FlightGlobal.com
Home
Premium
Archive
Video
Images
Forum
Blogs
Jobs
Shop
RSS
Email Newsletters
You are in:
Home
Aviation History
1963
1963 - 2085.PDF
SYSTEMS Flying controls Pitch (type + operation) Yaw (type+operation) 4 integral on Super B)j Integral 4-fin ntegral+fin Conv elev, man'l Conv elev, man'l Conv elev, manual + variable incidence tail- plane, electric Conv elev, dupl hydr + man'l rev+v.i. t.p. Conv elev, man'l 1 Conv elev, man'l servo tabs Conv elev and servo ^tabs, man'l; vari in cidence t'plane. hydr 1 Conv elev, man'l; V variable incidence tail- J plane, hydraulic Conv elev, man'l Conv elevators, raan'l with servo tabs; vari able incidence tail- plane, hydraulic J-Conv elev, manual; + variable lift engine thrust Conv elev, manual toBV elev, man'l, var inc t/plane, elee/h/dr .Conv elev, manual Conv elev, manual Conv elev, manual with geared tab Conv elev, hydraulic (3 services) Conv elev, variable incidence t/plane, hy draulic (3 channels) Combined elev Conv elev, manual Conv elev, manual + hydraulic boost Conv elev, manual Conv elev, manual Conv elev, manual \Conv elev, manual Conv elev, manual Conv elev, manual Conv elev, man'l servo tabs+spring+'q'feel Conv elev, manual Conv rud, man'l Conv rud, man'l Conv rud, manual + hydraulic boost Conv rud, dupl hydr -f- man'l reversion Conv rud, man'l; diff prop pitch Conv rud, man'l servo tabs Conv rud, dupl hydr jacks, with emerg man'l reversion Conv rud, manual Conv rud, man'l Conv rud, hydraulic with manual rever- Conv rud, manual Conv rud, manual Conv rud, hydraulic boost Conv rud, manual Conv rud, manual Conv rud, manual with geared tab Conv rud, hydraulic (3 services) Conv rud, hydraulic (3 channels) -4- rud manual Conv rud, manual + spring tab Conv rud, manual + hydraulic boost Conv rud, manual Conv rud, manual Conv rud, manual Conv rud, manual Conv rud, manual Conv rud, manual Conv rud, man'l servo/spring tabs Conv rud, manual Roll (type+operation) Conv ail. man'l Conv ail, man'l Conv ail outboard and inboard for high speed and spoilers, manual •+• hydraulic Conv ail, dupl hydr + man'l reversion Conv ail, man'l; diff prop pitch Conv ail, man'l servo tabs Conv ail, man'l servo tabs; spoiler/a-brakes intercon ails, hydr As Bristol Britannia Conv ail manual spoilers, hydraulic Conv ail, man'l Conv ailerons in 2 sections (outer at low speed only);<; hydr with manual j reversion Conv ail, manual + variable lift engine thrust Conv ail, manual Conv ail + spoil, hydraulic Conv ail, manual Conv ail, manual Conv ail, manual with spring tab Conv ail, hydraulic (3 services) Conv ail, hydraulic (3 channels) Conv ail, manual Conv ail, manual Conv ail. manual + hydraulic boost Conv ail, manual Conv ail, manual, spoilers, hydraulic Conv ait, manual Conv ail, manual Conv ail, manual Conv ail, manual Conv ail, man'l servo