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FAA AD on Airbus model A-330/243, -341, -342, and -343 airplanes equipped with Rolls-Royce RB211 TRENT 700 engines (2005-25-21)

Washington, Usa - To prevent fatigue cracking of the hinges integrated into the 12 o'clock beam of the thrust reversers, which could result in separation of a thrust reverser from the airplane, and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: December 14, 2005 (Volume 70, Number 239)] [Page 73919-73921] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-23252; Directorate Identifier 2004-NM-146-AD; Amendment 39-14414; AD 2005-25-21] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 133151

AVIONEWS - World Aeronautical Press Agency
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