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Engine designed for training aircraft with controllable or fixed pitch airscrews.
All photographs and text copyright Arizona Aerospace Foundation, 2009 and may not be used in any way without express written permission.
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| Cylinders |
9 |
| Displacement/ Compressions |
680 cu in/ 7 to 1 |
| Rated Output |
285 hp at 2,200 r.p.m. |
| Dry Weight |
515 lbs |
| Commonly Used On |
Training Aircraft, AT-9A |
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