| Manufacturer | Canadair |
| Model | CL- 41 Tutor |
| Modification | СТ-114 |
| Country | Canada |
| Years | 1960 |
| Type | Attack aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.13 m |
| Length | 9.75 m |
| Height | 2.84 m |
| Wing area | 20.44 m2 |
| Zero fuel weight | - |
| Empty weight | 2220 kg |
| Maximum takeoff weight | 3532 kg |
| Normal takeoff weight | 3355 kg |
| Flight duration | - |
| Engine | 1 ТРД Orenda (General Elecrtic) J85-CAN-J4 |
| Power | - |
| Thrust | 1 x 13.12 kN |
| Maximum speed | 801 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 1002 km |
| Service ceiling | 13105 m |
| Hovering ceiling | - |
| Crew | 2 |
