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  2. Piper J-3 Cub - Wikipedia

    en.wikipedia.org/wiki/Piper_J-3_Cub

    The Piper J-3 Cub is an American light aircraft that was built between 1938 and ... flat-4 piston engine driving a fixed-pitch ... Max takeoff weight: 1,220 lb ...

  3. List of STOL aircraft - Wikipedia

    en.wikipedia.org/wiki/List_of_STOL_aircraft

    Piper J-3 Cub: US 1938 Utility Production 755 ft (230 m) 885 ft (270 m) [34] PZL-104 Wilga: Poland 1962 Utility Production 625 ft (191 m) 780 ft (238 m) [35] PZL-105M: Poland 1989 Utility Prototype 1,109 ft (338 m) 1,070 ft (326 m) [36] Quest Kodiak: US 2005 Transport Production 760 ft (232 m) 915 ft (279 m) [37] Scottish Aviation Pioneer: UK

  4. Piper PA-18 Super Cub - Wikipedia

    en.wikipedia.org/wiki/Piper_PA-18_Super_Cub

    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.

  5. CubCrafters CC11-160 Carbon Cub SS - Wikipedia

    en.wikipedia.org/wiki/CubCrafters_CC11-160...

    The CubCrafters CC11-160 Carbon Cub SS is an ASTM certified light-sport aircraft based on the Piper J-3 Cub manufactured by Cub Crafters. It is modernized, with light-weight carbon fiber components and a 180 hp (130 kW) engine. [1] In January 2016 the Carbon Cub was named AVweb's "Airplane of the Year" for 2015. [2]

  6. Piper J-4 - Wikipedia

    en.wikipedia.org/wiki/Piper_J-4

    The Piper J-4 Cub Coupe is a two place side-by-side version of the Piper J-3 that was built between 1938 and 1942 by Piper Aircraft. It was Piper's first model with ...

  7. List of Piper models - Wikipedia

    en.wikipedia.org/wiki/List_of_Piper_models

    Piper J-3 Cub Piper PA-28-180 Cherokee C Piper PA-34-220T Seneca. Model name First flight Number built Type J-2 Cub: 1936 1,207 Single-engined high-wing cabin monoplane

  8. Balanced field takeoff - Wikipedia

    en.wikipedia.org/wiki/Balanced_field_takeoff

    The speed will ensure the aircraft achieves the required height above the takeoff surface within the takeoff distance. [citation needed] To achieve a balanced field takeoff, V 1 is selected so the take-off distance with one engine inoperative, and the accelerate-stop distance, are equal. [1]

  9. STOL - Wikipedia

    en.wikipedia.org/wiki/STOL

    STOL (Short Take Off and Landing). STOL performance of an aircraft is the ability of aircraft to take off and clear a 50-foot obstruction in a distance of 1,500 feet from beginning the takeoff run. It must also be able to stop within 1,500 feet after crossing a 50-foot obstacle on landing. —