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FAA AD on McDonnell Douglas model DC-8 airplanes

Washington, Usa - To minimize the possibility of crank assembly failure when the assembly is exposed to abnormal load conditions

Airworthiness Directive Federal Register Information [Federal Register: March 18, 2005 (Volume 70, Number 52)] [Page 13092-13093] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-19541; Directorate Identifier 2004-NM-129-AD; Amendment 39-14013; AD 2005-06-05] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 116749
Rome, Italy, 03/21/2005 13:40
AVIONEWS - World Aeronautical Press Agency

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