Vehicle

Beechcraft Skipper

General Aviation and Light Aircraft

The Beechcraft Model 77 Skipper is a two-seat, fixed tricycle gear general aviation airplane, designed originally for flight training but also used for touring and personal flying. Design work began in 1974 as the PD 285, which first flew on 6 February 1975, as Beechcraft's attempt to enter the two-place trainer market against the popular Cessna 150 line. It entered production with a T-tail, uses side-by-side seating and a Lycoming O-235 engine, and is an all-metal design with tubular spars and a wing airfoil developed from 1970s NASA research. It was built at the Liberal, Kansas division alongside the Duchess and the Musketeer, and was introduced at the start of a severe downturn in United States general aviation. Production stopped in 1983 after 312 aircraft, most delivered to the Beech Aero Centers flight schools.

Facts
Year
1975 1
Engine Class
Piston 1
Status
Out of production 1
Units Built
312 1
Mass (kg)
499 1
Maximum Mass (kg)
760 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Source Beechcraft Skipper (Wikipedia)

Of Make

Source Beechcraft Skipper (Wikipedia)
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Manufactured By

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Source Beechcraft Skipper (Wikipedia)Lead
Quote, Lead
is a two-seat, fixed tricycle gear general aviation airplane

Originated In

Also in Geography Atlas: where this subject originated.

Source Beechcraft Skipper (Wikipedia)Design and development
Quote, Design and development
introduced at the beginning of a severe downturn in general aviation aircraft production in the United States
Sources
1. Beechcraft Skipper (Wikipedia)
  • Design and development, first flight
    which made its maiden flight on February 6, 1975
  • Lead
    is a two-seat, fixed tricycle gear general aviation airplane
  • Specifications
    Lycoming O-235-L2C four-cylinder, air-cooled, horizontally opposed, piston aero engine
  • Production, production end
    Production stopped in 1983
  • Production, units built
    A total of 312 aircraft were built
  • Specifications, empty weight
    Empty weight: 1,100 lb (499 kg)
  • Specifications, max takeoff weight
    Max takeoff weight: 1,675 lb (760 kg)
  • Design and development
    introduced at the beginning of a severe downturn in general aviation aircraft production in the United States
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