DeHav Dash 8 AMM CH06

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06 − Effective Pages 1 * Sep 20/2005 06 − Contents 1 Jun 05/2004 2 Jun 05/2004 3 * Sep 20/2005 06−00−00 1 Nov 25/1999 06−10−00 1 Nov 25/1999 2 Nov 25/1999 3 Aug 27/2002 06−20−00 1 Nov 25/1999 2 Nov 25/1999 3 Aug 27/2002 4 Aug 27/2002 5 Aug 27/2002 6 Aug 27/2002 7 Aug 27/2002 8 Aug 27/2002 9 Aug 27/2002 10 Aug 27/2002 11 Aug 27/2002 06−30−00 1 Nov 25/1999 2 Nov 25/1999 3 Nov 25/1999 4 Nov 25/1999 5 Nov 25/1999 6 Nov 25/1999 7 Nov 25/1999 8 Aug 27/2002 9 Aug 27/2002 10 Aug 27/2002 11 Aug 27/2002 12 Aug 27/2002 13 Aug 27/2002 14 Aug 27/2002 15 Aug 27/2002 16 Aug 27/2002 06−40−00 1 Nov 25/1999 06−41−00 1 Nov 25/1999 2 Mar 20/2005 3 Aug 20/2004 4 Aug 20/2004 5 Aug 20/2004 6 Aug 20/2004 7 Aug 20/2004 8 Aug 20/2004 9 Aug 20/2004 10 Aug 20/2004 11 Aug 20/2004 12 Aug 27/2002 13 Mar 20/2005 14 Aug 27/2002 15 Aug 27/2002 16 Aug 27/2002 17 Aug 27/2002 18 Aug 27/2002 19 Aug 27/2002 20 Aug 27/2002 06−43−00 1 * Sep 20/2005 2 * Sep 20/2005 3 * Sep 20/2005 4 * Sep 20/2005 5 * Sep 20/2005 6 * Sep 20/2005 7 * Sep 20/2005 8 * Sep 20/2005 9 * Sep 20/2005

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AIRCRAFT MAINTENANCE MANUAL

DIMENSIONS AND AREAS LIST OF EFFECTIVE PAGES

Chapter Section

Subject Config Page Date

Chapter Section

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DIMENSIONS AND AREAS 06−00−00

Description and Operation 1

Effectivity: ON A/C ALL

General

DIMENSIONS AND AREAS 06−10−00

General Description

AIRCRAFT STATIONS 06−20−00

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

General Description

Major Zones Major Sub−Zones

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DIMENSIONS AND AREAS TABLE OF CONTENTS

Subject

Chapter Section

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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 Nacelles

4

Sub−Zones/Zones 500 − Left Wing

Sub−Zones/Zones 600 − Right Wing 5

Sub−Zones/Zones 700 − Landing Gear and Doors

6

Sub−Zones/Zones 800 − Doors

ACCESS PANELS AND DOORS 06−40−00

General Description

ACCESS PANELS AND DOORS − EXTERNAL 06−41−00

General Description

Front Fuselage − Panels and Doors

Center Fuselage − Panels 2

Wing/Fuselage − Fairings

Vertical Stabilizer and Aft Fuselage − Panels and Doors

3

Horizontal Stabilizer − Panels 5

Left Nacelle − Panels and Doors 6

Right Nacelle − Panels and Doors 7

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Subject

Chapter Section

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Left Wing − Panels 8

Right Wing − Panels 10

ACCESS PANELS AND DOORS − INTERNAL 06−43−00

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

Panels

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Subject

Chapter Section

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**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.

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**ON A/C ALL

DIMENSIONS AND AREAS − DESCRIPTION

1. General

A. This section contains information on the dimensions and areas of the aircraft when supported on the landing gear.

2. Description Refer to Figure 1. A. Dimensions (1) Overall dimensions Span 85 ft. 0 in. (25.90 m) Length 73 ft. 0.125 in. (22.25 m) *Height 24 ft. 7 in. (7.49 m)

*Propeller ground clearance (static) 3 ft. 0.90 in. (0.94 m) (2) Wings

Root chord 8 ft. 4 in. (2.54 m)

Tip chord 4 ft. 3 in. (1.30 m)

Aspect ratio 12

Incidence 2 degrees

Dihedral 2 1/2 degrees

(3) Horizontal stabilizer and elevators

Span 26 ft. 0 in. (7.93 m)

Aspect ratio 4.489

Incidence +1 degree

Dihedral 0 degrees

(4) Vertical stabilizer and rudders

Height 13 ft. 3 in. (4.04 m)

Aspect ratio 1.155

(5) Fuselage

Width Outside 8 ft. 10 in. (2.69 m)

Inside 8 ft. 2 in. (2.49 m)

Height Outside 8 ft. 5 in. (2.57 m)

Inside 6 ft. 2 in. (1.88 m)

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(6) Landing gear

Longitudinal dimension between main

and nose wheel centers 26 ft. 1 in. (7.95 m)

Main wheel track 25 ft. 10.4 in. (7.88 m)

Nose wheel steering angle High Speed Taxi 14 degrees Slow Speed Taxi 120 degrees (7) Propeller

Diameter 13 ft. 0 in. (3.96 m)

B. Areas

(1) The main areas are as follows:

Wing 585 sq. ft. (54.35 sq. m)

Horizontal stabilizers and elevators 150 sq. ft. (13.94 sq. m) Vertical stabilizer and rudders 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.

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(762 mm) 12 ft. 11 in. (3.94 m) 11 ft. 11 in. * (3.63 m) 37 in. (937 mm) 27 ft. 3 in. (8.28 m) WING SPAN 85 ft. (25.89 m) 77 in. (1.96 m)

DIMENSIONS ARE APPROXIMATE AND MAY VARY DEPENDING ON AIRCRAFT CONFIGURATION AND LOADING CONDITIONS. * DIAMETER 13 ft. (3.96 m) 25 ft. 10 in. (7.88 m) 26 ft. (7.93 m) 10 ft. 5 in. * (3.17 m) 26 ft. 1 in. (7.95 m) LENGTH 73 ft. (22.25 m) 43 in. (1.09 m *) HEIGHT * 24 ft. 7 in. (7.49 m) NOTE: 8 ft. 4 in. (2.54 m) 4 ft. 11 in. (1.50 m) 6 ft. 8 in. (2.03 m) 4 ft 3 in. (1.30 m) 30 in. dam0610000_001.dg, pt, 12/11/94

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Aircraft Dimensions Figure 1

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**ON A/C ALL

AIRCRAFT STATIONS − DESCRIPTION

1. 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.

2. 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

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aircraft centerline (YC 0.00). G. 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).

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WING ORIGIN

NACELLE ORIGIN

BASIC AIRCRAFT AND FUSELAGE ORIGIN

ZW YW XW ZN XN YN ZH XH YH HORIZONTAL STABLIIZER ORIGIN NOTE Z Y Y X dam0620000_001.dg, pt, 24/10/94 Vertical stabilizer is included in fuselage co−ordinate system, X, Y, and Z.

