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
Top Speed (km/h) Maximum Mass (kg) EngineJacobs R-755 radial engine, 300 hp 1 Comparison
Body StyleAircraft (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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