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
Engine Class Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Beechcraft Skipper (Wikipedia)
Of Make
Source Beechcraft Skipper (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Beechcraft Skipper (Wikipedia)LeadQuote, 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 developmentQuote, 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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