The Extra 230 was a single-seat aerobatic aircraft developed in Germany in the early 1980s. Designed by aerobatic pilot Walter Extra based on the layout of the Laser 200 he was previously flying, the Extra 230 was a conventional (if short-coupled) mid-wing cantilever monoplane with fixed tailwheel undercarriage and a wire-braced empennage. The fuselage and empennage were of steel tube construction, but the wings were wooden. Production continued until 1990, at which time it was replaced by the Extra 300
Lambert, Mark (1990). Jane's All The World's Aircraft 1990–91. Coulsdon, UK: Jane's Defence Data. ISBN0-7106-0908-6.
Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 926.
World Aircraft Information Files. London: Bright Star Publishing. pp. File 893 Sheet 11.
April 12, 2024
extra, extra, single, seat, aerobatic, aircraft, developed, germany, early, 1980s, designed, aerobatic, pilot, walter, extra, based, layout, laser, previously, flying, extra, conventional, short, coupled, wing, cantilever, monoplane, with, fixed, tailwheel, un. The Extra 230 was a single seat aerobatic aircraft developed in Germany in the early 1980s Designed by aerobatic pilot Walter Extra based on the layout of the Laser 200 he was previously flying the Extra 230 was a conventional if short coupled mid wing cantilever monoplane with fixed tailwheel undercarriage and a wire braced empennage The fuselage and empennage were of steel tube construction but the wings were wooden Production continued until 1990 at which time it was replaced by the Extra 300230Role Aerobatic sportsplaneManufacturer ExtraDesigner Walter ExtraFirst flight 14 July 1983Status ActiveProduced 1983 1990Specifications editData from Jane s All The World s Aircraft 1990 1991 1 General characteristicsCrew 1 Length 5 82 m 19 ft 1 in Wingspan 7 40 m 24 ft 3 in Height 1 73 m 5 ft 8 in Airfoil MA 15S root MA12S tip Empty weight 440 kg 970 lb Max takeoff weight 560 kg 1 235 lb Fuel capacity 80 L 21 US gal 18 imp gal Powerplant 1 Lycoming AEIO 360 A1E air cooled flat four 150 kW 200 hp Propellers 2 bladed Muhlbauer constant speed propellerPerformance Maximum speed 352 km h 219 mph 190 kn IAS Stall speed 71 km h 44 mph 38 kn IAS Never exceed speed 407 km h 253 mph 220 kn Endurance 2 hr 30 min g limits 10 10 Roll rate 200 degrees sec Rate of climb 15 0 m s 2 950 ft min References edit nbsp Wikimedia Commons has media related to Extra 230 Lambert 1990 p 99 Lambert Mark 1990 Jane s All The World s Aircraft 1990 91 Coulsdon UK Jane s Defence Data ISBN 0 7106 0908 6 Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions p 926 World Aircraft Information Files London Bright Star Publishing pp File 893 Sheet 11 Retrieved from https en wikipedia org w index php title Extra EA 230 amp oldid 965710061, wikipedia, wiki, book, books, library,
