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
1995: 312 Gilstrap Dr, Liberty, SC 29657, USA.
2008: RagWing Aircraft Designs, 1705 Trail Road, Belton, SC 29627, USA
UL builder
Poland
Founded 1989, Radwan Ltd offered the KR-2PM Swift two-seat monoplane in two versions.
A single seat single engined mid wing monoplane with conventional three axis control circa 1983.
1989: AB Radah, Box 92054, S 12006 Stockholm, Sweden.
1983: AB Radah, Box 81054, S 104 81 Stockholm, Sweden.
LSA builder
A reproduction of the 1918 Spad XIII, the Spad has a spaceframe fuselage and wings of tube and riveted sheet dural.
Engine: Geo Tracker, 80 hp
Wing span: 6.10 m
Wing area: 13.20 sq.m
MAUW: 362 kg
Empty weight: 249 kg
Fuel capacity: 38 lt
Max speed: 160 kph
Cruise speed: 130 kph
Minimum speed: 65 kph
Climb rate: 5 m/s
Fuel consumption: 15 lt/hr
Seats: 1
Plan price (1998): US$125
Kit price (1998): US$15,500
1998:
Meadowlake Airport
8242 Cessna Dr
CO 80831 Peyton
USA
UL builder
All Aero 