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FAA AD on Airbus model A-320-111, -211, -212, and -231 series airplanes (2004-03-07)
Usa - To detect and correct fatigue cracking around the fasteners connecting the pressure panel to the flexible bracket at frame 36, adjacent to the longitudinal beams on the left and right sides of the airplane, which could result in reduced structural
Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-107-AD; Amendment 39-13451; AD 2004-03-07] RIN 2120-AA64 Airworthiness Directives; Airbus Model A320-111, -211, -212, and -231 Series Airplanes PDF Copy (If Available): Preamble Information AGENCY:...
fra/pec - 58041
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency