The Condor is a single seat, high wing, wire braced ultralight, featuring
a tri-cycle landing gear suspension system.
The control system is conventional stick and rudder, with spoilerons on
the wings for aiding in roll control.
Empty Weight:
234
lbs.
Gross
Weight:
475
lbs.
Wing
Span:
32
ft.
Wing
Area:
160
sq. ft
Engine:
440
Kawasaki
Cruise Speed:
35
.mph
Stall
Speed:
25
.mph
VNE:
65
.mph
Construction:
Aluminum tube, dacron, bolt together
Building time:
75
hrs.
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.
Original Manufacturer Seahawk Industries.
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