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Data from Piper PA-22-160 pilot's operating handbook, issued January 1960 General characteristics Crew: one Capacity: three passengers Length: 20 ft 6 in (6.25 m) Wingspan: 29 ft 3 in (8.92 m) Height: 8 ft 4 in (2.54 m) Wing area: 147.5 sq ft (13.70 m 2) Empty weight: 1,110 lb (503 kg) Gross weight: 2,000 lb (907 kg) Fuel capacity: 36 US gal (140 L; 30 imp gal) Powerplant: 1 × Lycoming O-320 ...
In 1958, the Apache 160 was produced by upgrading the engines to 160 hp (119 kW); 816 were built. [ citation needed ] The Apache 160 was superseded in 1962 by the Aztec-derived Apache 235 . [ citation needed ] With a 1962 price of $45,000, the Apache 235 featured the Aztec's 235 hp (175 kW) engines and swept tail surfaces [ 3 ] (119 built).
Piper PA-22 Tri-Pacer, an American light aircraft; U.S. Route 22 in Pennsylvania This page was last edited on 27 ...
The Piper PA-30 Twin Comanche was designed as a twin-engined variant of the Piper PA-24 Comanche.A complex light twin, with retractable landing gear, seating 4 (in original models) to 6 (in later models), and cruise speeds ranging from 160–210 mph on twin 160 horsepower engines, it competed with the more-powerful Cessna 310 and Beech Baron, and later with Piper's other light twins.
The Piper Aerostar (formerly the Ted Smith Aerostar) is an American twin-engined propeller-driven executive or light transport aircraft, designed by Ted R. Smith.It was originally built by Ted Smith Aircraft Company, but the design was acquired in 1978 by the Piper Aircraft Corporation, which continued production of the aircraft as the PA-60.
Float-equipped PA-11S at Seattle Renton in 1973. A small number of PA-11s have been modified to use a Tricycle landing gear. [3] The PA-11 was one of the first aircraft to be used by Piper for experiments with the nose wheel (also known as tricycle gear) configuration. Although its original design is intended to be a tail-dragger, a ...
The PA-44-180T Turbo Seminole version was certified on November 29, 1979. It features two turbocharged 180 hp (135 kW) Lycoming TO-360-E1A6D engines, which offer a significant improvement in performance at high density altitude. The Turbo Seminole had its takeoff gross weight raised to 3925 lb (1780 kg), while the landing weight remained at ...
Ryan PT-22 Recruit instrument panel PT-22 Military version of the Model ST.3KR powered by a 160 hp R-540-1, 1,023 built. PT-22A Model ST-3S twin-float seaplanes ordered by the Netherlands Navy powered by 160 hp Menasco D4B, ordered cancelled and completed for the United States Army Air Corps with 160 hp R-540-1 engines, 25 built.