tab, + spoilers, el/hy Conv slot ail, man'l High lift (type, operation, + CL max) Conv elevator, rudder and ailerons, hydraulic power-operated through Automotive Products Serodyne (duplicated). A third system, for standby, is charged by an electric pump Conv elev, manual Conv elev, hydraulic Conv elev, manual Conv elev, manual Conv elev, manual + server tabs Conv elev + var inc'd tstlplane; electro-hy draulic Conv elev, manual Conv rud, manual + hydraulic boost Conv rud, hydr Conv rud, manual Conv rud, manual Conv rud, manual + servo tabs Conv rud, hydraulic electro- Conv rud, manual Conv ail, manual Conv ail, hydr Conv ail, manual Conv ail manual Conv ail, manual + servo tabs Conv ail + spoilers; electro-hydraulic Conv ail, manual D.-slot, hydr, 2.6 Fowler, hydr, 2.6 D.-slotted + wing leading edge flaps; hydraulic; 1.85 (-120) 1.88 (-320) l.95(-320B) 2.16 (-720) 3-slot flaps + I.e. slots + flaps; 2.9 3-slot flaps in prop s/st'm, hydr, 4 (p. on) Double-slot flaps; electric; 2.60 Fowler flaps; hydrau lic; 2.34 D.-slot flaps + I.e. slots, hydr, 2.08 Split flaps, hydr Double slot flaps 4- I.e. slats; hydraulic, 1.93 (series 10), 2.0 (series 30) fD.-slot, hydr None Single-slot, electric, 2.7 Fowler + lift spoil; hydraulic Fowler, hydraulic, 2.59 Fowler + t.e. tabs, electric, 2.43 D.-slotted flaps, hy draulic, 2.55 Plain/split, hydraulic, 1.77 D.-slotted flaps, I.e. slats + Kruger flaps, hydraulic, 2.05 Fowler, hydraulic Fowler, hydraulic, 2.5 Fowler, hydr, 2.53 Triple-slot, hydr. 2.4 Fowler, hydr, 1.9 D.-slotted, hydraulic 2.66 D.-slot, hydr, 2.43 D.-slot, hydraulic D.-slot, hydraulic D.-slot, hydr S.-slot, hydraulic Semi-Fowler/plain flaps, hydraulic, 2.08 Fowler, hydr, 1.87 Fowler, hydr, 1.95 Fowler, hydr, 1.90 Double-slotted, elec, 2.24 Fowler, hydr, 2.43 Fowler 4- full span I.e. slats; hydraulic; •Ml D.-slot, hydr Speed brakes (type+operation) None None 32 sections on top and bottom wing surfaces, hydraulic 28 sect on t + b wing surface Rev pitch, flap defl >90° None 4-wing-top surface spoilers 4 upper wing sur face spoilers None 10 sections on wing top surfaces 6 sections on wing-" top surface J Thrust deflection None Aft fuse hydraulic None None None Slotted plates on top and bott'm wi'g surfaces, hydraulic 4 plates on top sur face of wing, hy draulic None 3 sections under wing centre section Spoilers (also for roll control), hydr Lift dumpers on wing-top surface None None None None None 4 spoilers on top and bottom wing surfaces, hydraulic Spoilers on wing top surface None None Plates on top sur face of wing; hy draulic Electrical power source Hydraulic and or pneumatic (pressure, Ib/sq in; functions) 4x30kVA II5/2O0V 3- phase 400c/s AC alter nators + 3 x 50A TRUs giving 28V DC 3x 115V AC alt, 400 cps -I-27V DC, trans, rects 4x47kVA Rotax alter nators 208V AC, 112V DC, 28V DC 2 x W'st'ghouse 30kVA AC const't fre gens+2 I0OA silicon trans-recti. 