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Aircraft Stations Coordinate System Figure 1

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LIGHTNING DIVERTER STRIPS ( 5 PLACES ) Y 12.500 Y 09.000 Y 09.000 Y 12.500 X 97.000 X 110.000 X 115.359 X 123.000 X 136.800 X 151.600 X 167.000 X 182.000 X 190.900 X 201.150 X 82.660 X 110.300 X 132.020 X 160.500 X 170.400 X 191.000 X 43.000 Z 182.000 Z 163.250 Z 144.000 M. H. B. Z 112.000 FLIGHT DECK FLOOR

Z 100.032 Z 81.000 Z 129.000 M. H. B. Z 112.000 Z 100.440 Z 98.860 PRESSURE BULKHEAD LOWER PRESSURE BULKHEAD UPPER PILOT’S BLKH’D AIRCRAFT Z 64.800 Z 57.000 STATIC GROUND LINE C_L dam0620000_010.dg, pt, 25/10/94 X 66.000

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Fuselage Stations Diagram Figure 2 (Sheet 1 of 3)

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X 202.750 X 215.500 X 222.000 X 234.500 X 240.500 X 242.200 X 253.400 X 259.400 X 262.400 X 264.100 X 270.500 X 291.400 X 312.350 X 333.300 X 354.250 X 370.800 X 377.850 X 384.500 F/S DATUM X 387.350 F/S FRAME DATUM X 405.737 X 201.300 X 222.700 X 252.300 X 252.700 X 282.400 X 302.400 X 342.300 X 355.950 X 366.050 X 376.110 X 396.150 CONTINUED ON SHEET 3 Z 182.000 CEILING Z 174.000 Z 168.300 Z 155.550 STR 16 M. H. B. Z 129.000 Z 100.032 FLOOR LEVEL ( NOMINAL −X 182.000 TO X 545.000) Z 81.000 Z 140.000 STR 13 20.00 30.00 Z 100.300 Z 100.300 Z 98.600 M. B. H. 20.00 2 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 32 31 33 AIRCRAFT DORSAL FIN LH DORSAL TUNNEL SEAT RAILS Z 111.893 Z 143.000 Z 81.000 Y 28.220 Y 9.250 Y 40.950 CL CL CL 53.00 R 62.00 R 20.00 R

Z 102.750 SEAT RAIL OUTBD Z 100.032 FLOOR LEVEL NOMINAL

RH LH

TYPICAL SECTION THROUGH CENTER FUSELAGE. Z 129.000 M. B. H. RH LH Doors dimensions are approximate. NOTE dam0620000_011.dg, pt, 23/11/94 Z 189.00 Z 182.00

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CONTINUED ON SHEET 2 X 426.974 (R/S DATUM) X 434.500 X 445.500 X 467.000 X 488.500 Z 189.000 X 510.000 X 531.500 X 539.000 X 545.000 X 549.500 X 564.500 X 580.500 X 600.000 X 606.000 X 618.000 X 636.000 X 646.445 X 663.445 X 436.500 X 456.500 X 487.500 X 521.000 X 547.500 X 597.500 X 625.500 X 649.897 X 653.349 (SECTION CHANGE BELOW M. B. H.) X 501.000 Z 81.000 Z 181.025 Z 180.367 Z 160.000 Z 141.105 Z 101.842 Z 99.000 50.00 M. B. H. Z 100.00 FLOOR (545.000−X600.00) Z 111.500 FLOOR

MAXIMUM HALF BREATH

X 424.124 (REAR SPAR FRAME DATUM)

Y 42.000 Y 24.050 CL Y 42.000 Y 26.521 Z 174.540 Z 175.750 VIEW LOOKING FWD ON X 387.350 ( SYM ) VIEW LOOKING AFT ON X 424.124 ( SYM ) FRONT SPAR FRAME

FRONT SPAR STRUT

REAR SPAR STRUT

REAR SPAR FRAME

Z 129.000 M. H. B. AIRCRAFT

TYPICAL SECTION AT WING ATTACHMENT FRAMES

Door dimension is approximate.

NOTE

dam0620000_012.dg, pt, 23/11/94

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X 802.123 X 813.823 X 820.104 X 830.203 F/S DATUM X 851.263 MID/S DATUM X 866.154 (XH 0.0) X 867.424 R/S DATUM X 877.123 FORE RUDDER H/L X 898.123 AFT RUDDER X 900.104 X 919.123

AFT RUDDER HINGE (3 PLCS) AFT RUDDER AUX HINGE (2 PLCS) FORE RUDDER HINGE (4 PLCS) FORE RUDDER AUX HINGE (2 PLCS)

X 653.349 X 670.349 X 683.200 X 699.374 X 699.600 X 700.409 X 718.252 X 736.096 X 753.949 X 771.803 X 789.656 X 816.824 FORE RUDDER H/L X 837.824 AFT RUDDER H/L X 858.824 X 861.000

X 646.445 X 663.445 X 699.824 Z 181.025 Z 141.105 Z 101.842 Z 150.000 Z 342.500 (ZH 0.0) Z 335.500 Z 176.500 RIBS (TYP) SKIN STIFFENERS (TYP) RIB 12 RIB 11 RIB 10 RIB 9 RIB 8 RIB 7 RIB 6 RIB 5 RIB 4 RIB 3 RIB 2 RIB 1

FORE RUDDER HINGE LINE AFT RUDDER HINGE LINE

FR No. 4 FR No. 5 FR No. 6 FR No. 7 FR No. 1 FR No. 2 FR No. 3 L/E SPAR RIB 11A dam0620000_013.dg, pt, 09/11/94

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Stabilizer Stations Diagram Figure 3 (Sheet 1 of 2)

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RIB 13 RIB 12 RIB 11 FRONT SPAR RIB 10 RIB 9 RIB 8 RIB 7 RIB 6 RIB 5 RIB 4 RIB 3 RIB 2 RIB 1 MID SPAR YH 0.000 (Y 0.000) YH 6.150 YH 14.000 YH 22.000 YH 30.000 YH 40.000 YH 52.000 YH 64.600 YH 77.500 YH 90.900 YH 105.850 YH 120.800 YH 135.500 YH 139.000 YH 156.000 YH 139.000 YH 132.200 YH 120.700 YH 103.700 YH 100.000 YH 92.200 YH 76.200 TAB HINGES YH 59.000 YH 45.000 YH 31.000 REAR SPAR YH 13.800 AIRCRAFT CL YH 6.000 SPRING TAB YH 64.600 YH 84.000 TRIM TAB YH 135.500 YH 140.200 ELEVATOR HINGES

XH 33.950 XH 28.200 TAB HINGE LINE XH 9.250 ELEVATOR HINGE LINE XH 0.000 (XH 866.154) REAR SPAR XH 20.800 XH 25.050

STR No. 5 STR No. 4 STR No. 3 STR No. 2 STR No. 1

dam0620000_014.dg, pt, 10/11/94

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Stabilizer Stations Diagram Figure 3 (Sheet 2 of 2)

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YW 490.000 YW 474.000 YW 457.000 YW 444.000 YW 423.000 YW 405.000 YW 387.000 YW 369.000 YW 351.000 YW 333.000 YW 326.000 APPROX YW 315.000 YW 297.000 YW 288.000 APPROX YW 279.000 YW 261.000 YW 243.000

YW 510.120 APPROX YW 490.190 YW 475.000 APPROX YW 457.030 YW 423.030 YW 405.650 YW 405.100 APPROX YW 404.650 YW 333.000 YW 327.000 YW 260.975 YW 232.200

XW 13.604 XW 15.485 XW 8.190 WING BOX FLANGED STRINGERS (TYP) FRONT SPAR PLANE O/WING REAR SPAR PLANE CL AILERON HINGE OUTER FLAP FRONT SPAR FLAP STRINGERS (TYP) FLAP RIBS (TYP) GAP IN TRAILING EDGE − 2 PLACES 2 30’ DIHEDRAL FLAP TRACKS 2 PLACES O/WING REF PLANE FUEL SURGE BAY FUEL TANK CONTINUED ON SHEET 2 FWD OUTBD LEFT WING dam0620000_015.dg, pt, 23/11/94

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Wing Stations Diagram Figure 4 (Sheet 1 of 2)

