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FAA AD on Airbus model A-320-111, -211, and -231 series airplanes

Washington, Usa - To detect and correct fatigue cracking in the transition and pick-up angles of the lower part of the center fuselage, which could result in reduced structural integrity of the wing-fuselage support and fuselage pressure vessel

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-118-AD; Amendment 39-13463; AD 2004-03-19] RIN 2120-AA64 Airworthiness Directives; Airbus Model A320-111, -211, and -231 Series Airplanes PDF Copy (If Available): Preamble Information AGENCY: Federal...

fra/pec - 58203

AVIONEWS - World Aeronautical Press Agency
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