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Cessna 195

General Aviation and Light Aircraft

The Cessna 195 is a light, single radial-engine, tailwheel utility aircraft that Cessna built from 1947 to 1954 alongside the Cessna 190, which used a Continental radial of 240 horsepower where the 195 used a Jacobs radial of 300 horsepower. It was the first Cessna airplane constructed entirely of aluminum, with a cantilever wing derived from the pre-war Cessna 165, and its fuselage is large for a Cessna because a 42 inch diameter radial engine had to fit in the nose. Seating is in two rows, with two individual front seats and a bench seat behind, and many aircraft carry swivelling crosswind landing gear. The United States Air Force, Army and Army National Guard used the 195 as a light transport and utility aircraft under the designations LC-126 and U-20. The first prototype flew in 1945 and 1,180 190s and 195s were built.

Facts
Year
1947 1
Status
Out of production 1
Power (kW)
220 1
Top Speed (km/h)
286 1
Mass (kg)
953 1
Maximum Mass (kg)
1520 1
Engine
Jacobs R-755 radial engine, 300 hp 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Source Cessna 195 (Wikipedia)

Of Make

Source Cessna 195 (Wikipedia)
Sources
1. Cessna 195 (Wikipedia)
  • Development
    The Cessna 190 and 195 were Cessna's only postwar radial-engined aircraft. The first prototype flew in 1945, after the end of World War II and both the 190 and 195 entered production in 1947.
  • Specifications (Cessna 195)
    Powerplant: 1 × Jacobs R-755 radial engine, 300 hp (220 kW)
  • Specifications (Cessna 195), empty weight
    Empty weight: 2,100 lb (953 kg)
  • Specifications (Cessna 195), gross weight
    Gross weight: 3,350 lb (1,520 kg)
  • Specifications (Cessna 195), maximum speed
    Maximum speed: 178 mph (286 km/h, 155 kn)
  • Lead
    The Cessna 190 and 195 Businessliner are a family of light single radial engine powered, conventional landing gear equipped, general aviation aircraft which were manufactured by Cessna between 1947 and 1954.
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