Fuji T-7

The Fuji T-7 aircraft is build by Fuji Heavy Industries.

The Fuji T-7 was developed to meet a requirement of Japan's Air Self Defence Force for a primary or basic trainer to replace the Fuji T-3. It was a modified version of the T-3, (itself descended via the Fuji KM-2 from the Beech T-34). It is a single-engined low-winged monoplane with an Rolls-Royce 250 turboprop engine.

Fuji T-7 has a seating capacity of 2.

Fuji T-7 has an overall length of 8.59 meters (28.1_ft). It has a wing span of 10.04 meters (32.8_ft). The overall height of 2.96 meters (9.7_ft). The wing area of Fuji T-7 is of about 16.5 sq.meters (177.6_sq.ft.). And it has a maximum take-off weight of about 1585 kilograms (3,487.0_lbs). Fuji T-7 can reach a maximum speed of about 376 km/hr (203.0_knots, 233.7_mph). Aircraft can reach a service height of about 7620 meters (24,917.4_ft).

The turboprop engine powered Fuji T-7 uses 1, Rolls-Royce (Allison) 250-B17F. It can deliver a total power of approximately 336 kilowatts (450.6_shaft horsepower).

Updated On: 18.10.15