McCulloch TSIR-5190
# McCulloch TSIR-5190

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

## 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
