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Allison T40

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Early turbo prop engine deployed in several experimental aircraft. This engine was a pair to T38s connected with a transmission almost doubling the length of the engine assembly. Engine designed in 1953.

Technical Specifications
Rated Output 5,035 hp Plus 1,225 lbs thrust
Compressor Axial 19 Stage
Turbine Axial 3 Stage
After Burner Not Equipped
Commonly Used On XA2D-1, XA2J-1, XP5Y-1, XF-84H, XFY-1, XFV-1


Location: Restoration