3X4QkVA 3-phase 400 c/salt 115V 4x40kVA II5/208V AC generators+4 28V DC rectifiers 4xll5/208V3-phase400 c/s AC alternators + 4 transformer-rectifiers to DC 2xDC engine driven generators, 400A 30V 2 eng driv gen + a.p.u.; all AC 120,208V 2 eng driv 28V 6kW DC generators+2 x 7.2kVA 208V alternators 2 eng driv 6kW 28V DC + inv's 115V 3-phase| 400 c/s 4 x 6kW 28V DC gens + 3-phase 115V 400 c/s 4 eng driven l4kVA alt/rect combination 3 eng driven BTH AC gens + trans-rects, 400 c/t 1I5/200V3-P +28V DC 8 DC gens at l2kW, 28.5V l-ph AC inverts 4 eng driv 60kVA GE gen 400c/sAC+228VDCrec 2 eng driv 12kW 28V DC gens 4- const-freq AC 2 eng driv 6kW + 28V battery 2 eng driv 30V DC gen erators, 115V DC 400 c/s AC through inverters 4 eng driv 6kW DC 4 eng driv 6 kW DC (4 eng driv 9kW DC) 6 VF 50kVA AC alt + 4 trans-rect 28V DC 4 eng driv 40kVA gens II5/200V 400 3-phuc system, 28V PC -r emerg ram-air turb-alt 2 eng driv 9kVA gens 115/220V 400c/s const/fre I—, u/c ret, n/w steer, flaps, I w/brakes 3,000, u/c retraction, nw/| steer, w/brakes, flaps, flyingj controls, air brakes 3.000, u/c retr, n/w steer, w/ br'k's, f/contr, flaps, a brakes 4,000; u/c retr, n/w steer, w/brakes 3,000; u/c retr, n/w steer w/brakes, a/brakes, flaps 3,000; u/c w/brakes 3.000; u/c w/brakes, controls retr, n/w ctaer. retr, n/w a/brakes, 3,000; u/c ret, n/w w/brakes, a/brakes, controls, flaps steer, flying steer, flying Pneumatic, 3,300, u/c retract, n/wheel steer, w/brakes 3,000; f/cont'l, u/c retr, n/w steer, brakes 3,000; u/c retr, n/w steer, w/brakes, flaps 2,500, u/c retr, n/w steer, w/brakes 2,500/3,000, u/c retract, n/w steer, w/brak es, flaps 2,500, u/c retraction, n/w steer, w/brakes, flaps, dive brakes, flying controls 3,000, u/e retract, n/w steer, w/brakes, flaps, dive brakes flying controls 3,000, u/c retr, n/w steer w/brakes, flaps 3,000, u/c retr, n/w steer, w/ brakes, flaps, a/brakes, f/cont I 3,000. u/c retr, n/w steer, w/ brakes, flaps 2,500, u/c retr, n/w steer w/brakes, flaps H 4,000; u/c retr. n/w steer, w/brakes, flaps, spoilers 2,500; u/c retr, n/w steer, w/brakes, flying controls, air brakes 2.500; w/brakes, u/e retr, n/w steer 3,000; w/brakes, u/c, flap, n/w steer 3,000; w/brakes, u/c, flaps + slats, n/w steer, d/brakes, flying controls Air-conditioning (dP Ib/sq in; method; heat; refrig; humid) 7.1, 4.2, , 8.6; 3 engine driven AiResearcn turbo-compressors, by com pression, cold air or vapour cycle unit, optional 8.6, bleed from eng, eomp, dual cycle, none Pressurized 7.25 (8.3, -320), eng comp. comp.J Godfrey cold air, yes i 7.0, eng comp, comp. yes, none e.55, 1 eng comp. comp 8.2, eng driv comp, comp, Freon vapour cycle, none None 8.77, engine driven turbo com pressors, by compression, closed- circuit Freon system by