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FAA AD on McDonnell Douglas model DC-8-61, DC-8- 61F, DC-8-63, DC-8-63F, DC-8-71F, and DC-8-73F airplanes (2008-16-11)

Washington, Usa - To detect and correct fatigue cracking of door jamb corners of the forward and aft service doors, which could adversely affect the structural integrity of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 47043-47044] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-0497; Directorate Identifier 2007-NM-096-AD; Amendment 39-15629; AD 2008-16-11] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas Model DC-8-61, DC-8- 61F,...

fra/pec - 1093519

AVIONEWS - World Aeronautical Press Agency
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