Fuji T-1A

Once the Japanese aircraft industry had been cleared to begin production again in 1953, the government awarded a number of substantial contracts to Fuji with the aim of producing indigenous jet-powered aircraft to replace American-supplied piston-engined T-6 Texans. The company had already constructed a small turbojet engine to power just such an aircraft, hut the first T1F1 was powered by an imported Bristol Siddeley Orpheus engine. The design leant heavily on the North American F-86 Sabre. Designated T-1 A by the JASDF, the Orpheus powered aircraft began to enter service in 1961 and by July of the following year 40 had been delivered. The company also produced a T1-B version, powered, or rather underpowered, by the Japan Jet Engine Co. J3-3. This engine delivered only two-thirds of the thrust of the Bristol engine.

Fuji T-1A Specifications

Country of origin: Japan

Type: two-seat intermediate jet trainer

Powerplant: one 1814kg (4000lb) Rolls-Royce (Bristol Siddeley) Orpheus Mk 805 turbojet

Fuji T-1APerformance: maximum speed 925km/h (575mph) at high altitude; service ceiling 14,400m (47,250ft); range 1860km (1156 miles) at high altitude with drop tanks

Weights: empty 2420kg (5335lb); maximum take-off 5000kg (11,023lb)

Dimensions: wingspan 10.49m (34ft 5in); length 12.12m (39ft 9.2in); height 4.08m (13ft 4.6in); wing area 22.22sq m (239.2sq ft)

Armament: optional 0.5in Browning M53-2 gun in nose; two underwing pylons with provision for up to 680kg (1500lb) of stores, including bombs, Sidewinder air-to-air missiles, or gun pods; usually only tanks carried.