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YW 225.000 YW 207.000 YW 202.000 APPROX YW 189.970 YW 189.000 YW 178.000 APPROX YW 171.400

YW 171.200 (NACELLE) YW 155.200 (YN 0.000) YW 139.200 (NACELLE)

YW 139.000 YW 123.000 YW 106.800 YW 90.600 YW 74.400 YW 58.200 YW 57.000 YW 42.000 YW 23.858 YW 8.680 YW 8.680 YW 23.858 YW 42.000 YW 58.200

YW 224.840 YW 174.000 APPROX YW 172.503 YW 138.700 APPROX YW 106.800 YW 58.200 YW 48.000 APPROX

YW 26.712 YW 26.712 FUEL COLLECTOR BAY X 257.000 (XN 0.000) X 269.360 (XN 12.360) AIRCRAFT CL WING LEADING EDGE X 369.511 X 384.500 FRONT SPAR FRAME − C/WING X 426.974 REAR SPAR PLANE X 469.450 WING TRAILING EDGE INNER FLAP HINGE Y 0.000 XW 9.740 XW 9.740 NACELLE C_L OUTER FLAP HINGE INNER FLAP FRONT SPAR INNER FLAP REAR SPAR SHROUD LINE SHROUD LINE OUTER FLAP REAR SPAR C_L AIRCRAFT CL C/WING REFERENCE PLANE dam0620000_016.dg, pt, 23/11/94 CONTINUED ON SHEET 1 LEFT WING FWD

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Wing Stations Diagram Figure 4 (Sheet 2 of 2)

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XN 121.20 XN 130.60 XN 137.35 XN 146.40 XN 155.30 XN 164.20 XN 100.93 REAR GROUND HANDLING MOUNT PLANE

XN 125.50 XN 134.68 XN 141.95 XN 150.85 XN 159.75 XN 168.87 XN 179.10 XN 182.70 XN 52.90 _{XN 224.76} XN 57.00 XN 64.00 XN 72.00 XN 78.50 XN 98.00 XN 95.00 XN 102.19 XN 107.80 FIRE WALL XN 110.50 XN 117.05 XN 122.00

XN 127.50 WING F/S DATUM XN 169.973 WING R/S DATUM

XN 176.50 XN 182.70 XN 190.00 XN 206.00 XN 197.32 XN 55.00 XN 60.00 XN 68.00 XN 82.70 XN 87.00 XN 75.00 XN 91.00 XN 107.18 LOWER ACCESS COWLING SIDE SUPPORT TUBES CL XN 44.49 XN 24.60 XN 35.564 _{XN 190.00} ZN − 7.00 ENGINE CL NACELLE ORIGIN XN 0.00 (XN 257.00) XN 12.36 ZN 0.00 (Z 171.90) PROPELLER PROPELLER PLANE FRONT LWR MOUNT PLANE CL

MAIN GEAR LEG XN 170.383 (X 427.383) AFT ACCESS PANEL ( BOTH SIDES ) CENTER ACCESS PANEL (BOTH SIDES) ZN 9.5 WING REF. PLANE ZN 24.25 LOWER LONGERON DATUM ZN 0.06 UPPER LONGERON DATUM ZN 15.00 DOOR HINGE LINE Z 57.00

STATIC GROUND LINE

YW 139.200 YW 171.200 NACELLE CL W.R.P. ZN 9.5 ZN 0.00 NACELLE FRAME DRAG STRUT MAIN GEAR LEG

VIEW ON NACELLE FRONT

YN 0.00 (Y155.20) NACELLE CL XN 60.00 XN 64.00 ACCESS DOOR OPENING ACCESS DOOR OPENING

MAIN LANDING GEAR DOOR OPENING

DOOR HINGE LINE − 1 PLC

XN 104.75

DOOR HINGE LINE − 3 PLCS ACCESS DOOR OPENING dam0620000_009.dg, pt, 23/11/94 SIDE VIEW PLAN VIEW

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Nacelle Stations Diagram Figure 5

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**ON A/C ALL

AIRCRAFT ZONES − DESCRIPTION

1. General

A. The aircraft zoning system provides positive identification of areas in the aircraft as follows: – Major zones – Major sub−zones – Zones. 2. Description A. Major Zones Refer to Figure 1.

(1) The aircraft is divided into eight major zones identified as follows:

MAJOR ZONES DESCRIPTION

100 Lower half of the fuselage 200 Upper half of the fuselage

300 Empennage

400 Power plant and nacelles

500 Left wing

600 Right wing

700 Landing gear and landing gear doors

800 Doors

B. 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.

C. 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.

D. Sub−Zones/Zones 100 − Lower Fuselage Refer to Figure 2.

SUB−ZONES/ZONES DESCRIPTION

Major Sub−Zone 110 Radome and nose compartment sta. X43.00 to sta. X110.00

Zone 111 Radome sta. X43.00 to X66.00

Zone 112 Nose compartment R.H. under floor X66.00 to X110.00

Zone 113 Nose compartment L.H. under floor X66.00 to X110.00

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SUB−ZONES/ZONES DESCRIPTION Zone 114 N.L.G. wheel well

Major Sub−Zone 120 Flight compartment, under floor area sta. X110.00 to X182.00

Zone 121 Under floor L.H. Zone 122 Under floor R.H.

Major Sub−Zone 130 Fuselage under floor area sta. X182.00 to X424.12 Zone 131 Under floor cabin L.H.

Zone 132 Under floor cabin R.H. Zone 133 Under floor cabin center

Major Sub−Zone 140 Fuselage, under floor sta. X424.12 to X653.34 (Including pressure dome)

Zone 141 Under floor cabin L.H. Zone 142 Under floor cabin R.H. Zone 143 Under floor cabin center Zone 144 Under floor, rear cargo forward Zone 145 Under floor, rear cargo, rear E. Sub−Zones/Zones 200 − Upper Fuselage

Refer to Figure 3.

Major Sub−Zone 210 Upper fuselage sta. X66.00 to sta. X182.00 Zone 211 Flight compartment, above floor sta. X110.00 to

X182.00

Zone 212 Nose compartment, above floor sta. X 66.00 to X110.00

Major Sub−Zone 220 Fuselage sta. X182.00 to sta. X240.50 Zone 221 Avionics shelves L.H. X182.00 to X199.25

Zone 222 Lavatory R.H. X182.00 to X212.50 (approximately). Zone 223 Wardrobe L.H. X199.25 to X219.25

Zone 224 Galley R.H. X212.50 to X237.50

Zone 225 Electrical boxes L.H. X182.00 to X220.00 (approximately).

Major Sub−Zone 230 Fuselage sta. X182.00 to sta. X424.12 Zone 231 Cabin floor to top of sidewall L.H. Zone 232 Cabin floor to top of sidewall R.H. Zone 234 Cabin roof R.H.

Zone 235 Cabin roof, center

Major Sub−Zone 240 Fuselage sta. X424.12 to sta. X545.50 Zone 241 Cabin floor to top of sidewall L.H. Zone 242 Cabin floor to top of sidewall R.H. Zone 243 Cabin roof L.H.

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SUB−ZONES/ZONES DESCRIPTION Zone 244 Cabin roof R.H.

Zone 245 Cabin roof, center

Major Sub−Zone 250 Fuselage sta. X545.50 to sta. X653.34 (including pressure dome)

Zone 251 Rear baggage compartment Major Sub−Zone 260 Wing−to−fuselage fairings

Zone 261 Forward root fairing, forward of front spar sta. X387.35

Zone 262 Rear root fairings, rear of rear spar sta. X424.12 Zone 263 Left hand root fairing, X387.35 to X424.12 Zone 264 Right hand root fairing, X387.35 to X424.12 F. Sub−Zones/Zones 300 − Empennage

Refer to Figure 4.

