道格拉斯 DC-3

982 FLIGHT, 23 December 1960 DOUGLAS DC-3 (drawn ai s. After taking a long look at the possibility of drawing a DC-3 as it migh 25 years ago, "Flight" artist Arthur Bowbeer finally decided to work h one of BEA's Pionairs, built as military C-47s, and now standardized stairs, disc brakes and two-crew opeia Structural and General: (1) Hinged nose cowl; (2) Four spring-catches; (3) L- section stringers over rolled channel-section frames; (4) Tail-section joint r ing; (5) Three-spar torsion box; (6) Fuselage/wing attachments; four each side; (7) Fuselage attachment angle; (8) Auxiliary spar; (9) Corrugated centre-section skin; (10) Arch-ribs in fuel tank bays; (11) Corrugations continue as inner skin; (12) Multi-bolt wing joint; (13) Centre section closing-rib (floating); (14) Spar double boom fades out; (15) Centre-section skin 19 s.w.g.; (16) Wing skin 21 s.w.g.; (17) Fuselage skin 21 s.w.g.; (18) Multi-spar fin and tailplane; (19) tailplane halves bolted on centre-fine; (20) Tailplane/fuselage multi-bolt attachment; (21) Wing slinging point; (22) Tail slinging point access; (23) Nacelle slinging points; (24) Flap well; (25) Permanently attached nacelles; (26) Fairing strip over wing-joint; (27) Alloy floor-beams; (28) Alloy floor panels forward of cabin; (29) i in multi-ply cabin floor; (30) j in multi-ply vestibule floor; (31) Balsa and ply toilet floor; (32) Passenger cabin bulkhead; (33) Tailwheel truss-frame; (34) External doublers; (35) Detachable wingtip; (36) Crew and forward freight door; (37) Passenger door and steps; (38) Three door latches; (39) Operating handle for (38); (40) Flexible handrails: (41) Battery compartment doors; (42) Astro-hatch provision; (43) One-piece fillet; (44) Bird-proof windscreens; (45) Snubber for (37). Cabin Air System: (A1) Air to exhaust-muff heat-exchanger; (A2) Warm-air trunks; (A3) Mixing chamber; (A4) Cold air to (A3); (A5) Hot air overboard;(A6) Spill valve; (A7) Cabin wall delivery duct; (A8) Ground warm-air connection(starboard); (A9) Pilots' warm air outlets; (A10) Air out via roof lights. Controls: (C1) Dual control-columns; (C2) Rudder pedal/toe-brake units: (C3) Side-kicking length adjustment; (C4) Centre console; (C5) Access panel below; (C6) Brake cross-shaft; (C7) Magneto switches; (C8) Propeller de-icing control: (C9) Cockpit hot-air control; (C10) Cabin-air control (on aft face); (C11) Sperry A3 autopilot; (C12) Elevator cables; (C13) Rudder cables; (C14) Elevator trim cables, drums (C15) Rudder tr im cables, drums; (C16) Rudder-stop cables; (C17) Tailwheel-lock cables; (C18) Aileron cables and levers; (C19) Control-lock lugs; (C20) Flap actuator; (C21) Flap linkage; (C22) Limit of split flaps; (C23) Aileron trim tab (starboard only); (C24) Fabric-covered controls. Emergency Equipment: (E1) Emergency lighting box (inertia switch and 6V battery); (E2) Hand fire-extinguisher; (E3) Two fire bottles in each nacelle; (E4) Graviner spray-rings; (E5) Two floating survival-cots under rear seats; (E6) Life jackets; (E7) Four emergency windows; (E8) Crew escape hatch; (E9) Two crash- inertia switches on beam; (E10) First-aid box. Fuel System: (F1) Main tanks, 168 Imp gal each side; (F2) Aux tanks; 167 Imp gal each side; (F3) Gravity filling points; (F4) Twin wobble-pumps; (F5) Pilots' handie for (F4); (F6) Tank bay vents; (F7) Tank vent pipes; (F8) Fuel selector valves; (F9) Fuel-gauge unit access. 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 f t ) ; (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 tai l 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;