DeHav Dash 8 AMM CH06

D AIRCRAFT MAINTENANCE MANUAL

DIMENSIONS AND AREAS LIST OF EFFECTIVE PAGES Chapter Section Subject

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Page 1 Sep 20/2005

D AIRCRAFT MAINTENANCE MANUAL

DIMENSIONS AND AREAS TABLE OF CONTENTS

Subject

Chapter Section Subject

DIMENSIONS AND AREAS

06−00−00

Description and Operation

Page

1

Effectivity: ON A/C ALL General DIMENSIONS AND AREAS

06−10−00

Description and Operation

1

Effectivity: ON A/C ALL General Description AIRCRAFT STATIONS

06−20−00

Description and Operation

1

Effectivity: ON A/C ALL General Description Aircraft Coordinate System (X, Y and Z Axes) Major Assembly Datum Points Fuselage Stations Vertical Stabilizer Stations Horizontal Stabilizer Stations Wing Stations AIRCRAFT ZONES

06−30−00

Description and Operation

1

Effectivity: ON A/C ALL General Description Major Zones Major Sub−Zones MASTER EFFECTIVITY: ALL

06−Contents

Page 1 Jun 05/2004

D AIRCRAFT MAINTENANCE MANUAL

Chapter Section Subject

Subject

Page

Zones Sub−Zones/Zones 100 − Lower Fuselage Sub−Zones/Zones 200 − Upper Fuselage

2

Sub−Zones/Zones 300 − Empennage

3

Sub−Zones/Zones 400 − Power Plant and

4

Nacelles Sub−Zones/Zones 500 − Left Wing Sub−Zones/Zones 600 − Right Wing

5

Sub−Zones/Zones 700 − Landing Gear and

6

Doors Sub−Zones/Zones 800 − Doors ACCESS PANELS AND DOORS

06−40−00

Description and Operation

1

Effectivity: ON A/C ALL General Description ACCESS PANELS AND DOORS − EXTERNAL

06−41−00

Description and Operation

1

Effectivity: ON A/C ALL General Description Front Fuselage − Panels and Doors Center Fuselage − Panels

2

Wing/Fuselage − Fairings Vertical Stabilizer and Aft Fuselage − Panels

3

and Doors Horizontal Stabilizer − Panels

5

Left Nacelle − Panels and Doors

6

Right Nacelle − Panels and Doors

7

MASTER EFFECTIVITY: ALL

06−Contents

Page 2 Jun 05/2004

D AIRCRAFT MAINTENANCE MANUAL

Chapter Section Subject

Subject Left Wing − Panels

8

Right Wing − Panels ACCESS PANELS AND DOORS − INTERNAL

Page

10 06−43−00

Description and Operation

1

Effectivity: ON A/C ALL General Description Passenger Compartment − Floor Boards Passenger Compartment − Sidewall Panels

2

Passenger Compartment − Ceiling Panels

3

Passenger Compartment − Overhead Bins Baggage Compartment − Floor Boards and

4

Panels

MASTER EFFECTIVITY: ALL

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Page 3 Sep 20/2005

D AIRCRAFT MAINTENANCE MANUAL

**ON A/C ALL AIRCRAFT DIMENSIONS AND AREAS − DESCRIPTION 1.

General A. This chapter contains the description of the aircraft dimensions and areas, stations, zones, internal and external access panels and doors which are detailed in the sections as follows: – Dimensions and Areas − 06−10−00 – Aircraft Stations − 06−20−00 – Aircraft Zones − 06−30−00 – Access Panels and Doors − General − 06−40−00 – Access Panels and Doors − External − 06−41−00 – Access Panels and Doors − Internal − 06−43−00.

MASTER EFFECTIVITY: See Pageblock 06−00−00 page 1

06−00−00

Page 1 Nov 25/1999

D AIRCRAFT MAINTENANCE MANUAL

**ON A/C ALL DIMENSIONS AND AREAS − DESCRIPTION 1.

2.

General A. This section contains information on the dimensions and areas of the aircraft when supported on the landing gear. Description Refer to Figure 1. A. Dimensions

(1) Overall dimensions Span Length *Height *Propeller ground clearance (static)

85 ft. 0 in. (25.90 m) 73 ft. 0.125 in. (22.25 m) 24 ft. 7 in. (7.49 m) 3 ft. 0.90 in. (0.94 m)

(2) Wings Root chord Tip chord Aspect ratio Incidence Dihedral

8 ft. 4 in. (2.54 m) 4 ft. 3 in. (1.30 m) 12 2 degrees 2 1/2 degrees

(3) Horizontal stabilizer and elevators Span Root chord Tip chord Aspect ratio Incidence Dihedral

26 ft. 0 in. (7.93 m) 6 ft. 8 in. (2.03 m) 4 ft. 11 in. (1.50 m) 4.489 +1 degree 0 degrees

(4) Vertical stabilizer and rudders Height Root chord Tip chord Aspect ratio

13 ft. 3 in. (4.04 m) 13 ft. 3 in. (4.04 m) 9 ft. 9 in. (2.97 m) 1.155

(5) Fuselage Width Height

MASTER EFFECTIVITY: See Pageblock 06−10−00 page 1

Outside 8 ft. 10 in. (2.69 m) Inside 8 ft. 2 in. (2.49 m) Outside 8 ft. 5 in. (2.57 m) Inside 6 ft. 2 in. (1.88 m)

06−10−00

Page 1 Nov 25/1999

D AIRCRAFT MAINTENANCE MANUAL

(6) Landing gear Longitudinal dimension between main and nose wheel centers Main wheel track Nose wheel steering angle (7) Propeller Diameter B.

26 ft. 1 in. (7.95 m) 25 ft. 10.4 in. (7.88 m) High Speed Taxi 14 degrees Slow Speed Taxi 120 degrees 13 ft. 0 in. (3.96 m)

Areas

(1) The main areas are as follows: Wing Horizontal stabilizers and elevators Vertical stabilizer and rudders

585 sq. ft. (54.35 sq. m) 150 sq. ft. (13.94 sq. m) 152 sq. ft. (14.12 sq. m)

(1) *The dimensions to Ground Line are approximate and vary depending on the aircraft configuration and loading conditions.

MASTER EFFECTIVITY: See Pageblock 06−10−00 page 1

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Page 2 Nov 25/1999

D AIRCRAFT MAINTENANCE MANUAL

30 in. (762 mm)

12 ft. 11 in. (3.94 m)

37 in. (937 mm) DIAMETER 13 ft. (3.96 m)

11 ft. 11 in. * (3.63 m)

25 ft. 10 in. (7.88 m) * NOTE: DIMENSIONS ARE APPROXIMATE AND MAY VARY DEPENDING ON AIRCRAFT CONFIGURATION AND LOADING CONDITIONS.

27 ft. 3 in. (8.28 m)

77 in. (1.96 m) 4 ft 3 in. (1.30 m)

8 ft. 4 in. (2.54 m) WING SPAN 85 ft. (25.89 m)

6 ft. 8 in. (2.03 m)

4 ft. 11 in. (1.50 m) 26 ft. (7.93 m)

10 ft. 5 in. * (3.17 m) 43 in. (1.09 m *) 26 ft. 1 in. (7.95 m) LENGTH 73 ft. (22.25 m)

dam0610000_001.dg, pt, 12/11/94

HEIGHT * 24 ft. 7 in. (7.49 m)

Aircraft Dimensions Figure 1 MASTER EFFECTIVITY: See Pageblock 06−10−00 page 1

06−10−00

Page 3 Aug 27/2002

D AIRCRAFT MAINTENANCE MANUAL

**ON A/C ALL AIRCRAFT STATIONS − DESCRIPTION 1.

2.

General A. The aircraft stations and major structural components are made up of a coordinate system using three main reference axes, the X, Y and Z axes. Description Refer to Figure 1. A. Aircraft Coordinate System (X, Y and Z Axes) (1) The three main reference axes are identified X, Y and Z and their ordinates are located along these axes from a point of origin. The point of origin for the longitudinal axis X 00.00, is 43 inches in front of aircraft nose. The point of origin for the lateral axis Y 00.00, is the center line of the aircraft fuselage. The point of origin for the vertical axis Z 00.00, is located 81 inches below the fuselage skin. (2) Identification of the ordinates is by the dimension in inches from the point of origin prefixed by a letter denoting the axis. Station X 182.00 represents a position 182 inches along the X axis from the point of origin X 00.00. B. Major Assembly Datum Points (1) Within the X, Y, Z axis system, additional points of origin are selected in the aircraft as datum points for locating major assemblies, i.e., wings, horizontal stabilizer and nacelles. The ordinates in these areas are identified by the letter for the major axis with a suffix letter indicating the assembly, followed by the dimension in inches from the assembly point of origin, example: XN 55.00 represents a position 55.00 inches aft of the point of origin for the engine nacelle. The point of origin XN 00.00 is located 12.36 inches forward of the spinner tip. This point of origin coincides with the basic aircraft ordinate X312.00. C. Fuselage Stations Refer to Figure 2. (1) The fuselage components are located by dimensions along the X, Y and Z axis from the point of origin for the basic aircraft. D. Vertical Stabilizer Stations Refer to Figure 3. (1) The vertical stabilizer is included in fuselage coordinate system. E. Horizontal Stabilizer Stations Refer to Figure 3. (1) The horizontal stabilizer assembly components are located by dimensions along the X axis from a point of origin XH 0.00 (aircraft ordinate X 866.15). Dimensions forward of XH 0.00 are negative. Along the Y axis dimensions are prefixed YH for identification although YH 0.00 is coincident with Y 0.00 on the aircraft centerline. F. Wing Stations Refer to Figure 4. (1) The wing components are located by dimensions along the X axis from a point of origin XW 0.00 (aircraft ordinate X 426.97). Along the Y axis dimensions are prefixed YW for identification although YW 0.00 is coincident with Y 0.00 on the

MASTER EFFECTIVITY: See Pageblock 06−20−00 page 1

06−20−00

Page 1 Nov 25/1999

D AIRCRAFT MAINTENANCE MANUAL

G.

aircraft centerline (YC 0.00). Nacelle Stations Refer to Figure 5. (1) The nacelle components are located by dimensions along the X axis from a point of origin XN 0.00 which is located 12.36 inches forward of the spinner tip and at aircraft ordinate X 257.00 and along Z axis from a point or origin ZN 0.00 (engine centerline) which is aircraft ordinate Z 171.90. Dimensions below ZN 0.00 are negative. The main landing gear support frame is located at XN 127.50 (aircraft ordinate X 384.50).

