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Aviation History
1992
1992 - 0417.PDF
<<i55 Up 124.5mm Down 12.7mm "" Tailplane leading edge Spar mountings -, Spar carry-through beam- Cabin cross-section T 07 EW Fuel system F1 Underfloor tanks - total useable fuel, 164Btres (Engineer Fabrics) F2 Centre tanks - total useable fuel, 349litres (Engineer Fabrics) F3 Integral wing tanks - total useable fuel, 1,617litres F4 Forward rear tank-total usea ble fuel, 439litres (Engineer Fabrics) F5 Aft rear tank - total useable fuel, 212litres (Engineer Fabrics) F6 Vent/surge tank F7 Aft vent/surge tank F8 Collector tank F9 Gravity refuelling point (fcree) F10 Tank Interconnect lines Ft 1 Engine feedline F12 Float check valve Powerplant PI Pratt & Whitney Canada JT15D-5 two-shaft turbofan P2 Starter/generator P3 Forward engine mounting Pi Hear engine mountfrtB PS Engine mounting beam P6 Exhaust jet pipe P? Tailcone without thrust reverser P8 Thrust reversar doors - shown deployed - (Rohr) P9 Thrust reverser hydraulic actuation unit - (Rohr) P1« HP blead-alr take-off Undercarriage U1 Forward retracting, steerable nose landing gear U2 Nosewheel - foiled aluminium Wted with 18 x 4.4 tubeless fere - (Aircraft Sraktng Systems) U3 Nosedoor - retracted with gear down U4 Inward retracting main landing gear Wed with hydraulic anti-skid disc brakes US Main wheel • forged aluminium fitted with 24 x 7.7 tubeless tyre - (Aircraft Braking Systems © Reed Business Publishing
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