The Wichita Engineering TG-10 was a proposed American training glider conceived by Wichita Engineering in the early 1940s.
Design and development The TG-10 was designed as a two-seat training glider with a side-by-side cockpit configuration. One aircraft was ordered on 25 June 1942 with the serial 42-57197. However, the contract was cancelled on 1 March 1943 before the aircraft was completed.
Specifications Data from General characteristics Crew: one Length: 25 ft 1 in (7.65 m) Wingspan: 50 ft 1 in (15.27 m) Performance
Maximum speed: 90 mph (145 km/h, 78 kn)
See also List of gliders
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