MASTER EFFECTIVITY: See Pageblock 06−20−00 page 1

06−20−00

Page 2 Nov 25/1999

D AIRCRAFT MAINTENANCE MANUAL

HORIZONTAL STABLIIZER ORIGIN

ZH

XH

ZW

YH

YW XW

WING ORIGIN

NOTE

ZN

Vertical stabilizer is included in fuselage co−ordinate system, X, Y, and Z.

XN YN NACELLE ORIGIN Z Y

X Y

dam0620000_001.dg, pt, 24/10/94

BASIC AIRCRAFT AND FUSELAGE ORIGIN

Aircraft Stations Coordinate System Figure 1 MASTER EFFECTIVITY: See Pageblock 06−20−00 page 1

06−20−00

Page 3 Aug 27/2002

D AIRCRAFT MAINTENANCE MANUAL

X 82.660

PRESSURE BULKHEAD UPPER

X 191.000

X 170.400

X 160.500

X 110.300

X 132.020

PILOT’S BLKH’D

Z 182.000

Z 163.250

Z 144.000 M. H. B. Z 112.000 FLIGHT DECK FLOOR Z 100.032

Z 100.440 Z 98.860

Z 81.000

X 201.150

X 190.900

X 182.000

X 167.000

X 151.600

X 136.800

X 123.000

X 110.000 X 115.359

X 66.000

Z 57.000 STATIC GROUND LINE

X 43.000

Z 64.800

X 97.000

PRESSURE BULKHEAD LOWER

AIRCRAFT CL

Z 129.000 M. H. B.

Y 09.000 Y 12.500

Y 12.500 Y 09.000

LIGHTNING DIVERTER STRIPS ( 5 PLACES )

dam0620000_010.dg, pt, 25/10/94

Z 112.000

Fuselage Stations Diagram Figure 2 (Sheet 1 of 3) MASTER EFFECTIVITY: See Pageblock 06−20−00 page 1

06−20−00

Page 4 Aug 27/2002

D X 405.737

X 387.350 F/S FRAME DATUM

X 384.500 F/S DATUM

X 377.850

X 370.800

X 354.250

X 333.300

X 312.350

X 270.500 X 291.400

X 264.100

X 262.400

X 253.400 X 259.400

X 242.200

X 234.500 X 240.500

X 215.500 X 222.000

X 202.750

AIRCRAFT MAINTENANCE MANUAL

Z 182.000

CONTINUED ON SHEET 3

CEILING Z 174.000 Z 168.300 Z 155.550 STR 13 Z 140.000 STR 16 20.00

20.00 M. H. B. Z 129.000

M. B. H. 30.00

Z 100.300

Z 100.032 FLOOR LEVEL ( NOMINAL −X 182.000 TO X 545.000) Z 81.000

NOTE Doors dimensions are approximate.

AIRCRAFT DORSAL FIN CL LH LH DORSAL TUNNEL 2 3 2

X 396.150

X 376.110

X 366.050

X 355.950

X 342.300

Z 100.300

X 302.400

X 282.400

X 252.700

X 252.300

X 222.700

X 201.300

Z 98.600

RH

7

6

5 4

Z 189.00 Z 182.00

8

Z 143.000

Y 40.950

CL

SEAT RAILS

Z 129.000 M. B. H.

CL 23

24

Z 102.750 SEAT RAIL OUTBD Z 100.032 FLOOR LEVEL NOMINAL

25

26

27

28 30 Y 28.220

RH

31

32 33

29

Z 81.000

LH

TYPICAL SECTION THROUGH CENTER FUSELAGE.

dam0620000_011.dg, pt, 23/11/94

0R

Y 9.250

62.0

Z 111.893

9 10 11 12 53 .00 13 R 14 15 16 17 18 19 R .00 20 20 21 22

Fuselage Stations Diagram Figure 2 (Sheet 2 of 3) MASTER EFFECTIVITY: See Pageblock 06−20−00 page 1

06−20−00

Page 5 Aug 27/2002

D X 663.445

X 646.445

X 636.000

X 618.000

X 600.000 X 606.000

X 580.500

X 564.500

X 539.000 X 545.000 X 549.500

X 531.500

X 510.000

X 488.500

Z 189.000

X 467.000

X 445.500

X 434.500

X 424.124 (REAR SPAR FRAME DATUM) X 426.974 (R/S DATUM)

AIRCRAFT MAINTENANCE MANUAL

Z 181.025

CONTINUED ON SHEET 2

Z 180.367

Z 160.000 50.00 MAXIMUM

TH

HALF BREA

Z 141.105

M. B. H. Z 100.00 FLOOR (545.000−X600.00)

Z 111.500 FLOOR Z 101.842 Z 99.000

X 653.349

X 649.897

X 625.500

X 597.500

X 547.500

X 521.000

X 501.000

X 487.500 (SECTION CHANGE BELOW M. B. H.)

X 456.500

X 436.500

Z 81.000

NOTE AIRCRAFT CL

Y 24.050

Door dimension is approximate.

Y 42.000

Y 42.000 Y 26.521

Z 174.540

Z 175.750

FRONT SPAR FRAME

REAR SPAR STRUT

FRONT SPAR STRUT

REAR SPAR FRAME

VIEW LOOKING AFT ON X 424.124 ( SYM )

TYPICAL SECTION AT WING ATTACHMENT FRAMES

dam0620000_012.dg, pt, 23/11/94

Z 129.000 M. H. B. VIEW LOOKING FWD ON X 387.350 ( SYM )

Fuselage Stations Diagram Figure 2 (Sheet 3 of 3) MASTER EFFECTIVITY: See Pageblock 06−20−00 page 1

06−20−00

Page 6 Aug 27/2002

MASTER EFFECTIVITY: See Pageblock 06−20−00 page 1

dam0620000_013.dg, pt, 09/11/94

X 861.000

X 858.824

5

E

LIN

9

8

7

10

06−20−00

FORE RUDDER AUX HINGE (2 PLCS)

FORE RUDDER HINGE (4 PLCS)

AFT RUDDER AUX HINGE (2 PLCS)

AFT RUDDER HINGE (3 PLCS)

E

LIN

GE

6

GE

RIB

RIB

HIN

RIB

11

ER

RIB

HIN

RIB

DD

4

DER

UD

3

ER

RIB

RU

SKIN STIFFENERS (TYP)

AFT

RIB

RIB

X 837.824 AFT RUDDER H/L

2

FOR

AR

SP

RIBS (TYP)

X 816.824 FORE RUDDER H/L

L/E

X 699.824

X 663.445

RIB

X 789.656

No

RIB

FR

RIB

.7

.6

No

.4

No

RIB

X 771.803

FR

.5

No

FR

X 646.445

RIB

X 753.949

FR

FR No. 3

FR No. 2

FR No. 1

Z 141.105

X 736.096

X 718.252

X 699.374 X 699.600 X 700.409

X 683.200

X 670.349

X 653.349

X 900.104 X 919.123

X 898.123 AFT RUDDER

X 866.154 (XH 0.0) X 867.424 R/S DATUM X 877.123 FORE RUDDER H/L

X 851.263 MID/S DATUM

X 830.203 F/S DATUM

X 820.104

X 813.823

X 802.123

D

AIRCRAFT MAINTENANCE MANUAL

Z 342.500 (ZH 0.0)

12

Z 335.500

11A

Z 181.025 1

Z 176.500

Z 150.000

Z 101.842

Stabilizer Stations Diagram Figure 3 (Sheet 1 of 2)

Page 7 Aug 27/2002

D XH 20.800 XH 25.050

XH 0.000 (XH 866.154) REAR SPAR

XH 9.250 ELEVATOR HINGE LINE

XH 33.950 XH 28.200 TAB HINGE LINE

AIRCRAFT MAINTENANCE MANUAL

YH 156.000

YH 139.000

RIB 13 RIB 12

YH 132.200

RIB 11

YH 120.700 FRONT SPAR

RIB 10

YH 103.700 YH 100.000 YH 92.200

RIB 9 RIB 8

YH 76.200 MID SPAR TAB HINGES

RIB 7

YH 59.000 RIB 6 YH 45.000

RIB 5

REAR SPAR YH 31.000

RIB 4 RIB 3

YH 13.800

RIB 2

YH 6.000

RIB 1 YH 0.000 (Y 0.000) YH 6.150

AIRCRAFT CL

YH 14.000 YH 22.000 YH 30.000

SPRING TAB

YH 40.000 YH 52.000 YH 64.600

YH 64.600 YH 77.500

YH 84.000 YH 90.900 YH 105.850

TRIM TAB

YH 135.500 YH 139.000

YH 135.500 YH 140.200

STR No. 1

STR No. 2

STR No. 3

STR No. 5 STR No. 4

ELEVATOR HINGES

dam0620000_014.dg, pt, 10/11/94

YH 120.800

Stabilizer Stations Diagram Figure 3 (Sheet 2 of 2) MASTER EFFECTIVITY: See Pageblock 06−20−00 page 1

06−20−00

Page 8 Aug 27/2002

D AIRCRAFT MAINTENANCE MANUAL FUEL SURGE BAY

FWD

FUEL TANK

YW 243.000

YW 261.000

YW 288.000 APPROX YW 279.000

YW 297.000

YW 326.000 APPROX YW 315.000

YW 333.000

YW 351.000

YW 369.000

YW 387.000

YW 405.000

YW 423.000

YW 444.000

YW 457.000

YW 474.000

YW 490.000

OUTBD

WING BOX FLANGED STRINGERS (TYP)

