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FAA AD on General Electric Company CF6-6 series turbofan engines

Washington, Usa - To prevent cracks in high pressure turbine rotor (HPTR) rear shafts, which could result in uncontained engine failure and damage to the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-24-AD; Amendment 39-13144; AD 2003-10-01] RIN 2120-AA64 Airworthiness Directives; General Electric Company CF6-6 Series Turbofan Engines PDF Copy (If Available): Preamble Information Regulatory Information 2003-10-01 General Electric...

AVIONEWS - World Aeronautical Press Agency - 45239
Rome, Italy, 05/14/2003 11:35
AVIONEWS - World Aeronautical Press Agency

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