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Rated maximum continuous power, with respect to reciprocating, turbopropeller, and turboshaft engines, – 14 CFR 1.1

Rated maximum continuous power, with respect to reciprocating, turbopropeller, and turboshaft engines, means the approved brake horsepower that is developed statically or in flight, in standard atmosphere at a specified altitude, within the engine operating limitations established under Part 33, and approved for unrestricted periods of use.

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