REAR SPAR PLANE CL AILERON HINGE XW 13.604

OUTER FLAP FRONT SPAR

GAP IN TRAILING EDGE − 2 PLACES

YW 232.200

FLAP STRINGERS (TYP)

FLAP RIBS (TYP) YW 260.975

YW 333.000 YW 327.000

YW 405.100 APPROX YW 404.650

YW 423.030

YW 405.650

XW 8.190

YW 457.030

YW 475.000 APPROX

YW 490.190

YW 510.120 APPROX

XW 15.485

CONTINUED ON SHEET 2

FRONT SPAR PLANE O/WING

O/WING REF PLANE FLAP TRACKS 2 PLACES

2 30’ DIHEDRAL

dam0620000_015.dg, pt, 23/11/94

LEFT WING

Wing Stations Diagram Figure 4 (Sheet 1 of 2) MASTER EFFECTIVITY: See Pageblock 06−20−00 page 1

06−20−00

Page 9 Aug 27/2002

D YW 139.200 (NACELLE)

YW 155.200 (YN 0.000)

YW 171.200 (NACELLE)

AIRCRAFT MAINTENANCE MANUAL

YW 58.200

YW 42.000

YW 23.858

YW 8.680

YW 8.680

YW 23.858

YW 42.000

YW 58.200 YW 57.000

YW 74.400

YW 90.600

YW 106.800

YW 139.000

YW 123.000

AIRCRAFT CL

YW 178.000 APPROX YW 171.400

YW 189.970 YW 189.000

X 269.360 (XN 12.360)

YW 207.000 YW 202.000 APPROX

YW 225.000

FWD

X 257.000 (XN 0.000)

FUEL COLLECTOR BAY

CONTINUED ON SHEET 1

WING LEADING EDGE X 369.511 X 384.500 FRONT SPAR FRAME − C/WING

INNER FLAP REAR SPAR

SHROUD LINE

SHROUD LINE

X 469.450

WING TRAILING EDGE

YW 48.000 APPROX

Y 0.000 YW 58.200

YW 106.800

YW 138.700 APPROX

YW 174.000 APPROX YW 172.503

YW 224.840

INNER FLAP FRONT SPAR

YW 26.712

YW 26.712

XW 9.740

XW 9.740 OUTER FLAP REAR SPAR

X 426.974 REAR SPAR PLANE

INNER FLAP HINGE

CL OUTER FLAP HINGE

AIRCRAFT CL

NACELLE CL

LEFT WING

dam0620000_016.dg, pt, 23/11/94

C/WING REFERENCE PLANE

Wing Stations Diagram Figure 4 (Sheet 2 of 2) MASTER EFFECTIVITY: See Pageblock 06−20−00 page 1

06−20−00

Page 10 Aug 27/2002

D

NACELLE CL

ZN 9.5 WING REF. PLANE

ZN 0.06 UPPER LONGERON ZN 15.00 DATUM

YW 171.200

YW 139.200

XN 206.00 XN 197.32

AFT ACCESS PANEL ( BOTH SIDES )

XN 169.973 WING R/S DATUM XN 176.50 XN 182.70 XN 190.00

XN 0.00 (XN 257.00) XN 12.36

XN 57.00 XN 64.00 XN 72.00 XN 78.50 XN 87.00

ZN 0.00 (Z 171.90) PROPELLER CL CENTER ACCESS PANEL (BOTH SIDES)

XN 91.00 XN 95.00 XN 98.00 XN 102.19 XN 107.18 XN 107.80 FIRE WALL XN 110.50 XN 117.05 XN 122.00 XN 127.50 WING F/S DATUM

XN 55.00

XN 60.00 XN 68.00 XN 75.00 XN 82.70

AIRCRAFT MAINTENANCE MANUAL

W.R.P.

ZN 9.5 ZN 0.00 NACELLE FRAME

FRONT LWR MOUNT PLANE

XN 224.76

SIDE SUPPORT TUBES CL

XN 179.10 XN 182.70 XN 190.00

LOWER ACCESS COWLING

XN 100.93 REAR GROUND HANDLING MOUNT PLANE XN 121.20 XN 125.50 XN 130.60 XN 134.68 XN 137.35 XN 141.95 XN 146.40 XN 150.85 XN 155.30 XN 159.75 XN 164.20 XN 168.87

PROPELLER PLANE

XN 52.90

ZN − 7.00 ENGINE CL

XN 24.60 XN 35.564 XN 44.49

NACELLE ORIGIN

DOOR HINGE LINE

ZN 24.25 LOWER LONGERON DATUM

DRAG STRUT

MAIN GEAR LEG

MAIN GEAR LEG XN 170.383 (X 427.383)

Z 57.00 STATIC GROUND LINE

VIEW ON NACELLE FRONT

XN 64.00

YN 0.00 (Y155.20) NACELLE CL

XN 60.00

SIDE VIEW

ACCESS DOOR OPENING

ACCESS DOOR OPENING

MAIN LANDING GEAR DOOR OPENING DOOR HINGE LINE − 1 PLC

DOOR HINGE LINE − 3 PLCS ACCESS DOOR OPENING

PLAN VIEW

dam0620000_009.dg, pt, 23/11/94

XN 104.75

Nacelle Stations Diagram Figure 5 MASTER EFFECTIVITY: See Pageblock 06−20−00 page 1

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Page 11 Aug 27/2002

D AIRCRAFT MAINTENANCE MANUAL

**ON A/C ALL AIRCRAFT ZONES − DESCRIPTION 1.

2.

General A. The aircraft zoning system provides positive identification of areas in the aircraft as follows: – Major zones – Major sub−zones – Zones. Description A. Major Zones Refer to Figure 1. (1) The aircraft is divided into eight major zones identified as follows: MAJOR ZONES 100 200 300 400 500 600 700 800 B.

C.

D.

DESCRIPTION Lower half of the fuselage Upper half of the fuselage Empennage Power plant and nacelles Left wing Right wing Landing gear and landing gear doors Doors

Major Sub−Zones (1) The major sub−zones are subdivisions of the major zones using the second digit of the major zone number, for example, the major zone 100, lower fuselage is divided into major sub−zones 110, 120, 130 and 140. Zones (1) The major sub−zones are further divided into zones using the third digit of the major zone number, for example, the major sub−zone 120, flight compartment under floor area X 97.00 to X 182.00 is divided into zones 121 and 122. Sub−Zones/Zones 100 − Lower Fuselage Refer to Figure 2. SUB−ZONES/ZONES Major Sub−Zone 110 Zone 111 Zone 112 Zone 113

DESCRIPTION Radome and nose compartment sta. X43.00 to sta. X110.00 Radome sta. X43.00 to X66.00 Nose compartment R.H. under floor X66.00 to X110.00 Nose compartment L.H. under floor X66.00 to X110.00

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SUB−ZONES/ZONES Zone 114 Major Sub−Zone 120 Zone 121 Zone 122 Major Sub−Zone 130 Zone 131 Zone 132 Zone 133 Major Sub−Zone 140 Zone 141 Zone 142 Zone 143 Zone 144 Zone 145 E.

DESCRIPTION N.L.G. wheel well Flight compartment, under floor area sta. X110.00 to X182.00 Under floor L.H. Under floor R.H. Fuselage under floor area sta. X182.00 to X424.12 Under floor cabin L.H. Under floor cabin R.H. Under floor cabin center Fuselage, under floor sta. X424.12 to X653.34 (Including pressure dome) Under floor cabin L.H. Under floor cabin R.H. Under floor cabin center Under floor, rear cargo forward Under floor, rear cargo, rear

Sub−Zones/Zones 200 − Upper Fuselage Refer to Figure 3. SUB−ZONES/ZONES Major Sub−Zone 210 Zone 211 Zone 212 Major Sub−Zone 220 Zone 221 Zone 222 Zone 223 Zone 224 Zone 225 Major Sub−Zone 230 Zone 231 Zone 232 Zone 234 Zone 235 Major Sub−Zone 240 Zone 241 Zone 242 Zone 243

DESCRIPTION Upper fuselage sta. X66.00 to sta. X182.00 Flight compartment, above floor sta. X110.00 to X182.00 Nose compartment, above floor sta. X 66.00 to X110.00 Fuselage sta. X182.00 to sta. X240.50 Avionics shelves L.H. X182.00 to X199.25 Lavatory R.H. X182.00 to X212.50 (approximately). Wardrobe L.H. X199.25 to X219.25 Galley R.H. X212.50 to X237.50 Electrical boxes L.H. X182.00 to X220.00 (approximately). Fuselage sta. X182.00 to sta. X424.12 Cabin floor to top of sidewall L.H. Cabin floor to top of sidewall R.H. Cabin roof R.H. Cabin roof, center Fuselage sta. X424.12 to sta. X545.50 Cabin floor to top of sidewall L.H. Cabin floor to top of sidewall R.H. Cabin roof L.H.

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SUB−ZONES/ZONES Zone 244 Zone 245 Major Sub−Zone 250 Zone 251 Major Sub−Zone 260 Zone 261 Zone 262 Zone 263 Zone 264 F.