Major Sub−Zone 310 Rear fuselage sta. X653.34 to sta. X861.00 Zone 311 Rear fuselage sta. X653.34 to X807.12 Zone 312 Rear fuselage sta. X807.12 to X861.00 Major Sub−Zone 320 Vertical stabilizer and rudder assembly

Zone 321 Vertical stabilizer leading edge

Zone 322 Vertical stabilizer, between front and rear spars (Including trailing edge shroud)

Zone 323 Fore rudder

Zone 324 Trailing rudder

Zone 325 Fairing

Major Sub−Zone 330 Horizontal Stabilizer and elevator assembly L.H. sta. XH 0.00 to XH 33.95

Zone 331 Stabilizer leading edge

Zone 332 Stabilizer between front and rear spar

Zone 333 Elevator

Zone 334 Elevator trim tap Zone 335 Elevator spring tab

Major Sub−Zone 340 Horizontal stabilizer and elevator R.H. sta. XH 0.00 to XH 33.95

Zone 341 Stabilizer leading edge

Zone 342 Stabilizer between front and rears spars

Zone 343 Elevator

Zone 344 Elevator trim tab Zone 345 Elevator spring tab

Major Sub−Zone 350 Dorsal fairing sta. X503.50 to X653.34

Zone 351 Tunnel

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SUB−ZONES/ZONES DESCRIPTION Zone 352 Dorsal fairing

G. Sub−Zones/Zones 400 − Power Plant and Nacelles Refer to Figure 5.

Major Sub−Zone 410 Engine and nacelle L.H.

Zone 411 Propeller

Zone 412 Top structure including area between firewall and wing front spar

Zone 413 Forward side cowling L.H. O/B Zone 414 Forward side cowling R.H. I/B Zone 415 Rear side cowling L.H. O/B Zone 416 Rear side cowling R.H. I/B

Zone 417 Bottom cowling

Zone 418 Engine No. 1

Zone 419 Nacelle rear section including exhaust pipe and shrouds

Major Sub−Zone 420 Engine and nacelle R.H.

Zone 421 Propeller

Zone 422 Top structure including area between firewall and wing front spar

Zone 423 Forward side cowling L.H. O/B Zone 424 Forward side cowling R.H. I/B Zone 425 Rear side cowling L.H. O/B Zone 426 Rear side cowling R.H. I/B

Zone 427 Bottom cowling

Zone 428 Engine No. 2

Zone 429 Nacelle rear section including exhaust pipe and shrouds

H. Sub−Zones/Zones 500 − Left Wing Refer to Figure 6.

Major Sub−Zone 510 Leading edge sta. YW 45.00 to sta. YW 490.00 Zone 511 Area between fuselage and No.1 engine

Zone 512 Area between No. 1 engine and sta. YW288.00 Zone 513 Area between sta. YW 288.00 and YW 490.00 Major Sub−Zone 520 Wing box area sta. YC 00.00 to sta. YW 510.00

Zone 521 Area sta. YC 0.00 to YW 45.00 including No. 1 flap track

Zone 522 Area sta. YW 45.00 to YW 139.00

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Zone 523 Area sta. YW139.00 to YW 171.00 including #2 and #3 flap tracks

Zone 524 Area sta. YW 171.00 to YW 405.00 including #4 and #5 flap tracks

Zone 525 Area sta. YW 405.00 to YW 490.00 Zone 526 Area sta. YW 261.00 − flap track No. 4 Zone 527 Area sta. YW 369.00 − flap track No. 5 Zone 528 Wing tip YW 490.00 to YW 510.00

Major Sub−Zone 530 Trailing edge shroud sta. YW 45.00 to sta. YW 490.00

Zone 531 Area sta. YW 45.00 to YW 139.00 Zone 532 Area sta. YW 171.00 to YW 490.00 Zone 533 Inner ground spoiler

Zone 534 Outer ground spoiler Zone 535 Inner roll spoiler Zone 536 Outer roll spoiler

Major Sub−Zone 540 Wing flaps and ailerons, sta. YW 45.00 to sta. YW 510.00

Zone 541 Flap inboard

Zone 542 Flap outboard

Zone 543 Aileron L.H.

Zone 544 Aileron tab L.H. I. Sub−Zones/Zones 600 − Right Wing

Refer to Figure 7.

Major Sub−Zone 610 Leading edge sta. YW 45.00 to sta. YW 490.00 Zone 611 Area between fuselage and No. 2 engine Zone 612 Area between No. 2 engine and sta. YW 288.00 Zone 613 Area between sta. YW 288.00 and YW 490.00 Major Sub−Zone 620 Area sta. YC 0.00 to YW 510.00

Zone 621 Area sta. YC 0.00 to YW 45.00 including No. 1 flap track

Zone 622 Area sta. YW 45.00 to YW 139.00

Zone 623 Area sta. YW 139.00 to YW 171.00 including No. 2 and 3 flap tracks

Zone 624 Area sta. YW 171.00 to YW 405.00 including No. 4 and 5 flap tracks

Zone 625 Area sta. YW 405.00 to YW 490.00 Zone 626 Area sta. YW 261.00 − flap track No. 4 Zone 627 Area sta. YW 369.00 − flap track No. 5

D

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SUB−ZONES/ZONES DESCRIPTION Zone 628 Wing tip YW 490.00 to YW 510.00

Major Sub−Zone 630 Trailing edge shroud sta. YW 45.00 to sta. YW 490.00

Zone 631 Area sta. YW 45.00 to YW 139.00 Zone 632 Area sta. YW 171.00 to YW 490.00 Zone 633 Inner ground spoiler

Zone 634 Outer ground spoiler Zone 635 Inner roll spoiler Zone 636 Outer roll spoiler

Major Sub−Zone 640 Wing flaps, and ailerons sta. YW 45.00 to sta. YW 501.00

Zone 641 Flap inboard

Zone 642 Flap outboard

Zone 643 Aileron R.H.

Zone 644 Aileron tab R.H. J. Sub−Zones/Zones 700 − Landing Gear and Doors

Refer to Figure 8.

Major Sub−Zone 710 Nose gear and doors

Zone 711 Nose gear

Zone 712 Forward side door R.H. Zone 713 Forward side door L.H.

Zone 714 Rear door R.H.

Zone 715 Rear door L.H.

Major Sub−Zone 720 Main gear and doors L.H.

Zone 721 Main gear

Zone 722 Forward door

Zone 723 Mid door

Major Sub−Zone 730 Main gear and doors R.H.

Zone 731 Main gear

Zone 732 Forward door

Zone 733 Mid door

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

D

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SUB−ZONE/ZONES DESCRIPTION Major Sub−Zone 820 Fuselage doors

Zone 821 Flight compartment escape hatch Zone 822 Emergency exit, fwd. R.H.

