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Aviation History
2003
2003 - 2370.PDF
9 1 Variable geometry droci ' 2 Droop-guide rails 3 Droop hinge-joint 4 Retracing visor 5 Visor-guide rails 6 Visor refracting link 7 Visor jack 8 Outward-opening plug-type passenger door (66in x 30in, still 16ft 5in above ground) 9 Service door (48in x 24in) 10 Underfloor baggage hold (pressurised) 26ft x 38in x 55in (308 cu ft) 11 Rear baggage compartment (pressurised) 26ft door to stbd (429 cu ft) 12 Middle passenger doors (port and stbd) 73in x34in 13 Metal-faced floor panels 14 Rear emergency doors (port and stbd), 68in x34in 15 Light alloy/balsa sandwich floor panels 16 Machined window panel 17 Triple-gap window - removable as a unit 18 Multi-layer windscreen - removable as a unit *"i» *£ ,«, 41 Vapour seal over tank roof 42 Unpressurised aft systems bay 43 Pressurised forward systems bay 44 Fin support structure-tube and extruded members 45 Machined fin spars - riveted to fuselage frames 46 Removable leading-edge sections 47 Machined ribs 48 Chemically milled skin 49 Expansion joints between sections 50 Removable outer wing - tank 5A, port, and 7A, stbd 51 Wing fixing by 340 high-tensile steel bolts 52 Quick-look removable inspection panels 53 Inspection panels, screw-fixed 54 Honeycomb structure (control surfaces, engine nacelles and intakes) 55 Seat rails 56 Floor supports - permit longitudinal expansion 57 Toilet 58 Galley unit 59 Coat stowage 60 Overhead baggage racks with doors 61 Passenger-service units on underside of baggage racks 62 Pilot heads A10 Riser to distribution duct A11 Duct to forward risers A12 Window ventilating air - all windows A13 Air-recirculating duct A14 Individual punkahs on service panels, adjustabl to seating arrangement A15 Cabin-air exhaust through roof filter via trim to under-floor A16 Heat and sound insulation - glass-fibre and polyester sheet A17 Baggage-compartment cooling air A18 Cabin-floor-level exhaust duct to ventilate equipment bays A19 Flight-deck air duct A20 Window demisting A21 Equipment venting air A22 Equipment-air extraction duct A23 Automatic discharge/relief valve - normal diff. 10.7lb/sqin A24 Manual discharge valve A25 Thrust-recovery nozzle A26 Low-pressure venting air between vapour seal and tank roof A27 Ground-conditioning connection A28 Undercarriage-bay cooling air Flying controls C1 Control cable runs under floor C2 Rod linkage to surface power control C3 Power control unit mounting 44 21-27 OCTOBER 2003 FLIGHT INTERNATIONAL www.flightinternational.com
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