Rotax 275
| BRP-Rotax | |
|---|---|
| Image does not exist |
|
| Rotax 275 | |
| Production period: | unknown |
| Manufacturer: | BRP-Rotax |
| Developing country: |
 Austria
|
| Working principle: | Otto |
| Motor design: | Single cylinder |
| Drilling: | 72 mm |
| Hub: | 66 mm |
| Displacement: | 268.7 cm 3 |
| Mixture preparation: | Carburetor |
| Engine charging: | - |
| Cooling system: | Air cooling |
| Power: | 18 kW |
| Dimensions: | 25 kg |
| Previous model: | none |
| Successor: | none |
The Rotax 275 is an air-cooled single-cylinder , two-stroke aircraft engine . It is built by the Austrian company BRP-Rotax for installation in motor gliders . It has a single magneto ignition and a gearbox to drive a propeller . He was admitted in November 1988 in Austria.
use
Web links
Commons : Rotax 275 - collection of images, videos and audio files
Individual evidence
- ↑ EASA Type-Certificate Data Sheet No E.210 for Rotax 275 series engines. (pdf) EASA, accessed on January 17, 2020 (English).
