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FAA AD on Airbus model A-300 B4-600 and A-300 B4- 600R series airplanes; and A-300 F4-605R and A-300 C4-605R Variant F airplanes (2005-23-08)

Washington, Usa - To prevent fatigue cracking of the forward fitting of fuselage frame FR47, which could result in reduced structural integrity of the frame

Airworthiness Directive Federal Register Information [Federal Register: November 14, 2005 (Volume 70, Number 218)] [Page 69056-69059] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22110; Directorate Identifier 2004-NM-205-AD; Amendment 39-14366; AD 2005-23-08] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 131006
Rome, Italy, 11/15/2005 11:59
AVIONEWS - World Aeronautical Press Agency

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