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The Cameron P-51G (originally Cameron Grand 51) is an American two-seat turboprop representation of the 1940s North American P-51 Mustang, designed and built by Cameron & Sons Aircraft of Coeur d'Alene, Idaho for sale as completed aircraft or kits for amateur construction.
The VP-2 is externally similar in appearance to the VP-1 but with a 1 ft (30 cm) wider fuselage and enlarged cockpit section to accommodate two side-by-side configuration seats. The aircraft is 1 ft (30 cm) longer and has a 3 ft (0.9 m) addition to wingspan. The VP-2 can use any Volkswagen air-cooled engine model from 1,834 to 2,100 cc.
The Dragonfly is a two-seater aircraft that features a tandem wing layout with a forward wing mounted low and the other behind the cockpit in a shoulder position, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed landing gear and a single engine in tractor configuration. The cockpit is 43 in (109 cm) wide [3]
The General Avia F.22 Pinguino is an Italian two-seat aircraft by GeneralAvia. [1] The aircraft has two side-by-side seats in an enclosed canopy cockpit. It was the 22nd aircraft designed by Stelio Frati. The aircraft was manufactured in four configurations, as well as a prototype four-seater. The F.22 is used as a military trainer in several ...
The Pipistrel Alpha Trainer is a Slovenian two-seat, single-engine light-sport aircraft intended ... California starting in late 2017 ... Wing area: 9.51 m 2 (102. ...
The Lancair 320 is a two-seat single-engined light aircraft marketed in kit form by the U.S. general aviation manufacturer Lancair.It is based on the Lancair 235, but with a larger fuselage and more powerful engine, and like the 235, it is a low-winged monoplane of composite construction with a retractable tricycle undercarriage, with side-by-side seating in an enclosed cockpit.
Data from Kitplanes, Cliche and Purdy General characteristics Crew: one Capacity: one passenger Length: 19 ft 0 in (5.79 m) Wingspan: 22 ft 0 in (6.71 m) Height: 6 ft 9 in (2.06 m) Wing area: 110 sq ft (10 m 2) Empty weight: 345 lb (156 kg) Gross weight: 850 lb (386 kg) Fuel capacity: 10 US gallons (38 litres) Powerplant: 1 × Rotax 582 twin cylinder, two-stroke aircraft engine, 64 hp (48 kW ...
Development of the Sling 2 commenced in 2006. The Sling is a two-seat, low wing, all metal aircraft with tricycle landing gear made from composites. The aircraft is powered by an 80 hp (60 kW) Rotax 912UL,100 hp (75 kW), a Rotax 912ULS, or a 912iS engine, or optionally a turbocharged 115 hp (86 kW) Rotax 914 UL, driving a 3-bladed Warp Drive Inc propeller.