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The NAA T-2 Buckeye, more commonly known as the North American T-2 Buckeye, is a jet trainer designed and manufactured by North American Aviation (NAA). The T-2 Buckeye was produced over the years between 1958 to 1970, and 529 units were produced in total. During its years of service, the T-2 Buckeye has operated under a variety of users, including those such as the United States Navy, Venezuelan Air Force, and Hellenic Air Force. Originally designed for the United States Navy as a trainer, almost every Naval Aviator and Naval Flight Officer from the 1950’s and into the early 2000’s have been trained in a T-2 Buckeye.

Aircraft Model Naa T 2 Buckeye Details

Model No : Naa T 2 Buckeye
Category : Private Jets
Aircraft Type : Military Jets
Manufacturer : North American Aviation NAA
Country : United States
Manufactured : 1959 to: 2007
ICAO : NA
Avionics : NA
Engine : 2 × General Electric J85-GE-4 turbojets
Power : 2,950 pound-force
Max Cruise Speed : 450 knots - 833 Km/h
Approach Speed : NA
Travel Range : 786 Nautical Miles - 1,456 Kilometers
Fuel Economy : 2 nautical mile / gallon - 0.978 kilometres / litre
Service Ceiling : 44,400 feet
Rate of Climb : NA
Take Off Distance : 400 metre - 1,312.32 feet
Landing Distance : 520 metre - 1,706.02 feet
Max Tak eOff Weight : 5,978 Kg - 13,179 lbs
Max Payload : NA
Fuel Tank Capacity : 387 gallon - 1,465 litre
Baggage Volume : NA
Seats Economy/General Class : 2 seats
Seats Business Class : 0
Seats First Class : 0
Cabin Height : NA
Cabin Width : NA
Cabin Length : NA
Exterior Length : 11 metre - 36.09 feet
Tail Height : NA
Fuselage Diameter : NA
Wing Span Rotor Diameter : 10.3 metre - 33.79 feet
Wing Tips : NA
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To generate propulsion for flight, the NAA T-2 Buckeye relies on two General Electric J85-GE-4 turbojets engines that produce 2,950 horsepower each. With such an engine configuration, the jet trainer is capable of reaching a maximum speed of 453 knots. The fuel tank capacity of the aircraft is 691 gallons, permitting a travel range of 909 nautical miles. In general, two pilots are required for the operation of the aircraft, and the aircraft may operate with a maximum takeoff weight of 13,179 pounds.

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