To optimize the performance of a canard airplane with an engine in front,
the canard is mounted forward of its location in existing canard
airplanes. Specifically, the canard is located with its leading edge
significantly ahead of the firewall. This allows the canard to be mounted
higher on the fuselage, providing aerodynamic improvements. The engine
may be mounted to, or near, the canard spar, simplifying the structure.
The added leverage of the further-forward canard allows the wing to be
moved forward also. This makes possible a low wing under the occupants of
the airplane. Efficient loading of the lifting surfaces is maintained by
using a high aspect ratio canard.