Back to all projects

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

 


Unless specifically stated otherwise, all images herein are property of ADA (Advanced Design Alliance) Engineering and cannot be reproduced, distributed, or transmitted, in any form or by any means, or stored in a data base or retrieval system, without prior written consent of ADA Engineering owner
.