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Northrop T-38A Talon  


The prototype YT-38 supersonic trainer was first flown in 1959. It entered service as the T-38A with the USAF in 1961 and is still operational today. When production ended in 1972 the USAF had received 1187 examples of the T-38A. 46 were operated by the Luftwaffe for training in the United States and 12 were supplied to the Portuguese Air Force. The AT-38B is a fighter trainer version with weapons hardpoints for practice bombs. Many T-38A's have undergone upgrading to T-38C standard with improved avionics. A T-38C is illustrated below.

68-8121                 c/n T6126                          USA

2 seat supersonic trainer first flown in 1959

Engines: 2x 3850lb.s.t.(17.13kN) GE J85-GE-5A                                                                                Length: 46’4.5"(14.14m)                                                                                 Height: 12’10.5"(3.92m)Wingspan: 25’3"(7.7m)                                                                                                 No.built: 1187 Range: 1090miles(1754km)                                                             Cruising speed: 575mph(925kmh) Empty weight: 7164lb(3250kg)                                           Maximum take-off weight: 12,093lb(5485kg)

A T-38A is shown below.

 

        64-13247              c/n N5676                                       

 

64-13301                c/n N5730                             

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