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FAA AD on McDonnell Douglas model DC-8-11, DC-8- 12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43; DC-8-50; DC-8F-54 and DC-8F-55; DC-8-60; DC-8-60F; DC-8-70 Series Airplanes

To ensure that the unsafe condition will be addressed on all affected airplanes so that cracking in the lower cargo doorjamb corners is detected and corrected before it can result in rapid decompression of the fuselage and consequent reduced integrity

Airworthiness Directive Federal Register Information [Federal Register: September 2, 2005 (Volume 70, Number 170)] [Page 52285-52288] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-19536; Directorate Identifier 2004-NM-86-AD; Amendment 39-14247; AD 2005-18-07] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 126175

AVIONEWS - World Aeronautical Press Agency
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