DESCRIPTION Cabin roof R.H. Cabin roof, center Fuselage sta. X545.50 to sta. X653.34 (including pressure dome) Rear baggage compartment Wing−to−fuselage fairings Forward root fairing, forward of front spar sta. X387.35 Rear root fairings, rear of rear spar sta. X424.12 Left hand root fairing, X387.35 to X424.12 Right hand root fairing, X387.35 to X424.12

Sub−Zones/Zones 300 − Empennage Refer to Figure 4. SUB−ZONES/ZONES Major Sub−Zone 310 Zone 311 Zone 312 Major Sub−Zone 320 Zone 321 Zone 322 Zone 323 Zone 324 Zone 325 Major Sub−Zone 330 Zone 331 Zone 332 Zone 333 Zone 334 Zone 335 Major Sub−Zone 340 Zone 341 Zone 342 Zone 343 Zone 344 Zone 345 Major Sub−Zone 350 Zone 351

DESCRIPTION Rear fuselage sta. X653.34 to sta. X861.00 Rear fuselage sta. X653.34 to X807.12 Rear fuselage sta. X807.12 to X861.00 Vertical stabilizer and rudder assembly Vertical stabilizer leading edge Vertical stabilizer, between front and rear spars (Including trailing edge shroud) Fore rudder Trailing rudder Fairing Horizontal Stabilizer and elevator assembly L.H. sta. XH 0.00 to XH 33.95 Stabilizer leading edge Stabilizer between front and rear spar Elevator Elevator trim tap Elevator spring tab Horizontal stabilizer and elevator R.H. sta. XH 0.00 to XH 33.95 Stabilizer leading edge Stabilizer between front and rears spars Elevator Elevator trim tab Elevator spring tab Dorsal fairing sta. X503.50 to X653.34 Tunnel

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D AIRCRAFT MAINTENANCE MANUAL

SUB−ZONES/ZONES Zone 352 G.

Dorsal fairing

Sub−Zones/Zones 400 − Power Plant and Nacelles Refer to Figure 5. SUB−ZONES/ZONES Major Sub−Zone 410 Zone 411 Zone 412 Zone 413 Zone 414 Zone 415 Zone 416 Zone 417 Zone 418 Zone 419 Major Sub−Zone 420 Zone 421 Zone 422 Zone 423 Zone 424 Zone 425 Zone 426 Zone 427 Zone 428 Zone 429

H.

DESCRIPTION

DESCRIPTION Engine and nacelle L.H. Propeller Top structure including area between firewall and wing front spar Forward side cowling L.H. O/B Forward side cowling R.H. I/B Rear side cowling L.H. O/B Rear side cowling R.H. I/B Bottom cowling Engine No. 1 Nacelle rear section including exhaust pipe and shrouds Engine and nacelle R.H. Propeller Top structure including area between firewall and wing front spar Forward side cowling L.H. O/B Forward side cowling R.H. I/B Rear side cowling L.H. O/B Rear side cowling R.H. I/B Bottom cowling Engine No. 2 Nacelle rear section including exhaust pipe and shrouds

Sub−Zones/Zones 500 − Left Wing Refer to Figure 6. SUB−ZONES/ZONES Major Sub−Zone 510 Zone 511 Zone 512 Zone 513 Major Sub−Zone 520 Zone 521 Zone 522

DESCRIPTION Leading edge sta. YW 45.00 to sta. YW 490.00 Area between fuselage and No.1 engine Area between No. 1 engine and sta. YW288.00 Area between sta. YW 288.00 and YW 490.00 Wing box area sta. YC 00.00 to sta. YW 510.00 Area sta. YC 0.00 to YW 45.00 including No. 1 flap track Area sta. YW 45.00 to YW 139.00

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SUB−ZONES/ZONES Zone 523 Zone 524 Zone 525 Zone 526 Zone 527 Zone 528 Major Sub−Zone 530 Zone 531 Zone 532 Zone 533 Zone 534 Zone 535 Zone 536 Major Sub−Zone 540 Zone 541 Zone 542 Zone 543 Zone 544 I.

DESCRIPTION Area sta. YW139.00 to YW 171.00 including #2 and #3 flap tracks Area sta. YW 171.00 to YW 405.00 including #4 and #5 flap tracks Area sta. YW 405.00 to YW 490.00 Area sta. YW 261.00 − flap track No. 4 Area sta. YW 369.00 − flap track No. 5 Wing tip YW 490.00 to YW 510.00 Trailing edge shroud sta. YW 45.00 to sta. YW 490.00 Area sta. YW 45.00 to YW 139.00 Area sta. YW 171.00 to YW 490.00 Inner ground spoiler Outer ground spoiler Inner roll spoiler Outer roll spoiler Wing flaps and ailerons, sta. YW 45.00 to sta. YW 510.00 Flap inboard Flap outboard Aileron L.H. Aileron tab L.H.

Sub−Zones/Zones 600 − Right Wing Refer to Figure 7. SUB−ZONES/ZONES Major Sub−Zone 610 Zone 611 Zone 612 Zone 613 Major Sub−Zone 620 Zone 621 Zone 622 Zone 623 Zone 624 Zone 625 Zone 626 Zone 627

DESCRIPTION Leading edge sta. YW 45.00 to sta. YW 490.00 Area between fuselage and No. 2 engine Area between No. 2 engine and sta. YW 288.00 Area between sta. YW 288.00 and YW 490.00 Area sta. YC 0.00 to YW 510.00 Area sta. YC 0.00 to YW 45.00 including No. 1 flap track Area sta. YW 45.00 to YW 139.00 Area sta. YW 139.00 to YW 171.00 including No. 2 and 3 flap tracks Area sta. YW 171.00 to YW 405.00 including No. 4 and 5 flap tracks Area sta. YW 405.00 to YW 490.00 Area sta. YW 261.00 − flap track No. 4 Area sta. YW 369.00 − flap track No. 5

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SUB−ZONES/ZONES Zone 628 Major Sub−Zone 630 Zone 631 Zone 632 Zone 633 Zone 634 Zone 635 Zone 636 Major Sub−Zone 640 Zone 641 Zone 642 Zone 643 Zone 644 J.

Sub−Zones/Zones 700 − Landing Gear and Doors Refer to Figure 8. SUB−ZONES/ZONES Major Sub−Zone 710 Zone 711 Zone 712 Zone 713 Zone 714 Zone 715 Major Sub−Zone 720 Zone 721 Zone 722 Zone 723 Zone 724 Zone 725 Major Sub−Zone 730 Zone 731 Zone 732 Zone 733 Zone 734 Zone 735

K.

DESCRIPTION Wing tip YW 490.00 to YW 510.00 Trailing edge shroud sta. YW 45.00 to sta. YW 490.00 Area sta. YW 45.00 to YW 139.00 Area sta. YW 171.00 to YW 490.00 Inner ground spoiler Outer ground spoiler Inner roll spoiler Outer roll spoiler Wing flaps, and ailerons sta. YW 45.00 to sta. YW 501.00 Flap inboard Flap outboard Aileron R.H. Aileron tab R.H.

DESCRIPTION Nose gear and doors Nose gear Forward side door R.H. Forward side door L.H. Rear door R.H. Rear door L.H. Main gear and doors L.H. Main gear Forward door Mid door Rear door R.H. Rear door L.H. Main gear and doors R.H. Main gear Forward door Mid door Rear door R.H. Rear door L.H.

Sub−Zones/Zones 800 − Doors Refer to Figure 9.

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SUB−ZONE/ZONES Major Sub−Zone 820 Zone 821 Zone 822 Zone 823 Zone 824 Zone 825 Zone 826

DESCRIPTION Fuselage doors Flight compartment escape hatch Emergency exit, fwd. R.H. Passenger door Emergency exit, mid R.H. Emergency exit, mid L.H. Baggage compartment door

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600

500

300

400

700

700

700

400

800

100

800

800

200

800

300 dam0630000_009.dg, kms, 19/04/96

800

400

Major Zones − General Figure 1 MASTER EFFECTIVITY: See Pageblock 06−30−00 page 1

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X 653.34

X 545.50

145

X 424.12 144 143

142 141

X 182.00 140

X 110.00 X 66.00

133

132 131

X 43.00

122 130 112 121 113 111

120

114

dam0630000_001.dg, pt, 23/11/94

110

Zones 100 − Lower Fuselage Figure 2 MASTER EFFECTIVITY: See Pageblock 06−30−00 page 1

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D AIRCRAFT MAINTENANCE MANUAL X 424.12 262

X 387.35 264 263

X 545.50

261 260

245

244 X 424.12

243

235 X 182.00

234 X 653.34

233

251

X 212.50 X X 182.00 182.00 PRESSURE BULKHEAD X 110.00

242 250

X 237.50

241 232 240 231

224 222

230 223 211 212

X 199.25

221 X 219.25 225

210 X 66.00

dam0630000_002.dg, pt, 23/11/94

220

X 110.00

Zones 200 − Upper Fuselage Figure 3 MASTER EFFECTIVITY: See Pageblock 06−30−00 page 1

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D AIRCRAFT MAINTENANCE MANUAL 340 344

343

330

345 335

334

342

XH 33.95

XH 0.00

341

333 332 331 XH 0.00 320

XV 0.00 (X 919.00)

325

324 323 322 X 861.00

321 X 807.12

352

312 350

X 653.34 dam0630000_003.dg, pt, 23/11/94

351

310 311

Zones 300 − Empennage Figure 4 MASTER EFFECTIVITY: See Pageblock 06−30−00 page 1

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422

426 425

424 423

429 428

421 420 427 412

416 415

414 413 418

411 410 417

dam0630000_004.dg, pt, 14/11/94

419

Zones 400 − Power Plant and Nacelles Figure 5 MASTER EFFECTIVITY: See Pageblock 06−30−00 page 1

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540

541

YW 45.00

544

542 533 543

530 534 531 YW 139.00 YW 45.00

536

YW 171.00

521

532

YW 139.00 YW 171.00

522

YW 490.00

YW 261.00

523 526 YW 45.00

524

YW 369.00

YW 405.00 527

YW 490.00 525

520

528

511

YW 510.00

512 YW 288.00

513

510

YW 490.00

dam0630000_005.dg, pt/kms, 30/04/96

YC 0.00

YW 510.00

535

Zones 500 − Left Wing Figure 6 MASTER EFFECTIVITY: See Pageblock 06−30−00 page 1

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D AIRCRAFT MAINTENANCE MANUAL YW 510.00 643 644 640

642 YW 490.00

632 641

636 635

YW 510.00 YW 490.00 628

630

634

YW 405.00 YW 369.00

625

633 627

YW 261.00

YW 171.00 YW 171.00 YW 139.00 626 YW 139.00

624 YW 490.00

631

YW 45.00 620 613

YW 45.00

623 622

YW288.00

621

YC0.00

612

611 YW 45.00

dam0630000_006.dg, pt/kms, 30/04/96

610

Zones 600 − Right Wing Figure 7 MASTER EFFECTIVITY: See Pageblock 06−30−00 page 1

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734

735

733

724

731

732

730

725

723

714 715 712 722

713

721

720

711

dam0630000_007.dg, pt, 17/11/94

710

Zones 700 − Landing Gear and Landing Gear Doors Figure 8 MASTER EFFECTIVITY: See Pageblock 06−30−00 page 1

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820

824 821

822 826

825

dam0630000_008.dg, pt, 14/11/94

823

Zones 800 − Doors Figure 9 MASTER EFFECTIVITY: See Pageblock 06−30−00 page 1

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**ON A/C ALL ACCESS PANELS AND DOORS − DESCRIPTION 1.

