[1][2][3] The aircraft preceded the US FAR 103 Ultralight Vehicles rules, but fits into the category, including FAR 103's maximum empty weight of 254 lb (115 kg).
It features a cantilever high-wing, a single-seat, partially enclosed cockpit, tricycle landing gear and twin 11.5 hp (9 kW) Soarmaster engines powering a single propeller in pusher configuration.
The FLAC has laminated fiberglass main landing gear legs and a nose wheel that is steerable.
The aircraft was also designed to be at least nominally foot-launchable to comply with the informal US requirements for ultralights of that period that they be able to do so.
Foot launching was carried out by opening a hinged door in the fuselage floor.