Zone 823 Passenger door

Zone 824 Emergency exit, mid R.H. Zone 825 Emergency exit, mid L.H. Zone 826 Baggage compartment door

D

(32)

dam0630000_009.dg, kms, 19/04/96 600 300 500 400 700 700 700 400 800 400 800 800 800 100 800 200 300

D

Major Zones − General Figure 1

(33)

X 110.00 X 182.00 X 424.12 X 545.50 X 653.34 111 114 112 113 122 121 110 120 133 ₁₃₂ 131 130 143 ₁₄₂ 141 140 144 145 X 43.00 X 66.00 dam0630000_001.dg, pt, 23/11/94

D

Zones 100 − Lower Fuselage Figure 2

(34)

PRESSURE BULKHEAD X 110.00 X 66.00 212 211 222 224 221 223 225 232 231 230 234 233 242 241 240 251 250 243 244 235 260 262 264 263 261 X 199.25 X 182.00 X 182.00 X 212.50 X 237.50 X 219.25 X 387.35 X 424.12 X 653.34 220 210 X 182.00 X 424.12 X 545.50 X 110.00 dam0630000_002.dg, pt, 23/11/94 245

D

Zones 200 − Upper Fuselage Figure 3

(35)

340 330 344 345 335 334 343 XH 33.95 XH 0.00 342 332 341 331 XH 0.00 XV 0.00 (X 919.00) 320 325 324 323 322 321 352 351 ₃₅₀ 311 310 312 X 861.00 X 807.12 X 653.34 dam0630000_003.dg, pt, 23/11/94 333

D

Zones 300 − Empennage Figure 4

(36)

422 426 424 423 425 421 428 429 420 427 412 414 416 413 415 418 411 417 419 410 dam0630000_004.dg, pt, 14/11/94

D

Zones 400 − Power Plant and Nacelles Figure 5

(37)

540 544 543 YW 510.00 541 542 530 YW 45.00 533 534 535 536 YW 45.00 YW 139.00 531 YW 171.00 YW 261.00 526 369.00YW 532 YW 405.00 YW 490.00 YW 490.00 YW 510.00 528 525 524 523 522 521 520 511 512 510 513 YW 288.00 YW 139.00 YW 171.00 YW 45.00 YC 0.00 527 YW 490.00 dam0630000_005.dg, pt/kms, 30/04/96

D

Zones 500 − Left Wing Figure 6

(38)

YW 510.00 643 644 640 630 642 641 YW 490.00 632 636 635 634 633 631 YW 510.00 YW 490.00 YW 405.00 YW 369.00 YW 261.00 627 624 626 YW 171.00 YW 139.00 623 622 621 YW 45.00 YC0.00 628 YW 490.00 613 YW288.00 620 612 610 611 YW 45.00 YW 45.00 YW 139.00 625 YW 171.00 dam0630000_006.dg, pt/kms, 30/04/96

D

Zones 600 − Right Wing Figure 7

(39)

734 733 735 730 731 732 714 715 711 710 713 712 724 723 725 721 ₇₂₀ 722 dam0630000_007.dg, pt, 17/11/94

D

Zones 700 − Landing Gear and Landing Gear Doors Figure 8

(40)

820 821 822 824 823 825 826 dam0630000_008.dg, pt, 14/11/94

D

Zones 800 − Doors Figure 9

(41)

**ON A/C ALL

ACCESS PANELS AND DOORS − DESCRIPTION

1. 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). 2. 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.

D

(42)

(43)

**ON A/C ALL

ACCESS PANELS AND DOORS (EXTERNAL) − DESCRIPTION

1. General

A. This section contains description and location of the access panels and doors on the external surfaces of the aircraft.

2. 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 TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT 111AT Radome Weather radar antenna, VOR/Localize antenna,

glide slope antenna 112AR

Panels

Crew oxygen bottle, oxygen lines, nose wheel steering electronic control unit, hydraulic lines 112BR Crew manifold, nose gear doors solenoid sequence

valve, emergency reservoir (main gear extend)

113AL Battery

121AL Brake linkage, rudder control interconnect push rod, rudder input quadrant, rudder pedal adjustment mechanism, rudder control cables

121BL 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 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 122AR Brake linkage, rudder input quadrant, rudder pedal

adjustment mechanism, rudder control cables, rudder restriction mechanism

122BR 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

212AL

Doors

Transformer/rectifier units, pilot’s wiper motor, dc contactor box

212BR Copilot’s wiper motor, flight compartment fan, nose landing light, windshield washer reservoir

D

(44)

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 TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT

132AR Toilet servicing panel

261QR Inspection panels

261RL Inspection panels

262QL Inboard flap track

262RR Inboard flap track

263AL Deicing lines, electrical wiring

263BL & 263CL Brake control valves, hydraulic lines, deice lines, deice line moisture drain plug

263DL Panels Hydraulic lines

263EL, 263FL Fire extinguisher cartage

264AR Deicing lines, electrical wiring

264BR Brake control valve, hydraulic lines, deicing lines, deice line moisture drain plug (elevator)

264CR Landing gear selector valve, hydraulic lines, deice lines 264DR Hydraulic lines 351AT, 351BT, 352AL, 352BL, 352CL, 352CR, 352DR

Bleed air duct, hydraulic lines, deice lines, gust lock cable (elevator)

C. 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.

261AT Inspection panels

261BT Inspection panels

261DT Bleed air pipe, bleed air over temperature switch, deice pressure transducer, deice lines, engine control cables, electrical wiring

261ET Inspection panels

261FT Inspection panels

261GT Engine control cables, bleed air pipe

261HT Inspection panel

261JT Deice isolate valve, engine control cables, bleed air pipe

261KT Inspection panels

D

(45)

261LT Inspection panels

261MT Inspection panels

261NT Bleed air pipe, bleed air over temperature switch, deice pressure transducer, deice lines, engine control cables, electrical wiring

262AT Spoiler splitter clutch quadrant, flap drive shaft, aileron and spoiler control cables, fuel line, hydraulic lines, ground spoiler selector solenoid valves

262BT Panels Inspection panel

262CT Inspection panel

262DT Fire extinguisher bottles, fire extinguisher discharge cartridges, fire extinguisher distribution lines,

hydraulic lines

262ET Inspection panel

262FT Inspection panel

262GT Inspection panel

262HT Inspection panel

262JT Bleed air pipe, aileron and spoiler control cables 262KT Bleed air pipe, gust lock control cables

262LT Flap power unit, aileron splitter quadrant, flap drive shaft, aileron and spoiler

262MT Inspection panel

262NT Inspection panel

262PT Hydraulic lines, fuel lines, deice lines

262QT Inspection panel

262RT Inspection panel

262ST Inspection panel

262TT Inspection panel

D. 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.

D

(46)

CODE NUMBERS TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT 311AB 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

311BZ Inspection panels

311CB Inspection panels

312AB Inspection panels

321AT Emergency locator transmitter

321BL Inspection panel

321CL Bleed air duct, hydraulic lines, deice lines, gust lock cable

321DR Bleed air duct, hydraulic lines, deice lines, gust lock cable

321EL Inspection panel

321FL Deice lines

321GT Panels Deice lines

321HT Inspection panels

321JL Inspection panels

321KR Inspection panels

322AL Elevator trim quadrants, elevator trim cables 322ER Elevator trim quadrants, elevator trim cables

322BL Inspection panels

322CL Inspection panels

322FR Inspection panels

322DL Rudder actuators, yaw damper, rudder control

cables

322HR Rudder actuators, yaw damper, rudder control

cables

322GR Rudder pulley quadrant, rudder control cables 322HL Rudder pulley quadrant, rudder control cables 322JL Rudder pulley quadrant, rudder control cables

323AL, 323BL Fore rudder attachments

323CL, 323DL Fore rudder attachments

323ER, 323FR Fore rudder attachments

323GR, 323HR Fore rudder attachments

D

(47)

324AL, 324BL Trailing rudder attachments

324CL, 324DL Trailing rudder attachments

324ER, 324FR Panels Trailing rudder attachments

324GR, 324HR Trailing rudder attachments

325DL, 325EL Inspection panels

325FR, 325GR Inspection panels

325AT Anti collision light, deice lines, electrical wiring

325BT Inspection panel

325CT Elevator gust lock

E. 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 TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT 325AT Anti collision light, deice lines, electrical wiring