2.

General A. This section contains the description of the identification code of various access panels and doors that are on the exterior and interior of the aircraft. Each access panel and door on the aircraft is given an identification alphanumeric code number. B. For this chapter, the interior furnishing panels and floor panels are also regarded as access panels. The external and internal access panels and doors are given in two sections as follows: – External Access Panels and Doors, (Ref. 06−41−00) – Internal Access Panels and Doors, (Ref. 06−43−00). Description A. Identification Code Number (1) Each access panel is identified in relation to the aircraft zone in which the panel or door is located. The identification code for each panel and door consists of a three digit zone number followed by two letters as follows: – 322CL (a) The first letter (given in alpha sequence), determines the position of panels in the zone, as follows: – C = The third letter in the alpha sequence. (b) The second letter indicates the location of the access, as follows: – T = top – B = bottom – L = left – R = right – Z = internal. (2) The identification code number for the access panel − 322CL is as follows: – 322 = Zone 322 of the vertical stabilizer between front and rear spars – C = The third access panel or door within Zone 322 – L = On the left side of the vertical stabilizer.

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**ON A/C ALL ACCESS PANELS AND DOORS (EXTERNAL) − DESCRIPTION 1.

2.

General A. This section contains description and location of the access panels and doors on the external surfaces of the aircraft. Description A. Front Fuselage − Panels and Doors (1) The list of code numbers for the access panels and doors that are located on the front fuselage of the aircraft are as follows: Refer to Figure 1.

CODE NUMBERS 111AT 112AR 112BR 113AL 121AL

121BL

122AR

122BR

212AL 212BR

TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT Radome Weather radar antenna, VOR/Localize antenna, glide slope antenna Crew oxygen bottle, oxygen lines, nose wheel steering electronic control unit, hydraulic lines Crew manifold, nose gear doors solenoid sequence valve, emergency reservoir (main gear extend) Battery Brake linkage, rudder control interconnect push rod, rudder input quadrant, rudder pedal adjustment mechanism, rudder control cables Roll spoiler quadrant, roll spoiler control cables, roll interconnect torque tube, elevator output quadrant, pitch disconnect clutch, pitch disconnect cable, gust lock quadrant, gust lock control cables, power lever Panels lay shaft, power lever limit switches, condition lever lay shaft, condition lever limit switches, engine control cables, electrical wiring, engine intake adapter heater and elevator horn heater thermostats Brake linkage, rudder input quadrant, rudder pedal adjustment mechanism, rudder control cables, rudder restriction mechanism Aileron quadrant, aileron servo, aileron control cables, roll disconnect clutch, roll disconnect cables, elevator output quadrant, elevator trim chain and cable assembly, power lever lay shaft, power lever limit switches, condition lever limit switches, engine control cables, electrical wiring Transformer/rectifier units, pilot’s wiper motor, dc contactor box Doors Copilot’s wiper motor, flight compartment fan, nose landing light, windshield washer reservoir

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B.

Center Fuselage − Panels (1) The list of code numbers for the access panels and doors on the center fuselage of the aircraft are as follows: Refer to Figure 2.

CODE NUMBERS 132AR 261QR 261RL 262QL 262RR 263AL 263BL & 263CL 263DL 263EL, 263FL 264AR 264BR 264CR 264DR 351AT, 351BT, 352AL, 352BL, 352CL, 352CR, 352DR C.

TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT Toilet servicing panel Inspection panels Inspection panels Inboard flap track Inboard flap track Deicing lines, electrical wiring Brake control valves, hydraulic lines, deice lines, deice line moisture drain plug Panels Hydraulic lines Fire extinguisher cartage Deicing lines, electrical wiring Brake control valve, hydraulic lines, deicing lines, deice line moisture drain plug (elevator) Landing gear selector valve, hydraulic lines, deice lines Hydraulic lines Bleed air duct, hydraulic lines, deice lines, gust lock cable (elevator)

Wing/Fuselage − Fairings (1) The list of code numbers for the fairings that are located on top of the wing/fuselage section of the aircraft is as follows: Refer to Figure 3.

CODE NUMBERS 261AT 261BT 261DT

261ET 261FT 261GT 261HT 261JT 261KT

TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT Inspection panels Inspection panels Bleed air pipe, bleed air over temperature switch, deice pressure transducer, deice lines, engine control cables, electrical wiring Inspection panels Inspection panels Engine control cables, bleed air pipe Inspection panel Deice isolate valve, engine control cables, bleed air pipe Inspection panels

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CODE NUMBERS 261LT 261MT 261NT

262AT

262BT 262CT 262DT

262ET 262FT 262GT 262HT 262JT 262KT 262LT 262MT 262NT 262PT 262QT 262RT 262ST 262TT D.

TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT Inspection panels Inspection panels Bleed air pipe, bleed air over temperature switch, deice pressure transducer, deice lines, engine control cables, electrical wiring Spoiler splitter clutch quadrant, flap drive shaft, aileron and spoiler control cables, fuel line, hydraulic lines, ground spoiler selector solenoid valves Panels Inspection panel Inspection panel Fire extinguisher bottles, fire extinguisher discharge cartridges, fire extinguisher distribution lines, hydraulic lines Inspection panel Inspection panel Inspection panel Inspection panel Bleed air pipe, aileron and spoiler control cables Bleed air pipe, gust lock control cables Flap power unit, aileron splitter quadrant, flap drive shaft, aileron and spoiler Inspection panel Inspection panel Hydraulic lines, fuel lines, deice lines Inspection panel Inspection panel Inspection panel Inspection panel

Vertical Stabilizer and Aft Fuselage − Panels and Doors (1) The list of code numbers for the access panels and doors that are located on vertical stabilizer and the aft fuselage section of the aircraft are as follows: Refer to Figure 4.

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CODE NUMBERS 311AB

311BZ 311CB 312AB 321AT 321BL 321CL 321DR 321EL 321FL 321GT 321HT 321JL 321KR 322AL 322ER 322BL 322CL 322FR 322DL 322HR 322GR 322HL 322JL 323AL, 323BL 323CL, 323DL 323ER, 323FR 323GR, 323HR

TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT Door Air cycle machine, heat exchanger, condenser/mixer, pack temperature control valves, temperature trim valves, compressor discharge over−temperature switch, deice system distributor valves, water separators, drains, heated drains, No. 2 hydraulic system case drain assembly (only for aircraft with post Mod 8/2892), check valves, restriction, main feed lines and thermostats, hydraulic lines, elevator trim servo, rudder control cables, normal outflow valve, cockpit voice recorder, flight data recorder Inspection panels Inspection panels Inspection panels Emergency locator transmitter Inspection panel Bleed air duct, hydraulic lines, deice lines, gust lock cable Bleed air duct, hydraulic lines, deice lines, gust lock cable Inspection panel Deice lines Panels Deice lines Inspection panels Inspection panels Inspection panels Elevator trim quadrants, elevator trim cables Elevator trim quadrants, elevator trim cables Inspection panels Inspection panels Inspection panels Rudder actuators, yaw damper, rudder control cables Rudder actuators, yaw damper, rudder control cables Rudder pulley quadrant, rudder control cables Rudder pulley quadrant, rudder control cables Rudder pulley quadrant, rudder control cables Fore rudder attachments Fore rudder attachments Fore rudder attachments Fore rudder attachments

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CODE NUMBERS 324AL, 324BL 324CL, 324DL 324ER, 324FR 324GR, 324HR 325DL, 325EL 325FR, 325GR 325AT 325BT 325CT E.

TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT Trailing rudder attachments Trailing rudder attachments Panels Trailing rudder attachments Trailing rudder attachments Inspection panels Inspection panels Anti collision light, deice lines, electrical wiring Inspection panel Elevator gust lock

Horizontal Stabilizer − Panels (1) The list of code numbers for the access panels and doors that are located on the horizontal stabilizer of the aircraft are as follows: Refer to Figure 5.

CODE NUMBERS 325AT 325BT 325CT 332AT 332BL 332CL 333AL 333BT 333CT 333DT 333ET 333FT 333VB 333WB 333XB 333YB 333BBL 333CCT 342AT

TYPE OF ACCESS

Panels

342BR 342CR 343AR 343BT

MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

ACCESS TO EQUIPMENT/COMPONENT Anti collision light, deice lines, electrical wiring Inspection panel Elevator gust lock Elevator trim tab actuator, elevator trim position transmitter, elevator trim chain/cable Deice lines Deice lines Elevator mass balance, elevator horn heat Elevator attachments Elevator attachments Elevator trim tab actuator attachments Elevator attachments Elevator attachments Elevator attachments Elevator attachments Elevator trim tab actuator attachments Elevator trim tab actuator attachments Elevator spring tab mechanism Elevator spring tab mechanism Elevator trim tab actuator, elevator trim position transmitter, elevator trim chain/cable Deice lines Deice lines Elevator mass balance, elevator horn heat Elevator attachments

06−41−00

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D AIRCRAFT MAINTENANCE MANUAL

CODE NUMBERS 343CT 343DT 343ET 343FT 343VB 343WB 343XB 343YB 343ZB 343AAT 343BBR 343CCT F.

