- Fuji T-3
infobox Aircraft
name = T-3
caption =
type = Primary trainer
manufacturer =Fuji
designer =
first flight = 1974
introduced =
retired =
produced =
number built = 50
status =
unit cost =
primary user =Japan Air Self Defense Force
more users =
developed from =Fuji KM-2
variants with their own articles =The Fuji T-3 is a primary military
trainer aircraft used by theJapan Air Self Defense Force , manufactured byFuji Heavy Industries . Its first flight was in 1974. In the course of its service life, 50 units were produced. It is being replaced by theFuji T-7 .Development
The KM-2B was a further development of the
Fuji KM-2 (itself a four seat development of theT-34 Mentor with a more powerful engine) for use as a primary trainer for the Japan Air Self-Defense Force (JASDF). It combined the structure and engine of the KM-2 with the tandem cockpit of the T-34 Mentor, first flying on17 January 1978 cite book |last= Donald|first=David |coauthors= Lake, Jon (editors) |title= Encyclopedia of World Military Aircraft |year= 1996 |publisher= Aerospace Publishing|location= London |isbn= 1 874023 95 6] . Fifty were purchased by the JASDF as the Fuji T-3, production continuing until 1982 cite book|author=Donald, David (Editor)|title = The Encyclopedia of World Aircraft|year = 1997|publisher = Aerospace Publishing|location=London|isbn= 1-85605-375-X] .Operational history
The Fuji T-3 served with the 11 and 12 Hiko Kyoikudan (flying training wings) of the JASDF. It is currently being replaced with the
Fuji T-7 , aturboprop variant of the T-3 cite book |last=Taylor|first=M J H (editor) | title = Brassey's World Aircraft & Systems Directory 1999/2000 Edition | year = 1999 | publisher = Brassey's |location=London| isbn = 1 85753 245 7 ] with a 400 shp Allison 250 engine.Operators
;JPN:
Japan Air Self-Defence Force pecifications (T-3)
aircraft specifications
plane or copter?=plane
jet or prop?=propref=Jane's Aircraft Recognition Guide, Jane's All the World's Aircraft, 1976-1977 [cite book|title=Jane's Aircraft Recognition Guide|last=Rendall|first=David|pages=p.505|year=1995|id=ISBN 0-00-4709802|publisher=HarperCollinsPublishers|location=Glasgow, UK] cite book| last = Taylor| first = JWR (Editor)| title = Jane's All the World's Aircraft, 1976-1977 | year = 1976| publisher = Macdonald and Jane's|location=London| isbn =0 354 00538 3 ]
crew=2: student, instructor
length main=8.04 m
length alt=26 ft 4½ in
span main=10.0 m
span alt=32 ft 9¾ in
height main=3.02 m
height alt=9 ft 11 in
area main=16.5 m²
area alt=178 ft²
empty weight main=1,120 kg
empty weight alt=2,460 lb
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main=1,510 kg
max takeoff weight alt=3,329 lbengine (prop)=Lycoming IGSO-480
type of prop= 6-cylinder, horizontally-opposed aircooledpiston engine
number of props=1
power main=254 kW
power alt=340 hpmax speed main=377 km/h
max speed alt=203 knots, 234 mph
max speed more=at 4,875 m (16,000 ft)
cruise speed main=254 km/h
cruise speed alt=137 knots, 158 mph
cruise speed more=Economy cruise at 2,440 m (8,000 ft)
never exceed speed main=413 km/h
never exceed speed alt=223 knots, 257 mph
never exceed speed more=EASrange main=1,038 km
range alt=560 nm, 645 mi
ceiling main=8,170 m
ceiling alt=26,800 ft
climb rate main=7.7 m/s
climb rate alt=1,520 ft/min
loading main=91.5 kg/m²
loading alt=18.7 lb/ft²ee also
aircontent
related=
*Fuji KM-2
*Fuji T-5
*Fuji T-7 similar aircraft=
lists=
*List of military aircraft of Japan see also=
References
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