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McCulloch TSIR 5190

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

Contents

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.

General characteristics

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

    • Components

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

    • Performance

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

    • References

    McCulloch TSIR-5190 Wikipedia
    (Text) CC BY-SA