| Manufacturer |
Aerospace Industrial Development Corporation |
CANADAIR |
| Description |
The AIDC T-CH-1 Chung Hsing () was a turboprop-powered military trainer aircraft produced in Taiwan (Republic of China). |
The Canadair CT-114 Tutor (company model CL-41) is a jet trainer that was designed and produced by Canadian aircraft manufacturer Canadair. |
| ICAO Code |
|
CL41 |
| First Flight |
1973-11-23 |
1960-01-13 |
| Production End |
|
1966-01-01 |
| Service End |
|
2000-01-01 |
| Designer |
Aerospace Industrial Development Corporation |
CANADAIR |
| Type |
Trainer |
Trainer, Ground-attack aircraft |
| Length (m) |
10.26 |
9.7536 |
| Height (m) |
3.66 |
2.7432 |
| Cockpit Crew |
2 |
2 |
| Max Speed (km/h) |
592.6395 |
782.1412 |
| Cruise Speed (km/h) |
314.8397 |
|
| Min Speed (km/h) |
92.5999 |
|
| Max Ceiling (m) |
9753.6 |
13563.6 |
| Rate of Climb (m/s) |
17.272 |
21.4376 |
| Armament |
|
2 |
| National Origin |
Taiwan |
Canada |
| Number Built |
52 |
212 |
| Powerplant Description |
1 × Avco Lycoming T53-L-701 turboprop, 1082 kW (1451 hp) each |
1 × Orenda J85-CAN-40 turbojet |
| Primary Users |
Republic of China Air Force |
Canadian Armed Forces, Royal Canadian Air Force , Royal Malaysian Air Force |
| Status |
Retired |
In process of Retirement, Airframes assigned to Snowbirds scheduled to fly until November 2026. |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/AIDC_T-CH-1 |
en.wikipedia.org/wiki/Canadair_CT-114_Tutor |
| Flat Wing Span (m) |
12.19 |
10.9728 |
| Flat Wing Area (m²) |
25.18 |
20.4387 |
| Flat Wing Aspect Ratio |
6 |
|
| Wake Category |
|
L |
| Aircraft Engine |
|
General Electric J85 |
| Number of Engines |
1 |
1 |