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This simple, easy to build ultralight can be powered
by engines up to 45hp, some having the 40hp(30kW) Hirth 2702 installed.
The fuselage is constructed of chrome molybdenum steel sheet and tube
with an aluminium tail arm. The landing gear is of the spring strut type
and the strut-braced wings have press-formed ribs riveted to the main
spars and covered by heat-shrinked aircraft fabric.
Registration unknown
USA
Single seat ultralight first flown in 1996
Engine: 28hp(21kW) Rotax 277
Length: 18’0"(5.48m)
Height: 6’0"(1.82m)Wingspan: 28’0"(8.52m)
No.built: 30+ Range: 120miles(192km)
Cruising speed: 60mph(96kmh) Empty weight: 240lb(109kg)
Maximum take-off weight: 575lb(261kg)
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