The prototype T-45 Goshawk first flew in 1988 and became operational with the US Navy in 1991. Two variants of the T-45 Goshawk exist, the T-45A Goshawk and the T-45C Goshawk, this is a result of updated avionics needed to keep pace with operational aircraft, the current variant, the T-45C, utilises an all digital "glass cockpit" instrument display, it is intended to upgrade the older aircraft to this specification. McDonnell Douglas T-45A Goshawk Specifications: - Crew: Pilot and Instructor
- Length: 39 ft 4 in (11.99 m)
- Wingspan: 30 ft 10 in (9.39 m)
- Height: 13 ft 5 in (4.08 m)
- Wing area: 190.1 ft² (17.7 m²)
- Empty weight: 10,403 lb (4,460 kg)
- Maximum takeoff weight: 14,081 lb (6,387 kg)
- Engine: Single 5,527 lbf (26 kN) Rolls-Royce Turbomeca Adour F405-RR-401 turbofan
- Maximum speed: 645 mph (560 kt, 1,038 km/h)
- Range: 805 mi ( 700 nmi, 1288 km)
- Service ceiling 42,500 ft (12,950 m)
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