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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
![](https://avionews.it/resources/big/cf1da682e8579f98b60323cdcae6ef68.jpg.webp)
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
AVIONEWS - World Aeronautical Press Agency