325BT Inspection panel

325CT Elevator gust lock

332AT Elevator trim tab actuator, elevator trim position transmitter, elevator trim chain/cable

332BL Deice lines

332CL Deice lines

333AL Elevator mass balance, elevator horn heat

333BT Elevator attachments

333CT Panels Elevator attachments

333DT Elevator trim tab actuator attachments

333ET Elevator attachments

333FT Elevator attachments

333VB Elevator attachments

333WB Elevator attachments

333XB Elevator trim tab actuator attachments

333YB Elevator trim tab actuator attachments

333BBL Elevator spring tab mechanism

333CCT Elevator spring tab mechanism

342AT Elevator trim tab actuator, elevator trim position transmitter, elevator trim chain/cable

342BR Deice lines

342CR Deice lines

343AR Elevator mass balance, elevator horn heat

343BT Elevator attachments

D

(48)

343CT Panels Elevator attachments

343DT Elevator trim tab actuator attachments

343ET Elevator attachments

343FT Elevator attachments

343VB Elevator attachments

343WB Elevator attachments

343XB Elevator trim tab actuator attachments

343YB Elevator trim tab actuator attachments

343ZB Elevator spring tab attachments

343AAT Elevator spring tab attachments

343BBR Elevator spring tab attachments

343CCT Elevator spring tab attachments

F. 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.

411AL Propeller dome

412AT Engine forward lift points, engine front top mounts, engine front side mounts, propeller deicing slip rings, propeller brush block, reduction gearbox

412BT Panels AC generator, hydraulic pump

412CT High pressure compressor speed sensor, fuel

pump

412DT 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

412ET Inspection panels

413AL 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

D

(49)

414AR 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

415AL, 416AR Engine hot end, fuel injectors (nozzles), interturbine thermocouples, fire detection loop, engine rear mounts, spark igniters, fuel manifold 417AB Panels Oil cooler, oil tank chip detector, total inlet

pressure line, ambient pressure orifice, reduction gearbox chip detector, torque compensation system, engine intake

419AT, 419BT Inspection panels

419CT, 419DT

419EL Oil cooler door attachments

419FL

419GL Landing gear attachments

419JR

419HR Hydraulic service

419KR Inspection panel

G. 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.

421AR Propeller dome

422AT Engine forward lift points, engine front top mounts, engine front side mounts, propeller deicing slip rings, propeller brush block, reduction gearbox

422BT AC generator, hydraulic pump

422CT High pressure compressor speed sensor, fuel

pump

422DT 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

422ET Inspection panel

D

(50)

423AL 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

424AR 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

425AL, 426AR Panels Engine hot end, fuel injectors (nozzles), intertubine thermocouple, fire detection loop, engine rear mounts, spark ingniters, fuel manifold

427AB Oil cooler, oil tank chip detector, total inlet

pressure line, ambient pressure orifice, reduction gearbox chip detector torque compensation system, engine intake

429AT, 429BT Inspection panels

429CT, 429DT Inspection panels

429EL Oil cooler door attachments

429FL Landing gear attachments

429HL Landing gear attachments

429KR Landing gear attachments

429GL Power supply

429JL Inspection panel

429LR Hydraulic service

429MB Fuel service panel

H. 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 TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT 511AL Bleed air line, deice lines, engine control cables,

electrical wiring

512AL High pressure switch, waste fuel return line, deice lines, electrical wiring, current transformer

512BL, 512CL Landing lights

512DL Fuel quantity system disconnect plug, deice lines,

electrical wiring

D

(51)

513BL Deice lines, electrical wiring

513CL Deice lines, electrical wiring

521AT Inspection panel

522AT Long range fuel tank (if installed)

524AT 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

524BT Panels Fuel tank, fuel quantity probes

524CT Fuel tank, surge bay, pressure relief and dump

valve, pressure refueling pilot valve, vent float valve, fuel quantity probes

525BB Aileron terminal quadrant

525CB Flux valve

525DB, 525EB, 525FB, 525GB

Inspection panel (aileron hinge)

526AB Flap track No. 4

528AL Position light

528BL Wing tip

528CB Inspection panel

531AB Ground spoiler actuator, flap screw jack

531BB Flap screw jack

532AB Fuel emergency shutoff valve,

refuel/duffel/transfer shutoff valve, arming valve, flap screw jack, ground spoiler actuator

532BB Spoiler position transmitter

532CB, 532DT Inboard roll spoiler actuator

532DB, 532CT Wing spoiler clutch

532EB, 532BT Outboard roll spoiler actuator, flap screw jack

532FB Spoiler position transmitter

532AT Aileron terminal quadrant

541CB, 541DB Flap track No. 1 and Flap track No. 2

541AL, 541BL Flap screw jacks and flap attachments

542AL, 542BL Flap screw jacks and flap attachments

542CL, 542DL Flap screw jacks and flap attachments

542EB, 542FB Flap screw jacks and flap attachments

542GB Flap track No. 3

543AL Aileron mass balance weights

D

(52)

CODE NUMBERS TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT 543BL, 543CL,

543DL, 543EL

Aileron attachments, spring tab lever and spring assembly

543FL Aileron attachments

543GB Panels Aileron push rod

543HB Aileron trim tab push rod

I. 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 TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT 611AR Bleed air line, deice lines, engine control cables,

electrical wiring

612AR High pressure switch, waste fuel return line, deice lines, electrical wiring, current transformer

612BR, 612CR Landing lights

612DR Panels Fuel quantity system disconnect plug, deice lines, electrical wiring

613AR Deice distributor valves, deice water separator,

electrical wiring 613DB

613BR, 613CR Deice lines, electrical wiring

622AT Long range fuel tanks (if installed)

623AT Panels Inspection panel

624AT Fuel tank, flow control valve, no flow pressure

switch, scavenge ejector pump, auxiliary pump pressure switch, fuel low level float switch, boost ejector pump

624BT Fuel tank, fuel quantity probes

624CT Fuel tank, surge bay pressure relief and dump

valve pressure refueling quantity probes

625BB Aileron terminal quadrant, aileron position

transmitter

625BB Aileron terminal quadrant, aileron position

transmitter

625CB Flux valve

625DB, 625EB Inspection panels (aileron hinge)

625FB, 625GB Inspection panels (aileron hinge)

628AR Position light

D

(53)

628BR Wing tip

628CB Inspection panel

631AB Ground spoiler actuator, flap screw jack

631BB Panels Flap screw jacks

632AB Fuel emergency shutoff valve,

refuel/defuel/transfer shutoff valve, pre−check valve, refuel/transfer servo valve, arming valve, flap screw jack, ground spoiler actuator.

