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Aviation History
1957
1957 - 1103.PDF
HNS LOWERED FOR ADDITIONAL CLEARANCE DURING RUN-DOWN OF ROTOR TRIMMING SURFACE WITH BALANCE TAB (NO ELEVATORS) TYPICAL PASSENGER SEATS (MAX. AT MM PITCH. «> 102* POWER-OPERATED CLAM-SHELL FREIGHT DOORS SPACE AVAILABLE FOR TOILETS. GALLEY. ETC. RUDDERS DIRECTIONAL _-1 CONTROL FOR CRUISING FLIGHT ONLY) .58 STEEL TUBES CARRYING AIR TO BLADE-TIPS LIGHT ALLOY TRAILING-EDGE FAIRINGS 94 a o » » t ( < -TRIM TAB (NO AILERONS) FAIREY HIGH-PRESSURE COMBUSTION CHAMBER ON EACH BLADE (TIP SPEED Dimensions and weights: Fuselage length, 58ft Sin; heiaht overall (to top of rotor head), 22ft 2in; fuselage interior, 46ft long, ait wide, 6ft high; floor height above ground, 3ft Sin; wing span, 46ft 6in; wing gross area, 475 Kg ft; rotor diameter, 90ft; rotor due loading, 6.14 Ib/sq ft; rotor blade chord. 27in; Roto I propellers. 13ft diameter; tare weight, 24,030 Ib [weight breakdown (Ib): structure, 7,039; rotor system, 5,312: power plant, 7,364; fuel and air supply, 881; fixed power services, 1,987; safety measures, 279; equipment, 528; fixed furnishings, 640]: laden weight, 39,0001£ (removable load, 1,797 1b; operating load, 6,273 1b; pay load, 7,400 Ib). Basic performance data are given on page 196. 59 Pitch-change mechanism, outer casing. *© rv-£h-change linkage. *1 Scissor link. ,-- • • W Fuel distributor. 43 Cyclic (lateral) jacks (see p. 197). 44 Cyclic (fore and aft and collective) jacks. 65 Shaft drive to 66. 46 Rotor gearbox (high-pressure fuel pump, hydraulic pump, tachometer, generator). 67 Rotor brake. 48 Oil tank (head lubrication). 4? Steel casting; duct takes control system loads. 70 Lightweight ducting. 71 Bellows walls to allow expansion of duct. 72 Fluid coupling. 73 Plenum chamber. 74 Auxiliary compressor (mass-flow (19.5 Ib/sec). 75 Firewalls. 76 Tubular engine mounting, four- point attachment. 77 Engine air intake. 78 Engine compressor section. 79 Engine combustion section. 80 Engine turbine section. 81 Bifurcated jet-pipes. 62 Starter motor. 83 Oil cooler and fan unit (low-speed cooling). 84 Oil tank. 85 Oil-cooler airflow. 86 Drive shaft to 87. 87 Auxiliary gearbox (28 v and 112 v generators), hydraulic pump. 88 Generator cooling air. 89 Napier Spraymat de-icing. 90 Main undercarriage retraction jack. 91 Drag strut. 92 Sway braces. 93 Leg door linked to leg. 94 Twin wheel-doors, lin'tge and snubber. 95 Glass-fibre moulding. 96 Hinged leading edge (to engine and propeller controls). 97 inspection panels. 98 Fuel tank bay inner skin Reduxed to ribs. 99 Retractable landing lamp (each wing). 100 Rubber mouldings. 101 Emergency undercarriage-down valve. 102 Emergency fin-fold valve. 101 Tailplane mounting points. 104 Door-operating jacks. 105 Door-operating buttons on fuse- lage wall. 106 Door latch. 107 Electric trimming actuator. 108 Rudder power actuator. 109 Fin-tolding jack. 110 Tail bumper.
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