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Aviation History
1964
1964 - 2945.PDF
FLIGHT International, 26 November 1964 FUGhlT InU SYSTEMS Fuel Flying control* Capacityj Imp Type of gal) tankage Pitch(type f operation) Yaw(type + operation) Roll(type+operation) High lifti (type, operation,i CL max) Speed brakei(type + operation) Electricalpower source Hydraulic andor pneumatic (pressure, Ib/sq in;functions) 2,800 1,100 14,350 14,350 14,350 19,800 19,800 19,800 19,800 12,400 12,400 5,820 6,245 6,245 6,690 8,486 (8,589) 2,2003,050 3,050 21,750 10,150 1,283 1,440 8,900 12,950 155 326 14,600 14,600 19.500 19,500 19.500 19,500 3,100 1.1301 1,130 J 2,170 1.080 1,080 1,408 1.408 2,268 3,300 (3,400) 8,9001 7,800 V 8.900J4,940\ 6,000/ 1,025 5,270 21,560 4,600 19.200 1,562 455 3,592 650 12,000 Bags Int'g't'g'l + bag Integral Integral Integral Integral Integral Integral Integral Integral Integral IntegralIntegral Integral 18 bags 24 bags +2 integral Integral Integral Integral Integral Integral Integral Integral Integral Integral 6 tanks Bag tanksIntegral Integral Integral Integral integralIntegral Integral 2 integral + 2 bags Integral 2 integral + 4 bags IntegralIntegral Integral Bag (Integral) 6 integral + 4 bags Integral Integral 2 integral + 20 bag Integral Integral Integral Integral and bag 6 bags Integral Integral (optional)Integral Conv elev, man'l Conv elev. man'l I Conv elev, manual + variable incidence tail- i plane, electric Conv elev, dupl hydr (• + man'l rev + v.i. t.p. Conv elev, man'l servo J-tabs J "1 Conv elev and servo j>tabs, man'l; vari in- J cidence t'plane. hydr \3 elevons per side, /power operated Conv elev, manualwith servo tabs 1 Conv elev, man'l; ^variable incidence tail- j plane, hydraulic Conv man'l elev Conv man'l etev 1 Conv elevators, man'l with servo tabs: vari- able incidence tait- plane, hydraulic I Conv elev, manual Conv elev, man'l, var inc t/plane, elec/hydr S-Conv elev, manual Conv alev, manual 1 Conv elev, manual with geared tab Conv elev, hydraulic (3 services) Conv elev, variable I t/plane, hydraulic ! man'l elev, geared tabs, spring strut Conv elev, manual 175 Bag 4,180 4 integral I (4,840op>: cm Super B)! Conv elev, manual + hydraulic boost Conv flying tail + ele- vators—hydraulic Conv elev, manualservo tab Conv elev, manual Conv elev, manual Conv elev, manual Conv elev, man'l servo tabs+spring + 'q'feel I Conv elev, manual Conv rud, man'l Conv rud. man'l Conv rud, manual hydraulic boost Conv rud, dupl hydr + standby hydraulic system Conv rud, man'l servo tabs Conv rud, dupl hydr jacks, with emerg man'l reversion Two-section rudder, power operated Conv manual rudder Conv rud, manual conv man'l rudder Conv man'l rudder Conv rud, hydraulic with manual rever- sion 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) Conv rud, man'I Conv rud, manual + spring tab Conv rud, manual + hydraulic boost Conv hyd rud. Ccnv rud, manual + spring tab Conv rud, manual Conv rud, manual Conv rud, manual Conv rud, man'l servo/spring tabs Conv rud, manual D.-slot, hydr, 2.6 Fowler, hydr, 2.6 D.