Fairchild Super 71

{{Infobox aircraft begin

|name= Fairchild Super 71

|image= File:Restored Super 71.JPG

|caption= Restored Fairchild Super 71

}}{{Infobox aircraft type

|type= Cargo transport

|manufacturer= Fairchild Aircraft Ltd. (Canada)

|designer=

|first flight= 31 October 1934

|introduced=

|retired=

|status=

|primary user=

|more users=

|produced=

|number built= 4

|developed from= Fairchild 71

|variants with their own articles=

}}

The Fairchild Super 71 was a Canadian parasol-mounted high-wing monoplane cargo aircraft built by Fairchild Aircraft Ltd. (Canada). The Super 71 was an entirely new design that was one of the first purpose-built civilian bush planes for use in remote and northern locales in Canada.Molson and Taylor 1982, p. 316.

File:Fairchild Super 71 CF-AUJ.jpg

Design and development

In 1933, the Fairchild Aircraft Company undertook a study of new designs based on their Model 71. A decision to mount a parasol wing above the fuselage coupled with a rear cockpit position, clearly distinguished this model from the rest of the Fairchild 71 series, although the company designation maintained the family lineage. The choice of the unusual cockpit was predicated on the need to have a large front cargo compartment as well as considering the load distribution in normal operation. In use, pilots found that forward vision was compromised to such an extent that few operators favoured the installation and when the Royal Canadian Air Force ordered the type, the specifications included a new cockpit position ahead of the wing and immediately behind the engine.[http://www.rcaf.com/aircraft/transports/super71/index.php?name=Super%2071 RCAF.com: The Aircraft: Fairchild Super 71]

The design featured a first-of-its-kind (for Canada) duralumin monocoque fuselage with a streamlined oval shape and strut-braced metal wing and tail surfaces. Wind-tunnel testing not only was used to model the fuselage shape but influenced the placement of the tailplane which was altered from its original T-tail position to a high-mounted tailplane intended to keep the tailplane out of the water spray on takeoff. Engine choices varied with six different powerplants offered: the {{cvt|493|hp}} Armstrong Siddeley Jaguar, {{cvt|520|hp}} Pratt & Whitney T1D1 Wasp, {{cvt|525|hp}} Pratt & Whitney S1D1 Wasp, {{cvt|560|hp}} Pratt & Whitney SD-1 Hornet, {{cvt|585|hp}} Wright SR-1820-F-41 Cyclone and {{cvt|610|hp}} Wright SR-1820-F-42 Cyclone.Molson and Taylor 1982, p. 317.

File:Fairchild Super71P.jpg

Operational history

Equipped with floats and powered by the {{cvt|525|hp}} S1D1 Wasp, the Super 71 prototype, CF-AUJ, flew for the first time on 31 October 1934. After the aircraft completed airworthiness tests. it was loaned to Canadian Airways which conducted operational trials in both Quebec and Ontario before the aircraft was written off after running into a submerged log and sinking off Sioux Lookout, Ontario on 3 October 1940. Although the airframe was salvaged, Fairchild did not replace the aircraft with a completed Super 71 still at the factory, as the company was involved in a complete redesign based on the Super 71P (for photographic) variant that had been developed for the RCAF. A new wing mount and the change to a front cockpit were the two visible changes but the variant also had provision for multiple cameras and additional radio equipment. Two examples were built and placed in service in 1936.Milberry 1979, p. 110.

The 71P had a chequered history as the type performed poorly in its aerial survey role with No. 666 crashing on 6 August 1937. The list of problems included structural problems with the floats, engine overheating (the prototype had the bottom half of the cowling removed to aid air circulation), adverse handling on the water and on the ground, and problems with the brakes.

The remaining aircraft, No. 665, was assigned to RCAF Station Trenton as an air ambulance but was not used extensively in this role.

File:Fairchild Super 71.1.JPG

The only surviving airframe is the prototype presently on display at the Royal Aviation Museum of Western Canada in Winnipeg, Manitoba.Fairchild Canada Super 71, CF-AUJ, Royal Aviation Museum of Western Canada. https://royalaviationmuseum.com/aircraft/fairchild-canada-super-71-cf-auj/

Variants

;Fairchild Super 71

:Prototype (second airframe completed but not flown)

;Fairchild Super 71P

:Production series with new cockpit location on the fuselage and new wing mounting (2 built)

Operators

;{{flag|Canada|1921}}

Specifications (Super 71)

{{Aircraft specs

|ref=Canadian Aircraft Since 1909Molson and Taylor 1982, p. 319.

|prime units? = imp

|crew=1

|length m=10.82

|length ft=35

|length in=6

|span m=17.67

|span ft=58

|span in=0

|height m=3.2

|height ft=10

|height in=6

|wing area sqm=34.56

|wing area sqft=392

|empty weight kg=1,733

|empty weight lb=3,817

|gross weight kg=3,178

|gross weight lb=7,000

|eng1 number=1

|eng1 name=Pratt & Whitney T1D1 Wasp 9-cylinder radial piston

|eng1 kw=388

|eng1 hp=525

|max speed kmh=223.6

|max speed mph=139

|cruise speed kmh=201.1

|cruise speed mph=125

|range km=1,314

|range miles=817

|climb rate note=or {{cvt|4.08|m/s|m/min|1|disp=out}}

|climb rate ms=4.08

|climb rate ftmin=800

}}

References

=Notes=

=Bibliography=

Bourgeois-Doyle, Richard I. Her Daughter the Engineer: The Life of Elsie Gregory MacGill. Ottawa: NRC Research Press, 2008. {{ISBN|978-0-660-19813-2}}.
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 Harold A. Taylor. Canadian Aircraft Since 1909. Stittsville, Ontario: Canada's Wings, Inc., 1982. {{ISBN|0-920002-11-0}}.