trainer / light attack
one pilot + student
2 x 3,520 lbs. ea.
42 ft. 8 in.
32 ft. 7 in.
The origin of the Kawasaki T-4 can be traced back to 1981. That is when Japan asked a team of aeronautical engineers to come up with a replacement for their aging trainer aircraft. All major Japanese aircraft companies were asked to bid on the engineering design.
In 1983 Kawasaki was awarded a contract to produce a total of 212 aircraft. The Kawasaki T-4 first took to the sky in July of 1985, with deployment taking place in 1988.
The Kawasaki T-4 uses conventional construction materials in its design. However the aircraft is extremely maneuverable. The maneuverability is the result of a wing design incorporating a notched leading-edge with a flattened top leading to a highly curved wing top at the trailing edge.
At sub-sonic speeds the wing is more resistant to stalls, produces less drag, and has more lift than conventional wings. These are highly desirable qualities for a training aircraft.
The dual redundant flight control system of the Kawasaki T-4 is hydraulically operated. Included are anti-skid brakes.
The pressurized cockpit has good all-around visibility. The instructor's seat in the rear cockpit is about 10 1/2 inches higher than the front seat. Avionics accommodate day/night all weather conditions, navigation, and a head-up display.
The Kawasaki T-4 has hard points under each wing for weapons or fuel tanks, plus the ability to fit an instrument pylon, ordnance, or an additional fuel tank on the aircraft center line.
Flying the Kawasaki T-4 makes it a pilot favorite. It has excellent power to weight and a low wing loading which make for great maneuverability. The aircraft is responsive, even at low landing speeds, yet tracks straight in moderate cross-winds. Ground crews appreciate the reliability and low maintenance of the Kawasaki T-4.
A total of 212 Kawasaki T-4 aircraft were built.