The C.P. 150 Onyx is a single seat, canard, open cockpit aircraft designed by Claude Piel. Construction materials are wood & fabric. The landing gear is a fixed trigear, and the engine is in a pusher configuration. This aircraft qualifies as an ultralight in Canada and the United States.

Characteristics Span 24.0 ft Length 11.6 ft Total Area 137.7 sq ft Empty Weight 265 lbs Max Takeoff Weight 475 lbs Engine (prototype) 12 HP Fuel (US gallons) 5 Propeller 35" dia. x 14" pitch

Performance 12 HP 18 HP Max Speed (mph) 62 70 Minimum Speed (mph) 28 30 Cruise Speed (mph) 50 60 V.N.E. (mph) 85 85 Stall Speed (mph) 22 25 Takeoff Distance 200 150 Landing Distance 100 100 Rate Of Climb (ft/min) 300 450