Beechcraft Skipper

· Beechcraft · 1 × Lycoming O-235

Airplanes

Length

7.32 m

Flat Wing Span

9.14 m

Height

2.41 m

Flat Wing Area

12.1 m²

Cruise Speed

195 km/h

Max Ceiling

3930 m

Number of Engines

Aircraft Engine

First Flight

1978-09-12

Entry Into service

1979-01-01

Number Built

312

Maximum Take-Off Weight

0.76 t (paragliders: kg)

Maximum Range

764 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Beechcraft Skipper	0.76	764

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
AMD Alarus	Lycoming O-235	7.0104	8.5344	Compare
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Aquila A 211		7.4	10.3	Compare

All data (22 fields)

Name: Beechcraft Skipper
Manufacturer: Beechcraft
Description: The Beechcraft Model 77 Skipper is a two-seat, fixed tricycle gear general aviation airplane, originally designed for flight training but also used for touring and personal flying.
First Flight: 1978-09-12
Entry Into service: 1979-01-01
Production End: 1983-01-01
Designer: Beechcraft
Type: Light utility aircraft
Length (m): 7.32
Height (m): 2.41
Cockpit Crew: 2
Cruise Speed (km/h): 195
Min Speed (km/h): 87
Max Ceiling (m): 3930
Rate of Climb (m/s): 3.65
Number Built: 312
Powerplant Description: 1 × Lycoming O-235-L2C four-cylinder, air-cooled, horizontally opposed, piston aero engine, 86 kW (115 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Beechcraft_Skipper
Flat Wing Span (m): 9.14
Flat Wing Area (m²): 12.1
Aircraft Engine: Lycoming O-235
Number of Engines: 1