avia.wikisort.org - Engine

The TSIR-5190 is a five cylinder two-stroke radial piston aircraft engine developed for aircraft applications by McCulloch Motors Corporation.

McCulloch TSIR-5190
Type	Air-cooled five-cylinder radial piston aircraft engine
National origin	United States
Manufacturer	McCulloch Motors Corporation

Joe Crover and his father patented new technologies to complete development of the engine for production use. A pair of TRAD-4180s four cylinder diesels and a single TSIR-5190 from the Western Museum of Flight are in use for development.[1]

Specifications (TSIR-5190)

General characteristics

• Type: Five-cylinder liquid cooled radial engine
• Displacement: 190 cu in (3,114 cc)

Components

• Oil system: dry sump
• Cooling system: liquid cooled

Performance

• Power output: 270 hp (201 kW) @ 3600 rpm

References

External links

• Crover Diesel
• Video of dis-assembly
• Video of restoration
• Video of McCulloch TSIR-5190 Animation and Test Run

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