632BB Spoiler position transmitter

632CB Inboard roll spoiler actuator

632DT Inboard roll spoiler actuator

632DB Wing spoiler clutch

632CT Wing spoiler clutch

632EB Outboard roll spoiler actuator, flap screw jack

632BT Outboard roll spoiler actuator, flap screw jack

632FB Spoiler position transmitter

632AT Aileron terminal quadrant

641CB, 641DB

642AR, 642BR Flap screw jacks and flap attachments

642CR, 642DR 642EB, 642FB

642GB Flap track No. 3

643AR Aileron mass balance weights

643BR, 643CR Aileron attachments

643DR, 643FR Aileron attachments

643ER Panels Aileron trim tab actuator, aileron trim tab position potentiometer

643GB Aileron push rod

643HB Aileron trim tab push rod

D

(54)

212BR 111AT 122BR 122AR 112BR 112AR 212BR 112AR 111AT 113AL 212AL 212AL 111AT 113AL 121AL 121BL RIGHT LEFT _{damo641000_001.dg, pt, 01/12/94}

D

Access Panels and Doors − Front Fuselage Figure 1

(55)

261RL 263AL 263BL 263CL 263DL 262QL 351BT 352AL 352BL 263EL 263FL 352CR 352DR 351BT 262RR 264DR 264CR 264BR 264AR 261QR 132AR FWD FWD d amo641000_002.dg, pt/kms, 04/01/05 351AT 351AT

D

Access Panels and Doors − Center Fuselage Figure 2

(56)

261KT 261LT 261MT 261NT 261HT 261FT 261ET 261AT 261BT 261CT 261DT 261JT 261GT 262MT 262NT 262PT 262QT 262RT 262ST 262LT 262JT 262AT 262BT 262CT 262DT 262ET 262FT 262GT 262HT 262KT 262TT dam0641000_003.dg, pt, 01/12/94 FWD FWD

D

Access Panels and Doors − Wing/Fuselage Fairing Figure 3

(57)

325AT 322AL 322BL 322CL 321GT 322HL 322JL 322DL 321FL 321EL 321HT 321AT 321BL 321CL 325DL 325BT 325EL 325CT 323AL 324AL 324BL 323BL 324CL 323CL 323DL 324DL 312AB 311BZ 311CZ

311AB ACCESSIBLE FROM_{INSIDE TAILCONE} 325CT 325FR 323ER 324ER 323FR 324FR 323GR 323HR 324GR 324HR 312AB 311BZ 311CZ 311AB 321HT 321AT 321KR 321DR 325BT _325GR 325AT 322ER 322FR 321GT 322GR 322HR 1 321JL 1 1 1 1 dam0641000_004.dg, pt, 02/12/94 LEFT SIDE RIGHT SIDE NOTE

D

Access Panels and Doors − Vertical Stabilizer, Rear Fuselage Figure 4

(58)

332AT 332BL 332CL 325AT 325BT 325CT342CR 342BR _342AT 343AR 343BT 343CT 333AL 333BT 333CT 333DT 333ET 333FT 333BBL 333AAT 333CCT 343BBR 343AAT 343FT 343ET 343DT 333YB 333ZB 343ZB 343YB 333AL 333VB 333WB 333XB _332BL 332CL _333BBL _343BBR 342CR 342BR 343XB 343WB 343VB 343AR 343CCT TOP VIEW BOTTOM VIEW FWD FWD dam0641000_005.dg, pt, 02/12/94

D

Access Panels and Doors − Horizontal Stabilizer Figure 5

(59)

419DT 417AB 411AL 412AT 412BT 413AL 412CT 412DT 415AL 419DT 419CT

411AL 417AB 419EL 419FL 419GL

419CT

419DT 419KR 419JR 419HR 417AB 411AL 416AR 412DT 412CT

414AR

412BT 412AT 411AL 412AT 412BT 412CT 412DT 412ET 419AT 419BT

419CT 419DT

dam0641000_006.dg, pt, 02/12/94

D

Access Panels and Doors − Left Nacelle Figure 6

(60)

dam0641000_007.dg, pt, 02/12/94 422AT 422BT 424AR 422DT 422CT 426AR 429DT 429CT 421AR 427AB 429LR 429KR 429CT 429DT 429JL 429EL 429FL 427AB 421AR 425AL 422DT 422CT 423AL 422BT 422AT 429DT 427AB 421AR

421AR 422AT 422BT 422CT 422DT 422ET 429AT 429BT

429CT 429DT 429MB 429GL 429HL

D

Access Panels and Doors − Right Nacelle Figure 7

(61)

525AT 513BL 513AL 524AT 512AL 513CL 532AT 524CT 524BT 512DL 512CL 512BL 528AL 528BL 543AL 543BL 543DL 543EL 543FL 543CL 532BT 542AL 542BL 542EB 532CT 1 1 532DT 542CL 542DL 542FB 541AL 541BL 1 1 523AT 511AL 522AT 521AT 525BB 532EB 532CB 525CB 532FB 532DB 532BB 532AB 542GB 525DB 528CB 528BL 528AL 525EB 513CL 525FB 525GB 513BL 527AB 513AL 513DB 526AB 512DL 512CL 512BL 512AL 511AL 541DB 531BB 541CB 543GB 543HB 531AB 1 1 1 1 1 1 1 1 dam0641000_008.dg, gw/jc, 22/11/00 FWD FWD BOTTOM LEFT TOP LEFT 1 1 NOTE

1 Accessible when flaps are down.

D

Access Panels and Doors − Left Wing Figure 8

(62)

ACCESSIBLE WHEN FLAPS ARE DOWN dam0641000_009.dg, pt/jc, 22/11/00

625AT 613BR 613AR 624AT 612AR 613CR 632AT 624CT 624BT 612DR 612CR 612BR 628AR 628BR 643AR 643BR 643DR 643ER 643FR 643CR 632BT 642AR 642BR 642EB 632CT 1 1 632DT 642CR 642DR 642FB 641AR 641BR 1 1 623AT 611AR 622AT 521AT 625BB 632EB 632CB 625CB 632FB 632DB 632BB 632AB 642GB 625DB 628CB 628BR 628AR 625EB 613CR 625FB 625GB 613BR 627AB 613AR 613DB 626AB 612DR 612CR 612BR 612AR 611AR 641DB 631BB 641CB 643GB 643HB 631AB 1 1 1 1 1 1 1 1 FWD FWD BOTTOM RIGHT TOP RIGHT 1 1 1 NOTE

D

Access Panels and Doors − Right Wing Figure 9

(63)

**ON A/C ALL

ACCESS PANELS AND DOORS (INTERNAL) − DESCRIPTION

1. 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.

2. 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).

131AZ Inspection panel

131BZ Inspection panel

131CZ Deicing system low pressure warning switch,

pneumatic lines

131DZ Recirculated air duct, flight compartment supply

duct, door sill drain lines, electrical wiring 131EZ, 131FZ,

131GZ

Roll spoiler cables, rudder cables, elevator cables, flight compartment supply duct, electrical wiring, ATC transponder antenna (131EZ)

132AZ, 132BZ, 132CZ

Rudder cables, elevator cables, elevator trim cables, hydraulic lines, flight compartment supply duct, ATC transponder antenna (132AZ).

133AZ Floor Boards Electrical wiring

133BZ Drain line, drain mast, VHF−2 antenna,

recirculating fan

133CZ Attitude heading and reference system (AHRES)

units, No. 2 radio altimeter antenna

133DZ ADF−1 and ADF−2 (if installed) antennas, rudder

mixing quadrant 141AZ, 141BZ,

141CZ,

Roll spoiler cables, rudder cables, elevator cables, electrical wiring, flight compartment supply duct 142AZ, 142BZ,

142CZ

Rudder cables, elevator cables, elevator trim cables, hydraulic lines, flight compartment supply duct

143BZ, 143CZ 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:

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Refer to Figure 1 (sheet 2 of 2).

131BZ Deicing system low pressure warning switch,

pneumatic lines

131CZ Recirculated air duct, flight compartment supply

duct, door sill drain lines, electrical wiring 131DZ, 131EZ,

131FZ

Roll spoiler cables, rudder cables, elevator cables, flight compartment supply duct, electrical wiring, ATC transponder antenna

132AZ, 132BZ, 132CZ, 132DZ

Rudder cables, elevator cables, elevator trim cables, hydraulic lines, flight compartment supply duct, ATC transponder antenna (132AZ).

