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FAA AD on General Electric Company CF6-50 series turbofan engines

Washington, Usa - To prevent LPT stage 1 disk cracking due to the potential for iron-rich inclusions introduced during manufacture, leading to uncontained disk failure

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-35-AD; Amendment 39-13135; AD 2003-09-06] RIN 2120-AA64 Airworthiness Directives; General Electric Company CF6-50 Series Turbofan Engines PDF Copy (If Available): Preamble Information Regulatory Information 2003-09-06 General Electric...

AVIONEWS - World Aeronautical Press Agency - 44636
Rome, Italy, 04/30/2003 13:45
AVIONEWS - World Aeronautical Press Agency

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