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Aviation History
1954
1954 - 1781.PDF
794 FLIGHT 28 HUREL-DUBOIS H.D. 32 . . . ,<^ KEY 1 Nosewheel steering/anti-shimmy cylinders. 2 Windscreen de-icing alcohol reservoir. 3 Alcohol spray-bar. 4 Warm-air duct. 5 Electric screen-heating elements. 6 Direct-vision panel. 7 Sunblinds. 8 Radio installation to customer's choice. 9 Control cables in bulkhead rising to roof- duct. 10 One of seven emergency exits. 11 D/F. loops. 12 Carburettor air. 13 Oil cooler. 14 Top and bottom cowlings (hinging at rear). 15 Oil tank (25 gal each engine). 16 Fuel collector tank (15 gal each engine). 17 Fire-suppression bottles. 18 Landing light. 19 Jacking points. 20 Undercarriage leg main attachment (stresses transferred to main spar via pylon top rib and tubular structure). WING DE-ICING COMBUSTION HEATERS 14^ ™* TWO 1200 HP PRATT & WHITNEY TWIN-WASP R1830-92 ENGINES DRIVING HAMILTON AIRSCREWS DUCT FOR ALL CONTROLS AND SERVICES mwkm>4Mv*m*Mt INTAKE TO COCKPIT/CABIN COMBUSTION HEATER \ \ FIXED NOSEWHEEL. STEERABLE LEVER SUSPENSION CREW DOOR COAT/BACGAGE SPACE IN LINE WITH AIRSCREWS
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