Fletcher FD-25

{{Infobox aircraft begin

|name=FD-25 Defender

|image=Fletcher FD-25B Defender.jpg

|caption=

}}{{Infobox aircraft type

|type=Counterinsurgency aircraft

|manufacturer=Fletcher

|designer=John Thorp

|first flight=1953

|introduced=

|retired=

|status=

|primary user= Royal Cambodian Air Force

|more users= Republic of Vietnam Air Force

Royal Thai Police

|produced=

|number built=13

|variants with their own articles=

}}

The Fletcher FD-25 Defender was a light ground-attack aircraft developed in the United States in the early 1950s.

Design and development

Designed by John Thorp, the Defender was a conventional low-wing cantilever monoplane with fixed tailwheel undercarriage. Provision was made for two machine guns in the wings, plus disposable stores carried on underwing pylons. Construction throughout was all-metal, and the pilot sat under a wide perspex canopy.

Operational history

Three prototypes were built, two single-seaters and a two-seater, but no orders were placed by the US military. In Japan, however, Toyo acquired the rights to the design, and built around a dozen aircraft, selling seven (five single-seater attack versions and two two-seat trainers) to Cambodia,Grandolini 1988, p. 39. and four to Vietnam. One example (FD-25B JA3051){{Cite web |url=http://dansa.minim.ne.jp/a3723FujisawaToyoAC.htm |title=東洋航空工業株式会社、藤沢海軍航空隊の燃料庫庫 |access-date=2020-02-16 |archive-date=2020-02-16 |archive-url=https://web.archive.org/web/20200216091917/http://dansa.minim.ne.jp/a3723FujisawaToyoAC.htm |url-status=dead }} served with the Royal Thai Police.

Survivors

One example (FD-25B N240D) remains in an airworthy condition today and appeared at the EAA AirVenture Oshkosh airshow in 2010. Two (a single-seater{{Cite web|url=https://flyteam.jp/photo/1745541/L|title = 東洋航空工業 JA3092 東京都立産業技術高等専門学校 航空フォト | by VICTER8929さん 撮影2015年12月17日}} and a two-seater{{Cite web|url=https://flyteam.jp/photo/753101/L|title=東洋航空工業 - 東京都立産業技術高等専門学校 航空フォト | by kanade/Ryo@S.O.R.A.さん 撮影2013年03月25日}}) are on museum display at the Tokyo Metropolitan College of Industrial Technology in Japan.

Related development

The wing design of the Fletcher FU-24 aerial topdressing plane was loosely based on that of the FD-25 Defender.{{cite news |last1=Deerness |first1=Ray |title=The Fletcher Is Fifty |url=http://www.ahsnz.org.nz/content/fletcher-fifty |accessdate=5 February 2022 |work=Pacific Wings |issue=September 2004}} Almost 300 were built under licence in New Zealand from the mid-1950s and used for agricultural and skydiving operations.{{cite news |last1=Neal |first1=Tracy |title=Fletcher operators defend aircraft |url=http://www.stuff.co.nz/nelson-mail/news/4640889/Fletcher-operators-defend-aircraft |accessdate=29 January 2019 |work=Stuff |date=10 February 2011}}

Specifications

File:Fletcher N91316 fullerton 060271-1-.jpg, California, in 1971]]

{{Aircraft specs

|ref=Jane's All the World's Aircraft 1955–56Bridgman 1955, p. 260.

|prime units?=imp

|genhide=

|crew=1

|capacity=

|length m=

|length ft=20

|length in=11

|length note=

|span m=

|span ft=30

|span in=0

|span note=

|height m=

|height ft=6

|height in=3

|height note=

|wing area sqm=

|wing area sqft=150

|wing area note=

|swept area sqm=

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|swept area note=

|volume m3=

|volume ft3=

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|aspect ratio=6:1

|airfoil=NACA 65.5-415

|empty weight kg=

|empty weight lb=1228

|empty weight note=

|gross weight kg=

|gross weight lb=2500

|gross weight note=

|max takeoff weight kg=

|max takeoff weight lb=

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|fuel capacity={{convert|60|USgal|impgal L|abbr=on}}

|eng1 number=1

|eng1 name=Continental E-225-8

|eng1 type=6-cylinder, air-cooled, horizontally-opposed pistonengine

|eng1 kw=

|eng1 hp=225

|prop blade number=

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|perfhide=

|max speed kmh=

|max speed mph=187

|max speed kts=

|max speed note=at sea level

|max speed mach=

|cruise speed kmh=

|cruise speed mph=162

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

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|never exceed speed kmh=

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|minimum control speed kts=

|minimum control speed note=

|range km=

|range miles=630

|range nmi=

|range note=

|endurance=

|ceiling m=

|ceiling ft=16500

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=1725

|climb rate note=

|time to altitude=

|more performance=

|guns=2 × wing-mounted .30-in (7.62 mm) machine guns

|bombs= 2 × 250 lb (113 kg) bombs

|rockets=

  • 40 × 2.75 inch rockets or
  • 4 × 5-inch rockets or
  • 20 × 8 cm rockets

|missiles=

|hardpoints=

|hardpoint capacity=

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}}

See also

{{aircontent

|see also=

|related=

|similar aircraft=

|lists=

}}

References

Notes

{{Reflist}}

Bibliography

{{Refbegin}}

  • Bridgeman, Leonard (ed.). Jane's All the World's Aircraft 1955–56. New York: The McGraw-Hill Book Company, Inc.
  • Grandolini, Albert. "L'Aviation Royale Khmere: The first 15 years of Cambodian military aviation". Air Enthusiast (Bromley, UK: Fine Scroll) (Thirty-seven, September–December 1988): pp. 39–47. ISSN 0143-5450.
  • Taylor, Michael J. H. Jane's Encyclopedia of Aviation. London: Studio Editions. 1989. p. 393. {{ISBN|0-517-69186-8}}.
  • World Aircraft Information Files. London: Bright Star Publishing, 1985, pp. File 894 Sheet 25.

{{Refend}}