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In 1922, the Army ordered three TA-3 (Trainer, Air-cooled, Type 3) machines for evaluation with the Le Rhone engine and dual controls. Evaluation showed that the type had the makings of a good trainer, but was somewhat lacking in power, so in 1923 Dayton-Wright modified one TA-3 with a more powerful 110 hp (82 kW) Le Rhone. [1]
Psalm 23 is the 23rd psalm of the Book of Psalms, beginning in English in the King James Version: "The Lord is my shepherd".In Latin, it is known by the incipit, "Dominus regit me ".
Czech Air Force designation C-106. Gomhouria Mk 1 Two-seat primary trainer aircraft, powered by a Walter Minor piston engine. Egyptian production version of the Zlín 381, built under licence in Egypt by the Heliopolis Aircraft Works. [11] Gomhouria Mk 2 Two-seat primary trainer aircraft, powered by a 145 hp (108 kW) Continental C-145 piston ...
Therefore, one PT-1 airframe was completed as XPT-2 with a 220 hp (164 kW) Wright J-5 Whirlwind radial engine. [1] The XPT-3 was almost identical to the XPT-2 except for the tail, revised wing panels and different shape. 130 production PT-3 aircraft were ordered in September 1927, [1] with one being completed as the XO-17.
The Shenyang JJ-1, also known as the Hong Zhuan-503 or Red Special, was a jet trainer developed in the People's Republic of China (PRC) during the 1950s. It was the first jet aircraft designed in China, with Xu Shunshou as the chief designer. [2] Two prototypes flew, but further development was abandoned. [3]
The Bü 133 was a development of the Bücker Bü 131 Jungmann two-seat basic trainer. First flown in 1935 (by Luise Hoffmann, the first female works [clarification needed] pilot in Germany), [1] it was slightly smaller than the Bü 131. The prototype, D-EVEO, was powered by a 140 hp (104 kW) Hirth HM506 inverted, air-cooled inline-6 engine. [1]
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 × ...
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