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Data from Sport Aviation, Plane & Pilot and Purdy General characteristics Crew: one Capacity: one passenger in tandem seating Length: 22 ft 5 in (6.83 m) Wingspan: 35 ft 3 in (10.74 m) Height: 6 ft 8 in (2.03 m) Wing area: 178.5 sq ft (16.58 m 2) Airfoil: USA 35B Empty weight: 695 lb (315 kg) Gross weight: 1,400 lb (635 kg) Fuel capacity: 12 US Gallons, 45.42 litres Powerplant: 1 × Lycoming O ...
Main spar of a de Havilland DH.60 Moth. In a fixed-wing aircraft, the spar is often the main structural member of the wing, running spanwise at right angles (or thereabouts depending on wing sweep) to the fuselage. The spar carries flight loads and the weight of the wings while on the ground.
Single-engined high-wing cabin monoplane P-5 1944 1 Single-engined high-wing cabin monoplane, also known as J-3X PT-1 Trainer: 1942 1 Two-seats in tandem, low-wing monoplane PWA-1 Skycoupe: 1943 1 Two-seat low wing twin-boom monoplane, later became PA-7 PWA-8 Cub Cycle: 1944 1 Single-seat, mid-wing single-engine monoplane LBP: 1945 3
In October 2007 Piper announced the Matrix, an unpressurized version of the Mirage. The new model was designated as the PA-46R-350T, indicating retractable landing gear, 350 horsepower (260 kW), and turbocharging. [28] Piper Aircraft marketed the Matrix as a cabin-class aircraft for Cirrus SR-22 and Cessna 400 owners to step up to.
Fisher Flying Products is a Canadian aircraft manufacturer that produces kits for a wide line of light aircraft. The company's kits all feature wooden construction with aircraft fabric covering. Many of the designs are reproductions of classic aircraft, such as the company's 80% Fisher R-80 Tiger Moth that is based upon the de Havilland Tiger ...
Ultra Pup N3 Pup Single seat variant designed to resemble a 3/4 scale Piper J-3 Cub.Originally named the Nostalgair N-3 Pup. Engine is a TEC Half VW of 40 hp (30 kW). Meets FAR 103 requirements with an empty weight of 254 lb (115 kg) and gross weight of 535 lb (243 kg). 830 had been completed by December 2011.
The AG-3 was a single-seat, low-wing monoplane with the wings braced to the fuselage with struts. It had a conventional landing gear with a tailwheel and was powered by a 135 hp engine. [ 1 ] The single seat was placed high in the fuselage to give the best visibility and an 800 lb-capacity hopper was fitted in front of the cockpit.
A 3-view drawing of a Piper PA-28R-200 Cherokee Arrow PA-28R-180 Cherokee Arrow Four-place, retractable landing gear landplane, Lycoming IO-360-B1E engine of 180 hp (134 kW), gross weight 2,500 lb (1,134 kg). First certified on 8 June 1967. [19] Built in the following variants: PA-28R-180 Cherokee Arrow, initial version. [35]
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