About: Fuji KM-2

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An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

The Fuji KM-2 is a Japanese propeller-driven light aircraft, which was developed by Fuji Heavy Industries from the Beech T-34 which Fuji built under licence. Various versions have been used as primary trainers by the Japan Self-Defense Forces, with the KM-2B remaining in service with the Japan Air Self-Defense Force

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	Fuji KM-2
rdfs:comment	The Fuji KM-2 is a Japanese propeller-driven light aircraft, which was developed by Fuji Heavy Industries from the Beech T-34 which Fuji built under licence. Various versions have been used as primary trainers by the Japan Self-Defense Forces, with the KM-2B remaining in service with the Japan Air Self-Defense Force
sameAs	dbr:Fuji_KM-2
dcterms:subject	dbkwik:resource/FUwnXua-41_8iqKSDDJhpQ== dbkwik:resource/I8GOm9KQ7JiIg_yG6YIF6g== dbkwik:resource/iMlwGhmMJJV362ccAvHqRg== dbkwik:resource/NtRKpkxNOhhnrJ_G0G1S3g==
dbkwik:military/pr...iPageUsesTemplate	dbkwik:resource/AaGpNMKXeCEx6k1ovZIRVg== dbkwik:resource/LgcM0IFcJS1HLKEAaCvrJw== dbkwik:resource/ODD2urn6xOTu5tfNx3dKHA== dbkwik:resource/ZbtrzLFw6TNwE1208cbZTA== dbkwik:resource/lcZWJ85OOwF-hB15BhcEBA== dbkwik:resource/pTEKXoXwy_QJD-cbbKl3EQ== dbkwik:resource/8c65HClsHBgkxfJdWXaRHw== dbkwik:resource/cbsrEQx1xy51eXd2rIQtLg== dbkwik:resource/7_dwHHF8FUA3XhGjI4-8Fw==
max takeoff weight alt	3860.0
max speed more	at
climb rate main	7.7
number of props	1(xsd:integer)
length alt	792.48
span main	10.00 m
cruise speed main	304.0
cruise speed alt	158(xsd:integer)
height alt	292.1
Introduced	1962(xsd:integer)
primary user	dbkwik:resource/fu_q7o0Ci_sx1VL5uabceg==
Type	Primary trainer
type of prop	air-cooled flat-six piston engine
range alt	526(xsd:integer)
length main	7.94 m
power alt	340.0
area main	16.49
power main	254.0
stall speed alt	54(xsd:integer)
height main	2.92 m
span alt	1000.76
range main	975.0
Manufacturer	dbkwik:resource/gS_PnMaCuwkquLC7ZA6LEA==
max speed main	378.0
engine (prop)	Lycoming IGSO-480-A1A6
stall speed more
climb rate alt	1520.0
ceiling main	8,170 m
empty weight main	1134.0
stall speed main	100.0
Developed From	dbkwik:resource/02ZbW6B7LcKtFNb7B5sSbQ==
area alt	177.6
First Flight	1962-01-16(xsd:date)
more users	dbkwik:resource/zBT7gEk8hBNvw30R6o9xuA== dbkwik:resource/pZvUB24fo_G2KKAPvcvDvA==
max speed alt	204(xsd:integer)
jet or prop?	prop
empty weight alt	2500.0
plane or copter?	plane
ceiling alt	26,800 m
max takeoff weight main	1750.0
variants with their own articles	Fuji T-3 Fuji T-5 Fuji T-7
cruise speed more	at
Crew	2(xsd:integer)
Number Built	64(xsd:integer)
ref	Jane's All The World's Aircraft 1966–1967
abstract	The Fuji KM-2 is a Japanese propeller-driven light aircraft, which was developed by Fuji Heavy Industries from the Beech T-34 which Fuji built under licence. Various versions have been used as primary trainers by the Japan Self-Defense Forces, with the KM-2B remaining in service with the Japan Air Self-Defense Force
is Developed From of	Fuji T-3 Fuji T-5
is variants with their own articles of	Fuji LM-1 Nikko

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