Carrier Corp, none 7.9 8.25 4.16, 2xeng driv Godfrey blow ers; Janitrol, Stratos booster air-' eycle+Freon vapour cycle, none I 6.6. eng comp 4.2, 2 eug driv Godfrey blow ers, compression, cold air unit-! (optional), none 4.2, 2xeng driv comp, by comp, cold air unit (optional), none* L 5.5, 3 x eng driv Godfrey blowers, by comp, Godfrey c.a. unit, none 8.75, from engine compressors, f by compression, HSD cold air^ units, none (_ 8.25, from engine compressors, I by compression, HSD cold air-;' unit, none (. 7.1, eng compressor, by comp, cold air unit, yes 6.55,2 x eng driv comp, by comp, 2 air cycle systems 4- Freon, none 7.0 4.16, 2 eng driv Godfrey blow ers, by eomp, —, none None / 4.06, eng comp, by turbo-cooler\ 4.59, 2 eng driv comp, by comp, Freon, none 4.3 6.55, eng driv comp, by comp, HSD cold air units, none None 8.25 2 turb compressors driven by engine comp air, by com pression, cold air unit, none 7.2 8.4 7.2 6.5, eng driv comp, elec-Freon. none 6.5, eng driv comp, int-eool+e.air none 6.5,2 eng driv, comp, Freon, none 9.0, 4 eng humidfier driv comp, Freon, PERFORMANCE Airfield Take-off to 35ft | Land'g from 50ft ISAfl 2,900 2,250 10,600 7,500 8,250 10,700 10.500 10.500 10,700 9,450 6,200 5,515 1,300 6,300 7.900 (8,000) 6,000 6.950 6.250 8.600 9,500 7,400 8,650 (7,600) 9,650 2,100* 9,600 9,450 9,650 9,400 9,400 9.400 5,400 (6.130) 4,500 4,000 5,000 4.100 4,500 4,400 3,430 3,260 1,950* 4,900 (5,100) 6,300 6,000 6,300 7,250 7,450 8,250 2.500 3,800* 5,050 6,000 1,900 4.050 2,800 3,600 3,050 5,150 2,900' 2.250' (0,600 2,025 6,000 6,400 6.750 6,080 (6,400)1 6,850 (5,920) 5,580 9,350 4,900 5,500 (5.600) 5,450 (6,100) 5.100 (6,000) 8,150 9,050 9,050 2,150 ISA 10 C 2,000ft 3,700 2,800 11,000 9,300 9,750 13,750 12,300 12,300 13,400 11.650 7,450 6,700 1,850 7,700 10,200 (10,200) 7,000 7,750 7,000 8.800 9,700 9,300 11,000 (9,750) 12,450 3,000* 10,100 9,900 10,150 9.900 9,900 9,900 6,300 (7,800) VTOL VTOL 4,750 4,300 6,600 4,500 4,900 4,750 3,590 3,900 2,150* 5,600 (5,800) 7,800 7,500 7,800 9,000 9.200 9,950 3,500 5,300* 6,900 7,400 2,200 4,400 3,500 5,050 3,550 5,200 3,800* 3,100* (2,000 2,575 7,400 7,800 8.200 7,150 (7,700) 8.200 (7,050) 6,500 10,200 5,650 6,300 (6.900) 6.550 (7,400) 6,950 (7,800) 9,750 10,950 10.950 2,400 ISA si 1,850 1,800 6,240 6,550 6,230 7.280 5,970 6,260 7,280 6,200 6,350 5,300 920 5,200 6.000 (6,000) 5,100 5,350 5,000 6.800 7.000 6,250 7,100 (6,130) 6,550 1,200* 6,700 6,700 6.800 6,800 6,800 7,050 5,010 (5,300) 3.100 3,100 4,500 3,550 3,750 4,200 2,500 2.130 1,500* 5,450 (5,500) 6,000 6,000 6,000 6,000 5,750 6,400 2,400 3,750' 5,400 6.550 2.080 3,100 3,790 1,900 1,900 2,300 2,200' 1,310* 5,400 1,860 5,900 6,450 5,650 5,180 (5,650) 5,180 (6,450) 4,350* 8,690 3,700*| 4,200 (4,200) 4,200 (4.300) 5,100 (5,800) 6.850 7,650 7,650 3,350 ISA - 10 C 2,000ft 