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FAA AD on Boeing model 747 airplanes (2005-10-21)
Washington, Usa - To detect and correct fatigue cracks in the BS 1000 bulkhead chord, which, if not repaired before they reach critical length, could result in the failure of the adjacent structure and skin and lead to in-flight depressurization of the a
Airworthiness Directive Federal Register Information [Federal Register: May 19, 2005 (Volume 70, Number 96)] [Page 28803-28806] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-19538; Directorate Identifier 2003-NM-99-AD; Amendment 39-14098; AD 2005-10-21] RIN 2120-AA64 Airworthiness Directives; Boeing...
fra/pec - 120875
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency