The prototype T-38 was first flown in 1959 powered by
2x 2100lb.s.t.(9.34kN) General Electrics and the production T-38A
entered service with the USAF in 1961. The Luftwaffe operated 46 for
training in the United States and the US Navy operated five examples.
Portugal was the only other user of the T-38A, 12 being delivered from
1977. Production ended in 1972 and although the type is still in service
with the USAF a small number have appeared in civil markings.
N903NA
c/n "63-8200"
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)
N908NA
c/n "65-10328"
N638TC
c/n N.5518
Northrop T-38A Talon Side view 1/144 scale
Side view 1/108 scale |