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trolley which would then be jettisoned, the aircraft landing on a ventral skid. Two large fuel tanks were mounted in the fuselage which, together with tip-tanks on the end of the wings, held 365 US Gallons (1,382 litres) of fuel. It was powered by a 135 hp (100 kW)
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to allow some sleep during the record flight, which was estimated to take about 80 hours. Sophisticated radio navigation gear was fitted to pinpoint the aircraft's position and to warn Jewett if it drifted off-course. The flight was planned to start and finish at
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While
Quickie Aircraft had made their name with the tandem-winged Quickie, their design for the round-the-world flight which was initially known as the "Big Bird", but later was named "Free Enterprise", was a more conventional single-engined high-winged
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kitplane, started development of an aircraft to attempt to make the first unrefuelled round-the-world flight. This would require a flight of at least 22,800 miles (36,700 km), almost double the existing unrefuelled
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long-range aircraft of the 1980s, designed to attempt the first unrefuelled flight round-the world flight. The Free
Enterprise was a single-engined high-winged
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to take advantage of stronger prevailing winds. It crashed, however, on 2 July 1982 while carrying out a test-flight near
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of conventional configuration. It first flew in March 1982, but was destroyed in a fatal crash later that year.
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The Free
Enterprise made its first public test flight on 8 March 1982, with the record flight scheduled for
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The plan was for Jewett to make the flight at high-altitude, to take advantage of
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tailwind expected. He was to carry out the flight on oxygen, using an
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In late 1979, Gene
Sheehan and Tom Jewett, co-founders of the
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Aircraft of comparable role, configuration, and era
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61 mph (98 km/h, 53 kn) (full flaps)
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337:24,500 mi (39,400 km, 21,300 nmi)
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95:Quickie Aircraft Corporation Free Enterprise
18:Quickie Aircraft Corporation Free Enterprise
458:"Round-the-world pilot killed in prototype"
156:all-metal wings were based on those of the
508:1980s United States experimental aircraft
325:200 mph (320 km/h, 170 kn)
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471:Jane's All The World's Aircraft 1982-83
246:Jane's All The World's Aircraft 1982–83
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446:"Around the world without refuelling"
454:, 30 January 1982. pp. 214–215.
272:51 ft 6 in (15.70 m)
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266:24 ft 8 in (7.52 m)
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473:. London:Jane's Yearbooks, 1982.
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343:20,000–30,000 ft (6,100–9,150 m)
201:Houston Intercontinental Airport
167:. The aircraft took off using a
523:Single-engined tractor aircraft
190:winds, with an average 50
27:American experimental aircraft
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1:
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419:30 January 1982, pp. 214–215.
284:4,250 lb (1,928 kg)
124:, builders of the successful
513:Aircraft first flown in 1982
464:, 24 July 1982. p. 193.
207:, flying eastwards over the
122:Quickie Aircraft Corporation
68:Quickie Aircraft Corporation
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369:Virgin Atlantic GlobalFlyer
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310:, 135 hp (101 kW)
278:1,700 lb (771 kg)
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138:Boeing B-52 Stratofortress
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303:air-cooled turbocharged
290:365 US Gallons (1,382 L)
140:bomber in January 1962.
58:United States of America
251:General characteristics
165:composite construction
134:flight distance record
116:Design and development
431:24 July 1982, p. 193.
150:tractor configuration
462:Flight International
451:Flight International
429:Flight International
417:Flight International
400:Taylor 1982, p. 564.
282:Max takeoff weight:
223:Operational history
97:(also known as the
44:long-range aircraft
518:High-wing aircraft
468:Taylor, John W. R.
235:, killing Jewett.
233:Mojave, California
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16:(Redirected from
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46:Type of aircraft
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174:PZL-Franklin
154:aspect ratio
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106:experimental
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83:Number built
42:Experimental
316:Performance
294:Powerplant:
176:air-cooled
152:. Its high-
502:Categories
439:References
359:Bede BD-2
305:flat-four
270:Wingspan:
244:Data from
196:autopilot
188:jetstream
161:sailplane
146:monoplane
110:monoplane
101:) was an
348:See also
209:Atlantic
178:flat-six
169:tricycle
103:American
99:Big Bird
264:Length:
126:Quickie
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335:Range:
229:autumn
493:Photo
377:Notes
258:Crew:
205:Texas
77:1982
38:Role
475:ISBN
296:1 ×
211:and
192:knot
93:The
148:of
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405:^
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87:1
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260:1
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