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model with structurally strengthening. The Condor III employs a benchseat and a single shared set of controls and so can be used by heavier pilots as well as for training.
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rules, including the category's maximum empty weight of 254 lb (115 kg). The aircraft has a standard empty weight of 240 lb (109 kg). It features a
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sailcloth. Its 32 ft (9.8 m) span wing is cable-braced from a single tube
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that was designed by Buddy Head, Bob
Carswell and Dave French and produced by
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does not incorporate suspension. The standard powerplant supplied was the
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The reported assembly time from the factory-supplied kit is 75 hours.
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which produces 40 hp (30 kW). The aircraft has a power-off
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The aircraft was produced in two versions, the Condor II and III.
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8th
Edition, page E-12. Cybair Limited Publishing, 2001.
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tubing, with the wings and tail surfaces covered in
136:. The aircraft closely resembles the contemporary
257:5 U.S. gallons (19 L; 4.2 imp gal)
117:The aircraft was designed to comply with the US
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271:snowmobile engine, 40 hp (30 kW)
143:The aircraft is made from bolted-together
105:. The aircraft was supplied as a kit for
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325:3.24 lb/sq ft (15.8 kg/m)
412:1980s United States ultralight aircraft
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301:60 mph (97 km/h, 52 kn)
292:19 mph (31 km/h, 17 kn)
286:55 mph (89 km/h, 48 kn)
20:
378:
376:
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359:Ultralight Aircraft Shopper's Guide
383:Virtual Ultralight Museum (n.d.).
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239:168 sq ft (15.6 m)
319:775 ft/min (3.94 m/s)
422:Single-engined pusher aircraft
1:
16:American ultralight aircraft
200:Specifications (Condor III)
119:FAR 103 Ultralight Vehicles
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193:side-by-side configuration
251:545 lb (247 kg)
245:240 lb (109 kg)
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267:twin-cylinder, in-line,
233:32 ft (9.8 m)
212:General characteristics
185:Basic single seat model
132:and a single engine in
113:Design and development
130:tricycle landing gear
71:Production completed
311:Maximum glide ratio:
134:pusher configuration
107:amateur construction
95:ultralight aircraft
33:Ultralight aircraft
417:Homebuilt aircraft
307:+5/-3 (calculated)
297:Never exceed speed
99:Seahawk Industries
82:Eipper Quicksilver
58:Seahawk Industries
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128:, open cockpit,
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36:Type of aircraft
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357:Cliche, Andre:
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103:Condor Aircraft
93:is an American
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62:Condor Aircraft
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43:National origin
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317:Rate of climb:
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138:Quicksliver MX
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91:Seahawk Condor
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77:Developed from
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323:Wing loading:
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284:Cruise speed:
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249:Gross weight:
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243:Empty weight:
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227:one passenger
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191:Two seats in
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101:and later by
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54:Manufacturer
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48:United States
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388:. Retrieved
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290:Stall speed:
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265:Kawasaki 440
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161:Kawasaki 440
157:landing gear
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123:cable-braced
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390:November 7,
277:Performance
261:Powerplant:
165:glide ratio
406:Categories
332:References
269:two-stroke
237:Wing area:
188:Condor III
305:g limits:
231:Wingspan:
225:Capacity:
205:Data from
182:Condor II
126:high-wing
385:"Condor"
177:Variants
167:of 7:1.
153:kingpost
145:aluminum
68:Status
24:Condor
365:
207:Cliche
155:. The
149:Dacron
219:Crew:
29:Role
392:2011
363:ISBN
263:1 ×
89:The
313:7:1
221:one
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373:^
340:^
140:.
109:.
394:.
299::
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