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Light Canard Airplane

Conceptual design of a high-performance light canard-configured airplane.

The project has been initiated by a North America based customer aiming to create a nicely looking canard-configured light airplane. The configuration implies a four full-size seat cabin. Also, the concept features carbon fiber composite structure, Lycoming TIO-540-A piston engine or TP100 small turboprop.


Preliminary Specifications Units
Service Ceiling FL 250
Max Cruise Speed @ FL250 KTAS 250
Economy Cruise Speed @ FL220 KTAS 220
Stall Speed (or Min Speed) knots 60
Range Full Fuel NM 1,460


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