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AMM6-00-00 1.0.0.0GENERAL
1. General
This chapter includes information on dimensions, areas, zoning, etc. and is presented as follows:
Measurements and Figures which show the stations of fuselage frames, wing and stabilizer ribs, etc.
Refer to 6-10-00, pb1.
The method of zoning used on this aircraft. Refer to 6-20-00, pb1.Information on access doors and panels. Refer to 6-30-00, pb1.
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AMM6-10-00 2.0.0.0DIMENSIONS, AREAS AND STATIONS
1. General
Principal dimensions of aircraft. Refer to Figure 1.
Fuselage stations. Refer to Figure 2.
Wing stations. Refer to Figure 3
Empennage stations. Refer to Figure 4. Refer to Figure 5.
The principal areas and volumes are as follows:-
Area Sq.ft. (m2)
Wing (gross) 454.0 42.18Flap (total) 83.3 7.74Horizontal stabilizer (gross) 05.8 9.83Vertical stabilizer (gross, excluding dorsal) 91.4 8.49Aileron (aft of hinge line), per side) 13.7 1.27Aileron (total), per side 17.6 1.64Elevator (aft of hinge line) 27.9 2.59Elevator (total) 39.8 3.70Rudder (aft of hinge line) 26.3 2.44Rudder (total) 35.8 3.33Passenger compartment floor, untrimmed 223.0 20.72
Volume cu.ft. (m3)
Baggage compartment (forward) 45 1.274Baggage compartment (aft) 170 4.814
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Principal DimensionsFigure 1
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Fuselage StationsFigure 2
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Wing StationsFigure 3
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Empennage Stations - Vert. Stab. & RudderFigure 4
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Empennage Stations - Horz. Stab. & ELevatorsFigure 5
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AMM6-20-00 3.0.0.0ZONING
1. General
This section includes a description of the method used in zoning the aircraft and defines the boundaries of the major zones and major sub-zones.
All zones are identified by three-digit numbers. The first digit defines the major zone. The major zones are as follows. Refer to Figure 1
The major sub-zones are identified by the remaining two digits. Refer to Figure 2. Refer to Figure 3. They are defined as follows:-
Major Zone No. Definition
100 Under floor area between fuselage stations -60 and 595200 Above floor area between fuselage nose and station 475300 Empennage. Includes stabilizers, rudder, elevators and tail section
of fuselage aft of station 475.400 Powerplant500 Left wing. Includes flaps, aileron and strut600 Right wing. Includes flaps, aileron and strut700 Landing gear. Includes stub wing800 Doors
Major Sub-zone No. Definition
110 Between fuselage stations -60 and 3121 (122) Between fuselage stations 3 and 74 left (right) but excluding the nose
wheel well which is part of major zone 700.130 Between fuselage stations 74 and 508140 Between fuselage stations 508 and 595210 Between the fuselage nose and fuselage station 3220 Between fuselage stations 3 and 74
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Major ZonesFigure 1
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Major Sub-zones - Fuselage and TailFigure 2
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Major Sub-zone No. Definition
230 Between fuselage stations 74 and 475 and between passenger compartment floor and roof levels
240 Between fuselage stations 74 and the wing centre section front spar frame above the passenger compartment roof
250 Between the wing centre section rear spar frame and fuselage station 475 above the passenger compartment roof
260 Passenger cabin - internal, sub-divided:-261 Station 74 - 146.2262 Station 146.2 - 249.2263 Station 249.2 - 351.9264 Station 351.9 - 475265 Station 475 - 508
311 The fuselage portion of the empennage, aft of station 475312 Aft baggage compartment331 Left horizontal stabilizer332 Left elevator333 Left horizontal stabilizer tip341 Right horizontal stabilizer342 Right elevator343 Right horizontal stabilizer tip351 Vertical stabilizer352 Rudder353 Vertical stabilizer tip410 Accessory bay420 Air intake430 Exhaust440 Nacelle rear fairing450 Nacelle/wing fairing
510 (610) Left (right) wing leading edge to rear spar between aircraft centre line and wing tip root rib
520 (620) Left (right) wing trailing edge aft of rear spar between fuselage side and wing tip root rib
530 (630) Left (right) inner flap540 (640) Left (right) mid flap550 (650) Left (right) outer flap
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560 (660) Left (right) aileron570 (670) Left (right) wing tip580 (680) Left (right) wing strut
710 Nose wheel well and doors720 (730) Right (left) main gear fairing. Includes doors, wheel well and stub wing
810 Nose baggage compartment door820 Crew ditching hatch830 Cargo door
840 (850) Right (left) forward emergency exit860 Right aft emergency exit870 Passenger door880 Aft baggage door
Major Sub-zone No. Definition
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Major Sub-zone - Wings and Tail PlaneFigure 3
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AMM6-30-00 4.0.0.0ACCESS DOORS AND PANELS
1. General
The figures which follow, which taken as a group, identify all access doors and panels throughout the aircraft (both external and internal). Refer to Figure 1.
2. Method of identification
Each access door or panel is identified by a numeric/alpha number. The numeric component of the number is the three digit number which identifies the smallest zone in which the door is located. The two-element alpha suffix designates the location of the door within the zone. The first alpha letter identifies each door within the zone in a logical sequence, i.e. inboard to outboard or front to rear, starting with `A' in each zone. The second alpha letter locates the door in its relationship to the aircraft, as follows:
For example, access door 230ER would be fifth access door aft of frame 74 on the fuselage right side.
T = TopB = BottomL = Left handR = Right handZ = Internal
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Access Panels - Figure IdentificationFigure 1
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Access Panels - Fwd. Baggage Compt.Figure 2
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Access Panels - Flight Compt.Figure 3
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Access Panels - Passenger Compt.Figure 4
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Access Panels - Aft Baggage Compt.Figure 5
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Access Panels - Fwd. Roof FairingFigure 6
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Access Panels - Aft Roof FairingFigure 7
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Access Panels - Power PlantFigure 8
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Access Panels - Centre & Outer WingsFigure 9
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Access Panels - M.L.G Fairings & Stub WingsFigure 10
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Access Panels - Vert. & Horiz StabilizersFigure 11
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Access Panels - FuselageFigure 12
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