Engine: Rotax 503DC, 52 hp
HP range: 28-52
Height: 5.5 ft
Length: 17 ft
Wing span: 28 ft
Wing area: 130 sq.ft
Fuel cap: 5 USG
Weight empty: 275 lb
Gross: 660 lb
Speed max: 100 mph
Cruise: 65 mph
Range: 200 sm
Stall: 22 mph
ROC: 1000 fpm
Take-off dist: 70 ft
Landing dist: 150 ft
Service ceiling: 12,500 ft
Seats: 1
Landing gear: tail wheel
Engine: Kawasaki 440A, 38 hp
HP range: 20-52
Height: 6 ft
Length: 16.5 ft
Wing span: 25.5 ft
Wing area: 117 sq.ft
Fuel cap: 5 USG
Weight empty: 242 lb
Gross: 550 lb
Speed max: 90 mph
Cruise: 65 mph
Range: 200 sm
Stall: 25 mph
ROC: 800 fpm
Take-off dist: 100 ft
Landing dist: 150 ft
Service ceiling: 10,000 ft
Seats: 1
Landing gear: tail wheel
Ultralight replica of the Heath Parasol.
Engine: Rotax 277, 28 hp
HP range: 20-48
Height: 5.5 ft
Length: 16 ft
Wing span: 25.6 ft
Wing area: 117 sq.ft
Fuel cap: 5 USG
Weight empty: 238 lb
Gross: 550 lb
Speed max: 90 mph
Cruise: 60 mph
Range: 125 sm
Stall: 25 mph
ROC: 600 fpm
Take-off dist: 150 ft
Landing dist: 200 ft
Service ceiling: 10,000 ft
Seats: 1
Landing gear: tail wheel
An ultralight replica of the Church Midwing Sport Monoplane.
Engine: Rotax 277, 28 hp
HP range: 20-48
Height: 4.5 ft
Length: 16 ft
Wing span: 26.8 ft
Wing area: 117 sq.ft
Fuel cap: 5 USG
Weight empty: 235 lb
Gross: 550 lb
Speed max: 95 mph
Cruise: 65 mph
Range: 125 sm
Stall: 26 mph
ROC: 600 fpm
Take-off dist: 125 ft
Landing dist: 150 ft
Service ceiling: 10,000 ft
Seats: 1
Landing gear: tail wheel
Engine: Rotax 503DC, 52 hp
HP range: 48-90
Height: 6 ft
Length: 17 ft
Wing span: 28.5 ft
Wing area: 142.5 sq.ft
Fuel cap: 10 USG
Weight empty: 450 lb
Gross: 900 lb
Speed max: 105 mph
Cruise: 80 mph
Range: 260 sm
Stall: 36 mph
ROC: 650 fpm
Take-off dist: 200 ft
Landing dist: 300 ft
Service ceiling: 10,000 ft
Seats: 2
Landing gear: tail wheel
The LSA RW-2 is built of wood and fabric, the RW-2 takes about 400 man ours to build. In 2009 plans cost US$125.
Engine: Kawasaki 440A, 38 hp
HP range: 35-65
Height: 5.5 ft
Length: 14.9 ft
Wing span: 18 ft
Wing area: 120 sq.ft
Fuel cap: 5 USG
Empty Weight: 126 kg / 278 lbs
MTOW Weight: 249 kg / 550 lbs
Vne: 109 kt / 125 mph / 201 kmh
Cruise: 61 kt / 70 mph / 113 kmh
Range: 125 sm
Stall: 26 kt / 30 mph / 48 kmh
ROC: 750 ft/min / 4 m/s
Take-off distance (50ft obstacle): 200 ft / 61 m
Landing distance (50ft obstacle): 400 ft / 122 m
Service ceiling: 10,000 ft
Seats: 1
Landing gear: tail wheel
Cockpit width: 24 in
Engine: 2si, 38 hp
HP range: 35-65
Height: 5.5 ft
Length: 14.9 ft
Wing span: 18 ft
Wing area: 120 sq.ft
Fuel cap: 5 USG
Empty Weight: 126 kg / 278 lbs
MTOW Weight: 249 kg / 550 lbs
Vne: 109 kt / 125 mph / 201 kmh
Cruise: 61 kt / 70 mph / 113 kmh
Range: 125 sm
Stall: 26 kt / 30 mph / 48 kmh
ROC: 750 ft/min / 4 m/s
Take-off distance (50ft obstacle): 200 ft / 61 m
Landing distance (50ft obstacle): 400 ft / 122 m
Service ceiling: 10,000 ft
Seats: 1
Landing gear: tail wheel
Cockpit width: 24 in
An ultralight replica of the Pietenpol Air Camper.
Engine: Kawasaki 440A, 35 hp / Rotax 503, 48 hp
HP range: 42-48
Height: 5.9 ft
Length: 15 ft
Wing span: 25.5 ft
Wing area: 117 sq.ft
Fuel cap: 5 USG
Weight empty: 254 lb
Gross: 550 lb
Speed max: 85 mph
Cruise: 55 mph
Range: 125 sm
Stall: 24 mph
ROC: 650 fpm
Take-off dist: 150 ft
Landing dist: 150 ft
Service ceiling: 10,000 ft
Seats: 1
Landing gear: tail wheel
The invention of 17-year-old Henri Ragot, aided by his father, Louis F. Ragot, a sculptor, and his brother, Charles. The canard monoplane had flexible wings which were based on the study of bird’s flight. After models the concept was built in real size in the hangar of the Aeronautic Society of America (Louis Ragot was a member) in 1910.
Designed and flown by E.C. Gordon England circa 1909. It had three engines, geared to a single propeller. Pilot and passengers sat in the twin floats.
The 1913 Radley England No. 2 waterplane was designed and built by James Radley and Eric England
1913 Radley England No. 2 waterplane
Span: top51′ 7.5″ bottom 45’10”
Length: 29’9″
Hull length: 18′
A single seat single engined mid wing monoplane with conventional three axis control circa 1983.
All Aero 