A high wing monoplane with cruciform tail, Dacron and aluminum tubing construction, pilot pod, spray equipment.
Engine: Rotax 503
Landing gear: Tricycle
1984 Price: $11,500
Wingspan 30’
Wing area 154 sq.ft
Empty weight 350 lbs
Gross weight 720 lbs
Cruise speed 60 mph
Stall speed 25 mph
Vmax 63 mph
Climb 500 fpm
Takeoff run 150’
Landing roll 150’
Two-place side-by-side, high-wing monoplane, cruciform tail, aluminum tubing and Dacron construction, 3-axis controls with spoilers.
Engine: Rotax 503
Prop: Worldwide scimitar wood
Wingspan 32’
Wing area 160 sq.ft
Empty weight 330 lbs
Gross weight 720 lbs
Cruise speed 40 mph
Stall speed 27 mph
Vmax 45 mph
Climb 500 fpm
Takeoff run 150’
Landing roll 150’
1984 Price: $7,195
A single-surface high wing monoplane, cruciform tail, open cockpit, 3-axis controls with spoilers, aluminum tubing construction.
Engine: Rotax 277, 27 hp
Prop: Worldwide wood
Wingspan 30’
Wing area 160 sq.ft
Empty weight 210 lbs
Gross weight 610 lbs
Cruise speed 40 mph
Stall speed 19 mph
Vmax 45 mph
Climb 500 fpm
Takeoff run 100 ft
Landing roll 100 ft
Lan¬ding gear: Tricycle
Price 1984: $3,995
The Spitfire has a centre mounted joy stick, rudder pedals, tail wheel steerable through rudder pedals. The Spitfire II is a side-by-side two place version.
Spitfire
Engine: Kawasaki 440A
Wing span: 30’
Wing area: 154 sq.ft
Max wt: 550 lbs
Empty wt: 250 lbs
Stall: 19 mph
Cruise: 60 mph
Vmax: 63 mph
Climb rate: 850 fpm
TO run: 100 ft
Ldg roll: 100 ft
Spitfire II
Engine: Rotax 503, 53 hp
Prop: 6-foot wood Worldwide
Landing gear: Tricycle
Wingspan 30’
Wing area: 154 sq.ft
Empty to 330 lb
Gross weight 720 lbs
Cruise speed 60 mph
Stall speed 25 mph
Vrnax 63 mph
Climb 500 fpm
Takeoff run 150 ft
Landing roll: 150 ft
Centre mounted joy stick, rudder pedals, tail wheel steerable through rudder pedals.
Empty wt: 252 lbs
Wing span: 30’
Wing area: 154 sq.ft
Height: 6’6”
Length: 17’10”
Fuel cap; 5 USG
Construction: Aluminium, Dacron
Engine: Rotax 277 (268 cc) 28 hp
Static thrust: 165 lbs
Max wt: 612 lbs
Stall: 20 mph
Max speed: 63 mph
Vne: 85 mph
Climb rate: 450 fpm @ 40 mph
Design limit: +6, -4g
Glide ratio: 10-1
Wing loading: 3.97 lbs/sq.ft
Power loading: 21.86 lbs/hp
1984: 27711 Interstate 10, Katy, TX 77450, USA.
UL builder
Circa 1998, the Wooky Design is a paramotor with an airbag. The bag is inflated by airflow and propwash.
1998:
Via Sospello 123
I-10147 Torino
Italy
Paramotor builder
Made in 1997 Mark Woodhams designed this new machine to incorporate some of his own ideas. It is not a Skyfloater but is designed to demonstrate the nimble soaring ability of early gliders without their sometimes dubious safety record. The 107/02 was built by John Ievers at Hiway and is a one off production.
A single seat partially enclosed autogyro. Composite body, airframe of round tubing. Steel parts are T45 and powder coated, alloy members are anodized. Large rudder. Two versions: one with 17 USG tank; one with 15 USG tank and low profile seat to allow a full blown canopy. Designed by Chris Jullian. Engine: Rotax 582 or Honda. Prop: 3 blade wood. Rotor blades: 23’ Rotor Hawk aluminium.
Rotax 532
Min speed: 20 mph
Cruise: 60-80 mph
Top speed: 115 mph
Gross wt: 1432 lbs
Width: 5’
Height: 7’6”
Length: 12’
All Aero 