Do you want to access to this and other private contents?
Log in if you are a subscriber or click here to request service
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
AVIONEWS - World Aeronautical Press Agency