TYPE OF ACCESS Panels

ACCESS TO EQUIPMENT/COMPONENT Elevator attachments Elevator trim tab actuator attachments Elevator attachments Elevator attachments Elevator attachments Elevator attachments Elevator trim tab actuator attachments Elevator trim tab actuator attachments Elevator spring tab attachments Elevator spring tab attachments Elevator spring tab attachments Elevator spring tab attachments

Left Nacelle − Panels and Doors (1) The list of code numbers for the access panels and doors that are located on the left nacelle are as follows: Refer to Figure 6.

CODE NUMBERS 411AL 412AT

TYPE OF ACCESS

412BT 412CT

Panels

412DT

412ET 413AL

MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

ACCESS TO EQUIPMENT/COMPONENT Propeller dome Engine forward lift points, engine front top mounts, engine front side mounts, propeller deicing slip rings, propeller brush block, reduction gearbox AC generator, hydraulic pump High pressure compressor speed sensor, fuel pump Pressure regulator and shutoff valve, flow control servo air filter deicing system pressure regulator, deice lines, engine control cables, electrical wiring, bleed air pipe, fuel lines, fire detection loop, hydraulic lines Inspection panels High pressure shutoff valve, oil pressure switch and transmitter, oil pressure regulator, oil tank gauge and filter, electronic control unit, signal conditioner unit fuel filter/heater, low pressure compressor speed sensor, fuel low pressure switch propeller control unit, AC generator, hydraulic pump, oil temperature bulb, hydromechanical fuel control unit

06−41−00

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D AIRCRAFT MAINTENANCE MANUAL

CODE NUMBERS 414AR

TYPE OF ACCESS

415AL, 416AR

417AB

Panels

419AT, 419BT 419CT, 419DT 419EL 419FL 419GL 419JR 419HR 419KR G.

ACCESS TO EQUIPMENT/COMPONENT Starter−generator, fuel flow transmitter, accessory gearbox, total inlet temperature sensor, ignition exciter, engine oil pump, engine oil scavenger pumps, hyrdromechanical fuel control unit, over speed governor and pump Engine hot end, fuel injectors (nozzles), interturbine thermocouples, fire detection loop, engine rear mounts, spark igniters, fuel manifold Oil cooler, oil tank chip detector, total inlet pressure line, ambient pressure orifice, reduction gearbox chip detector, torque compensation system, engine intake Inspection panels Oil cooler door attachments Landing gear attachments Hydraulic service Inspection panel

Right Nacelle − Panels and Doors (1) The list of code numbers for the access panels and doors that are located on the right nacelle are as follows: Refer to Figure 7.

CODE NUMBERS 421AR 422AT

TYPE OF ACCESS

422BT 422CT 422DT

422ET

MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

ACCESS TO EQUIPMENT/COMPONENT Propeller dome Engine forward lift points, engine front top mounts, engine front side mounts, propeller deicing slip rings, propeller brush block, reduction gearbox AC generator, hydraulic pump High pressure compressor speed sensor, fuel pump Pressure regulator and shutoff valve, flow control servo, servo air filter, deicing system pressure regulator, deice lines, engine control cables, electrical wiring, bleed air pipe, fuel lines, fire detection loop, hydraulic lines Inspection panel

06−41−00

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D AIRCRAFT MAINTENANCE MANUAL

CODE NUMBERS 423AL

TYPE OF ACCESS

424AR

425AL, 426AR

Panels

427AB

429AT, 429BT 429CT, 429DT 429EL 429FL 429HL 429KR 429GL 429JL 429LR 429MB H.

ACCESS TO EQUIPMENT/COMPONENT High pressure shutoff valve, oil pressure switch and transmitter, oil pressure regulator, oil tank gauge and filler, oil pressure filter, electronic control unit, signal conditioner unit, fuel filter/heater, low pressure bleed check valve, low pressure compressor speed sensor, fuel low pressure switch, propeller control unit, AC generator, hydraulic pump, oil temperature bulb, hydromechanical fuel control unit Starter−generator, fuel flow transmitter, accessory gearbox, total inlet temperature sensor, ignition exciter, engine oil pump, engine oil scavenger pumps, hydromechanical fuel control unit, over speed governor and pump Engine hot end, fuel injectors (nozzles), intertubine thermocouple, fire detection loop, engine rear mounts, spark ingniters, fuel manifold Oil cooler, oil tank chip detector, total inlet pressure line, ambient pressure orifice, reduction gearbox chip detector torque compensation system, engine intake Inspection panels Inspection panels Oil cooler door attachments Landing gear attachments Landing gear attachments Landing gear attachments Power supply Inspection panel Hydraulic service Fuel service panel

Left Wing − Panels (1) The list of code numbers for the access panels and doors that are located in the left wing (top and bottom) are as follows: Refer to Figure 8.

CODE NUMBERS 511AL

TYPE OF ACCESS

512AL 512BL, 512CL 512DL

MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

ACCESS TO EQUIPMENT/COMPONENT Bleed air line, deice lines, engine control cables, electrical wiring High pressure switch, waste fuel return line, deice lines, electrical wiring, current transformer Landing lights Fuel quantity system disconnect plug, deice lines, electrical wiring

06−41−00

Page 8 Aug 20/2004

D AIRCRAFT MAINTENANCE MANUAL

CODE NUMBERS 513BL 513CL 521AT 522AT 523AT 524AT

TYPE OF ACCESS

524BT 524CT

Panels

525AT 525BB 525CB 525DB, 525EB, 525FB, 525GB 526AB 527AB 528AL 528BL 528CB 531AB 531BB 532AB

532BB 532CB, 532DT 532DB, 532CT 532EB, 532BT 532FB 532AT 541CB, 541DB 541AL, 541BL 542AL, 542BL 542CL, 542DL 542EB, 542FB 542GB 543AL

MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

ACCESS TO EQUIPMENT/COMPONENT Deice lines, electrical wiring Deice lines, electrical wiring Inspection panel Long range fuel tank (if installed) Inspection panel Fuel tank, flow control valve, no flow pressure switch, scavenge ejector pump, fuel quantity probes, auxiliary pump, auxiliary pump pressure switch, fuel low level switch boost ejector pump Fuel tank, fuel quantity probes Fuel tank, surge bay, pressure relief and dump valve, pressure refueling pilot valve, vent float valve, fuel quantity probes Inspection panel Aileron terminal quadrant Flux valve Inspection panel (aileron hinge) Flap track No. 4 Flap track No. 5 Position light Wing tip Inspection panel Ground spoiler actuator, flap screw jack Flap screw jack Fuel emergency shutoff valve, refuel/duffel/transfer shutoff valve, arming valve, flap screw jack, ground spoiler actuator Spoiler position transmitter Inboard roll spoiler actuator Wing spoiler clutch Outboard roll spoiler actuator, flap screw jack Spoiler position transmitter Aileron terminal quadrant Flap track No. 1 and Flap track No. 2 Flap screw jacks and flap attachments Flap screw jacks and flap attachments Flap screw jacks and flap attachments Flap screw jacks and flap attachments Flap track No. 3 Aileron mass balance weights

06−41−00

Page 9 Aug 20/2004

D AIRCRAFT MAINTENANCE MANUAL

CODE NUMBERS 543BL, 543CL, 543DL, 543EL 543FL 543GB 543HB I.

TYPE OF ACCESS

Panels

ACCESS TO EQUIPMENT/COMPONENT Aileron attachments, spring tab lever and spring assembly Aileron attachments Aileron push rod Aileron trim tab push rod

Right Wing − Panels (1) The list of code numbers for the access panels and doors that are located on the right wing (top and bottom) are as follows: Refer to Figure 9.

CODE NUMBERS 611AR

TYPE OF ACCESS

612AR 612BR, 612CR 612DR

Panels

613AR 613DB 613BR, 613CR 622AT 623AT 624AT

Panels

624BT 624CT 625AT 625BB 625BB 625CB 625DB, 625EB 625FB, 625GB 626AB 627AB 628AR

MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

ACCESS TO EQUIPMENT/COMPONENT Bleed air line, deice lines, engine control cables, electrical wiring High pressure switch, waste fuel return line, deice lines, electrical wiring, current transformer Landing lights Fuel quantity system disconnect plug, deice lines, electrical wiring Deice distributor valves, deice water separator, electrical wiring Deice lines, electrical wiring Long range fuel tanks (if installed) Inspection panel Fuel tank, flow control valve, no flow pressure switch, scavenge ejector pump, auxiliary pump pressure switch, fuel low level float switch, boost ejector pump Fuel tank, fuel quantity probes Fuel tank, surge bay pressure relief and dump valve pressure refueling quantity probes Inspection panel Aileron terminal quadrant, aileron position transmitter Aileron terminal quadrant, aileron position transmitter Flux valve Inspection panels (aileron hinge) Inspection panels (aileron hinge) Flap track No. 4 Flap track No. 5 Position light

06−41−00

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D AIRCRAFT MAINTENANCE MANUAL

CODE NUMBERS 628BR 628CB 631AB 631BB 632AB

632BB 632CB 632DT 632DB 632CT 632EB 632BT 632FB 632AT 641CB, 641DB 642AR, 642BR 642CR, 642DR 642EB, 642FB 642GB 643AR 643BR, 643CR 643DR, 643FR 643ER

TYPE OF ACCESS

Panels

ACCESS TO EQUIPMENT/COMPONENT Wing tip Inspection panel Ground spoiler actuator, flap screw jack Flap screw jacks Fuel emergency shutoff valve, refuel/defuel/transfer shutoff valve, pre−check valve, refuel/transfer servo valve, arming valve, flap screw jack, ground spoiler actuator. Spoiler position transmitter Inboard roll spoiler actuator Inboard roll spoiler actuator Wing spoiler clutch Wing spoiler clutch Outboard roll spoiler actuator, flap screw jack Outboard roll spoiler actuator, flap screw jack Spoiler position transmitter Aileron terminal quadrant Flap screw jacks and flap attachments

Panels

643GB 643HB

MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

Flap track No. 3 Aileron mass balance weights Aileron attachments Aileron attachments Aileron trim tab actuator, aileron trim tab position potentiometer Aileron push rod Aileron trim tab push rod

