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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 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]
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.
The TR-2 has a cruise propeller and the trainer has a climb prop. Typically the TR-2 came with more navigation instruments and was better for cross country flying because of its speed and lower fuel consumption. The family also includes the Grumman American AA-1B Trainer and TR-2, plus the Gulfstream American AA-1C Lynx and T-Cat. [1]
A modified Berkut with a single canopy and automated flight equipment where the second seat would be located, for UAV research and development with a 20-hour endurance. [17] Two aircraft have been built with a third one in development. N442LT is the first tail number. N497LT is the second. [18] [19] Berkut Jet
Stretched version with two seats in tandem, a gross weight of 950 lb (431 kg), an acceptable power range of 60 to 80 hp (45 to 60 kW). Engines used include the two-stroke 50 hp (37 kW) Rotax 503 and the four-stroke 60 hp (45 kW) HKS 700E engine. Described as an "intimate tandem two seater" due to the small rear seat space. Production completed.
Certified versions of the Pitts are now produced by Aviat Aircraft in Afton, Wyoming.It is available as the S-1 single-seater with an up to 200 hp (150 kW) flat-4 Lycoming engine and a 17 ft 4 in (5.28 m) wingspan, or as the S-2 two-seater variant featuring a 260 hp (194 kW) flat-6 Lycoming and a 20 ft (6.1 m) wingspan.