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.^[1]

Specifications

Data from ^[1]

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)