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FAA AD on Airbus model A-310 series airplanes (2004-14-06)

Usa - To detect and correct fatigue cracking and corrosion around and under chafing plates of the wing root between fuselage frame 36 and frame 39, 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 41401-41403] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-175-AD; Amendment 39-13715; AD 2004-14-06] RIN 2120-AA64 Airworthiness...

fra/pec - 100412
Rome, Italy, 07/21/2004 13:44
AVIONEWS - World Aeronautical Press Agency

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