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FAA AD on General Electric Company (GE) CF6-45, - 50, -80A, -80C2, and -80E1 turbofan Engines

Washington, USA - To detect cracks, which can cause separation of the HPCR stage 3-9 spool and possible uncontained engine failure

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NE-26-AD; Amendment 39-12984; AD 2002-25-08] RIN 2120-AA64 Airworthiness Directives; General Electric Company (GE) CF6-45, - 50, -80A, -80C2, and -80E1 Turbofan Engines PDF Copy (If Available): Preamble Information Regulatory Information 2002-25-08...

AVIONEWS - World Aeronautical Press Agency - 37758
Rome, Italy, 12/23/2002 17:13
AVIONEWS - World Aeronautical Press Agency

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