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Aviation History
1961
1961 - 0183.PDF
FLIGHT, 10 February 1961 183 Hydraulic and Electric System* H1, hydraulic reservoirs in boom; H2, junction box; H3, cupboard for two SAFT batteries; H4, inverters in underfloor bay; H5, freight-door jacks; H6, double-acting ramp jacks; H7, multiple hydraulic bolts; H8, main fuse panels; H9, Rotax voltage control and protection; H10. AAPP in port boom; H11, intake to H10; H12, exhaust from H10; H13, generator cooling air also cools H12; H14, stainless-steel fireproof box; H15, tail light on each side of boom; H16, loading lights Load Furnishing L1, toilet and washroom in nose; L2, hot-liquid dispensers and sterilizers (cas-evac. role); L3t captain's seat; L4, co-pilot's seat; L5t engineer's seat; L6, rails on which L5 can move to central console; L7, navigator's seat; L8, desks; L9, bulkhead, two frames further aft than in AW.650; L10, nose entry hatch; L11, flight-deck hatch incorporating supernumerary seat; L12, lightweight ladder; L13, drop-controller's window under nose; L15, 161 main-deck lashing points (max 10,0001b); L16, 35 ramp lashing points (max 5,000lb); L17, 36 wall lashing points (max 2,000lb); L18, floor-illuminating lamps; L19, paratroop doors on each side; L20, freight shackles engage in floor rails Powerplant PI, Rolls-Royce Dart RDa.8 Mk 101 turboprop; P2, airflow through oil cooler; P3, cowl-vent intakes; P4, oil filler; P5, access to P4; P6, com- pressor section; P7f combustion section; P8, auxiliary gearbox, driving generator and cabin blower and (engines 1, 2 and 3) hydraulic pump; P9, drive shaft to P8; P10, stainless-steel tray for P8; P11, cool-air shroud around jetpipes; P12, shroud around turbine section ; P13, cooling air to auxiliaries; P14,11ft 6in Rotoi propeller leads; C13, rudder spring-tab torsion-bar assembly; C14, flap gearbox; C15, hydraulic motor driving C14; C16, flap torque-tubes; C17. flap drive units; C18, three slotted flap sections on each side; C19, flap hinges below wing; C20, ramp inching control for truck-bed loading Emergency Equipment E1, crew ditching exit; E2, passenger ditching exit, with inflatable seal; E3, ladder for E2, released at wall fitting; E4, emergency exits (four); E5, hand extinguisher; E6, emergency hydraulic pack; E7, inter-zone firewall; E8, firewall on tubular nacelle structure; E9, explosion-suppression devices in each tank; E10, twin photo-cells to trigger E9; E11, dinghy stowage; E12, dinghy release adjacent to E1 and E2; E13, fire access doors Fuel Systems F1, pressure fuelling/defuelling socket on each leg; F2, water methanol pressure-filling sockets; F3, water/methanol tanks, each 82 gal; F4, auxiliary fuel tank. 43Ogal: F5, No 1 tank, 374gol; fi, No 2 tank, 451gal; F7, No 3 tank, 4O5gal; F8, No 4 tank, 320gal; F9, No 5 tank, 100gal; F10, gravity flt-ers to all tanks; F11, fuel-gauge access; F12, all fuel tanks are flexible cells jwjn tanks, rigid metal); F13, flight-refuelling probe; F14, non-return valve; '"- tank-valve pressure switch; F16, fuel line outside pressure hull Radio R1, Rebecca aerial; R2, HF aerial; R3, Doppler aeriol box; R4, VOR aerial (port fin only); R5, Decca Flight Log Mk 1; R6, Ekco E.160 radar; R7, aerial tuner unit; R8, Autoland leader-cable aerial. The AW.660 could, in certain mili- tary roles, be equipped with additional electronic equipment Undercarriage U1, forged light-alloy lower leg; U2, forged upper member; U3, knee joint pulled forward by U4; U4, folding strut; U5, retraction jack; U6, upper anchorage for U5; U7, tubular radius rod; U8, fulcrum for U7 on tubular pyramid; U9, torque link; U10, hinge blocks for triple brake pipes; U11, multi- disc brakes; U12, Maxaret skid-sensing unit; U13, forward door linked to leg; U14, intermediate doors; U15, wheel-well doors, jack (top of boom) and linkage; U16, up-locklug Weather Protection W1, NESA-glass electrically heated windscreens; W2, intake to de-icing heat exchanger; W3, exhaust-gas deflector feeds hot side of heat exchanger: W4, hot delivery from heat exchanger; W5, de-icing air duct: W6, warm air through double-skin leading edge; W7, exhausts from W6; W8, Napier Spraymat protection on tail surfaces; W9, Dunlop electro-thermal mats on spinners and intakes
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