Condor
ultralight, Condor II ultralight aircraft, Seahawk
Industries Condor ultralight aircraft, Ultralight News
newsmagazine.
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Ultralight News is a directory of aircraft that generally fit
into what are described as ultralight aircraft, advanced ultralight
aircraft,
ultralite aircraft, ultralight planes, experimental
aircraft, amateur built aircraft, or homebuilt
or kit built aircraft in the United States and Canada. These include weight shift aircraft, more commonly known as microlight trikes, powered parachutes, and powered para-gliders.
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Condor
ultralight, ultra lite aircraft, amateur built, experimental,
homebuilt aircraft.
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The Condor is a single seat, high wing, wire braced ultralight, featuring
a tri-cycle landing gear suspension system, in a pusher configuration.The control system is conventional stick and rudder, with spoilerons on
the wings for aiding in roll control. |
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The plane is has a single surface wing, and is wire braced. The kit
came as a simple bolt together assembly taking approximately 75 hours to
assemble.
The Condor single was powered by Kawasaki 440 engines, with some of the
two seaters equipped with Kawasaki liquid cooled engines of 80 hp.
The Condor single place and two place were produced up until about
1984. |
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Condor single place ultralight
specifications and performance data. |
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Empty Weight: |
234
lbs. |
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Gross
Weight: |
475
lbs. |
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Wing
Span: |
32
ft. |
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Wing
Area: |
160
sq. ft |
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Engine:
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440
Kawasaki |
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Cruise Speed: |
35
.mph |
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Stall
Speed: |
25
.mph |
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VNE: |
65
.mph |
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Construction: |
Aluminum tube, dacron, bolt together |
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Building time: |
75
hrs. |
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Original Manufacturer Seahawk Industries.
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Condor 11 |
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Condor II |
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