2,000 (.950 6,620 6,830 6.500 7,620 6,200 6,500 7,620 6,520 6,570 5.500 1,070 5,700 6.550 (6,550) 5,400 5,650 5,300 7,100 7.200 6,400 7,430 (6,430) 7,200 1,500* 6,950 6,950 7,000 7,000 7,000 7,250 5,280 (5,570) 3.400 3,400 4.850 3,700 3,900 4,500 3,470 2,700 1,650* 5,850 (5,900) 6,500 6,500 6,500 6,400 6,300 6,900 2,800 3,900* 5,800 7,000 2,230 3,370 4,050 2,000 2,000 2,500 2,320* 1,420* 5,900 2,000 6.550 6,750 5,950 5,500 (5.950) 5,500 (6,750) 4,500* 130 133 138 138 (133) 138 (133) 145 8,800 3,900* 4,300 (4.300) 4,300 (4,500) 5,300 (6,100) 7,300 8,350 8,350 3,600 Speeds (kt) Ranges (n.m.) T-O (EAS) 163 152 160 166 164 164 172 147 144 130 66 126 137 13! 134 127 95 126 (140) 90 90 :I8 !00 !C5 100 105 105 100 125 125 i25 146 I4G 148 Cruising Econ i Max (TAS),(TAS) !30 MO 132 S4 124 98 85 85 I 10 102 85 148 115 (114) 116 (118) 130 350 256 477 484 467 473 478 478 46! 484 484 215 286 310 469 469 469 1,260 1.260 325 475 485 230 455 455 455 464 473 505 470 (470) 495 455 234 260 426 237 ^38 220 240 242 238 (226) 438 457 457 502 502 501 •135 340 470 325 460 200 4t2 257 131 198 270 216 216 316 186 390 427 424 443 (422) 431 (427) 435 415 435 270 265 (265); 339 480 480 _ ! 480 95 360 496 532 523 522 522 522 515 510 532 495 240 315 345 469 469 469 1,260 1,260 410 248 505 505 487 (487) 495 455 440 375 250 27! 278 (238) 450 465 465 517 515 510 365 352 485 200 <!70 261 204 280 245 270 341 186 435 456 456 473 (442) 451 (445) 435 275 (309) 358 493 473 493 Appr' (IAS) 132 94 145 138 145 141 126 137 141 129 132 120 50 107 115 118 123 123 122 93 132 132 132 132 132 132 120 (122) 86 8u 112 92 95 92 94 10! 109 128 128 128 136 134 140 128 120 135 95 125 94 80 80 105 100 82 123 126 128 128 (128) 128 (126) 142 147 126 116 (115) 117 (114) 127 126 134 134 Design VC |VNO (EAS)/ I (IAS)/ MC | MNO 360/0.9 375/0.9 360/0.9 360/0.9 375/0.9 375/0.9 360/0.9 375/0.9 375/0.9 225 234/0.57 245/0.6 285 -/0.57! 250/0.6 320/0.781 320/0.78 354/0.781 354/0.78 354/0.78J 354/0.78J 257/0.62 375/0.89 375-415/0.91 VD I VNE (EAS) /1 (IAS)/ MD I MNE 425/0.95 445/0.95 425/0.95 425/0.95 445/0.95 445/0.95 425/0.95 445/0.95 445/0.95J 285 295/0.7 285/0.7 390/0.9 255 276/- 306/- 403/0.86! — 4I0/0.86| — 410/0.86] — 265/0.63 340/0.88 340/0.88 340/0.88! 340/0.88 340/0.88 340/0.88 350/0.84 350/0.84 306/0.84 281/0.77 223 223 186 206 206 -/0.63 225 225 220 230 340/0.84 340/0.84 340/0.84 340/0.84 340/0.84 340/0.84 350/0.84 350/0.84 306/0.84 281/0.77 223 223 330/0.75! 206 206 324/- 225 225 220 230 420/0.95! 420/0.95; 420/0.95! 420/0.95 420/0.95| 420/0.95, 430/0.891 430/0.89)! 270/0.75 275/0.76 275/0.76 360/0.88 340/0.88 340/0.88 325/0.615 350/0.825 ~340/0.8l 245/0.475 208 208 262 270 171 320/0.64 270 170 300/0.77 300/0.77 320/0.77 330/0.81 (320/0.77) 330/0.81 (325/0.77) - I « 220 235 (264) 313/0.64! 303/0.86 303/0.86 303/0.B6 380/0 380/0 380/0 380/0 390/0 390/0 351/0.96! 