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| Manufacturer | Canadair |
| Model | CL-13 Sabre Mk.5(6) |
| Modification | CL-13B Sabre Mk.6 |
| Country | Canada |
| Years | 1953 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.30 m |
| Length | 11.43 m |
| Height | 4.45 m |
| Wing area | 26.75 m2 |
| Zero fuel weight | - |
| Empty weight | 4905 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 7990 kg |
| Flight duration | - |
| Engine | 1 ТРД Avro Orenda 14 |
| Power | - |
| Thrust | 1 x 3300 kN |
| Maximum speed | - |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 1120 km |
| Service ceiling | 15200 m |
| Hovering ceiling | - |
| Crew | - |
