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Aviation History
1964
1964 - 2288.PDF
fLIGHT International, 20 August 1964 293 basic trainer; two General Electric J85-5 turbojets with reheat, of 3,8501b thrust each; span, 25ft 3in; length, 46ft 4in; gross weight, 11,7001b; max Mach number, 1.27; in service, 1961. North American T-2A Buckeye NAA Columbus Division, Columbus, Ohio, USA; basic trainer; Westinghouse J34-36 turbojet of 3,4001b thrust; span, 36ft; length, 38ft 8in; gross weight, 10,0001b; max speed, 495 m.p.h.; in service, 1959. North American T-39A Sabreliner NAA Los Angeles Division, Los Angeles, Calif, USA; combat-readiness trainer and utility; two Pratt & Whitney J60-3 turbojets of 3,0001b thrust each; span, 44ft 5in; length, 43ft 9in; gross weight, 17,7601b; max speed, 540 m.p.h.; in service, 1961. Lockheed T-33A Lockheed-California Co, Burbank, Calif, USA; advanced trainer; Allison J33-35 turbojet of 5,4001b (wet) thrust; span, 38ft lOJin; length, 37ft 9in; gross weight, 14,4421b; max speed, 600 m.p.h.; in service, 1949. Beech T-34A Mentor Beech Aircraft Corp, Wichita, Kansas, USA; primary trainer; Continental O-470 piston engine of 225 h.p.; span, 32ft 9Jin; length, 25ft 11 tin; gross weight, 2,9501b; max speed, 188 m.p.h.; in service, 1952. North American T-6 Texan (Harvard) North American Aviation Inc, Los Angeles, Calif, USA (also made in other plants and countries); basic trainer; Pratt & Whitney R-1340-AN-1 piston engine of 550 h.p.; span, 42ft OJin; length, 29ft; gross weight, 5,6171b; max speed, 212 m.p.h.; in service, 1939. North American T-28 Fennec NAA Colum- bus Division, modified by Sud-Aviation; basic trainer and counter-insurgent strike; Wright R-1820-56S piston engine of 1,425 h.p.; span, 40ft 7Jin; length, 32ft 9in; gross weight, 8,2471b; max speed, 380 m.p.h.; in service, 1960 (as trainer with US Navy, 1953). Yak-11 Soviet Government design bureau led by Aleksander Yakovlev; intermediate trainer; Shvetsov ASh-21 piston engine of 730 h.p.; span, 30ft lOin; length, 27ft lOiin; gross weight, 5,5121b; max speed, 286 m.p.h.; in service, 1947. Yak-18 Soviet Government design bureau led by Aleksander Yakovlev; primary trainer; M-11FR piston engine of 160 h.p.; span, 33ft 9Jin; length, 26ft 6in (later versions, 28ft); gross weight, 2,4701b (later versions, 2,8661b); max speed, 153 m.p.h.; in service, 1946. Mig-15UTI Soviet Government design bureau led by Artem Mikoyan and Mikhail Gurevich; advanced trainer; Klimov VK-1 turbojet of 5,9501b thrust; span, 33ft lin; length, 36ft 3in; gross weight, about 13,0001b; max speed, about 650 m.p.h.; in service, 1952. Soko Galeb Preduzece Soko, Mostar, Yugo- slavia; basic trainer; Bristol Siddeley Viper 22-6 turbojet of 2,5001b thrust; span, 34ft 0i in (38ft liin with tip tanks); length 33ft 11 Jin; gross weight, 8,2001b; max speed, 505 m.p.h.; in service, 1964. Aero 3 Government Factories, Yugoslavia; primary trainer; Lycoming O-435A piston engine of 185 h.p.; span, 34ft 5in; length, 28ft lin; gross weight, 2,6461b; max speed, 143 m.p.h.; in service, about 1957. L-29 Delfin State Aircraft Industry, Czecho- slovakia; basic trainer; M-701 turbojet of 1,9201b thrust; span, 33ft 9Jin; length, 35ft 5in; gross weight, 7,9151b; max speed, 423 m.p.h.; in service, 1963. Potez C.M.170 Magister Etablissements Henry Potez SARL, Paris 16e, France (example illustrated made by Vahnet OY, Finland); basic trainer; two Turbomeca Marbore IIA turbojets of 8801b