor matio n f or Categor y 3 i tem
Over spillage Impossibility to use the total quantity of fuel on board (transfer defect) LP valves fail to close
X X X
Cross feed system defect (detected either by flight or maintenan crews)
X
Indication difficulties (FQI freeze, over-read, under-read)
X
Loss of one hydraulic system
X X
X X X
Loss of hydraulic system pressurization (air) FSOV failure to close Total I partial loss of winq de icinq system
30-21
X
X
Total I partial loss of air intake de icing system
Probe Ice Protection (PHC)
30-31
X
X
X
Total l partial loss of more than one probe heatinq system
Windshield Anti-Icing & Defogging Flight Warning Computer (FWC) SDAC Display Units (PFD, ND, SD, WD) DMC ADIRS
30-42 31-53 31-54 31-60 31-62 34-12
X X X X X X
X X X X X
Air data (ADM)
34-13
X
X
X X
Significant misleading or loss of indication
X
Loss of one ADIRU
X Page 2 of
THIS PRINTED COPY IS AN UNCONTROLLED DOCUMENT
Appendi x II - A 330 ETOPS SIGNIFICANT SYS
ATA Chapter
Category
Significant System category Ad di ti on al i nfor matio n f or Categor y 3 i tem
ATA Sect.
1
Weather Radar System
34-41
X
ADF I VOR (if required in area of ops) PRV/HPV Engine Bleed Air Supply System
34-50 36-10 36-11
X X X
36-12
X
Leak Detection APU Power Plant
36-22 49-10
X
Loss of leak detection system without warninq Uncommanded shut down
APU Engine Fuel & Control
49-30
X
Significant overspeed lover EGT
APU Ignition & Starting
49-40
X
APU Engine Controls
49-60
X
APU Indicating APU Oil System
49-70 49-90 71-50 70 72 73 74 75 76 77 79 78 80
X X
" ETOPS Signi fi cant" System
2
3
X X X
X X X
Complete loss of 1 or more bleed air systems
APU Bleed Air Supply & Cross-bleed 36 - Pneumatic
X
System
49 - Auxiliary Power Unit
70 to 80
Non ATA related
All items related to engine ATA chapters are ETOPS Significant except most ATA 71 sub-chapters, ATA 78, and ATA 80.
X
X
Uncontained burst (compressorI turbine cooling fan) Severe fuel I oil leak in the APU compartment No relight in flight
X
X Commanded or uncommanded in-flight shut down
X
X
N/A N/A
N/A N/A
X
Uncommanded power loss I changes Nacelle fire warning oil I fuel leaks Surges Inability to control the engine power
N/A N/A N/A N/A X
Aborted take off / Diversion / Air turn back
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