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FAA AD on General Electric Company (GE) CF6- 80E1A1, -80E1A2, -80E1A3, -80E1A4, and -80E1A4/B turbofan engines

Washington, Usa - To prevent failure of the HPC case aft mount flange, due to cracking

Airworthiness Directive Federal Register Information [Federal Register: November 9, 2005 (Volume 70, Number 216)] [Page 67901-67903] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22712; Directorate Identifier 2005-NE-24-AD; Amendment 39-14367; AD 2005-23-09] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 130747
Rome, Italy, 11/10/2005 15:58
AVIONEWS - World Aeronautical Press Agency

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