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Piper purchased the design from Ted R. Smith: PiperSport: 2010 85 Two-seat light-sport aircraft marketed by Piper between January 2010 and January 2011. It was produced by Czech Sport Aircraft and previously known as the SportCruiser Piper M350: 2015 69 Six-seat pressurized piston single; formerly named Malibu Mirage; only M350 production listed
The M350 is an updated version of the Mirage and is recognized as one of the safest single-engines by the airplane insurance industry. [3] The M350 is fitted with the same 350 hp (261 kW) turbocharged Lycoming TIO-540-AE2A engine and Hartzell three-bladed propeller as the Mirage. Improvements over the Mirage are an Ametek digital fuel quantity ...
Today, FAA Advisory Circular 43.18 provides guidance for the fabrication of parts to be consumed purely during a maintenance operation, [25] and additional guidance is expected to be released in the near future. One of the key features of FAC 43.18 is that it recommends implementation of a quality assurance system quite similar to the ...
The PA-31 series was manufactured under licence in several countries from kits of parts supplied by Piper. [20] [21] Chincul SACAIFI in Argentina assembled most of the series as the PA-A-31, PA-A-31-325, PA-A-31P and PA-A-31-350 and Aero Industrial Colombiana SA (AICSA) in Colombia assembled PA-31, PA-31-325 and PA-31-350 aircraft. [22]
On 21 January 2010, Piper Aircraft announced that they had licensed a derivative of the SportCruiser and would market it as the PiperSport.Piper CEO Kevin Gould said: "The PiperSport is an amazing entry-level aircraft that will bring new customers into Piper and lead the way for those customers to step up into more sophisticated and higher performance aircraft within our line over time."
Introduced in 1953, it is commonly used on light aircraft such as the Cessna 172 and Piper Cherokee, and remains in production as of 2024. Different variants are rated for 150 or 160 horsepower (112 or 119 kilowatts). [1]
Wag-Aero Super Sport (front) with a Piper PA-12. CUBy Base model, powered by a recommended standard Continental C-85 engine of 85 hp (63 kW) [2] CUBy Acro Trainer Developed in 1977, the aircraft was fitted with a 135 hp (101 kW) Lycoming and clipped wings.
Data from Jane's All the World's Aircraft 1976–77 General characteristics Crew: 2 Capacity: 4–6 passengers Length: 34 ft 8 in (10.57 m) Wingspan: 42 ft 8 + 1 ⁄ 4 in (13.011 m) (over tip tanks) Height: 12 ft 9 in (3.89 m) Wing area: 229 sq ft (21.3 m 2) Airfoil: NACA 63 2 -415 at root, 63A212 at tip Empty weight: 4,870 lb (2,209 kg) Max takeoff weight: 9,000 lb (4,082 kg) Fuel capacity ...
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