Titan Missile Museum
 

Lycoming R-680

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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.

Technical Specifications
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


Location: Hangar 3