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FAA AD on General Electric Company model CF6- 80C2D1F turbofan engines (2006-06-08)

Washington, Usa - To prevent release of the thrust reverser cascade on landing, which could result in runway debris and a possible hazard to other aircraft

Airworthiness Directive Federal Register Information [Federal Register: March 21, 2006 (Volume 71, Number 54)] [Page 14092-14094] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22055; Directorate Identifier 2005-NE-31-AD; Amendment 39-14517; AD 2006-06-08] RIN 2120-AA64 Airworthiness Directives; General...

fra/pec - 137968

AVIONEWS - World Aeronautical Press Agency
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