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Aviation History
1963
1963 - 0669.PDF
6 2 FLIGHT International, 2 May 1963 Structure I Upward-hinging nose radome 1 Thermally de-iced windscreen panels 3 Front pressure bulkhead 4 Hydraulic wipers (three) 5 Eyebrow window 6 D.v. window 7 Pressure head 8 Ice detectors 9 q-feel venturi 10 Upward-sliding service door 11 Open position of forward passenger door 12 Passenger-door rails 13 Passenger doors 14 External door handle 15 Etched reinforcing panel 16 Airstairs door 17 Nose-undercarriage bay 18 Production break 19 Nose-undercarriage frame 20 Forward freight hold 21 Floor strut (discontinued in three bays opposite freight door) 22 Freight door 23 Typical door cut-out reinforcing (detail) 24 Cabin-window surround (detail) 25 Skin/stringer/frame joint (detail) 26 Frame 36 and first tank baffle (detail) 27 Front-spar frame 35 28 Doubler band around frame 29 Reduxed doubler-plates around emergency-exit cut-out 30 Front-spar centre-section baffle 31 Top skin of centre-section tank 32 Main keel member 33 Bracing strut 34 Rear-spar frame 41 35 Reinforcement strip 36 Stowage box for (HI) 37 Frame 41 pressure bulkhead (under floor) 38 Main-undercarriage bay 39 Pressure floor over (38) 40 Frame 44 41 Frame-44 bulkhead forms front wall of rear hold 42 Extension web to frame 44 43 Machined tension plate above Rib I 44 Rear freight hold 45 Seat rail 46 Rear freight door 47 frame 53 carries side-engine front countings 48 Section of beam across frame 53 carrying side engines (detail) 49 Section of lower periphery of frame 53 (detail) 50 Rear pressure bulkhead 51 Centre-engine intake duct 52 Cabin heat-exchanger intake 53 20 s.w.g. titanium panel inboard of engine stub 54 Fin front-spar bulkhead 55 Elevation of (54) with integral structure shaded (detail) 56 Section of beam across (54) carrying side-engine rear mountings (detail) 57 Section of lower segment of (54) (detail) 58 Bracing struts 59 Fin rear-spar bulkhead 60 Elevation of (59) with integral structure shaded (detail) 61 Firewall 62 Access hatch incorporating stairway and tail bumper 63 Centre-engine mountings 64 Engine mounting struts 65 Centre-engine doors 66 Cut-out for 140-gal water-injection tank 67 Fin front spar 68 Fin rear spar 69 Tailplane-bullet nose (fixed) 70 Tailplane bullet (moving) 71 Tailplane "coffin" box 72 Tailplane fulcrum block 73 Tailplane pivot bearing 74 Access doors 75 Machined lower skin of (71) 76 Tailplane front spar 77 Tailplane rib 78 Inboard section has reversed camber 79 Elevator hinge 80 Rudder-shroud access doors 81 Rudder 82 Removable frame segment beneath centre engine 83 Tailplane skin planks 84 Static discharge wicks 85 Top skin of wing, rib I to rib 8 86 Nose flap 87 Slat (four sections) 88 Slat tracks 89 Front spar 90 Rib I (machined) reinforcement strap 91 Rib 4 (ahead of main leg) 92 Centre spar 93 Joint doubler strap 94 Rib8(production and dihedral break) 95 Top skin, rib 8 to rib 21 96 Rear spar 97 Bottom skin 98 Rib 12 (outboard-flap outer track) 99 Inspection manholes 100 Reduxed stringer (shown in section in separate detail) 101 Aileron hinges 102 Aileron 103 Flap tracks 104 Airbrake 105 Outboard flap 106 Inboard flap 107 Lift dumper 108 Rear false (undercarriage) spar inboard 109 Undercarriage sidestay beam 110 Extension rib 5 111 Extension rib 6 112 Rear false spar outboard A Air Systems AI Warm air to flight crew A2 Cross-feed under flight-deck floor A3 Discharge valve A4 6in dump valve A5 Dump-valve duct A6 2in radio cooling valve A7 Ground pressure-test connections A8 Feed to (T16) punkah louvre (cold- air "gasper") A9 Port punkah-louvre duct in forward cabin A10 Flight-deck air All Forward-cabin supply AI2 Passenger-cabin air AI3 Warm flow up walls to inlets under racks AI4 Punkah-louvre duct in (T27) A15 Cabin-air water extractor AI6 Punkah and flight-deck water extractors AI7 Heat exchangers AI8 Supply from centre engine or APU AI9 Heat-exchanger and CAU discharge A20 2.5in blow-off valve A2I Inlet pipe to heat exchangers A22 Cabin air supply duct C Flying Controls CI Cable runs under cabin floor C2 Stat screwjacks, two per section C3 Slat drive motor C4 Aileron jacks, three in parallel C5 Airbrake jacks, two in parallel C6 Flap screwjacks, two per section C7 Flap drive motor C8 Tailplane and rudder cables behind pressure bulkhead C9 Tailplane control group CIO Input cable to (CI I) CI I Tailplane jacks, three in parallel CI2 Elevator bell-crank linkage to fin CI3 Rudder jacks, three in parallel CI4 Yaw-damper unit D De-icing (all engine bleed air) Dl Delivery to wing leading edge D2 Engine intake cowl D3 Engine i.g.v.s and nose bullet D4 Centre-engine intake lip D5 Centre intake duct through double skin D6 Heat-exchanger intake lip D7 Delivery to (D4) D8 Delivery to fin and tailplane D9 Delivery to fin leading edge DI0 Circulation round (69) DM Delivery through tailplane to leading edge F Fuel System Fl Float-operated refuel switch F2 Booster pumps F3 Jet pump F4 Blow-off valve F5 Integral tank (port and stbd) from rib I to rib 8 F6 Pressure fuelling coupling (port and stbd) F7 Magnetic fuel-level indicator (No I, outer)
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