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FAA AD on McDonnell Douglas Model DC-8-55, DC-8F- 54, and DC-8F-55 airplanes; and DC-8-60, DC-8-70, DC-8-60F, and DC-8-70F series airplanes (2008-06-23)

Washington, Usa - To detect and correct cracks in the aft fuselage skin at the longeron 28 skin splice, which could lead to loss of structural integrity of the aft fuselage, resulting in rapid decompression of the airplane

Airworthiness Directive Federal Register Information Federal Register: March 18, 2008 [Page 14378-14381] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-0216; Directorate Identifier 2007-NM-122-AD; Amendment 39-15435; AD 2008-06-23] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas Model DC-8-55,...

fra/pec - 1087414
Rome, Italy, 03/21/2008 14:23
AVIONEWS - World Aeronautical Press Agency

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