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FAA AD on General Electric CF34-8C1 turbofan engines

Washington, Usa - To prevent rupture of the combustion chamber assembly and possible engine fire

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-23-AD; Amendment 39-13143; AD 2003-09-14] RIN 2120-AA64 Airworthiness Directives; General Electric CF34-8C1 Turbofan Engines PDF Copy (If Available): Preamble Information Regulatory Information 2003-09-14 General Electric: Amendment...

AVIONEWS - World Aeronautical Press Agency - 45038
Rome, Italy, 05/09/2003 13:24
AVIONEWS - World Aeronautical Press Agency

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