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The plans for the Pietenpol Aircamper were originally published in a four-part serial in the "Flying and Glider" Manual of 1932-33. [4] [5] The original model was flown using an Ace four cylinder water-cooled engine. [4] The Model A Ford engine later became the standard powerplant used; the design was first flown with one in May 1929. [1]
Data from United States Military Aircraft since 1909 General characteristics Crew: 2 Length: 24 ft 9 in (7.54 m) Wingspan: 32 ft 2 in (9.80 m) Height: 9 ft 8 in (2.95 m) Wing area: 298 sq ft (27.7 m 2) Empty weight: 1,931 lb (876 kg) Max takeoff weight: 2,635 lb (1,195 kg) Fuel capacity: 46 US gal (38 imp gal; 170 L) Powerplant: 1 × Continental R-670-5 7-cylinder air-cooled radial piston ...
Data from EAA, 1931 flying and gliding manual General characteristics Length: 18 ft 3 in (5.56 m) Wingspan: 27 ft (8.2 m) Height: 5 ft 1 in (1.55 m) Empty weight: 425 lb (193 kg) Powerplant: 1 × Anzani 3-cyl. Y radial engine, 35 hp (26 kW) Propellers: 2-bladed, 6 ft (1.8 m) diameter Performance Maximum speed: 79 kn (91 mph, 146 km/h) Range: 100 nmi (120 mi, 190 km) See also Aircraft of ...
The recommended engines for the Rebel are the 160 hp (120 kW) Lycoming O-320, the 116 hp ... Wingspan: 30 ft 0 in (9.2 m) Wing area: 150 sq ft (14 m 2)
The 1954 model year introduced a 225 hp (168 kW) O-470-J engine and interior refinements. 1956 introduced a 230 hp (172 kW) O-470-K engine with a new air intake duct. Certified on 23 December 1952. 641 (1953), 620 (1954), 891 (1955), and 512 (1956) built. [5] [6] A 1957 Cessna on display at Hullavington Airfield, England. 180A
The Beechcraft Model 99 is a civilian aircraft produced by American manufacturer Beechcraft. It is also known as the Beech 99 Airliner and the Commuter 99 . The 99 is a twin-engine, unpressurized, 15 to 17 passenger seat turboprop aircraft, derived from the earlier Beechcraft King Air and Queen Air .
Data from EAA Museum, Federal Aviation Administration, Plane & Pilot General characteristics Crew: one Capacity: one passenger Length: 20 ft 9 in (6.32 m) Wingspan: 30 ft 0 in (9.14 m) Height: 5 ft 11 in (1.80 m) Wing area: 142.6 sq ft (13.25 m 2) Airfoil: NACA 43013 Powerplant: 1 × Continental C75-12 4-cylinder air-cooled horizontally-opposed piston engine, 75 hp (56 kW) Propellers: 2-bladed ...
The Aerostar emerged as a mid-wing cantilever monoplane powered by two wing-mounted piston engines, with retractable landing gear in a tricycle configuration. It is designed to seat six, and is distinguished from light twins of similar size and weight by its high wing loading, careful attention to fine aerodynamic details, a mid wing, and in early models, the absence of cowl flaps; Smith was ...