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FAA AD on Airbus model A-320/111, -211, -212, and -231 series airplanes (2004-14-09)

Usa - To prevent fatigue cracking of the lower surface panel on the wing center box, which could result in reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 9, 2004 (Volume 69, Number 131)] [Page 41398-41401] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-177-AD; Amendment 39-13718; AD 2004-14-09] RIN 2120-AA64 Airworthiness...

fra/pec - 100367

AVIONEWS - World Aeronautical Press Agency
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