CT-114 / CL-41 Tutor
| Data for (Version) | Canadair CL-41 | |
| ICAO Code | CL41 | |
| First Flight | 13.01.1960 | |
| Production Status | out of production | |
| Crew | 2 | |
| Empty Weight | 2,220 kg | 4,840-4,894 lbs |
| Gross Weight | 3,532 kg | 7,787 lbs |
| max. Takeoff Weight | 11,000lbs | |
| Wing Span | 11.13 m | 36 ft 6 in 36 feet, 4 inches |
| Wing Area | 20,4 m² | 220 ft² |
| Length | 9.75 m | "31 ft 12 in" 32 feet, 0 inches |
| Height | 2.76 m | 9 ft 1 in 9 feet, 4.5 inches |
| Propulsion | 1 Turbojet Engine | |
| Engine Model | General Electric J85-CAN-J4 Orenda J85-CAN-40 | |
| Engine Power | 13,1 kN | 2950 lbf |
| Speed | 772 km/h | 417 kts 480- 486 mph |
| Service Ceiling | 12.802 m | 42,000-44,500 ft |
| Range | 1,563 km | 844 NM 971 mi. |
| Armament |
combat load is 907 kg at 2 suspension nodes
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