Specifications
| Mark I model | Mark II model | |
| Type | two-seat all-weather long range interceptor | two-seat all-weather long range interceptor |
| Contractor | Avro Canada | Avro Canada |
| Country of Origin | Canada | Canada |
| Powerplant | two Pratt & Whitney J75-P-5 afterburning turbojet engines | two OrendaPS-13 Iroquois afterburning turbojet engines |
| Thrust | J75-P-5 12,500lbs (18,500lbs full afterburn) each | PS-13 19,250lbs (26,000lbs full afterburn) each |
| Length | 80ft 10in | 85ft 6in |
| Height | 16ft | 16ft |
| Wingspan | 50ft | 50ft |
| Wing Area | 1,225 Sq. ft | 1,225 Sq. ft |
| Speeds | Max 1,325mph (mach 2) @ 40,000ft Combat Mach 1.5 Cruise Mach 0.92 | Max 1,325mph (mach 2) @ 40,000ft Combat Mach 1.5 Cruise Mach 0.92 |
| Climb Rate | 38,450ft/minute | 44,500ft/minute |
| Service Ceiling | 53,000ft | 58,500ft |
| Range | unknown | 408 miles |
| Empty Weight | 49,040lbs | 45,000lbs |
| Max Take-Off Weight | 68,602lbs | 68,847lbs |
| Armament | none | six Sparrow II or eight Falcon air-to-air missiles |
