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This engine design was a Russian re-engineered version of the Wright R-1820.
All photographs and text copyright Arizona Aerospace Foundation, 2006 and may not be used in any way without express written permission.
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| Cylinders |
9 |
| Rated Output |
1,000 hp at 2,000 r.p.m. |
| Dry Weight |
1,200 lbs |
| Commonly Used On |
An-2, An-2M |
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