The Pelican has an unconventional layout, based on the Fauvel AV.36, with a low aspect ratio wing, twin rudders mounted at mid-span and a pusher configuration Solo 210 engine mounted in the rear fuselage producing 90NaN0.[2]
The aircraft is constructed from fibreglass, with some surfaces fabric covered. The 7.21NaN1 span wing is semi-tapered, tapering outside the rudders and employs a Fauvel F4 17% airfoil. The fuselage is just 21NaN1 in length, making the aircraft very compact. The landing gear is monowheel gear, with a small tail wheel and outrigger wheels at midspan.
With the Solo engine the take-off distance is 1800NaN0 and the landing distance 670NaN0. Cruise speed is 930NaN0. A variety of engines can be fitted.
In 1998 a completed aircraft was US$12,950 and a kit was US$8,000. The kit did not include the engine, propeller or instruments. Construction time from the supplied kit was estimated at 300 hours. One example was reportedly completed and flying in 1998.