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J-3 Cub: 1938 19,888 Single-engined high-wing cabin monoplane J-4 Cub Coupe: 1939 1,252 Single-engined high-wing cabin monoplane J-5 Cub Cruiser: 1940 1,507 Single-engined high-wing cabin monoplane P-1 Applegate Duck 1940 1 Amphibian: P-2 Cub 1941 1 Single-engined high-wing cabin monoplane P-3 0 Single-engined high-wing cabin monoplane P-4 Cub ...
The Cub is Piper Aircraft's second most-produced model after the PA-28 Cherokee series (>32,000 produced) with over 20,000 built in the United States. Its simplicity, affordability and popularity invokes comparisons to the Ford Model T automobile. The aircraft is a high-wing, strut-braced monoplane with a large-area
The Piper PA-18 Super Cub is a two-seat, single-engine monoplane. Introduced in 1949 by Piper Aircraft , it was developed from the PA-11 Cub Special , and traces its lineage back through the J-3 Cub to the Taylor E-2 Cub of the 1930s.
Cub Crafters, Inc. (often styled CubCrafters) is an aircraft manufacturer based in Yakima, Washington. Founded in 1980, by Jim Richmond, to build parts and supplementary type certificate (STC) modifications for the Piper PA-18 Super Cub , its CC18-180 Top Cub was Federal Aviation Administration -certified on December 16, 2004 and remained in ...
The Piper J-5 Cub Cruiser was a larger, more powerful version of the basic Piper J-3 Cub. It was designed just two years after the J-3 Cub, and differed by having a wider fuselage with the pilot sitting in the front seat and two passengers sitting in the rear seat. Equipped with a 75-hp Continental engine the plane's cruising speed was 75 mph ...
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 manufacturer General characteristics Crew: 1 Capacity: 1 Length: 6.39 m (21 ft 0 in) Wingspan: 9.31 m (30 ft 7 in) Height: 2.03 m (6 ft 8 in) Wing area: 14.2 m 2 (153 sq ft) Airfoil: Modified NACA 4412 Empty weight: 288 kg (635 lb) Gross weight: 560 kg (1,235 lb) Fuel capacity: 64 litres (14 imp gal; 17 US gal) Powerplant: 1 × Rotax 912UL Four cylinder horizontally opposed piston ...
Its 35.00 ft (10.7 m) span wing employs a USA 35B airfoil, has a wing area of 178.0 sq ft (16.54 m 2) and is supported by "V" struts and jury struts. The cabin width is 28 in (71 cm). The acceptable power range is 65 to 100 hp (48 to 75 kW) and the standard engine used is the 65 hp (48 kW) Continental A65. [1]