06−41−00

Page 11 Aug 20/2004

D AIRCRAFT MAINTENANCE MANUAL

212BR

111AT

122BR

122AR

112BR

112AR

RIGHT

212AL

212BR

113AL

112AR 111AT

212AL

113AL

121AL

121BL

LEFT

damo641000_001.dg, pt, 01/12/94

111AT

Access Panels and Doors − Front Fuselage Figure 1 MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

06−41−00

Page 12 Aug 27/2002

D AIRCRAFT MAINTENANCE MANUAL

261RL

263AL

263BL 263CL 351AT 262QL 351BT

352AL

352BL

FWD

263DL

352CR 352DR 351BT

263FL

263EL

262RR 351AT 264CR 264BR

261QR

264DR

264AR

132AR

damo641000_002.dg, pt/kms, 04/01/05

FWD

Access Panels and Doors − Center Fuselage Figure 2 MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

06−41−00

Page 13 Mar 20/2005

D AIRCRAFT MAINTENANCE MANUAL

261KT

261LT

261MT

261NT

261HT 261JT FWD

261FT 261GT

261ET

261DT

261AT

261BT

262MT

261CT

262NT

262PT

262RT

262QT

262ST

262LT

262TT 262KT FWD 262JT

262AT

262BT

262CT

262DT

262ET

262FT

262GT

dam0641000_003.dg, pt, 01/12/94

262HT

Access Panels and Doors − Wing/Fuselage Fairing Figure 3 MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

06−41−00

Page 14 Aug 27/2002

D AIRCRAFT MAINTENANCE MANUAL 325AT 325DL 325BT 325EL 322BL 325CT 322CL 322AL 321GT 323AL 322HL 324AL 322JL 324BL 322DL

LEFT SIDE

321FL

323BL

321EL

321HT 321AT

324CL 323CL

321BL

323DL 324DL

321JL 321CL 312AB

NOTE

311BZ 311CZ 311AB 325CT

1

1

1 325BT

325FR

ACCESSIBLE FROM INSIDE TAILCONE

325GR 325AT

323ER

322ER 322FR 321GT

324ER

RIGHT SIDE

322GR

323FR

322HR 321HT

324FR

321AT 323GR 323HR 324GR 324HR

321KR

312AB

311BZ 1

311CZ 1

311AB

dam0641000_004.dg, pt, 02/12/94

321DR

Access Panels and Doors − Vertical Stabilizer, Rear Fuselage Figure 4 MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

06−41−00

Page 15 Aug 27/2002

D FWD

AIRCRAFT MAINTENANCE MANUAL

TOP VIEW

332AT

332BL

325AT

332CL

325BT 325CT 342CR

342BR

342AT

333AL

343AR

333BT

343BT

333CT

343CT 343AAT 343FT 343ET 343DT

333DT 333ET 333FT 333AAT

343BBR

333BBL 333CCT

333YB

333ZB

343CCT

343ZB

343YB

333WB

343WB

333VB

343VB

333AL

343AR

332CL

333BBL

343BBR

BOTTOM VIEW

342CR

342BR

343XB dam0641000_005.dg, pt, 02/12/94

332BL

FWD

333XB

Access Panels and Doors − Horizontal Stabilizer Figure 5 MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

06−41−00

Page 16 Aug 27/2002

D AIRCRAFT MAINTENANCE MANUAL 411AL

412AT 412BT 412CT 412DT 412ET 419AT 419BT

419DT 419CT 419CT

411AL

413AL

417AB

419CT

419DT

419KR

416AR

419JR

419DT

419EL

419FL

412DT 412CT

419HR

419GL

419DT

412BT 412AT

414AR 417AB

411AL

411AL

417AB

dam0641000_006.dg, pt, 02/12/94

412AT 412BT 412CT 412DT 415AL

Access Panels and Doors − Left Nacelle Figure 6 MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

06−41−00

Page 17 Aug 27/2002

D AIRCRAFT MAINTENANCE MANUAL

429DT

429MB

429CT

429DT

421AR

427AB

422CT 422DT

423AL

429EL

425AL

429FL

424AR

421AR

429CT

429HL

429GL

429JL

429DT

422AT 422BT 422CT 422DT 422ET 429AT 429BT

429DT 429CT

dam0641000_007.dg, pt, 02/12/94

421AR

426AR 422DT 422CT 422BT 422AT

429LR 429KR 427AB

422AT 422BT

421AR

427AB

Access Panels and Doors − Right Nacelle Figure 7 MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

06−41−00

Page 18 Aug 27/2002

D AIRCRAFT MAINTENANCE MANUAL

513BL

525AT

524BT

512AL

524AT

512BL 532AT

524CT

513AL

512DL

532BT

542BL 542EB

532DT

FWD

513CL

511AL 522AT

523AT

512CL

521AT

528AL

528BL

543AL 543BL 543CL

543EL

542DL 542FB

1 543DL

1

542AL

543FL

532CT

543HB

525EB

525FB

525DB

1 532EB

543GB

1 532BB

1 532CB

1

1

TOP LEFT

1

1 532DB

541BL

542CL

1

1 532FB

541AL

542GB 1 532AB

531BB

541DB

1

531AB

1 541CB

528BL 528CB

525BB

527AB

526AB

512CL 512BL

513AL 525GB

513BL

513DB

512DL

511AL

512AL

FWD

513CL

NOTE 1

Accessible when flaps are down.

BOTTOM LEFT

dam0641000_008.dg, gw/jc, 22/11/00

528AL 525CB

Access Panels and Doors − Left Wing Figure 8 MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

06−41−00

Page 19 Aug 27/2002

D AIRCRAFT MAINTENANCE MANUAL

FWD

612AR

521AT

625AT

613CR

612BR

611AR 622AT

613BR

624BT

624AT

623AT

612CR

612DR

624CT

613AR

632AT 628AR

628BR

643AR 643BR 641BR

641AR

1

1

632DT

642DR 642FB

642CR

1

631AB

632CT

642AR

1

643CR

643FR

643DR

643HB

625EB

1

1 632BB

642GB

641DB

643ER

1

1

TOP RIGHT

1 631BB

632BT

642BR 642EB

1 632AB

1 632DB

1 632CB

1 632FB

1 632EB

643GB

625FB

625DB

641CB

628BR 628CB

612CR 611AR

626AB

FWD

612BR 612AR

627AB

625BB

613CR

613AR 612DR

613DB

613BR

625GB NOTE

1 BOTTOM RIGHT

ACCESSIBLE WHEN FLAPS ARE DOWN

dam0641000_009.dg, pt/jc, 22/11/00

628AR 625CB

Access Panels and Doors − Right Wing Figure 9 MASTER EFFECTIVITY: See Pageblock 06−41−00 page 1

06−41−00

Page 20 Aug 27/2002

D AIRCRAFT MAINTENANCE MANUAL

**ON A/C ALL ACCESS PANELS AND DOORS (INTERNAL) − DESCRIPTION 1.

2.

General A. This section contains description and location of the access panels that are on the internal surfaces of the aircraft. They include the ceiling and sidewall furnishing panels, overhead storage bins, and furnishing panels on the fixed bulkheads in the passenger compartment and baggage compartment. Description A. Passenger Compartment − Floor Boards (1) The identification code numbers for the floorboards in the passenger compartment (For Pre Modsum 8/2232) are listed in the table below as follows: Refer to Figure 1 (sheet 1 of 2).

CODE NUMBERS 131AZ 131BZ 131CZ

TYPE OF ACCESS

131DZ 131EZ, 131FZ, 131GZ 132AZ, 132BZ, 132CZ 133AZ 133BZ

Floor Boards

133CZ 133DZ 141AZ, 141BZ, 141CZ, 142AZ, 142BZ, 142CZ 143AZ 143BZ, 143CZ

ACCESS TO EQUIPMENT/COMPONENT Inspection panel Inspection panel Deicing system low pressure warning switch, pneumatic lines Recirculated air duct, flight compartment supply duct, door sill drain lines, electrical wiring Roll spoiler cables, rudder cables, elevator cables, flight compartment supply duct, electrical wiring, ATC transponder antenna (131EZ) Rudder cables, elevator cables, elevator trim cables, hydraulic lines, flight compartment supply duct, ATC transponder antenna (132AZ). Electrical wiring Drain line, drain mast, VHF−2 antenna, recirculating fan Attitude heading and reference system (AHRES) units, No. 2 radio altimeter antenna ADF−1 and ADF−2 (if installed) antennas, rudder mixing quadrant Roll spoiler cables, rudder cables, elevator cables, electrical wiring, flight compartment supply duct Rudder cables, elevator cables, elevator trim cables, hydraulic lines, flight compartment supply duct Inspection panel Flight compartment supply duct, recirculated air duct

(2) The identification code numbers for the floorboards in the passenger compartment (For Post Modsum 8/2232) are listed in the table below as follows:

MASTER EFFECTIVITY: See Pageblock 06−43−00 page 1

06−43−00

Page 1 Sep 20/2005

D AIRCRAFT MAINTENANCE MANUAL

Refer to Figure 1 (sheet 2 of 2). CODE NUMBERS 131AZ 131BZ

TYPE OF ACCESS

131CZ 131DZ, 131EZ, 131FZ 132AZ, 132BZ, 132CZ, 132DZ 133AZ 133BZ

Floor Boards

133CZ 133DZ, 133EZ 141AZ, 141BZ 142AZ, 142BZ

143AZ 143BZ B.

ACCESS TO EQUIPMENT/COMPONENT Inspection panel Deicing system low pressure warning switch, pneumatic lines Recirculated air duct, flight compartment supply duct, door sill drain lines, electrical wiring Roll spoiler cables, rudder cables, elevator cables, flight compartment supply duct, electrical wiring, ATC transponder antenna Rudder cables, elevator cables, elevator trim cables, hydraulic lines, flight compartment supply duct, ATC transponder antenna (132AZ). Electrical wiring Drain line, drain mast, VHF−2 antenna, recirculating fan Attitude heading and reference system (AHRES) units, No. 2 radio altimeter antenna ADF−1 and ADF−2 (if installed) antennas, rudder mixing quadrant Roll spoiler cables, rudder cables, elevator cables, electrical wiring, flight compartment supply duct Rudder cables, elevator cables, elevator trim cables, hydraulic lines, flight compartment supply duct Inspection panel Flight compartment supply duct, recirculated air duct

Passenger Compartment − Sidewall Panels (1) The identification code numbers for the sidewall panels in the passenger compartment are listed in the table below as follows: Refer to Figure 2.

