Beechcraft Skipper

Key Specifications

Overview

The Beechcraft Skipper is a two-seat, low-wing monoplane trainer aircraft designed primarily for flight training and personal use. Introduced in the late 1970s, it represents Beechcraft's entry into the ab initio trainer market. The aircraft features a cantilever low-wing design, retractable landing gear, and is powered by a single Lycoming O-235 engine. The Skipper gained popularity among flight schools and individual pilots for its forgiving handling characteristics, robust construction, and economical operating costs. Its stability and predictable flight characteristics make it an excellent platform for primary flight training. The aircraft is known for its durability and relatively simple maintenance requirements. While production ended in the early 1980s, the Skipper maintains a dedicated following in the general aviation community and continues to serve flight training operations worldwide. The type is particularly valued for its reasonable acquisition cost on the used market and modest fuel consumption, making it an affordable option for aspiring pilots and small flight operations.

Technical Specifications

Maximum Speed: 126 mph
Cruise Speed: 115 mph
Range: 440 nautical miles
Service Ceiling: 12,500 feet
Engine: Lycoming O-235-L2C (118 hp)
Maximum Takeoff Weight: 1,675 lbs
Empty Weight: 1,040 lbs
Fuel Capacity: 40 gallons