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Aviation History
1991
1991 - 3239.PDF
Cabin cross-section '' m i E9 F71 Fn F->7 c- Rudder movement left 22° right 30° ^^#^ Tim HallAMRAeS Llnkdplng, Sweden Antenna positions Electrics and Electronics E1 Rockwell-Collins WXR 840 weather radar E2 Total-temperature sensor - Rosemount E3 Angle-of-attack vane and trans mitter - Rosemount E4 Pitot heads, two each side E5 Rockwell-Collins EFIS(Six units) E6 Avionics rack E7 Sensor systems antennas MLS 1 & 2 antennas - optional E9 TCAS antennas - optional E10 GPS anterlna - optional E11 ATC 1 antenna E12 ATC 2 antenna - optional E13 VHF 1 antenna E14 ADF 1 & 2 antenna E15 HF antenna - optional E16 VOR/LOC antenna E17 Dual glideslope antenna Aileron movement up 24° down 20° E18 DME 1 antenna E19 DME 2 antenna - optional E20 Radio altimeter 1 E21 Radio altimeter 2 E22 Marker beacon E23 VHF 2 antenna E24 VHF 3 antenna - optional E25 Emergency- locator transmitter antenna E26 Flux valve, one in each wing leading edge E27 Anti-collison beacon E28 Landing lights E29 Taxi light E30 Ice inspection light E31 Navigation and strobe lights E32 Position light E33 Static-discharge wicks E34 28v batteries, two on port side ' and one on starboard side >E35 Three phase 115/200V 45kVa variable-frequency generators, one on each engine E36 FADEC I & II + nacelle interface \jnit E37 Bay housing VOR/LOC equipment and HF coupler Fuel system : F1 Two -fuel cells in each wing, total useable; fuel in both wings 5,185?litres F2 Pressure refuelling point F3 Gravity refuelling point F4 Pressure refuelling line F5 Fuel vent line F6 Fuel vent interconnect line F7 Fuel interconnect line F8 Engine feed line F9 Fire shut-off valve F10 Fuel-cell access panels F11 Fuel probes - Simmonds F12 Flight refuelling dipstick Powerplant P1 Allison GMA 2100 two shaft free turbine engine P2 Propeller gearbox P3 Engine-mounting structure P4 Forward frame P5 Aft beam P6 LP bleed duct to ECS P7 HP bleed duct to ECS P8 HP bleed shut-off valve P9 Air inlet plenum P10 Particle separator P11 Inlet for oil cooler P12 Oil cooler P13 Engine exhaust jetpipe P14 Fire extinguisher bottle P15 Dowty Rotol R381 propeller P16 Nacelle cowlings - Westland and Hispano Suiza jointly responsible P17 Top spine P18 Lower cowl P19 Hinged doors P20 Centre cowl P21 Overwing cow! P22 Sundstrand auxiliary power unit P23 Exhaust pipe P24 APU silencer - Technetics Undercarriage and Hydraulics U1 Forward-retracting steerable nose landing gear with twin wheels - AP Precision U2 Forward retracting main landing gear with twin wheels - AP Precision, wheels and carbon brakes - Aircraft Braking Systems U3 Goodyear tyres U4 Hydraulic reservoir U5 Hydraulic pump U6 Hydraulic filter manifold U7 Main gear spade door - main doors are in up-position when undercarriage is down
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