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engine. The aircraft has an empty weight of 1,650 lb (750 kg) and a gross weight of 2,250 lb (1,020 kg), giving a useful load of 600 lb (270 kg). With full fuel of 50 U.S. gallons (190 L; 42 imp gal) the payload is 300 lb (140 kg).
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wing designs and in particular the stability, controllability and capability of the configuration. The design was intended to be easily scalable to much larger aircraft. It has no complex curves and was designed to be easy to construct. It features a cantilever
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proof. Its standard day, sea level take off run is 1,200 ft (366 m) and landing roll is 1,000 ft (305 m).
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363:, page 152. Werner & Werner Corp, Santa Monica CA, 1977.
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in 1974, but its registration was cancelled in August 2013.
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that was designed and produced by Ralph V. Sawyer of
124:The Skyjacker II was designed to explore ultra-low
248:50 U.S. gallons (190 L; 42 imp gal)
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470:1970s United States experimental aircraft
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284:130 mph (210 km/h, 110 kn)
290:105 mph (169 km/h, 91 kn)
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302:525 mi (845 km, 456 nmi)
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296:45 mph (72 km/h, 39 kn)
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16:American homebuilt research aircraft
421:"N-Number Inquiry Results - N7317"
230:18 ft 0 in (5.49 m)
224:18 ft 0 in (5.49 m)
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156:The aircraft is made from sheet
116:and as such only one was built.
445:Photos of the Sykjacker in 2010
417:Federal Aviation Administration
185:Federal Aviation Administration
475:Single-engined pusher aircraft
308:400 ft/min (2.0 m/s)
183:in the United States with the
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382:"American airplanes: Sa - Si"
327:"American airplanes: Sa - Si"
242:2,250 lb (1,021 kg)
191:Specifications (Skyjacker II)
490:Aircraft first flown in 1975
76:Production completed (1974)
269:, 200 hp (150 kW)
258:four cylinder, air-cooled,
236:1,650 lb (748 kg)
179:The sole example built was
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168:The aircraft proved to be
137:enclosed cockpit under a
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450:Photos of the Skyjacker
361:1978 Aircraft Directory
203:General characteristics
149:and a single engine in
120:Design and development
256:Lycoming IO-360-A1B6D
162:Lycoming IO-360-A1B6D
143:tricycle landing gear
110:Lancaster, California
401:: CS1 maint: year (
151:pusher configuration
419:(18 October 2013).
102:Sawyer Skyjacker II
485:Homebuilt aircraft
380:Aerofiles (n.d.).
106:homebuilt aircraft
36:homebuilt aircraft
480:Mid-wing aircraft
359:Plane and Pilot:
133:, a two-seats-in-
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39:Type of aircraft
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424:. Retrieved
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334:. Retrieved
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90:Number built
68:3 July 1975
33:Experimental
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275:Performance
264:four stroke
252:Powerplant:
147:wheel pants
459:Categories
426:18 October
387:18 October
313:References
181:registered
228:Wingspan:
216:Capacity:
196:Data from
81:Produced
57:Designer
397:cite web
158:aluminum
141:, fixed
131:mid-wing
336:10 June
222:Length:
73:Status
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300:Range:
135:tandem
210:Crew:
170:stall
145:with
84:1974
29:Role
428:2013
403:link
389:2013
365:ISBN
338:2022
254:1 ×
174:spin
172:and
100:The
94:One
212:one
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395:{{
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