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FAA (Revision) AD on Boeing model 767-200, -300, and -300F series airplanes

Washington, Usa - To detect and correct fatigue cracking or corrosion of the fail-safe straps, which could result in cracking of adjacent structure and consequent reduced structural integrity of the fuselage

Airworthiness Directive Federal Register Information [Federal Register: October 5, 2005 (Volume 70, Number 192)] [Page 58000-58002] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22584; Directorate Identifier 2005-NM-044-AD; Amendment 39-14313; AD 2004-19-06 R1] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 128418
Rome, Italy, 10/06/2005 16:04
AVIONEWS - World Aeronautical Press Agency

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