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FAA AD on Pratt & Whitney (PW) JT9D-7 series turbofan engines (2009-04-18)

Washington, Usa - To prevent failure of the 2nd stage HPT rotor disk, which could result in uncontained engine failure, damage to the airplane, and the engine separating from the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 14458-14460] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-0759; Directorate Identifier 2008-NE-02-AD; Amendment 39-15824; AD 2009-04-18] RIN 2120-AA64 Airworthiness Directives; Pratt & Whitney (PW) JT9D-7 Series Turbofan...

fra/pec - 1103334

AVIONEWS - World Aeronautical Press Agency
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