The Specter II featured a canard configuration, a cantilever high-wing, a two-seats-in-tandem enclosed cockpit, with the pilot under a bubble canopy and the passenger supplied only with side windows. The aircraft had fixed tricycle landing gear with a retractable nosewheel and a single engine in pusher configuration. The design was stall-resistant.[1]
The aircraft was made from composite materials. Its 341NaN1 span wing, mounted wing-tip rudders and had a wing area of 147square feet. The cabin width was 22inches. The design power range was 90to and the standard engine used was the 1180NaN0 Subaru EA82 automotive-conversion powerplant.[1]
The aircraft had a typical empty weight of 1000lb and a gross weight of 1600lb, giving a useful load of 600lb. With full fuel of the payload for the pilot, passenger and baggage was 462lb.[1]
The fast-build kit was to include all the major structural parts bonded in place. The manufacturer estimated the construction time from the supplied kit to be 850 hours.[1]
By 1998 the company reported that one example had been completed and was flying.[1]
In April 2015 one example was registered in the United States with the Federal Aviation Administration, although its registration had expired in 2013.[2] It is unlikely any examples exist today.