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Aviation History
1974
1974 - 0083.PDF
Cessna FRA150 Aerobat Dimensions Span 33ft 2in, 10-1m Length 23ft 8in, 7-24m Height 8ft 7in, 2-62m Track 7ft 7in, 2-32m Wheelbase 4ft 10in, 1 -47m Wing area 159-5sq ft, 14-8m2 Wing section Naca 2412 modified Dihedral 1° Aspect ratio 6-9 Tailplane span 10ft, 3 04m Tailplane area 28 2sq ft, 2-62m2 Elevator deflection up 25°, down 15° Rudder deflection 23° Undercarriage cantilever sprung steel (main); oleo-pneumatic (nose) Tyres 600 x 6 (main); 500 x 5 (nose) Engine Rolls-Royce Continental 0-240 of 130 b.h.p. Propeller McCauley 1A 135/BRM7150; fixed pitch; 69in, 1 -75m diameter Fuel 21 -6 Imp gal, 26 US gal, 98lit Oil 5 Imp qt, 5-7lit Electrical system 14v d.c, 60A alternator Equipped empty weight 1,1001b, 499kg Wing loading 10-4lb/sq ft, 50-7kg/m2 Power loading 12-7lb/h.p., 5-8kg/h.p. HUES? Performance Flight manual limits VNE 168kt, 193 m.p.n., 311km/hr VNO 122kt, 140 m.p.h., 225km/hr Manoeuvre 103kt, 118 m.p.h., 190km/hr VFE 8 7kt,100 m.p.h., 161km/hr Maximum weight 1,6501b, 749kg e.g. datum engine firewall e.g. limits 33in to 37-5in aft of datum Loading +6g to -3g, clean; +3-5g, flaps down Climbing speed 72kt, 80 m.p.h., 129km/hr Take-off to 50ft 1,075ft, 316m Landing from 50ft 1,035ft, 328m Measured speeds Cruise 95kt, 105 m.p.h., 169km/hr IAS at 2,400 r.p.m. Stall, flaps up, power off 37kt, 41 m.p.h., 66km/hr Stall, flaps down, power off 31 kt, 35 m.p.h., 56km/hr Range without reserves 348 n.m., 389 statute miles, 625km at 75 per cent power, 7,000ft Marketing Maker Reims Aviation S.A., Reims, France European distributor Cessna Europe, Brussels United Kingdom dealers Air Service Training, Perth; Anderson Aviation, Biggin Hill; Blackbushe Aviation Services; Brymon Aviation, Fairoaks; Channel Island Engineering, Jersey; Lonmet Aviation, Biggin Hill; Miles Dufon, Shoreham; Northair Aviation, Leeds/ Bradford; Rogers Aviation, Cranfield; Westair Flying Services, Blackpool Price as tested £10,177 equipped with King KX170 Nav/Com and Cessna ARC ADF
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