[4] The Condor complies with the Fédération Aéronautique Internationale microlight category, but was never an accepted US light-sport aircraft.
[1][5] The Condor features a 540 sq ft (50 m2) parachute-style wing, two-seats-in-tandem accommodation, tricycle landing gear and a single 64 hp (48 kW) Rotax 582 engine in pusher configuration.
[1] The aircraft carriage was built from a combination of bolted aluminium and 4130 steel tubing by Aerostar of Romania and then assembled in the US.
In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw.
The main landing gear incorporates spring rod suspension.