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Development started in 1990-ties, simultaneously with a more advanced turbojet trainer YAK-130, based on the successful YAK-54 design. Both were supposed to have similar cockpits to allow for easy changeover from a lighter YAK-152 to bigger YAK-130. By 2001 the new type was selected as the future main primary air force trainer.
Egyptian Air Force Yak-11. The Yak-11 entered service in 1947, serving as a standard advanced trainer with the Soviet Air Forces and DOSAAF. [7] Both the Yak-11 and C-11 were used in all Warsaw Pact countries and were exported to eighteen countries, including many African, Middle Eastern and Asian countries.
The Curtiss-Wright AT-9 "Jeep" bomber-pilot trainer at the National Museum of the USAF. 41-12150 – AT-9 on static display at the National Museum of the United States Air Force in Dayton, Ohio . It required extensive restoration, and was the product of the museum staff incorporating two incomplete airframes together, along with parts ...
The Hispano HA-200 Saeta (English: Arrow) is a twin-seat jet advanced trainer designed and produced by Spanish aircraft manufacturer Hispano Aviación.It has the distinction of being the first Spanish aircraft to harness jet propulsion.
Aero L-29 at Kaunas airport A private L-29 Delfín at the 2006 Miramar Air Show.. In the late 1950s, the Soviet Air Force commenced the search for a suitable jet-powered replacement for its fleet of piston-engined trainers; over time, this requirement was progressively broadened towards the goal of developing a trainer aircraft that could be adopted and in widespread use throughout the ...
The Morane-Saulnier MS.230 aircraft was the main elementary trainer for the French Armée de l'Air throughout the 1930s. Almost all French pilots flying for the Armée de l'Air at the outbreak of World War II had had their earliest flight training in this machine.
The CT/4E was a significant update designed to compete for a USAF requirement. 1 aircraft was converted from an ex-RAAF CT/4A and the remaining 41 were new built CT/4Es. 13 for the RNZAF, 24 for the RTAF, 2 for the SYFC, 1 for an Israeli customer and a demonstrator built for PAC in 2007, the 155th and last CT/4 built to date.
Data from Jane's All the World's Aircraft 1988-1989 General characteristics Crew: 2 Length: 8.33 m (27 ft 4 in) Wingspan: 7.92 m (26 ft 0 in) Height: 3.25 m (10 ft 8 in) Wing area: 11.89 m 2 (128.0 sq ft) Aspect ratio: 5.28:1 Airfoil: NACA 23012 Empty weight: 1,117 kg (2,463 lb) Max takeoff weight: 1,633 kg (3,600 lb) Fuel capacity: 405 L (89 imp gal; 107 US gal) internal fuel Powerplant: 1 × ...