Jacobs R-755

From Wikipedia, the free encyclopedia

The Jacobs R-755 or L-4 was a seven-cylinder, air-cooled, radial engine for aircraft manufactured in the United States. It was first run in 1933 and was still in production in the 1970s. With a bore and stroke of 5.25 in × 5 in (133 mm × 127 mm), power ranged from 200 hp - 350 hp (150 kW - 260 kW)

[edit] Applications

 Mexico

• Anahuac Tauro

 France

• Morane-Saulnier MS-505

 United States

• Cessna AT-17
• Cessna 195

[edit] References

• Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens, 81. 

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