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FAA (Revision) AD on Pratt & Whitney JT8D-209, -217, -217C, and -219 turbofan engines (97-17-04R1)

Washington, Usa - To prevent fan hub rupture due to tierod, counterweight, or bushed hole cracking, which could result in an uncontained engine failure and damage to the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 12968-12971] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2009-0883; Directorate Identifier 97-ANE-08; Amendment 39-16237; AD 97-17-04 R1 ] RIN 2120-AA64 Airworthiness Directives; Pratt & Whitney JT8D-209, -217, -217C, and -219...

fra/pec - 1116260
Rome, Italy, 04/13/2010 14:24
AVIONEWS - World Aeronautical Press Agency

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