FlightGlobal.com
Home
Premium
Archive
Video
Images
Forum
Atlas
Blogs
Jobs
Shop
RSS
Email Newsletters
You are in:
Home
Aviation History
1960
1960 - 2688.PDF
800 FLIGHT, 18 November 1960 Commercial Aircraft of the World Explanatory Notes Page 781 Index by Aircraft Page 827 DOUGLAS DC-8 R&fBrencs: page 803 FORWARD PLUG-TYPE ENTRY DOOR (outward opening) 92 94 1 AVQ 10 weather radar, hinged radome 2 Intake to cabin air system (both sides) 3 Four cabin-air turbo-com- pressors 4 Turbine exhaust5 Heat-exchanger exhaust 6 Access door 7 Electrically heated multi-layer glass 8 Upper windows each side 9 Forward pressure bulkhead 10 Supernumerary seat 11 Engineer's panel 12 Radio racks (air cooled) 13 Coats 14 Pre-closing nosewheel-bay doors 15 DC-7-type nose-gear geometry 16 Steering cylinders 17 Retraction cylinder " 18 Galley service doors 19 Under-floor hold (door star- board) 20 Wall-fixed seats 21 Attendant's seat 22 Centre joint butt strap 23 Centre-section tank (gravity feed all engines) 24 Centre keel member (5ft deep) 25 Mainwheel doors (normally closed after gear extension) 26 Windows (18±inx15in) 27 Cabin air in, out at floor level 28 Passenger-address speaker 29 Hat racks 30 Emergency exits *'"j '-'•• 31 Emergency doors ~ - 32 "Hotwall" panelling 33 Inward-opening freight door 34 Concealed lighting 35 Integral three-spar fin 36 Sloping frames 37 Dielectric structural isolation 38 Bonded inner skin39 VOR aerial 40 HF aerials (1 and 2) 41 Taiiplane screwjacks 42 Taiiplane hydraulic and elec- tric motors43 Tail de-icing trunk 44 Retractable bumper 45 Integrally stiffened skin 46 Fully powered rudder 47 Manual elevators 48 Fuel system runs 49 De-icing duct (15th-stage air 232°C) 50 De-icing trunk 51 Hot air anti-icing 52 Production break 53 Pratt & Whitney JT4-9 54 Oil-cooler outlet 55 Inswept pylon tails 56 Intake to Sundstrand-drive oil coolers 57 Portion of flap hinged up to clear jet blast 58 Linkage to (57) 59 Three-spar fail-safe wing 60 Multiple scissor-links (inner to outer flap) 61 Flap-operating linkage 62 Main-leg subframe 63 Main-leg retraction jack 64 Tank bay end ribs (full depth) 65 Un-notched ribs (not full depth) 66 Divided powered ailerons 67 Bonded trailing-edge structure 68 Aileron power unit (emergency manual tab) 69 Rudder power unit 70 Tail plane hinge axis 71 Fuel-vent collector tank 72 Fire-suppression bottles (378 cu in CB and Freon) 73 Leading-edge venting , 74 Anti-collision beacon 75 Skin thickness 0.250in 76 Skin thickness 0.190in 77 Skin thickness 0.156in 78 Upper skin 0.064in, lower 0.063i n 79 Passenger-service panels (posi- tion variable with seat pitch) 80 Control tab 81 Geared tabs 82 HF aerial coupler and light- ning arrester 83 VHF aerials (two) 84 Glide-slope aerial 85 DME aerial 86 ADF aerial 87 Transponder 136 88 Radio altimeter 89 ADF sense aerials (four) 90 Oil tank 91 Noise suppressors 92 Rain-shedding hot-air blast, 120lb/min (no wipers) 93 Ground air-conditioning 94 Pressure head 95 Engineer's diffused lighting 96 Preset auto-fuelling 97 Circuit breakers 98 Auto-generator circuit panel, aft equipment panel, crew oxygen 99 Landing/taxi lamp 100 Rudder pedal steering 11°, wheel steering 75° 101 Nose gear compression/exten- sion controls: Reverse thrust on Nos. 1 and 4 engines Inboard spoilers, emergency decompression (800ft/min equivalent) Oil-cooler ground cooling ejec- tors Engine-bay ground venting ejectors Cabin-air turbo-compressor/ recirculation changeover 102 Engine earthing point 103 Forward and aft firewall ter- minating 175° zone 104 Vortex degenerator jets 105 Emergency starting access 106 Exhaust ejector, attenuator and reverser in retracted posi- tion 107 Exhaust ejector, attenuator and reverser in take-off (attenuator) position 108 Rails for 107 109 Pylon venting 110 Compressor bleed valve 111 Water filler valve 112 Compressor bleed outlet 113 Generator cooling air 114 Firex system access 115 Oil-filler access
Sign up to
Flight Digital Magazine
Flight Print Magazine
Airline Business Magazine
E-newsletters
RSS
Events
