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Aviation History
1960
1960 - 3051.PDF
FLIGHT, 23 December 1960 983 r-ort, November 1960) >>..\ed from Santa Monica itmq machine. He chose c-n floor-panels, integral © Niffe Transport Publications Ltd 1960 Load Furnishing: (L1) Forward freight hold (26 cu ft); (L2) Rear freight holds (total 67 cu ft); (L3) Freight-retaining webbing; (L4) Curtains; (L5) Toilet; Vickers Type 101; (L6) Door to L5: (L7) Handbag rack; (L8) Wash basin; (L9) Steward's tip-up seat; (L10) Liquid containers; (L11) Steward's switch-panel; (L12) Sixteen non-reclining double seats; (L13) Bar-unit stowage; (L14) "Lionide" wall-covering (L15) Plastic window moulding; (L16) Glasswool insulation (lightweight aft of e.g.); (L17) Tip-up seat for extra crew; (L18) Access door to tail section; (L19) Seat attachments/freight lashings; (L20) Pilot and co-pilot seats (adjustable reach and height); (L21) Toilet servicing (starboard); (L22) Hat racks and passenger service panels; (L23) Cabin fan. Instruments: (N1) Converter for ultra-violet panel lighting; (N2) Instrument panel; (N3) Blind-flying panel frame; (N4) Autopilot oil filter; (N5) Autopilot air filters; (N6); P12 magnetic compass; (N7) Separate pitot/static for each ASI. Powerplant: (P1) 1,200 b.h.p. Pratt and Whitney R-1830-92 Twin Wasp 14cylinder engines, single-stage one-speed superchargers; (P2) Bendix Stromberg injection carburettors; (P3) American-Bosch magnetos; (P4) Engine accessories—hydraulic pump, generator, tacho-generator, fuel pump, vacuum pump, electric starter; (P5) Hamilton Standard Hydromatic constant-speed quick-feathering propellers; (P6) Hydraulically actuated cowl-flaps; (P7) Firewall; (P8) Oil cooler with rear shutters; (P9) Oil tank—24.2 imp gal, centre cut out for U3; (P10) Oil filler; (P11) Bay vent; (P12) Exhaust-muff heat-exchanger; (P13) Constant-speed unit, cable operated; (P14) Tubular engine mounting. Radio Aids: (R1) MF (wire); (R2) MF'HF (wire); (R3) ADF loop, Bendix; (R4) ADF sense (wire) (R5) VHF No1: (R6) VHF No2; <R7) Gee Mk2; (R8) ILS localizer; (R9) ILS glide-path; (R10) ILS marker; (R11) MBA dipole; (R12) MBA radio equip- ment: (R13) MBA set; (R14) Intercom equipment; (R15) VHF STR12 and 12D; (R16) Gee Mk2 set; (R17) Localizer marker set; (R18) Glide-path; (R19) Radio fuse-panel; (R20) Spare headset stowage: (R21) Modulator unit. Undercarriage: (U1) Twin oleo-legs: (U2) Filling point for U1; (U3) Retraction jack; (U4) Bungee-cord assisters; (U5) Knuckle joint; (U6) Upper truss; (U7) Goodyear split-hub wheels, disc brakes; (U8) Tyres, 12-ply 17x16; (U9) Wheel well; (U10) Castoring tailwheel, fixed; (U11) Static ground conductor. Weather-protection Systems: (W1) Goodrich pneumatic de-icing shoes; (W2) Air pressure pipelines; (W3) Air distribution valve bay; (W4) Propeller de- icing fluid-tank; (W5) Propeller de-icing-pump group; (W6) Slinger ring and blade feed pipes; (W7) Carb and windscreen de-icing fluid tank (pump below); (W8) Windscreen wipers; (W9) Hydraulic lines to (W8); (W10) Windscreen de-icing spray (electric pump); (W11) Side windows fluid piping (hand pump); (W12) Hot- air demisting outlets; (W13) Access to disconnect (W2); (W14) Mast ice-proteccors; (W15) Wing inspection light. 10 Hydraulic and Electrical Services: (H1) Header tanksight-glass; (H2) Hydraulic fluid filler; (H3) Pressure accumulator; (H4) Hydraulic control panel; (H5) Engine pump selector; (H6) Flap control valve; (H7) Undercarriage control valve; (H8) Hand pump; (H9) External electrical socket; (H10) Two 28V 81Ah Dagenite batteries; (H11) Terminals auto-disconnect; (H12) Landing lamp (Dietz); (H13) Electrically heated pitot-heads; (H14) One 28V 50amp generator on each engine; (H15) Electrical duct with outside access; (H16) Switch panels; (H17) Main fuse panels; (H18) Roof lights; (H19) Nav. lights flasher selector and tell-tale; (H20) Inverter; (H21) Voltage regulators; (H22) Entry light; (H23) Navigation lights; (H24) Cockpit wander-lamp; (H25) Access to H12.
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