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CLARA MOSCHINI

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FAA AD on Airbus model A-300 B2 and B4; and A-300 B4-600, B4-600R, and F4-600R, and C4-605R Variant F airplanes (2006-15-04)

Washington, Usa - To detect and correct fatigue cracks in the lower flanges of gantries 1 through 5 inclusive in the MLG bay area, which could result in reduced structural integrity of the fuselage, and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 20, 2006 (Volume 71, Number 139)] [Page 41109-41113] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-23690; Directorate Identifier 2004-NM-133-AD; Amendment 39-14684; AD 2006-15-04] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 145889

AVIONEWS - World Aeronautical Press Agency
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