CODE NUMBERS 231AZ, 231BZ, 231CZ, 231DZ, 231EZ, 231FZ, 231GZ, 231HZ 231JZ, 231KZ 231LZ, 231MZ 232AZ, 232BZ, 232CZ, 232DZ, 232EZ, 232FZ, 232GZ

TYPE OF ACCESS

MASTER EFFECTIVITY: See Pageblock 06−43−00 page 1

ACCESS TO EQUIPMENT/COMPONENT Insulation, electrical wiring, gasper ducts, engine floodlight (231BZ), ground floodlight (231CZ), hydraulic lines (231HZ) Trim panels Trim panels Insulation, electrical wiring, gasper ducts, ground floodlight (232BZ) hydraulic lines (232FZ)

06−43−00

Page 2 Sep 20/2005

D AIRCRAFT MAINTENANCE MANUAL

CODE NUMBERS 232HZ, 232JZ 232KZ, 232LZ 241AZ, 241BZ, 241CZ, 241DZ 241EZ 242AZ, 242BZ, 242CZ, 242DZ 242EZ 242FZ C.

ACCESS TO EQUIPMENT/COMPONENT Trim panels Trim panels Insulation, electrical wiring, gasper ducts Trim panel Insulation, electrical wiring, gasper ducts Trim panel Trim panel

Passenger Compartment − Ceiling Panels (1) The identification code numbers for the ceiling panels in the passenger compartment are listed in the table below as follows: Refer to Figure 3.

CODE NUMBERS 233AZ, 233BZ, 233CZ, 233DZ 233EZ, 233FZ, 233GZ, 233HZ 233JZ, 233KZ 233LZ, 233MZ 234AZ, 234BZ, 234CZ, 234DZ, 234EZ, 234FZ, 234GZ, 234HZ, 234JZ, 234KZ, 234LZ, 234MZ 235AZ, 235BZ, 235CZ, 235DZ 243AZ, 243BZ, 243CZ, 243DZ, 243EZ, 243FZ, 243GZ 244AZ, 244BZ, 244CZ, 244DZ, 244EZ, 244FZ, 244GZ 245AZ, 245BZ, 245CZ D.

TYPE OF ACCESS Sidewall Panels

TYPE OF ACCESS

ACCESS TO EQUIPMENT/COMPONENT

Passenger service units and trim panels L.H. Gasper ducts, electrical wiring Ceiling Panels Passenger service units and trim panels R.H. Gasper ducts, electrical wiring

Panels

VHF−1 antenna, electrical wiring, emergency lighting panels Passenger service units and trim panels L.H. Gasper ducts, electrical wiring, PA speaker panels

Passenger service units and trim panels R.H. Gasper ducts, electrical wiring

Electrical wiring, emergency lighting panels

Passenger Compartment − Overhead Bins (1) The identification code numbers for the overhead bins in the passenger compartment are listed in the table below as follows: Refer to Figure 3.

MASTER EFFECTIVITY: See Pageblock 06−43−00 page 1

06−43−00

Page 3 Sep 20/2005

D AIRCRAFT MAINTENANCE MANUAL

CODE NUMBER 233AAZ, 233BBZ, 233CCZ, 233DDZ 234AAZ, 234BBZ, 234CCZ, 234DDZ, 234EEZ 243AAZ, 243BBZ, 243CCZ 244AAZ, 244BBZ, 244CCZ E.

TYPE OF ACCESS

Panels

ACCESS TO EQUIPMENT/COMPONENT Gust lock cables, electrical wiring, cabin supply duct Aileron cables, flap cables, electrical wiring, cabin supply duct Gust lock cables, roll spoiler cables, electrical wiring Electrical wiring, cabin supply duct

Baggage Compartment − Floor Boards and Panels (1) The identification code numbers for the floor boards and access panels in the baggage compartment are listed in the table below as follows: Refer to Figure 4.

CODE NUMBER 144AZ 144BZ

TYPE OF ACCESS Floor Boards

144CZ 144DZ, 144EZ, 144FZ, 144GZ 144HZ, 145AZ 145BZ 145CZ 145DZ 251AZ, 251BZ, 251CZ, 251DZ 251EZ

Panels

251FZ 251GZ

251HZ 251JZ, 251KZ 251LZ

MASTER EFFECTIVITY: See Pageblock 06−43−00 page 1

ACCESS TO EQUIPMENT/COMPONENT Under floor panels Recirculated air duct, flight compartment supply duct, duct over temperature switch, duct temperature sensor Elevator control cables, elevator trim control cables, electrical wiring Inspection panels Rudder cables Recirculating air duct, flight compartment supply duct Elevator control cables and trim cable, electrical wiring Inspection panels Trim panels Normal outflow valve, recirculating air duct, electrical wiring Roll spoiler cables, cabin supply duct Roll spoiler cables, cabin supply duct, duct over temperature switch, duct temperature sensor, cabin duct temperature sensor Cabin and flight compartment supply duct, roll spoiler cables, electrical wiring Trim panels Baggage door mechanism

06−43−00

Page 4 Sep 20/2005

D AIRCRAFT MAINTENANCE MANUAL

X 182.00

X 184.15

X 545.00

133AZ

131AZ

132CZ 133BZ 133CZ 132BZ 132AZ

131CZ

131BZ

131EZ

131FZ

142BZ 143AZ 143CZ 133DZ 142AZ 142CZ

131GZ

141AZ

131DZ

X 202.75

141BZ

141CZ

143BZ

X 253.40

X 333.30

X 488.50

X 405.737 X 445.50

X 291.40 FWD

dam0643000_001.dg, pt/gw, 13/07/05

PRE MODSUM 8/2232

Access Panels and Doors − Passenger Compartment Floor Boards Figure 1 (Sheet 1 of 2) MASTER EFFECTIVITY: See Pageblock 06−43−00 page 1

06−43−00

Page 5 Sep 20/2005

D AIRCRAFT MAINTENANCE MANUAL

X 182.00

X 244.10 X 184.15

X 270.57

X 545.00

133CZ

133DZ

133AZ

143AZ

133BZ

131AZ

132AZ 132BZ

132CZ

143BZ 142AZ

132DZ 133EZ

142BZ

131CZ 131DZ

131EZ

141AZ

131FZ

141BZ

131BZ

X 202.75

X 219.60

X 373.67

X 253.40

X 433.77

X 493.87

X 313.57 FWD

dam0643000_002.dg, pt/gw, 13/07/05

POST MODSUM 8/2232

Access Panels and Doors − Passenger Compartment Floor Boards Figure 1 (Sheet 2 of 2) MASTER EFFECTIVITY: See Pageblock 06−43−00 page 1

06−43−00

Page 6 Sep 20/2005

D AIRCRAFT MAINTENANCE MANUAL

232FZ

232DZ

232BZ 232CZ

232AZ

232EZ

242AZ 232GZ

242BZ

242CZ 242DZ

FWD

232HZ

232KZ

232JZ

232LZ

242FZ

242EZ

VIEW ON RIGHT SIDEWALL

241CZ 241DZ

231GZ

241AZ 241BZ

231HZ

231CZ

231EZ 231FZ

231DZ

231AZ 231BZ

241EZ

231MZ

231LZ

231KZ

231JZ

VIEW ON LEFT SIDEWALL

dam0643000_002.dg, pt, 24/11/94

FWD

Access Panels and Doors − Passenger Compartment Sidewall Panels Figure 2 MASTER EFFECTIVITY: See Pageblock 06−43−00 page 1

06−43−00

Page 7 Sep 20/2005

D AIRCRAFT MAINTENANCE MANUAL

234AAZ

234CCZ

234BBZ

234EEZ

234DDZ

244AAZ

244CCZ

244BBZ

FWD

VIEW ON RIGHT SIDE 243CCZ

243BBZ

243AAZ

233DDZ

233CCZ

233AAZ

233BBZ

FWD

VIEW ON LEFT SIDE 234BZ

235CZ

234AZ

234CZ

234EZ

234GZ 234JZ

235DZ 234MZ 244BZ

244CZ 244EZ

244GZ

234LZ 244AZ 245BZ 244DZ 244FZ

234DZ 234FZ 234HZ 234KZ

245CZ

235BZ

FWD 233AZ

233BZ 233CZ

233DZ 233FZ 233HZ 233KZ 233MZ 243AZ 243CZ 243EZ 233EZ

233GZ

233JZ

233LZ

245AZ

243BZ

243DZ

PLAN VIEW

243GZ 243FZ

dam0643000_003.dg, sw/gg, 06/07/05

235AZ

Access Panels and Doors − Passenger Compartment Ceiling Panels Figure 3 MASTER EFFECTIVITY: See Pageblock 06−43−00 page 1

06−43−00

Page 8 Sep 20/2005

D AIRCRAFT MAINTENANCE MANUAL

251BZ 251CZ

251EZ 145CZ

251AZ

251HZ

251DZ 251AZ

145BZ

144CZ 145AZ 144BZ

145DZ 144HZ 1 CL D

FW

144AZ

251KZ

144GZ 144FZ 144EZ 144DZ

1

251FZ (CEIL FWD)

251GZ (CEIL)

251JZ NOTE 1 Under floor panels of 144AZ.

145AZ

Sta. X646.4

144AZ

145BZ

Sta. X600.0

145DZ 144BZ

CL FW

D

dam0643000_004.dg, rt/sw, 17/07/03

251LZ BAGGAGE DOOR

Access Panels and Doors − Baggage Compartment Figure 4 MASTER EFFECTIVITY: See Pageblock 06−43−00 page 1

06−43−00

Page 9 Sep 20/2005