-slotted + leading edge hydraulic; 1.85 1.88 1.95 -120) -320) -320B) 2.16 (-720) 3-slot flaps + l.e. slots •flaps; 3.05 Double-slot electric; 2.60 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 servo tabs Conv ail, man'l servo tabs; spoiler/a-brakes intercon ails, hydr 3 elevens per side, sower operated As Bristol Britannia Conv man'l ailerons Conv ail manual spoilers, hydraulic Conv man'l ailerons Conv man'l ailerons Conv ailerons in 2 sections (outer at low speed only);-( hydr with manual 1 reversion | L Conv ail, manual Conv ail + spoil, hydraulic Conv ail, manual Conv ait, manual Conv ail, manual with spring tab Conv ail, hydraulic (3 services) Conv ail, hydraulic (3 channels) Conv ail, man'l Conv ail, manual Conv ail, manual hydraulic boost Conv ailerons-hyd ) Fowler, hyd, 2.4 wing flaps; flaps; Fowler flaps; hydrau- lic; 2.34 None Fowler, hydr, 2.32 (240-D), 2.69 (340/ 440-D) D-slot flaps + I.e. slots, hydr, 2.08 Slot flaps Slot flaps Double slot flaps + I.e. slats; hydraulic, 1.93 (series 10), 2.0 (series 30) D-slot, hydr Single-slot, electric, 2.94 Fowler + lift spoil; hydraulic Fowler, hydraulic, 2.59 Fowler + t.e. tabs, electric, 2.95 D.-slotted flaps, hy- draulic. 2.55 Plain/split, hydraulic, 1.77 D.-slotted flaps, I.e. slats + Kruger flaps, hydraulic, 1.97 S-slotted, hydraulic Fowler, hydraulic. 2.5 Fowler, hydr, 2.53 Conv ail, manual + spring tab Conv ail, manual Conv ail, manual Conv ail, manual Conv ail, man'l servo tab, r spoilers, el/hy Conv slot ail, man'l Conv elevator, rudder and ailerons, hydraulic power-operated through Automotive Products Serodyne (duplicated). A third system, for standby, is charged by an electric pump 7,465 16,540 Integral Integral 3.080 Integral 1,720 IS bags (1,967) 1,945 4 bags 5,100 17,998 19,411 19,411 Tip-tip integral Integral Integral+finIntegral + fin Conv elev, manual Conv elev, hydraulic Conv elev, manual ^Conv elev, manual Conv elev, manual servo tabs Conv rud, manual + hydraulic boost Conv rud, hydr 1 Conv rud, manual Conv rud, manual Conv ail, manual Conv ail, hydr Conv ail, manual Conv ail manual Fowler hydr D.-slot, hydr, 2.43 D.-slot, hydraulic D.-slot, hydraulic D.-slot, hydr S.-slot, hydraulic Semi-Fowler/plain flaps, hydraulic. 2.08 Conv rud, manual + j Conv ail, manual + servo tabs servo tabs None None 32 sections on top and bottom wing surfaces, hydraulic 28 sect on t + b wing surface None 4-wing-top surface spoilers None 4 upper wing sur- face spoilers None None 10 sections on wing top surfaces 6 sections on wing- top surface None Aft fuse mount; hydraulic None None None Slotted plates on top and bott'm wi'g surfaces, hydraulic 4 plates on top of wing, hydraulic 4 plates on top & btm wing surfaces None None Wing t.e. spoilers None None None None None None 4 spoilers on top and bottom wing surfaces, hydraulic Fowler, hydr, 1.87 Fowler, hydr. 1.95 Fowler, hydr, 1.90 Double-slotted, elec, ! None 2.24 Fowler, hydr. 2.43 | None Spoilers on wing top surface 4x30kVA II5/200V 3- phase 400c/s AC alter- nators + 3 x 50A TRUs giving 28V DC 3x115V AC alt, 400 cps + 27V DC, trans, rects 4x47kVA Rotax alter- nators 208V AC, 112V DC, 28V DC 2 x Wst'ghouse 30kVA AC const't fre gens+2 100A silicon trans-recti. 