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The Piper PA-38-112 Tomahawk is a two-seat, fixed tricycle gear general aviation airplane, ... Performance. Maximum speed: 126 mph (203 km/h, 109 kn) at sea level;
Retractable landing gear variant of the PA-32 PA-33 Comanche: 1966 1 Pressurized Comanche PA-34 Seneca: 1972 5,000+ Twin-engine derivative of PA-32R PA-35 Pocono: 1968 1 Twin-engined pressurized commuter airliner PA-36 Pawnee Brave: 1973 938 Single-engined agricultural monoplane PA-37 0 Proposed twin-engined PA-33 PA-38 Tomahawk: 1978 2,519
Well-known designs that use versions of the O-235 included the Cessna 152, Grumman American AA-1 series, Beechcraft Model 77 Skipper, Piper PA-38 Tomahawk, American Champion Citabria, Piper Clipper, and the Piper PA-22-108 Colt.
Nose, cowling, and engine installation adapted from the Piper PA-38 Tomahawk [2] Wings adapted from the Schweizer SGS 1-36 Sprite, including extensions to bring it from the Sprite's 46.2 feet (14.1 m) to 59.5 feet (18.1 m) and leading edge cuffs to improve stall characteristics [2] Tail from the Schweizer SGS 2-32 [2]
Though the aircraft first flew with a standard tail configuration, by the time it entered production, a T-tail configuration had been adopted, giving it an appearance very similar to its close competitor, the Piper PA-38 Tomahawk introduced in 1978. [1] [2]
Data from Jane's All The World's Aircraft 1971-72 General characteristics Crew: one Capacity: one passenger Length: 6.60 m (21 ft 8 in) Wingspan: 8.40 m (27 ft 7 in) Height: 2.20 m (7 ft 3 in) Wing area: 10.22 m 2 (110.0 sq ft) Aspect ratio: 6.8:1 Airfoil: NACA 64215 at root, NACA 64212 at tip Empty weight: 484 kg (1,067 lb) Max takeoff weight: 820 kg (1,808 lb) Fuel capacity: 140 L (37 US gal ...
Piper PA-38 Tomahawk [26] Piper PA-41P Aztec [27] Piper PT-1 [28] References External links. Official Website; This page was last edited on 24 December 2024, at ...
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