133AZ Floor Boards Electrical wiring

133BZ Drain line, drain mast, VHF−2 antenna,

recirculating fan

133CZ Attitude heading and reference system (AHRES)

units, No. 2 radio altimeter antenna

133DZ, 133EZ ADF−1 and ADF−2 (if installed) antennas, rudder mixing quadrant

141AZ, 141BZ Roll spoiler cables, rudder cables, elevator cables, electrical wiring, flight compartment supply duct 142AZ, 142BZ Rudder cables, elevator cables, elevator trim

cables, hydraulic lines, flight compartment supply duct

143BZ Flight compartment supply duct, recirculated air

duct B. 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 TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT 231AZ, 231BZ,

231CZ, 231DZ, 231EZ, 231FZ, 231GZ, 231HZ

Insulation, electrical wiring, gasper ducts, engine floodlight (231BZ), ground floodlight (231CZ), hydraulic lines (231HZ) 231JZ, 231KZ Trim panels 231LZ, 231MZ Trim panels 232AZ, 232BZ, 232CZ, 232DZ, 232EZ, 232FZ, 232GZ

Insulation, electrical wiring, gasper ducts, ground floodlight (232BZ) hydraulic lines (232FZ)

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CODE NUMBERS TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT 232HZ, 232JZ Sidewall Panels Trim panels

232KZ, 232LZ Trim panels

241AZ, 241BZ, 241CZ, 241DZ

Insulation, electrical wiring, gasper ducts

241EZ Trim panel

242AZ, 242BZ, 242CZ, 242DZ

Insulation, electrical wiring, gasper ducts

242EZ Trim panel

242FZ Trim panel

C. 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 TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT 233AZ, 233BZ,

233CZ, 233DZ 233EZ, 233FZ, 233GZ, 233HZ

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

233JZ, 233KZ Ceiling Panels 233LZ, 233MZ 234AZ, 234BZ, 234CZ, 234DZ, 234EZ, 234FZ, 234GZ, 234HZ, 234JZ, 234KZ, 234LZ, 234MZ

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

235AZ, 235BZ, 235CZ, 235DZ

VHF−1 antenna, electrical wiring, emergency lighting panels

243AZ, 243BZ, 243CZ, 243DZ, 243EZ, 243FZ,

243GZ

Panels Passenger service units and trim panels L.H. Gasper ducts, electrical wiring, PA speaker panels

244AZ, 244BZ, 244CZ, 244DZ, 244EZ, 244FZ,

244GZ

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

245AZ, 245BZ, 245CZ

Electrical wiring, emergency lighting panels

D. 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.

D

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CODE NUMBER TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT 233AAZ, 233BBZ,

233CCZ, 233DDZ

Gust lock cables, electrical wiring, cabin supply duct

234AAZ, 234BBZ, 234CCZ, 234DDZ,

234EEZ

Panels Aileron cables, flap cables, electrical wiring, cabin supply duct

243AAZ, 243BBZ, 243CCZ

Gust lock cables, roll spoiler cables, electrical wiring

244AAZ, 244BBZ, 244CCZ

Electrical wiring, cabin supply duct

E. 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 TYPE OF ACCESS ACCESS TO EQUIPMENT/COMPONENT

144AZ Under floor panels

144BZ Floor Boards Recirculated air duct, flight compartment supply duct, duct over temperature switch, duct

temperature sensor

144CZ Elevator control cables, elevator trim control

cables, electrical wiring 144DZ, 144EZ,

144FZ, 144GZ

Inspection panels

144HZ, 145AZ Rudder cables

145BZ Recirculating air duct, flight compartment supply

duct

145CZ Elevator control cables and trim cable, electrical wiring

145DZ Panels Inspection panels

251AZ, 251BZ, 251CZ, 251DZ

Trim panels

251EZ Normal outflow valve, recirculating air duct,

electrical wiring

251FZ Roll spoiler cables, cabin supply duct

251GZ Roll spoiler cables, cabin supply duct, duct over

temperature switch, duct temperature sensor, cabin duct temperature sensor

251HZ Cabin and flight compartment supply duct, roll

spoiler cables, electrical wiring

251JZ, 251KZ Trim panels

251LZ Baggage door mechanism

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131CZ 131DZ 131EZ 131FZ 131GZ 141AZ 141BZ 141CZ 133AZ 133BZ 132AZ 133CZ 132BZ 132CZ 133DZ 143AZ 142AZ 142BZ 143BZ 142CZ 143CZ X 182.00 X 545.00 X 202.75 X 253.40 X 291.40 X 333.30 X 405.737 X 445.50 X 488.50 d am0643000_001.dg, pt/gw, 13/07/05 131AZ 131BZ FWD X 184.15 PRE MODSUM 8/2232

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Access Panels and Doors − Passenger Compartment Floor Boards Figure 1 (Sheet 1 of 2)

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141AZ 133AZ 133BZ 132AZ 143AZ 142AZ X 182.00 X 545.00 X 202.75 X 253.40 d am0643000_002.dg, pt/gw, 13/07/05 131AZ FWD X 184.15 POST MODSUM 8/2232 141BZ 143BZ 142BZ 133EZ 132DZ 132CZ X 270.57 132BZ 133CZ 131EZ 131FZ X 433.77 X 493.87 X 219.60 131CZ 131BZ 131DZ X 244.10 133DZ X 313.57 X 373.67

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Access Panels and Doors − Passenger Compartment Floor Boards Figure 1 (Sheet 2 of 2)

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FWD FWD 232AZ 232BZ 232CZ 232DZ 232EZ 232FZ 232GZ 242AZ 242BZ 242CZ 242DZ 232HZ 232JZ 232KZ 232LZ 242EZ 242FZ 241DZ 241CZ 241BZ 241AZ 231HZ 231GZ 231FZ 231EZ 231CZ 231BZ 231AZ 241EZ 231MZ 231LZ 231KZ 231JZ

VIEW ON RIGHT SIDEWALL

VIEW ON LEFT SIDEWALL

231DZ

dam0643000_002.dg, pt, 24/11/94

D

Access Panels and Doors − Passenger Compartment Sidewall Panels Figure 2

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FWD

VIEW ON RIGHT SIDE

VIEW ON LEFT SIDE

PLAN VIEW

234AAZ 234BBZ 234CCZ 234DDZ 234EEZ 244AAZ 244BBZ 244CCZ

243CCZ 243BBZ 243AAZ 233DDZ 233CCZ 233BBZ 233AAZ 235BZ 234AZ 234BZ 234CZ 235CZ 234DZ 234EZ 234FZ 234GZ 234HZ 234JZ 235DZ 234KZ 234LZ 234MZ 244AZ 244BZ 245BZ 244CZ 244DZ 244EZ 244FZ 244GZ 245CZ

233AZ 233CZ 233EZ 233GZ 233JZ 233LZ 245AZ

243AZ 243CZ 243EZ 243GZ 233BZ 233DZ 233FZ 233HZ 233KZ 233MZ 243BZ 243DZ 243FZ dam0643000_003.dg, sw/gg, 06/07/05 235AZ

D

Access Panels and Doors − Passenger Compartment Ceiling Panels Figure 3

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NOTE

1 Under floor panels of 144AZ. 144AZ 144GZ 144FZ 144EZ 144DZ 1 144HZ 145BZ 251HZ 145CZ 251EZ 251BZ 251CZ 251DZ 144CZ 251AZ 1 C_L 251GZ (CEIL) 145AZ 251KZ 251FZ (CEIL FWD) 251JZ 251LZ BAGGAGE DOOR 144AZ 144BZ 145DZ 145BZ Sta. X646.4 Sta. X600.0 _C L FWD 144BZ 251AZ 145AZ 145DZ FWD dam0643000_004.dg, rt/sw, 17/07/03

D

Access Panels and Doors − Baggage Compartment Figure 4

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