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Aviation History
1962
1962 - 1535.PDF
DATA Power Two 145 b.h.p. Rolls-Royce Continental O-300 Spec 8 flat-six engines, driving Hartzell Compact HC-C2YF-2/7663-4 fully feathering, constant-speed, 72in propellers. Dimensions Span, 37ft; length (excluding nose undercarriage), 25ft 4in; height, 8ft 6in; wheelbase, 8ft 3in: track, I Ift 8in; tailplane span, I Ift; wing area, 170 sq ft; aspect ratio, 8.05; baggage volume (nose and behind cabin), 15 cu ft. Weights Dry basic equipped weight. 2,1641b; disposable load, i,0361b; gross weight, 3,2001b; wing loading, 18.8; power loading, 11.04. Performance The following figures are estimates, at max gross weight: max speed at sea level, 185 m.p.h. (I6lkt, 298km/hr); max recommended cruise at 5.100ft at 2,450 r.p.m. and 24in Hg, I52kt (175 m.p.h.. 282km/hr); cruise at 10,000ft at 2.100 r.p.m.. I39kt (160 m.p.h., 257km/hr); stall, clean, 6l.7kt e.a.s. (71 m.p.h.. I I4km/hr); stall with full flap, 50.4kt e.a.s. (58 m.p.h., 93km/hr); take-off to unstick. 790ft (241m); take-off to 50ft, 1,470ft (448m); initial climb, l,370ft/min (6.9m/sec): time to 5,100ft (1,553m), 4.2min; to 10,000ft (3,045m), 9.9min; service ceiling (100 ft/min), 21,700ft (6,610m); range with 7001b payload and 42 Imp gal at 1,900 r.p.m. at mean speed of 154 m.p.h. at 10,000ft, 578 miles (500 n.m., 925km); max range with 5001b payload and 70 Imp gal at same setting. 1,000 miles (870 n.m., 1.609km); landing from 50ft, !,485ft (453m); ground roll, 585ft (178m); single-engine initial climb, 350ft/min (l.72m/sec); single-engine service ceiling (lOOft/min), 7,000ft (2,130m). ) Hiffe Transport Publications Ltd 1962 This drawing was prepared at Shoreham by our head artist, who exper ienced some difficulty in keeping out of the way of the wen who were rushing to complete G-ASCK in time for the forthcoming SBAC Show. Design manager for the programme is Mr Grahame K. Gates, AFRAeS, and the project structural engineer Mr Ronald Dock PI PI P5 H P7 P8 « PIC Pll PIJ Pi' PI4 PIS Propeller charging-valve Propeller governor unit Tubular bearers Durestos-faced firewall Baffle Engine cooling air Intake to updraught carburettor Light-alloy spinners •J lass-fibre top and bottom cowlmgs attached only at fire wall ' Oil filler panel Throttle, controls Glass-fibre nacelle fairing Exhaust augmentor-tube dipstick, and access pitch and mixture PI6 Engine control cables along front spar PI7 Friction adjustment R Radio Rl Motorola VHF sets behind panel Power units and VOR sets to be on forward face of bulkhead VHF whip aerial (No 2 similar on belly) Roof-mounted loudspeaker R2 R3 R4 Aerials bonded into fibre-glass skins:— R5 VHF nav., nose-top R6 VOR glide-slope, nose R7 VOR marker, ahead of door R8 HF/MF, along dorsal fairing U Undercarriage Ul Cockpit control U2 Single-acting retraction jack U3 Retraction cables to port and starboard legs U4 Retraction cable to nose leg U5 Breaker-strut, cable-operated U6 Spring cylinder for wheels-down U7 Nosewheel spring-cylinder and linkage U8 Nosewheel-steering cables U9 Nosewheel-centring bungee UIO Single glass-fibre nosewheel door Ull Nosewheel-leg fulcrum UI2 Single-pad disc brake UI3 Brake lever UI4 Glass-fibre door attached to leg T Cabin Appointments Tl Four ashtrays 72 Seat-back pockets T3 Padded armrest recess T4 Dunlop foam-filled seats on Pirelli webbing base, from (21) to (36) in main key T5 Front seats mounted on box- spar (17) T6 Access tD baggage by seat-back tipping forward Blind-flying panel at centre T7 T8 Backs of front seats tip forward for rear-seat access '
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