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FAA (Correction) 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
![](https://www.avionews.it/layout/elements/default.jpg)
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 Engines...
fra/pec - 1106450
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency