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FAA AD on General Electric Company CF34 Series Turbofan Engines

Washington, Usa - To prevent rupture of the fan disk due to cracks that initiate at an electrical arc-out, which could result in an uncontained failure of the engine

Airworthiness Directive Federal Register Information [Federal Register: March 3, 2006 (Volume 71, Number 42)] [Page 10832-10834] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NE-42-AD; Amendment 39-14501; AD 2006-05-04] RIN 2120-AA64 Airworthiness Directives; General Electric Company CF34 Series Turbofan...

fra/pec - 136938
Rome, Italy, 03/06/2006 11:47
AVIONEWS - World Aeronautical Press Agency

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