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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
M350. 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 ...
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]
This model was used in the Gulfstream American GA-7 Cougar twin. O-320-D1F 160 hp (119 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as E1F except with high compression pistons. [4] A brand new Lycoming O-320-D2A engine with baffles already mounted O-320-D2A
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.
The Venture was designed by Griswold, a former chief engineer with Piper Aircraft, and used technology from the Piper Malibu, which Griswold led the design for as well. [3] The layout of the design was intended to combine a large two-seat side-by-side cabin with rear baggage space in the smallest possible airframe, having a highly streamlined ...
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 ...
Data from Piper Aircraft and their forerunners General characteristics Crew: 1 Capacity: 3 passengers Length: 23 ft 2 in (7.06 m) Wingspan: 35 ft 6 in (10.82 m) Height: 6 ft 5 in (1.96 m) Wing area: 179.3 sq ft (16.66 m 2) Airfoil: USA 35B Empty weight: 1,020 lb (463 kg) Max takeoff weight: 1,850 lb (839 kg) Powerplant: 1 × Lycoming O-235-C1 4-cylinder air-cooled horizontally-opposed piston ...