Construction began in November 1982, with the first flight being in November 1982. Single seat single engined high wing mono¬plane with conventional three axis control. Conventional tail. Control inputs through stick for pitch/roll and pedals for yaw. Wing braced from below by struts; wing profile; double surface. Undercarriage has three wheels in tail dragger formation. Push right go right tailwheel steering connected to yaw control. Aluminium tube framework, totally enclosed. Engine mounted below wing driving tractor propeller.
The cockpit is fully enclosed and there is only one seat. Equipped with doors, 4 position flaps, elevator trim, bungee suspension landing gear, steerable tailwheel, brakes, radio and headset. Rotax 503 with electric start gives a 70 mph cruise.
The Coyote S 5 is a nosewheel version.
Engine: Rotax 277 (268 cc), 28 hp
Static thrust: 220 lbs.
Empty wt: 240 lb
Wing span: 32ft.
Wing area: 138 sq.ft
Height: 5ft 6in
Length: 17ft
Fuel cap: 5 USG.
Construction: Aluminium, Dacron
Max wt: 535 lbs.
Stall: 25 mph
Max speed: 63 mph.
Vne: 75 mph
Climb rate: 800 fpm @ 30 mph.
Design limit: +6, -3g
Glide ratio: 11-1.
Wing loading: 3.88 lbs/sq.ft
Power loading: 19.11 lbs/hp.
Seats: 1.
RANS S4 single seat
Engine: Rotax 503
Fuel burn: 12 lt/hr
Fuel capacity: 60 lt
VSO: 28mph
VSI: 31mph
VFE: 50mph
VNO: 70mph
VNE: 94mph
All Aero 