Tube and fabric construction.
Cruise: 60 mph
Stall: 22 mph
Range: 290 sm
Rate of climb: 1200 fpm
Takeoff dist: 100 ft
Landing dist: 200 ft
Engines: 2 x Hirth 3203, 65 hp
Fuel capacity: 24 USG
Empty weight: 900 lb
Gross weight: 1500 lb
Length: 22 ft
Wing span: 32.5 ft
Wing area: 165 sq.ft
Seats: 2
Cockpit width: 24 in
Landing gear: nose or tailwheel
First flown in 1995, the Suer Solution has super tough landing gear. Kits did cost US$7500.
Engine: Rotax 503, 46 hp
HP range: 40-75
Top speed: 67 mph
Cruise: 50 mph
Stall: 22 mph
Rate of climb: 500 fpm
Takeoff dist: 100 ft
Landing dist: 150 ft
Service ceiling: 13,500 ft
Fuel capacity: 10 USG
Empty weight: 320 lb
Gross weight: 860 lb
Height: 7.5 ft
Length: 20 ft
Wing span: 31 ft
Wing area: 155 sq.ft
Seats: 2
Landing gear: tailwheel
Designed for training and also available with a strut braced wing. The kit did cost US$8495.
Top speed: 75 mph
Cruise: 55 mph
Stall: 27 mph
Range: 110 sm
Rate of climb: 750 fpm
Takeoff dist: 150 ft
Landing dist: 200 ft
Service ceiling: 14,000 ft
Engine: Rotax 582, 65 hp
HP range: 40-75
Fuel capacity: 10 USG
Empty weight: 390 lb
Gross weight: 890 lb
Height: 8 ft
Length: 20 ft
Wing span: 30 ft
Wing area: 150 sq.ft
Seats: 2
Landing gear: tailwheel
A tandem two-seat kit-built monoplane developed in Venezuela. First flown in January 1997.
Overlapping pusher propellers are mounted close in to the fuselage and the wingspan can be extended for special applications. Can be flown with or without the cabin doors. An optional ag-spray kit was available.
The kit did cost US$24,995.
Top speed: 100 mph
Cruise: 60 mph
Stall: 22 mph
Range: 250 sm
Rate of climb: 1200 fpm
Takeoff dist: 100 ft
Landing dist: 200 ft
Service ceiling: 15,000 ft
HP range: 52-100
Fuel capacity: 24 USG
Empty weight: 700 lb
Gross weight: 1400 lb
Height: 7.5 ft
Length: 22 ft
Wing span: 32 ft
Wing area: 160 sq.ft
Seats: 2
Landing gear: tailwheel
US agent for the Pairadigm tandem two-seat kit-built monoplane developed in Venezuela, and the single-seat Super Solution 2000.
1997: PO Box 7534, Ft. Myers, FL 33911, USA.
Designed for Formula racing, a sport version was available. The wings are detachable.
Top speed: 270 mph
Cruise: 200-220 mph
Stall: 65 mph
Range: 460 sm
Rate of climb: 2000 fpm
Takeoff dist: 900 ft
Landing dist: 1200 ft
Cockpit width: 24 in
Engine: Continental O-200, 100 hp
HP range: 85-130
Fuel capacity: 6 USG
Empty weight: 530 lb
Gross weight: 750 lb
Height: 4 ft
Length: 18 ft
Wing span: 20 ft
Wing area: 66 sq.ft
Seats: 1
Landing gear: tailwheel
1996: 1834 White Oak, Wichita, KS 67207, USA.
Sport plane builder
The Belgium Vreedenburgh biplane flew in 1910, powered by a 40 hp Anzani engine.
This is the one and only Vreeburg A-2M bomber was designed by HA Vreeburg as the chief of the Technical Service of the Dutch Air Force (The LVA = Luchtvaart Afdeling). The machine was built by the government works on the airfield of Soesterberg. Development started in 1918, and the machine was finished in 1919, making its first flight on February 10th in 1919.
The machine received no orders from the LVA and was scrapped in 1920.
Engines: 2 x Le Rhone, 110-120 hp
Max speed: 140 kph
Aerobatics aircraft, Czech Republic, 1964
Engine : Walter Minor 6-III, 116 hp
Length : 21.982 ft / 6.7 m
Wingspan : 25.098 ft / 7.65 m
Wing area : 96.876 sq.ft. / 9.0 sq.m
Max take off weight : 1455.3 lb / 660.0 kg
Weight empty : 1124.6 lb / 510.0 kg
Max. speed : 167 kt / 310 km/h
Cruising speed : 140 kt / 260 km/h
Initial climb rate : 2165.35 ft/min / 11.0 m/s
Service ceiling : 26247 ft / 8000 m
Wing load : 14.97 lb/sq.ft / 73.0 kg/sq.m
Range : 189 nm / 350 km
Crew : 1
