Tactical and technical characteristics of the aircraft:

Year of adopting – 1992
Wingspan – 9.39 m
Aircraft length – 11.97 m
Aircraft height – 4.27 m
Wing Area – 16.68 sqm
Weight, kg
- Empty – 4260
- Maximum Take-off – 5780
Internally fuel – 1310 kg
PTB – 2 x 590 hp
Engine Type – 1 HPT Rolls-Royce/Turbomeca F405-RR-401
Thirst – 2650 kgf
Maximum speed – 997 km / h
Operational range – 1854 km
Service ceiling – 12,875 m
Maximum operational load – 7,33
Crew – 2 people

Payload: up to 2,567 kg on three hardpoints: lightweight multi-purpose bombs and containers.

T-45 Goshawk – training aircraft primary and advanced flight training with the possibilities of working off of arms, established by the American firm McDonnell Douglas under license from the British firm British Aerospace on the basis of TCB Hawk Mk.60. Airplanes intended to replace the TCB U.S. Navy T-2 Buckeye and TA-4 Skyhawk. The first flight of the prototype was made in April 1988. Aircraft into service in January 1992.