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Aviation History
1958
1958 - 0407.PDF
28 March 1958 423 m 26 1 177 Rolls-Royce Avon RA.29 Engines: (105) Main mounting trunnions (106) Forward hanging points (107) Inlet guide-vanes actuator (108) Shaft drive to alternator (109) Fuel control group (110) Sump and pump group (111) R-R. thrust-reverser actuator (112) Thrust-reverser blast doors (top and bottom, outer engines only) (113) R-R. noise-suppressor nozzles (114) Outlet from compressor bleed valves (115) Engine cooling air outlet (116) Forward duct- ing removed (117) iet-pipes diverge from fuselage to reduce blast (118) Refrasil asbestos/aluminium covering. Miscellaneous: (119) Dielectric hinged nose cap (120) Pressure bulkheads (121) Cockpit floor (122) Control column (123) Hanging rudder pedals (124) Q-feel unit ond pitot (125) Aileron spring strut (126) Autopilot trim servo-motor (127) Fly- ing control primary pulleys: cables onward (128) Cables from pilots' console (129) Captain's chair (130) Navigator and radio officer (131) Table (132) Wall-mounted instruments and oxygen regu- lators (133) Pilots' flight panel (134) Flight engineer to st'b'd (135) Radio racks (136) A.S.I. ITS Lne •A1 •class or mixed-class layouts. Th'-s shows the all-first-class layout—56 seats at 40in 0 seats. Tourist seating (fire-abreast) accommodates 71, and maximum "734" [xed-class layouts are as follows: 16 de luxe forward, 48 economy aft; 24 first-clan • •'s present plan for Australian serf ices). The total hold capacity is 418 cu ft. TRANSVERSE DATUM STEWARD5 SERVING PCM NT EMERGENCY ACCESS DOOR TO EXIT DOOR FREIGHT HOLD I TOILET t i 6T>ITCH * MAIN CAftIN 32:5O FIRST CLASS-32 SEATS AT 4O-O" PITCH (4 ABREAST) / DIPLOMATIC MAIL LOCKER1 WAR0ROBE SPACE pressure heads (137) Galley box stowage (138) Toilets (two forward, two aft) (139) Waste water tanks (140) Four toilet servicing points (141) Four 26in X 29in emergency hatches (142) Full-size emergency door to st'b'd (143) Escape-chute stowage (144) Nose equipment-bay hatch (145) Passenger door, inward opening plug-type (146) Coats (147) Large vestibule (148) Production breaks (149) D.H. undercarriage units, forged main members (150) Access to hinge-pins (151) Breaker strut (1S2) Coupled wheels, 30 X 9.00 Dunlop tyres (153) Static-discharge whip, nosewheel leg (154) Static dischargers (155) Towing points (156) Doors linked to leg (157) Control cables in under- floor ducts except at centre section (158) Static apertures on skin (159) Jacking points (160) Sockets for datum levelling bar (161) Sockets for rigging sighting rods (162) Freight hold doors on bungee cord (163) Oxygen bottles (164) Hold capacity—front 172 cu ft, rear 246 cu ft (165) .030in glass-fibre wall and roof liners; alloy floor (166) Lashing points (167) Fuselage/centre-section links (168) Elevator and rudder cable compensators (169) Rear fuselage access hatch (170) Tail bumper with mooring point (171) Servo tabs (172) Mass balance (173) Dinghy stowage (174) Scissor link between plain flaps (175) Split flaps (176) Forged intake rings in spar web (177) Undercarriage beams (178) Main shock-absorber strut (179) Damper shock-absorber strut (180) Rocker arm (181) Articulated axle beams (182) Brake torque rods (183) 36 X 10.00 Dunlop tyres (184) Door closed except during retraction or extension, st'b'd shown disconnected (185) Spar joint and dihedral from Rib 7 (186) Stringers Reduxed to skin, ends riveted (187) Extensive use of machined skin on inner wings (188) Flow spoiler (189) Fixed aerodynamic slot (190) Nylon bumper-wheel in nacelle tanks (191) Air brake surfaces top and bottom (192) Bay for aileron operating mechanism (193) Internal light (194) Fuel drains (195) Fresh-water servicing point (196) Fresh-water tank in roof (197) Basic skin 18 s.w.g. (198) Skin around cut-outs 16 s.w.g. (199) Gyro compass master-unit stowage.
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