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The
Revolution II has a typical empty weight of 800 lb (360 kg) and a gross weight of 1,400 lb (640 kg), giving a useful load of 600 lb (270 kg). With full fuel of 17 U.S. gallons (64 L; 14 imp gal) the payload for the pilot, passenger and baggage is
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and has a wing area of 126.0 sq ft (11.71 m). The acceptable power range is 85 to 160 hp (63 to 119 kW) and the standard engines used are the 125 hp (93 kW)
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The standard day, sea level, no wind takeoff with a 125 hp (93 kW) engine is 400 ft (122 m) and the landing roll is 450 ft (137 m).
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132:. When it was available the aircraft was supplied as a kit or in the form of plans for amateur construction.
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The aircraft is intended to be reminiscent of the open cockpit monoplanes of the 1930s, such as the
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The aircraft is made from a combination of wood and metal tubing, covered in
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AeroCrafter - Homebuilt
Aircraft Sourcebook, Fifth Edition
220:, although a total of 30 had been registered at one time.
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287:17 U.S. gallons (64 L; 14 imp gal)
185:. Its 28.00 ft (8.5 m) span wing lacks
445:"Space Walker II Make / Model Inquiry Results"
398:, page 293. BAI Communications, 15 July 1998.
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420:"Revolution II Make / Model Inquiry Results"
582:1990s United States civil utility aircraft
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151:, the Revolution II features a cantilever
340:160 mph (260 km/h, 140 kn)
325:115 mph (185 km/h, 100 kn)
577:1990s United States ultralight aircraft
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346:300 mi (480 km, 260 nmi)
38:A Warner Revolution II equipped with a
364:11.1 lb/sq ft (54 kg/m)
331:42 mph (68 km/h, 36 kn)
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269:126.0 sq ft (11.71 m)
572:1990s United States sport aircraft
263:28 ft 0 in (8.53 m)
257:19 ft 8 in (5.99 m)
124:that was designed and produced by
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358:1,200 ft/min (6.1 m/s)
193:or the 125 hp (93 kW)
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587:Single-engined tractor aircraft
441:Federal Aviation Administration
416:Federal Aviation Administration
218:Federal Aviation Administration
147:Developed from the single-seat
224:Specifications (Revolution II)
216:in the United States with the
212:In May 2014, 19 examples were
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352:14,000 ft (4,300 m)
310:2-bladed metal, fixed pitch
297:four cylinder, air-cooled,
281:1,400 lb (635 kg)
201:498 lb (226 kg).
16:American homebuilt aircraft
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304:, 125 hp (93 kW)
567:Warner Aerocraft aircraft
275:800 lb (363 kg)
165:conventional landing gear
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236:General characteristics
171:and a single engine in
159:open cockpit with dual
116:, also marketed as the
143:Design and development
173:tractor configuration
84:Production completed
114:Warner Revolution II
518:Fixed-wing aircraft
208:Operational history
149:Warner Revolution I
105:Warner Revolution I
597:Homebuilt aircraft
336:Never exceed speed
122:homebuilt aircraft
50:Homebuilt aircraft
592:Low-wing aircraft
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191:Continental O-240
130:Seminole, Florida
120:, is an American
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509:Warner Aerocraft
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471:Official website
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75:Warner Aerocraft
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53:Type of aircraft
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118:Space Walker II
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60:National origin
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356:Rate of climb:
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100:Developed from
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251:one passenger
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155:, a two-seat
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65:United States
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526:Revolution I
448:. Retrieved
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423:. Retrieved
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394:Purdy, Don:
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329:Stall speed:
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94:At least 30
90:Number built
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316:Performance
308:Propellers:
299:four stroke
291:Powerplant:
231:AeroCrafter
169:wheel pants
161:windshields
561:Categories
369:References
267:Wing area:
214:registered
546:Sportster
261:Wingspan:
249:Capacity:
229:Data from
511:aircraft
163:, fixed
153:low wing
255:Length:
137:Ryan ST
81:Status
450:May 7,
425:May 7,
402:
344:Range:
157:tandem
243:Crew:
187:flaps
180:doped
167:with
46:Role
452:2014
427:2014
400:ISBN
293:1 ×
112:The
245:one
128:of
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377:^
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494:t
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338::
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
