ROLLS-ROYCE RB211-524G2-19, RB211-524G3-19, RB211-524H-36, and RB211-524H2-19 turbofan engines [Docket No. FAA-2013-1004; Directorate Identifier 2013-NE-34-AD; Amendment 39-17719; AD 2013-26-10] – requires a one-time reduction in the cyclic life of certain high-pressure (HP) compressor rotor stage 1...

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