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Fokker F.14

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Fokker F.14
Type Seven/Nine passenger transport monoplane
Manufacturer Atlantic Aircraft
Maiden flight 1929
Primary user United States Army Air Corps

The Fokker F.14 was an American seven/nine passenger transport aircraft designed by Fokker and built by their Atlantic Aircraft factory in New Jersey.

Development

The F.14 was a typical Fokker designed single-engine transport but unusually it had a parasol-type high wing carried on struts above the fuselage. It had a fixed tailwheel landing gear. The pilot had an cockpit behind the passenger cabin.


Variants

F.14
Civil production version with a 525hp (391kW) Wright R-1750-3 radial engine.
F.14A
Civilian aircraft with 575hp (429kW) Pratt & Whitney Hornet radial engine
Y1C-14
Designation for 20 Hornet-powered examples bought for the United States Army Air Corps in 1931, later became the C-14.
Y1C-14A
Last of the 20 Y1C-14s re-engined with a 575hp (429kW) Wright R-1820-7 Cyclone.
Y1C-14B
Re-engined with a 525hp (391kW) Pratt & Whitney Hornet R-1690-5 Hornet engine.
Y1C-15
Conversion of the ninth Y1C-14 as an air ambulance.
Y1C-15A
Y1C-15 re-engined with a 575hp (429kW) Wright R-1820 Cyclone, later C-15A.

Operators

Template:USA

Specifications (F.14)

Template:Aerospecs


Related lists

References

  • John Andrade, U.S.Military Aircraft Designations and Serials since 1909, Midland Counties Publications, 1979, ISBN 0 904597 22 9 (Page 62)
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1878.

Template:USAF transports Template:Fokker aircraft


This article is licensed under the GNU Free Documentation License.
It uses material from the Wikipedia article "Fokker F.14".