GOLDWING

Single-seated, single-engined, mid-wing monoplane with conventional three-axis control. Wing has swept back leading and trailing edges, and tapering chord; no tail, canard wing. Pitch control by elevator on canard; yaw control by tip rudders; roll control by half-span up-only ailerons and spoilers; control inputs through stick for pitch/roll and pedals for yaw.

Cantilever wing; main-wing profile, modified Liebeck; canard profile, GU25; both double-surface. Undercarriage has three wheels in tricycle formation; no suspension on nosewheel and glass-fibre suspension on main wheels. Push-right go-right nosewheel steering connected to yaw control. No brakes.

Aluminium-tube glassfibre fuselage, partially enclosed. Engine mounted above wing driving pusher propeller.

Composite-construction wing of foam and aluminium covered with glass-fibre skin.