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Manufacturer: Eurowing
Model: Goldwing
(Experimental category)
Operating Life: 1981
Registration: G-MJWS
UAS Locaxtion: Hangar 1
Maximum Speed:  75mph 
Cruise Speed: 65mph
Engine: Robin EC34PM, 30hp
Rate of Climb: 750ft/min
Length12ft
Wing Span: 30ft
Range: 220 miles
Fuel Tank Capacity: 22.7 Litres

GOLDWING

EuroWing-Goldwing-Hangar-IMG_3109-MJC.we

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.

Image: MARK J. CAIRNS