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Aviation History
1955
1955 - 1148.PDF
262 FLIGHT KEY TO DRAWING Fuselage 1 Transport joint. 2 Top-hat-section stringers, spot welded to skin. 3 Seat rails. 4 Removable floor panels (under-floor - access). 5 Main frames. 6 Wing to fuselage pick up. 7 Frames uncut. 8 Hinged panels, full length of roof. 9 Rods carrying stringer stress through centre section. 10 Main roof rail carrying roof lights. Fin and tail 11 Fin attachment. 12 Corrugated skin (all tail surfaces). 13 Tailplane attachment. 14 Centre spar floats through fuselage. Mainplane 15 Corrugated-sandwich centre web. 16 Corrugated-sandwich top and bottom booms. 17 Tank fillers. 18 Fuel contents units. 19 Cords lacing flexible tanks to top panels. 20 Z-section outer wing stringers. 21 Removable tips. 22 De-icing air outlets. 23 Outer wing joint. 24 Undercarriage. Cabin air 25 Intake to cabin supercharger. 24 Supercharger and silencer (air im spill valve and heat exchanger to cabin). 27 Non-return valve in duct from nacelle to cabin. 28 Main roof duct. 2f Cabin distribution duct. 30 Air piped to floor level duct. 31 Air to cockpit and windscreen de- misting. 32 Cockpit air louvres. 33 Mass-flow control. 34 Main discharge valve. 35 Inwards relief and safety valves. 36 Pipe from pressure controller in cockpit. 37 Individual punkah louvres. Da-icing 38 Intake to heat exchanger. 39 Control valve, exhaust to heat exchanger. 40 Heat exchanger. 41 Crossfeed and supply to tail surfaces. 42 Distributing corrugations, spot- welded to skin (all leading edges). Power units 43 Breathers. 44 Oil coolers. 45 Hot- and cold-air intakes, filters and blowback valve. 44 Engine cooling air gills. 47 Fire-suppression rings. 48 Oil cooler air duct. 49 Oil tank (all nacelles, total cap. 40 gal). Controls 50 Aileron torque rod from column cross- shaft. 51 Aileron push-pull rods. 52 Aileron spring tab torsion bar, 53 Aileron mass balance.54 Rudder and elevator levers. 55 Rudder and elevator tension rods (under floor). 56 Rudder push-pull rods. 57 Elevator push-pull rod. '"•'_ 58 Rudder sealed balance 59 Rudder pedals with toe brakes. 60 Pitch and power push-pull rods. 61 Trim and control lock cables. 62 Flap lowering chain. '••-;• 63 Flap ram. 64 Flap guide rails. 65 Flap operating cables. 66 Flap and undercarriage emergency lowering air bottles (3,000 Ib/sq in). (7 Starboard console, mainly electrics. (Port console removed, autopilot, lights, and Gyrotyn compass controls). 68 Trim tab.69 Balance tab. Radio and elactrics 70 No. 1 inverter. 71 Stand-by inverter. 72 Inverter change-over panel. 73 24 vole 25 amp accumulator.74 Battery relays. 75 Ground supply socket. 76 Main fuse panel. 77 Generator circuit breaker panel. 78 Standby battery and fuses. 79 Nacelle electric cable runs and access panel to leading edge. 80 Fuselage cable run. 81 Dual-purpose taxi/landing lamps. 82 C.L2 compass detector. HANDLEY PA( RADIO RACKS H.F. V.H.F. A.D.F. I.L.S. AND RADIO ALTIMETER 83 H.F. aerial mast. 84 V.H.F. suppressed aerial. (Aerials under floor and not shown: A.D.F. loops, A.D.F. sense, I.L.S. glide-path, I.L.S. marker and radio altimeter). Undercarriage 85 Twin nose wheels (steerable 110).86 Door linkage. 87 Hydraulic tank (3,000 Ib/sq in system). 88 Brake relay. 89 Top pick-up, undercarriage sub frame. Accommodation 90 Toilet (removable). 91 Rear bulkhead (removable). 92 Hinged hand-luggage racks (run full length). 93 Aft escape door. 94 Forward escape hatch. 95 Tip-up seat and buffet space.
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