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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. [1]
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]
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.
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 Model 3000/T-6 is a low-wing cantilever monoplane with enclosed tandem seating for two. It is powered by a single Pratt & Whitney Canada PT6A-68 turboprop engine in tractor configuration with an aluminum, 97-inch (8.1 ft; 2.5 m), four-blade, constant-speed, variable pitch, non-reversing, feathering propeller assembly and has retractable tricycle landing gear.
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]
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.
[1] [2] [3] The long conventional landing gear consist of sprung tubing for the main gear, with a steerable sprung tailwheel. [2] [3] The company described the Slingshot's two seat capabilities, "the rear passenger seat is designed for average size people, up to 175 pounds. The seating arrangement has the passenger's legs overlapping the pilot ...
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