4 x40kVAbrushless self- exciting alternators 3x40kVA 3-phase 400 c/s alt H5V&3x60kVA Existing DC gens may be used. 4x40kVA 115/208V AC generators+4 28V DC rectifiers 28V starter-gen 28V, 200amp starter-gen 4xll5/208V3-phase400 c/s AC alternators + 4 transformer-rectifiers to DC 2xDC engine driven generators, 375A 30V \—, u/c ret, n/w steer, flaps,/ J w/brakes \ 3,000. u/c retraction, nw steer, w/brakes, flaps, flyini 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 4,000 psi, hydraulic 3,000; u/c retr, n/w steer, w/brakes Hydr, 3,000, n/w steering, brakes, retraction, flaps 3,000; u/c retr, n/w steer, w/brakes, a/brakes, flying controls 3,000; u/c ret, n/w steer, w/brakes, a/brakes, flying controls, flaps Pneumatic, 3,300, u/c retract, n/wheel steer, w/brakes 2 eng driv gen + a.p.u.; allACI20/208V400c.p.s 2 eng driv 28V 6kW DC generators+ 2 x 7.2kVA 208V alternators i 2 eng driv 9kW 28V DC! + inv's 115V 3-phase 400 c/s 4x6kW28VDCgens + 3-phase 115V 400 c/s 4 eng driven l4kVA alt/rect combination 3 eng driven AEI AC gens + trans-rects, 400 c/s II5/200V 3-p + 28V DC 2 eng Rotax 28V st/gen; 115V AC inv. 8 DC gens at l2kW, 28.5V l-ph AC inverts 3,000; f/cont'l, u/e retr, n/N steer, brakes, spoilers, a/brake 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/brakes, flaps 2,500, u/c retraction, n/w steer, w/brakes, flaps, dive brakes, flying controls 3,000, u/c retract, n/w steer, w/brakes, flaps, dive brakes flying controls As above 3,000, u/c retr, n/w steei w/brakes, flaps 4engdriv60kVAGEgen 3,000, u/c retr, n/w steer, w/ 400 c/s AC J-2 28V DC reel brakes, flaps, a/brakes, f/cont' 440kVA AC gen.a.p.u. 2.5kVA hyd AC gen emerg 2 eng driv 12kW 28V DC gens + const-freq AC 2 eng dri battery -iv 6kW + 28V 3,000, 3 separate systems. 2 main + I standby 3,000, u/c retr, n/w steer, * brakes, flaps 2,500, u/e retr, n/w steer, w/brakes, flaps 4,000; u/c retr, n/w steer, w/brakes, flaps, spoilers 2,500, w/brakes, flaps 2 eng driv 30V DC gen- 2,500; u/c retr, n/w steer, eraton, 115V DC 400 | w/brakes, flying controls, air c/s AC through invercerti bnkei 4 eng driv 6kW DC j"\ 4 eng driv 6 kW DC (4 eng driv 9kW DC) 6 VF 50kVA AC alt + 4trans-rect 28V DC i-2,500; w'brakes, u/c retr,< n/w steer 3,000; w/brakes, u/c, flap, n/w steer i Conv elev + var ine'd Conv rud. electro- Conv ail + spoilers; j Fowler + full span l lh ! l lhdli i I l hdlitailplane; electro-hy- ; hydraulicdraulic + pelectro-hydraulic 989 ] Integral Conv elev, manual Conv rud, manual Conv ail, manual I.e. slats; hydraulic; 2.15 D.-slot, hydr Plates on top sur- j 4 eng driv 40kVA c/s | 3.000; w/brakes, u/c, flaps + f f i h II5/200V 400 / l / d/bksface of wing; hy- j gens II5/200 c/s " phase system. 28V DCdraulic 'ITp y | + emerg ram-air turb-alt slats, n/w steer, d/brakes, flying controls, tailplane in- cidence I 2 eng driv 9kVA gens | M5/220V400c/scon 'lire
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