SD3-60 AIRCRAFT MAINTENANCE MANUAL. This chapter includes information on dimensions, areas, zoning, etc. and is presented as follows:

Transcription

1 AMM GENERAL 1. General This chapter includes information on dimensions, areas, oning, etc. and is presented as follows: Measurements and Figures which show the stations of fuselage frames, wing and stabilier ribs, etc. The method of oning used on this aircraft. Information on access doors and panels. Refer to , pb1. Refer to , pb1. Refer to , pb Page 1

2 AMM DIMENSIONS, 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. (m 2 ) Wing (gross) Flap (total) Horiontal stabilier (gross) Vertical stabilier (gross, excluding dorsal) Aileron (aft of hinge line), per side) Aileron (total), per side Elevator (aft of hinge line) Elevator (total) Rudder (aft of hinge line) Rudder (total) Passenger compartment floor, untrimmed Volume cu.ft. (m 3 ) Baggage compartment (forward) Baggage compartment (aft) Page 1

3 SD3-60 AIRCRAFT MAINTENANCE MANUAL Principal Dimensions Figure Page 2

4 Fuselage Stations Figure Page 3

5 SD3-60 AIRCRAFT MAINTENANCE MANUAL Wing Stations Figure Page 4

6 Empennage Stations - Vert. Stab. & Rudder Figure Page 5

7 SD3-60 AIRCRAFT MAINTENANCE MANUAL Empennage Stations - Hor. Stab. & ELevators Figure Page 6

8 AMM ZONING 1. General This section includes a description of the method used in oning the aircraft and defines the boundaries of the major ones and major sub-ones. ones are identified by three-digit numbers. The first digit defines the major one. The major ones are as follows. Refer to Figure 1 Major Zone No. Definition 100 Under floor area between fuselage stations -60 and Above floor area between fuselage nose and station Empennage. Includes stabiliers, rudder, elevators and tail section of fuselage aft of station Powerplant 500 Left wing. Includes flaps, aileron and strut 600 Right wing. Includes flaps, aileron and strut 700 Landing gear. Includes stub wing 800 Doors The major sub-ones are identified by the remaining two digits. Refer to Figure 2. Refer to Figure 3. They are defined as follows:- Major Sub-one No. Definition 110 Between fuselage stations -60 and (122) Between fuselage stations 3 and 74 left (right) but excluding the nose wheel well which is part of major one Between fuselage stations 74 and Between fuselage stations 508 and Between the fuselage nose and fuselage station Between fuselage stations 3 and Page 1

9 SD3-60 AIRCRAFT MAINTENANCE MANUAL Major Zones Figure Page 2

10 Major Sub-ones - Fuselage and Tail Figure Page 3

11 SD3-60 AIRCRAFT MAINTENANCE MANUAL Major Sub-one 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 Station Station Station Station The fuselage portion of the empennage, aft of station Aft baggage compartment 331 Left horiontal stabilier 332 Left elevator 333 Left horiontal stabilier tip 341 Right horiontal stabilier 342 Right elevator 343 Right horiontal stabilier tip 351 Vertical stabilier 352 Rudder 353 Vertical stabilier tip 410 Accessory bay 420 Air intake 430 Exhaust 440 Nacelle rear fairing 450 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 flap 540 (640) Left (right) mid flap 550 (650) Left (right) outer flap Page 4

12 Major Sub-one No. Definition 560 (660) Left (right) aileron 570 (670) Left (right) wing tip 580 (680) Left (right) wing strut 710 Nose wheel well and doors 720 (730) Right (left) main gear fairing. Includes doors, wheel well and stub wing 810 Nose baggage compartment door 820 Crew ditching hatch 830 Cargo door 840 (850) Right (left) forward emergency exit 860 Right aft emergency exit 870 Passenger door 880 Aft baggage door Page 5

13 SD3-60 AIRCRAFT MAINTENANCE MANUAL Major Sub-one - Wings and Tail Plane Figure Page 6

14 AMM ACCESS 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 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 one in which the door is located. The two-element alpha suffix designates the location of the door within the one. The first alpha letter identifies each door within the one in a logical sequence, i.e. inboard to outboard or front to rear, starting with `A' in each one. The second alpha letter locates the door in its relationship to the aircraft, as follows: T = Top B = Bottom L = Left hand R = Right hand Z = Internal For example, access door 230ER would be fifth access door aft of frame 74 on the fuselage right side Page 1

15 SD3-60 AIRCRAFT MAINTENANCE MANUAL Access Panels - Figure Identification Figure Page 2

16 Access Panels - Fwd. Baggage Compt. Figure Page 3

17 SD3-60 AIRCRAFT MAINTENANCE MANUAL Access Panels - Flight Compt. Figure Page 4

18 Access Panels - Passenger Compt. Figure Page 5

19 SD3-60 AIRCRAFT MAINTENANCE MANUAL Access Panels - Aft Baggage Compt. Figure Page 6

20 Access Panels - Fwd. Roof Fairing Figure Page 7

21 SD3-60 AIRCRAFT MAINTENANCE MANUAL Access Panels - Aft Roof Fairing Figure Page 8

22 Access Panels - Power Plant Figure Page 9

23 SD3-60 AIRCRAFT MAINTENANCE MANUAL Access Panels - Centre & Outer Wings Figure Page 10

24 Access Panels - M.L.G Fairings & Stub Wings Figure Page 11

25 SD3-60 AIRCRAFT MAINTENANCE MANUAL Access Panels - Vert. & Hori Stabiliers Figure Page 12

26 Access Panels - Fuselage Figure Page 13