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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, DC-8-43, DC- 8F-54, DC-8F-55; DC-8-50, DC-8-60, DC-8-60F, DC-8-70, and DC-8-70F series airplanes

Washington, Usa - To prevent stress corrosion cracking in the forward tang of the upper inboard spar cap of the wing, which could result in structural damage to adjacent components of the wing and consequent reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 28, 2005 (Volume 70, Number 144)] [Page 43628-43631] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-343-AD; Amendment 39-14203; AD 2005-15-14] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas Model DC-8-11, DC-8- 12,...

fra/pec - 124630
Rome, Italy, 07/29/2005 13:54
AVIONEWS - World Aeronautical Press Agency

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