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Aviation History
1951
1951 - 0845.PDF
53O DUAL CONTROLS 8. THROTTLE AND AIRSCREW PITCH 9. ELEVATOR AND RUDDER TRIM 10. FLAPS PORT ONLY 11. CONTROL LOCK 12. P.I I MAGNETIC COMPASS t3. CANOPY OPERATING HANDLE AND EXTERNAL RELEVSE BUTTON AMBER SCREENS (RETRACTED) FLIGHT KNOCK-OUT PANEL(S) QUICK-RELEASE TAG T.B.A. CONTROL BOX CRASH , PYLON 25, SEATS \Vf. FLYING CONTROLS 14. TO ELEVATORS 15. TO AILERONS 16. TO RUDDER in ALVIS LEONIDES Mk 25 DRIVING 9ft fin dia AIRSCREW 1. CONSTANT SPEED UNIT ENGINE AUXILIARIES 2. STARTER 3. MAGNETOS 4. FUEL INJECTOR UNIT 5. GENERATOR 6. AIR COMPRESSOR 7. OIL TANK (6 gal OIL, 2 fal AIR SPACE ) INTAKE TO FUEL INJECTOR UNIT. AND OIL COOLER ENGINE COOLING AIR -OUTLET COOL AIR TO COCKPIT BAG-TYPE FUEL TANK 33 (al (EACH SIDE) TAXI LIGHT (EACH SIDE) OLEO-PNEUMATIC SHOCK STRUT *y. PERCIVAL P. 56 \T7 FITNESS for purpose in every particular sums up the design of the P. 56. The side-by-side seat cockpit affords the optimum working conditions for pupil and instructor alike; the aircraft is well-powered and has an excellent perfor- mance; everything which needs maintenance and servicing is readily accessible; and, as this drawing shows so well, the airframe is structurally simple and physically robust. V.H.F. AERIAL- PITOT HEAD (STATIC APERTURE ON FUSELAGE)
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