Fairchild 71

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Fairchild 71
Fairchild 71 in RCAF colours
Role passenger or cargo transport
Manufacturer Fairchild Aircraft
Fairchild Aircraft Ltd. (Canada)
First flight 1926

The Fairchild 71 was an American high-wing monoplane passenger and cargo aircraft built by Fairchild Aircraft and later built in Canada by Fairchild Aircraft Ltd. (Canada) for both military and civilian use as a rugged bush plane.

Contents

Design and development [edit]

The Fairchild Aircraft Company undertook a progressive development of the Fairchild FC-2W2 light transport. Its first improvement was the FC-2, whose several improvements included:

  • Slightly swept-back wings;
  • Wingspan increased to 50 feet;
  • Engine power nearly doubled;
  • Interior changes to improve passenger comfort.

The FC-2 first flew in 1926.

The FC-2W was a further development, featuring:

  • Camera bay for vertical aerial photography;
  • Low-cut aft windows for oblique aerial photography.

The FC-2 and FC-2W continued the usage of fabric-covered welded steel tubing for fuselage and empennage construction, and strut-braced wooden-structure fabric-covered wing.

The FC-2W, later known as the Model 71, was built in the United States between 1928 and 1930. In 1929 Fairchild formed a company in Canada (Fairchild Aircraft Limited) at Longueuil, Quebec in 1929 to support the Canadian operators of Fairchild aircraft. The Canadian company also set up a factory production line for the Model 71, developing a variant for the Canadian military. The Canadian-built aircraft differed from the US version in that all the passenger-comfort features were removed, and the craft were built specifically for aerial photography.[1]

Fairchild 71 in original PanAm colors

Operational history [edit]

The United States Army Air Service acquired one Model 71 for evaluation; it was designated XC-8, and later re-designated XF-8 and used for photographic work.

Eight more service-test aircraft, designated YF-1 were ordered; all nine were later re-designated C-8.

The Royal Canadian Air Force (RCAF), another major military operator, evaluated the Fairchild 71 in mid-June 1930. Thirty four RCAF FC-71s were operated from 1930 to 1946. Along with the earlier FC-2 series, the RCAF FC-71 was utilized primarily in the aerial photographic survey role as well as northern transport. In November 1934, the RCAF transferred the FC-71s to the five detachments flying in the amalgamated Maritimes No. 5 (Flying Boat) Squadron at RCAF Station Dartmouth. The squadron flew the FC-71 extensively on anti-smuggling (rum running) and illegal immigration patrols for the Royal Canadian Mounted Police (RCMP).[1]

Most of the Model 71 production ended up in the hands of bush plane operators in Canada and the United States. Civilian operators likewise found the 71 a rugged, reliable and highly useful utility transport, well suited for northern and remote operations.

Variants [edit]

Fairchild 71
Initial production variant
Fairchild 71A
Production variant with increased swept back on wings and improved interior
Fairchild 71C
Canadian-built version
Fairchild 71-CM
Canadian-built version with metal-skinned fuselage
Fairchild Super 71
Floatplane version with new fuselage and greater span wing
Fairchild 51/71
Canadian-built version with wings of Model 51 and fuselage of Model 71

United States military designations [edit]

One of the YF-1 aircraft
XC-8
One prototype Fairchild 71, later re-designated XF-1 when modified for photo survey.
YF-1
Eight service-test aircraft
C-8
YF-1 re-designated
C-8A
F-1A re-designated
XF-1
XC-8 re-designated for photo-survey
YF-1
Eight Fairchild 71 aircraft for evaluation with provision for seven passenger seats, later re-designated C-8A.
F-1A
Production aircraft (Fairchild 71A), six built later redesignated C-8A.
J2Q-1
One Fairchild 71 for evaluation by the United States Navy, re-designated XR2Q-1.

Operators [edit]

Military operators [edit]

 Canada
 United States

Specifications (Model 71C) [edit]

Data from Canadian Aircraft Since 1909[2]

General characteristics

  • Crew: 1
  • Capacity: 8
  • Length: 35 ft 10.25 in (10.93 m)
  • Wingspan: 50 ft 0 in (15.39 m)
  • Height: 9 ft 4 in (2.84 m)
  • Wing area: 309.6 ft2 (28.76 m2)
  • Empty weight: 3,168 lb (1,438 kg)
  • Gross weight: 6,000 lb (2,724 kg)
  • Powerplant: 1 × Pratt & Whitney Wasp B/C 9-cylinder radial piston, 420 hp ( kW) each

Performance

  • Maximum speed: 132 mph (212.4 km/h)
  • Cruise speed: 106 mph (170.5 km/h)
  • Range: 817 miles (1,314 km)
  • Service ceiling: 11,000 ft (3,353 m)
  • Rate of climb: 600 ft/min (3 m/s)

See also [edit]

Related lists

References [edit]

Notes [edit]

Bibliography [edit]

  • Donald, David, ed. The Encyclopedia of World Aircraft. Etobicoke, Ontario, Canada: Prospero Books, 1997. ISBN 1-85605-375-X.
  • Milberry, Larry. Aviation In Canada. Toronto: McGraw-Hill Ryerson Ltd., 1979. ISBN 0-07-082778-8.
  • Molson, Ken M. and Taylor, Harold A. Canadian Aircraft Since 1909. Stittsville, Ontario: Canada's Wings, Inc., 1982. ISBN 0-920002-11-0.

External links [edit]