High monowing, strut-braced, Kevlar/foam construction. Full three-axis control system. Powered by a WAE two-cylinder horizontally opposed British microlight engine. The landing gear was Chrome-moly steel, trike type.
After spending something like $200k developing the aircraft and all the tooling, the original designers found they couldn’t obtain product liability insurance and they decided to sell the project to someone who was going to manufacture it in Mexico. That never came to.
Only 10 came out of the factory.
Engine: WAE 2 cyl, 30 hp
Wingspan 31 ft
Wing area 112 sq.ft
Length 18 ft
Empty weight 245 lb
Payload 245 lb
Gross 600 lb
Wing loading 4 lbs/sq.ft
L/D 22:1
Cruise speed 60 mph
Stall speed 19 mph
Vmax 63 mph
Climb rate 1000 fpm
Takeoff run 150-200 ft
Landing roll 150-200 ft
Fuel capacity 5 USG
All Aero 