Fuji T-5: Difference between revisions
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==Operational history== |
==Operational history== |
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The KM-2Kai was ordered by the JMSDF as the T-5 in March [[1987 in aviation|1987]]<ref name="Military aircraft"/>, with deliveries of the KM2-Kai to the Japanese Self Defence Forces beginning in 1988, with a total of 40 being built. The T-5 serves with the 201 Training Squadron at [[Ozuki Air Field]]<ref> {{cite web |url= http://www.scramble.nl/jp.htm|title= Scramble|accessdate=2007-04-26 |format= |work= }}</ref>. The original KM-2 is no longer in service. |
The KM-2Kai was ordered by the JMSDF as the T-5 in March [[1987 in aviation|1987]]<ref name="Military aircraft"/>, with deliveries of the KM2-Kai to the Japanese Self Defence Forces beginning in 1988, with a total of 40 being built. The T-5 serves with the 201 Air Training Squadron at [[Ozuki Air Field]]<ref> {{cite web |url= http://www.scramble.nl/jp.htm|title= Scramble|accessdate=2007-04-26 |format= |work= }}</ref>. The original KM-2 is no longer in service. |
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==Operators== |
==Operators== |
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Revision as of 18:26, 4 April 2012
| T-5 | |
|---|---|
| Role | Basic trainer |
| Manufacturer | Fuji |
| First flight | 1988 |
| Introduction | 1988 |
| Primary user | Japan Maritime Self-Defense Force |
| Developed from | Fuji KM-2 |
Fuji T-5 or KM-2Kai is a Japanese turboprop-driven primary trainer aircraft, which is a development of the earlier Fuji KM-2. The student and the instructor sit side-by-side.
Design and development
The Fuji T-5 was developed by Fuji Heavy Industries as a replacement for the piston-engined Fuji KM-2 (itself a development of the Beechcraft T-34) as a primary trainer for the Japan Maritime Self-Defense Force. Fuji refitted a KM-2 with an Allison 250 turboprop engine in place of the original Lycoming piston engine, the resulting KM-2D first flying on 28 June 1984 [1] and being certified on 14 February 1985 [1][2]. The KM-2Kai is a further development of the KM-2D, with a modernised cockpit with side-by-side seating and a sliding canopy replacing the original KM-2's car type side doors [2] (which were retained by the KM-2D[1]).
The T-5 is an all-metal low-wing cantilever monoplane powered by an Allison 250-B17D turboprop with a three-bladed constant speed propeller. It has a retractable tricycle landing gear with the main gear retracting inwards and nose gear rearwards. The T-5 has an enclosed cabin with a sliding canopy and two side-by-side seats, and dual controls, in the aerobatic version and four seats in pairs in the utility version.
Operational history
The KM-2Kai was ordered by the JMSDF as the T-5 in March 1987[2], with deliveries of the KM2-Kai to the Japanese Self Defence Forces beginning in 1988, with a total of 40 being built. The T-5 serves with the 201 Air Training Squadron at Ozuki Air Field[3]. The original KM-2 is no longer in service.
Operators
Specifications (T-5)
Data from Jane's Aircraft Recognition Guide [4]
General characteristics
Performance
Armament
- None fitted as standard
References
- ^ a b c Taylor, JWR (Editor) (1988). Jane's All the World's Aircraft, 1988-1989. Coulsden, UK: Jane's Information Group. ISBN 0 7106-0867-5.
{{cite book}}:|first=has generic name (help) - ^ a b c d Donald, David (1996). Encyclopedia of World Military Aircraft. London: Aerospace Publishing. ISBN 1 874023 95 6.
{{cite book}}: Unknown parameter|coauthors=ignored (|author=suggested) (help) - ^ "Scramble". Retrieved 2007-04-26.
- ^ Rendall, David (1995). Jane's Aircraft Recognition Guide. Glasgow, UK: HarperCollinsPublishers. p. 505. ISBN 0-00-4709802.
- ^ a b Taylor, M J H (editor) (1999). Brassey's World Aircraft & Systems Directory 1999/2000 Edition. London: Brassey's. ISBN 1 85753 245 7.
{{cite book}}:|first=has generic name (help)