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Aviation History
1962
1962 - 0740.PDF
•jl, 10 May 196. 733-734 In this entirely new^drawing our artist has portrayed the salient features of a standard VCIO of the type now in production. Details indicate the disposition of items along the underside of the fuselage, which could not otherwise be depicted. Around the far side of the aircraft are deployed (reading from the powered stairway on the left): the servicing train for the toilets, liquid-oxygen system and e/ectncs; cabin-service vehicle (galley, bar stocks, etc); the new conveyor freight loader; the ground electric-power trolley; the (Shell) refueller; and another freight loader insport Publications Ltd 1962 110 Leading edge de-icing ducts 111 Removable sections (four) for access to de-icing ducts and tail- plane actuator piping 112 Access panels to fin attachments 113 Three-piece rudder, 100 sq ft 114 VOR aerial 115 Fin de-icing outlet 116 Hinged shrouds for access to control runs and rudder p.c.u.s 117 Variable-incidence tailplane, +4° —14° 118 Tailplane actuator 119 Access to motors, gearbox and oil sump 120 Glide/slope aerial 121 ILS aerial 122 Access to aerials 123 Access to tailplane actuator 124 Rotating beacon 125 Leading-edge inspection lamp 126 Removable panel 127 Removable panels for access to tailpiane hinge bearings 128 Tailplane hinge bearings 129 Access panel to elevator control run 130 Detachable tailcone 131 Navigation light 132 Removable leading edges and tip for access to de-icing ducts: five pieces 133 Tailplane de-icing outlets 134 Hinged elevator shrouds for access to control runs and p.c.u.s 135 Power control units 136 Two-piece elevator, 73 sq ft each side 137 On Super VCIO: fuel carried in fin torsion-box integral tank, 1,125 Imp gal 138 Services to engines each side, behind side-toilet bulkheads 139 Access to flying and engine con trols and air-conditioning bay through bulkhead of centre toilet 140 Toilet servicing points (port and starboard) 141 Thrust-reverser cascade, outers only on VCIO, all four on Super VCIO 142 Four Rolls-Royce Conway RCo. 42 Mk 540 engines, minimum take-off thrust 20,3701b, ISA sea- level static 143 Godfrey SRM air compressor 144 Constant-speed-drive oil tank 145 Alternator, 40kVA 146 Constant-speed drive 147 Rear fireproof bulkhead 148 Fire-extinguisher bottles stowage box 149 Removable fairing panel, access to thrust reverser and thermo couples 150 Thrust-reverser jacks 151 Access for rear engine attach ment, slinging point and anti- icing duct 152 Rear engine access door 153 Main engine access door 154 Fuel-filter access 155 Wheelcase, oil filter, filler and level-gauge access 156 Constant-speed-drive oil-filter filler and level-gauge access 157 Engine-bay ventilating air intakes 158 Fire-extinguisher access 159 Removable stressed access panel to engine controls 160 Engine control inspection 161 Door for front engine attach ment, aligning-point, air duct, cabin compressor and general servicing 162 General access to services 163 Removable nose ring 164 Air intake to cabin compressors 165 Drain collector point and outlets 166 Hoist gantry shown in position for lifting engine 167 Pre-Closing main gear doors 168 Door jack 169 Main undercarriage incorporating anti-skid disc brakes; Dunlop type VII tyres, 50 X 18 x 20, 115 Ib/sq in 170 Five sections of modified Fowler flaps, total area 508 sq ft 171 Flap mounting beams and tracks 172 Flap screwjacks and trolley 173 Bevel gearbox 174 Hydraulic flap drive and gearbox 175 Spoiler mixing box 176 Flap torque shaft 177 Access to flap motors and gear box 178 Re-fuel/de-fuel point 179 Access to refuel control panel, starboard side only 180 Engine ice inspection lamp 181 Spoilers open, 52 sq ft each side 182 Access to spoiler jacks and ser vices aft of trailing edge through doors in lower shroud skin with flaps extended 183 Spoiler torque shaft and jacks 184 Two-piece aileron, area aft of hinge line 73 sq ft 185 Aileron p.c.u. 186 Retractable landing lamp 187 Wing de-icing outlet 188 Detachable wing-tip 189 Navigation light 190 Four-piece slat, 260 sq ft total 191 Slat de-icing air 192 Detachable leading edge housing de-icing plenum duct 193 Bevel gear and screwjack 194 Slat torque tube 195 Slat holding-down unit 196 Slat-unit access 197 Slat drive and gearbox 198 Cranking point for slat manual operation 199 Freon cooling system 200 Removable leading-edge section for access to Freon pack 201 Access to Freon-pack components 202 Access to Freon-pack turbine oil- level and refill 203 Air intake to vapour-cycle condenser 204 Spill from Freon turbine 205 Elrat 206 Hyrat 207 Centre wing torque box: also integral transfer fuel tank, 4,550 Imp gal 208 Fail-safe wing torque-box forming integral fuel tank 209 Tanks 2 (port) and 3 (starboard) 3,350 Imp gal each 210 Tanks I (port) and 4 (starboard) 1,915 Imp gal each 211 Tanks la (port) and 4a (star board) 1,455 Imp gal each 212 Vent surge tank 213 Manhole access 214 Hand-holes 215 Over-wing gravity refuelling 216 Fuel drain points 217 Hinge shrouds giving access to trailing-edge control runs 218 Aerodynamic fence 219 Fuel jettison pipe The following numbers indicatt items along the ventral centreline, as illustrated in separate details :• 220 Forward Doppler aerial 221 Windscreen wiper and pedal brake reservoir 222 Access to nose-gear ground lock and groundcrew intercom 223 DME and Tacan aerial 224 Forward thrust-augmenter air outlet 225 External electrical supply point 226 Access hatch to radio and elec trical equipment bay 227 Radio-altimeter aerials 228 DME and Tacan aerial 229 Rotating beacon 230 ATC aerial transponder 231 Waste-water discharge (heated) 232 Domestic water tank drain valve 233 Intake to unpressurized-fliehi valve 234 Teletype aerial 235 Access to slat motors and gearbo* and c/s tank inspection manholes 236 Low-pressure starting air 237 Marker aerial 238 Dectra aerial 239 Centre-section-tank water drain 240 Centre-section-tank fuel-lrvel indicator 241 Fuel pump and water drain 242 Keel inspection access 243 ADF sense aerial 244 Hydraulic-accumulators charjinf 245 High-pressure starting air m
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