thrust each (later version, 1,0581b Marbore VI); span, 37ft Sin (39ft lOin with tip tanks); length, 33ft; gross weight, 7,0551b; max speed, 444 m.p.h.; in service, 1956. Nord 3202 Nord-Aviation SNCA, Paris 7e, France; basic trainer; Potez 4-D 32 piston engine of 240 h.p.; span, 31ft 2in; length, 26ft 8in; gross weight, 2,6901b; max speed, 161 m.p.h.; in service, 1959. Saab-91D Svenska Aeroplan AB, Lin- k oping, Sweden; primary trainer and liaison; Lycoming O-360-A1A piston engine of 180 h.p.; span, 34ft 9in; length, 26ft 4in; gross weight, 2,6601b; max speed, 165 m.p.h.; in service, 1947 (Saab 91 A). Saab-105 Sk 60 Svenska Aeroplan AB, Linkoping, Sweden; trainer, liaison, casualty- evacuation, strike, reconnaissance, survey and executive; two Turbomeca Aubisque turbofans of 1,5401b thrust each; span, 31ft 2in; length, 34ft 5in; gross weight, 8,8201b; max speed, 490 m.p.h.; in service, 1965. Piaggio P.149-D Rinaldo Piaggio SpA, Genoa, Italy (example shown built by Focke- Wulf under licence); basic trainer and liaison; Lycoming GO-480 piston engine of 270 h.p.; span, 36ft 6in; length, 28ft 9Jin; gross weight, 3,7041b; max speed, 192 m.p.h.; in service, 1956. Macchi MBJ26 Aeronautica Macchi SpA, Milan, Italy; basic trainer; Bristol Siddeley/ Piaggio Viper 11 turbojet of 2,5001b thrust; span, 32ft liin; length, 35ft; gross weight, 7,3201b; max speed, 501 m.p.h.; in service, 1962. DINFIA I.A.35 Huanquero Direction Nacional de Fabricaciones e Investigaciones Aeronauticas, Cordoba, Argentina; naviga- tion trainer (also liaison, bombing/gunnery, ambulance and photographic versions); two I.A.19R El Indio piston engines of 620 h.p. each (750 h.p. in other versions); span, 64ft 3in; length, 45ft lOin; gross weight, 12,5401b; max speed, 225 m.p.h.; in service, 1958. Belalang 90A Lembaga Persiapan Industri Penerbangan, Bandung, Indonesia; primary trainer; Continental O-200A piston engine of 100 h.p.; span, 31ft lin; length, 25ft 3Jin; gross weight, 1,5001b; max speed, 115 m.p.h. in service, 1960. Hindustan HT-2 Hindustan Aircraft Ltd, Bangalore (Mysore State), India; primary trainer; Bristol Siddeley Cirrus Major III piston engine of 155 h.p.; span, 35ft 2in; length, 24ft 8Jin; gross weight, 2,2401b; max speed, 130 m.p.h.; in service, 1953. TS-8 Bies Wytwornia Sprzetu Komunika- Cygnego-Mielec, Mielec,Poland; basic trainer; Narkiewicz WN-3 piston engine of 330 h.p.; span, 34ft 5Jin; length, 28ft; gross weight, 3,5251b; max speed, 194 m.p.h.; in service, 1958. Hispano HA-200 (E-14) Saeta La Hispano- Aviacion SA, Madrid (factory, Seville), Spain; advanced trainer; two Turbomeca Marbore IIA turbojets (licence-built by ENMA) of 8801b thrust each; span, 34ft 2in; length, 29ft ljin; gross weight, 6,9951b; max speed, 435 m.p.h.; in service, 1962. Fuji KM-2 Fuji Jukogyo Kabushiki Kaisha, Tokyo, Japan; primary trainer; Lycoming IGSO-480 piston engine of 340 h.p.; span, 32ft lOin; length, 26ft 0 in; gross weight, 3,2961b; max speed, 227 m.p.h.; in service, 1962. Fuji Tl-A Fuji Jukogyo Kabushiki Kaisha, Tokyo, Japan; intermediate trainer; Bristol Siddeley Orpheus 805 turbojet of 4,0001b thrust; span, 34ft 5in; length, 39ft 9in; gross weight, 11,0001b; max speed, 575 m.p.h.; in service, 1961. n U Hawker Siddeley Gnat T.I trainers of RAF Flying Training Command from Valley, Anglesey, where these diminutive Orpheus- powered machines have been in intensive service since 1962 wt^t^mm-
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