|T-CH-1 at the RoC Air Force Museum in Ganshan|
|National origin||Taiwan (Republic of China)|
|Manufacturer||Aerospace Industrial Development Corporation|
|First flight||23 November 1973|
|Primary user||Republic of China Air Force|
|Developed from||North American T-28 Trojan|
Derived from the North American T-28 Trojan trainer, the first T-CH-1 prototype flew on 23 November 1973. A second prototype flew the following year. The T-CH-1 was a conventional, low-wing monoplane with tricycle undercarriage that accommodated the student and instructor in tandem.
- T-CH-1 Chung Hsing : Two-seat basic trainer, light attack aircraft for the Republic of China Air Force.
- A-CH-1 : Two-seat weapons training aircraft for the Republic of China Air Force.
- R-CH-1 : Two-seat reconnaissance aircraft for the Republic of China Air Force.
Data from Jane's All The World's Aircraft 1980–81
- Crew: 2
- Length: 10.26 m (33 ft 8 in)
- Wingspan: 12.19 m (40 ft 0 in)
- Height: 3.66 m (12 ft 0 in)
- Wing area: 25.18 m2 (271.0 sq ft)
- Aspect ratio: 6:1
- Airfoil: NACA 64-2A215
- Empty weight: 2,608 kg (5,750 lb)
- Gross weight: 3,402 kg (7,500 lb)
- Max takeoff weight: 5,057 kg (11,149 lb)
- Fuel capacity: 963 L (212 imp gal; 254 US gal)
- Powerplant: 1 × Avco Lycoming T53-L-701 turboprop, 1,082 kW (1,451 hp)
- Maximum speed: 593 km/h; 368 mph (320 kn) at 15,000 ft (4,600 m)
- Cruise speed: 315 km/h; 196 mph (170 kn) at 15,000 ft (4,600 m) (econ cruise)
- Stall speed: 93 km/h; 58 mph (50 kn)
- Never exceed speed: 685 km/h; 426 mph (370 kn)
- Range: 2,010 km (1,249 mi; 1,085 nmi) (with maximum fuel)
- Service ceiling: 9,800 m (32,000 ft)
- Rate of climb: 17 m/s (3,400 ft/min)
- Related development
- Aircraft of comparable role, configuration and era
- Taylor 1980, pp. 176–177.
- Taylor, John W.R. (ed.) (1980). Jane's All The World's Aircraft 1980-81. London: Jane's Publishing. ISBN 0-7106-0705-9.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 44.
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