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FAA AD on General Electric Company CF34-1A, -3A, -3A1, -3A2, -3B, and -3B1 turbofan engines (2009-07-12)

Washington, Usa - To prevent the inability to restart both engines after flameout due to excessive friction of the 4-step seal, which could result in subsequent forced landing of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 14929-14931] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-0419; Directorate Identifier 2007-NE-52-AD; Amendment 39-15871; AD 2009-07-12] RIN 2120-AA64 Airworthiness Directives; General Electric Company CF34-1A, -3A, -3A1,...

fra/pec - 1103338

AVIONEWS - World Aeronautical Press Agency
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