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FAA (Revision) AD on Pratt & Whitney JT8D-1, -1A, -1B, -7, - 7A, -7B, -9, -9A, -11, -15, -15A, -17, -17A, -17R, -17AR, -209, -217, - 217A, -217C, and -219 turbofan engines (2006-17-07R1)

Washington, Usa - To prevent prevent a rupture of an HPC front hub or an HPC disk that could result in an uncontained engine failure and damage to the airplane

Airworthiness Directive Federal Register Information [Federal Register: October 18, 2006 (Volume 71, Number 201)] [Page 61395-61399] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-25809; Directorate Identifier 2001-NE-30-AD; Amendment 39-14791; AD 2006-17-07R1] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 67046

AVIONEWS - World Aeronautical Press Agency