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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.
PA-46R-350T Matrix. 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 ...
Proposed higher-power version of the PA-24 PA-27 Aztec: 1960 4,930 Improved version of the PA-23, kept PA-23 designation PA-28 Cherokee: 1961 10,896 Single-engined low-wing cabin monoplane PA-28-140 Cherokee: 1964 10,089 Two-seat training variant PA-28 Warrior: 1974 4,842 Improved PA-28 PA-28-235 Cherokee/Dakota: 1964 2,913 Higher-power PA-28 ...
A 1966 model Piper PA-32-260 Cherokee Six Piper PA-32-300. The Piper PA-32 Cherokee Six is a series of single-engine, fixed landing gear, light aircraft manufactured in the United States by Piper Aircraft between 1965 and 2007. [1] [2] The PA-32 is used around the world for private transportation, air taxi services, bush support, and medevac ...
Piper Aircraft Company factory in Lock Haven, Pennsylvania during the 1930s, with the Piper Cub logo superimposed at the top Piper PA-18-150 Super Cub.Built 1958. Piper PA-28-161 Warrior II Piper PA-34-200T Seneca Piper PA-31 Navajo airframe used for crash testing by NASA after a 1972 flood inundated Piper's factory Early-production PA-31 Navajo Piper PA-32RT-300T Turbo Lance II Piper PA-44 ...
The Piper PA-44 Seminole is fitted with one LO-360-E1A6D or one LO-360-A1H6 on the right wing along with one O-360-E1A6D or O-360-A1H6 on the left wing to eliminate the critical engine on this twin. LO-360-A1G6D 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1.
Data from Jane's all the World's Aircraft 1947 General characteristics Crew: 1 Capacity: 3 pax Length: 26 ft 0 in (7.93 m) Wingspan: 34 ft 8 in (10.56 m) Height: 7 ft 0 in (2.13 m) Airfoil: Modified USA 35B Empty weight: 1,360 lb (617 kg) Gross weight: 2,400 lb (1,089 kg) Fuel capacity: 40 US gal (33 imp gal; 150 L) fuel; 2.5 US gal (2.1 imp gal; 9.5 L) oil Powerplant: 1 × Continental E165 6 ...
Single engine piston aircraft with tricycle landing gear [1]; Model Engine Power hp Seats Wing Sq. Ft. MTOW lb Empty lb Cruise knots Range nmi AS 202 Bravo NG: L. AEIO-360: 180: 3: 149: 2,202: 1,389