351/0.96 288 288 267 267 300 300 300 29! 415/0.951 395/0.95 395/0.95 405/0.71 440 400/0.86; 310/0.6 269 269 330 232 254 254 240 240 360/- 260 260 270 256 300/0.781 305/0.79 305/0.79 38! 275/0.53 242 242 -/0.64 300 209 325/0.77J — 295 (325) 390/0.74| 379/0.84 379/0.84 379/0.84) 266 (292) 352 Max payi'd dist/payl'd 1,350/26,500 1.380/8,800 2,670/52.000 3,680/47,000 2.830/48.000 4.020/55.000 5,230/50,000 3,320/96,000 3,980/57,000 3,680/28,200 3,608/40.500 1,400/24,000 1,300/15.500 2.945/24,700 3,620/34,500 1,405/13,685 1,525/18.089 1,215/17,832 2,700/21,000 3.800/20.000 3.450/64,500 3,040/23,650 (3,140/24.400) 4,110/25,770 1,030/3,000 3,760/39,400 4,050/38,000 4,000/46,300 5,310/46,600 5,855/46,000 3,520/95,300 930/18,150 (1,410/18.150)] 650/24,000 190/12,100 600/11,500 1,030/11,400 (1,030/12,700) 800/12,700 470/10.700 500/11,200 1,330/12,200 320/13,000 940/12,400 870/15,100 650/27,500 (650/31,000) 3,500/24.500 3,000/24.200 3,075/24,000 1,770/22,040 2,320/24,950 1,630/28,950 950/4,700 2,000/27,000 3,750/50,700 2,700/24,500 3.400/83,500 216/7,400 940/12,400 710/12,130 135/6,570 200/7,435 1,240/35.275 800/2,000 920/4,500 3,200/I00,000| 278/4,000 1,615/17.265 1,985/16 965 2.025/17,570 2.175/18.230 (2,310/18,370) 2,230/20,080 (2.260/17,250) 2,030/26,000 4,850/44,100 2,160/12.600 1,310/10,800 (1,630/13,000) 1.120/13.800 (1,470/14,300) Max fuel dist/payl'd 1,900/18.600 1,750/6,300 4,040/23,400 4,580/31,640 4.040/22,450 5,860/18.400 6,610/25,170 6,750/31,170 5,850/20,400 4,550/11,630 5,373/11.930 2,300/11,000 1,900/10.000 3.690/13.500 4,530/23,500 (4,530/23,000, 1,600/11,835 2,135/11.939 2,180/8,182 3,300/0 4,400/0 5,350/35,500 3,040/23,650 (3,530/16,400) 4,110/25,770 1,450/0 4,067/27,800 4.425/26,600 5,250/25,500 5,905/23,400 6,550/25,900 6,550/29,500 2,075/5,600 (2.000/11,600, 2,100/7,700 1,350/3,800 1,550/6,000 1,570/8,450 (1,570/9,750) 1,700/4,500 1.500/7.000 1,420/9,400 1,980/7,500 1,710/4,281 1,780/7,700 2,600/3,960 2,100/11,000 (2,100/13,000) 3,820/14,500 3,300/15,700 3,745/10,500 2,900/8,200 3,200/13,230 2,800/13,430 1,620/4,300 3,000/15,000 5,400/0 3,000/17,500 5,500/36,000 1,240/3,000 1,650/8,450 1,680/5,400 815/3.850 920/4,650 2,930/19,400 1,590/900 2,000/2,050 5,000/69,000 528/3,400 2,535/6,400 2,535/10,300 2,445/12,000 2,765/11,590 (2,770/12,830)1 2.745/13.440 3.245/8,000 (2,820/10,620) 5,430/26,760 2.160/12,600 1,470/9.500 (1,680/10,500) 1,670/7,750 (1.510/14,100) PRICE (t Av. second hand) $6.75m $6.75m $5.7m $4.25m £570.000 £I.S5m $5.75m »6.75m $3.lm ($3.lm) DM2.2m $6.lm £230.000 I 800/22,700 2.620/16.200 (1.800/37,500) (2,620/24,000)| 4,700/39,765 3,950/57,760 3,950/63,300 110/10.800 5,650/22,000 5 570/24,060 5.570/29.600 995/7,500
Sign up to
Flight Digital Magazine
Flight Print Magazine
Airline Business Magazine
E-newsletters
RSS
Events
