| 词条 | Fuji T-7 | |||||||||||||||||||
| 释义 |
The Fuji T-7 (previously T-3 Kai) is a Japanese primary trainer aircraft built by Fuji Heavy Industries for the Japan Air Self-Defense Force. A development of Fuji's earlier T-3 trainer, it is a single-engined monoplane powered by a turboprop engine. Design and developmentThe 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. The resultant aircraft was a modified version of the T-3, (itself descended via the Fuji KM-2 from the Beech T-34) and shared the single-engined low-winged monoplane layout of the T-3, but replaced the Lycoming piston engine with an Allison 250 turboprop engine. The T-7 was selected in preference to the Pilatus PC-7 in 1998,[1] but this decision was cancelled and the competition restarted after a corruption scandal arose, with several managers from Fuji being arrested for bribing an official in Japan's ruling Liberal Democratic Party.[2] Fuji re-entered the T-7 (then known as the T-3 Kai) and again won the restarted competition in September 2000. Operational historyThe first production aircraft was handed over to the JASDF in September 2002.[3] Operators
Specifications (T-7){{aircraft specifications|plane or copter?= |jet or prop?=prop |ref="Military Aircraft Directory", Flight International[3] |crew=2 |capacity= |length main= 8.59 m |length alt= 28 ft 2 in |span main= 10.04 m |span alt= 32 ft 11 in |height main= 2.96 m |height alt= 9 ft 9 in |area main= 16.50 m² |area alt= 177.60 ft² |airfoil= |empty weight main= |empty weight alt= |loaded weight main= |loaded weight alt= |useful load main= |useful load alt= |max takeoff weight main= 1,585 kg |max takeoff weight alt= 3,487 lb |more general= |engine (prop)=Rolls-Royce (Allison) 250-B17F |type of prop=turboprop |number of props=1 |power main= 336 kW |power alt= 450 shp |power original= |max speed main= 376 km/h |max speed alt= 203 knots, 234 mph |cruise speed main= 296 km/h |cruise speed alt= 160 knots, 184 mph |stall speed main= 103 km/h |stall speed alt= 56 knots, 64 mph |never exceed speed main= |never exceed speed alt= |range main= |range alt= |ceiling main= 7,620 m |ceiling alt= 25,000 ft |climb rate main= |climb rate alt= |loading main= |loading alt= |thrust/weight= |power/mass main= |power/mass alt= |more performance= |armament= |avionics= }} See also{{aircontent||related=
|similar aircraft=
|lists= |see also= }} ReferencesNotes1. ^Mollet 1998, p.31. 2. ^Jeziorski 2000, p.20 3. ^1 Ripley 25–31 May 2004, p.57. Bibliography{{refbegin}}
External links{{commons category|Fuji T-7}}
6 : Fuji aircraft|Japanese military trainer aircraft 2000–2009|Single-engined tractor aircraft|Low-wing aircraft|Single-engined turboprop aircraft|Aircraft first flown in 2002 |
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