| 词条 | Fairchild 22 | |||||||||||||||
| 释义 |
The Fairchild 22 Model C7 was an American two-seat touring or training monoplane designed and built by the Kreider-Reisner division of the Fairchild Aircraft Corporation at Hagerstown, Maryland. DevelopmentThe aircraft was designed by Kreider-Reisner during negotiations by Sherman Fairchild to take a major share in the company. Marketed as the Fairchild 22 Model C7 the aircraft was certified in March 1931. The Fairchild 22 was a mixed-construction, braced parasol-wing monoplane with a fixed tailwheel landing gear and a braced tail unit. It had two tandem open cockpits and was initially powered by an 80 hp (60 kW) Armstrong Siddeley Genet radial engine. After test flying the prototype the first production aircraft were re-engined with a 75 hp (56 kW) Michigan Rover inverted inline engine. The aircraft was fitted with both inline and radial piston engines. Variants
Powered by a 75hp Michigan Rover four-cylinder inverted inline piston engine (13 built)
Powered by a 95hp Cirrus Hi-Drive four-cylinder inverted inline piston engine (58 built).
Powered by a 125hp Menasco C-4 Pirate four-cylinder inverted inline piston engine (eight built).
Powered by a 90hp Wright Gipsy four-cylinder upright inline piston engine (one C-7C and 22 C-7D built).
Powered by a 125hp Warner Scarab seven-cylinder radial piston engine (11 built).
Powered by a 145hp Warner Super Scarab seven-cylinder radial piston engine (nine built).
Aerobatic version, powered by a 145hp Warner Super Scarab seven-cylinder radial piston engine (six built).
Military designation for one Scarab powered Model 22 impressed into service and used by NACA.
Experimentally designed wing added to the 1933 Fairchild 22 owned by Charles Townsend Ludington under the Ludington-Griswold Incorporated company, Saybrook, CT. Test flown in 1944, the wing had a series of flaps and wing tip fins. The design proved disappointing and the airplane was later sold. Specifications (C7F){{aerospecs|ref=The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1640 |met or eng?=eng |crew=two |capacity= |length m=6.78 |length ft=22 |length in=3 |span m=10.06 |span ft=33 |span in=0 |swept m= |swept ft= |swept in= |rot number= |rot dia m= |rot dia ft= |rot dia in= |dia m= |dia ft= |dia in= |width m= |width ft= |width in= |height m=2.41 |height ft=7 |height in=11 |wing area sqm=16.07 |wing area sqft=173 |swept area sqm= |swept area sqft= |rot area sqm= |rot area sqft= |volume m3= |volume ft3= |aspect ratio= |empty weight kg=500 |empty weight lb=1102 |gross weight kg=794 |gross weight lb=1750 |lift kg= |lift lb= |eng1 number=1 |eng1 type=Warner Super Scarab 7-cyliner radial piston engine |eng1 kw=108 |eng1 hp=145 |eng1 kn= |eng1 lbf= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 type= |eng2 kw= |eng2 hp= |eng2 kn= |eng2 lbf= |eng2 kn-ab= |eng2 lbf-ab= |max speed kmh=214 |max speed mph=133 |max speed mach= |cruise speed kmh= |cruise speed mph= |range km=563 |range miles=350 |endurance h= |endurance min= |ceiling m=6095 |ceiling ft=20,000 |glide ratio= |climb rate ms= |climb rate ftmin= |sink rate ms= |sink rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }}{{aircontent |see also= |related= |similar aircraft= |sequence= |lists= }} Operators{{COL}}
References
External links{{commons category-inline|Fairchild 22}}{{Fairchild aircraft}}{{USN transports}}http://www.sim-outhouse.com/sohforums/showthread.php/17-The-Ongoing-Mystery-Aircraft-Thread-Part-Deux?p=878843&viewfull=1 5 : United States civil utility aircraft 1930–1939|Fairchild aircraft|Parasol-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1931 |
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