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FAA AD on Rolls-Royce plc RB211 Trent 800 Series Turbofan Engines (2009-21-09)

Washington, Usa - To prevent stage 5 and 6 disc crack initiation and propagation that might lead to uncontained disc failure and damage to the airplane

Airworthiness Directive Federal Register Information [Federal Register: (Volume 74, Number 199)] [Page 53154-53156] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2009-1369; Directorate Identifier 2003-NE-03-AD; Amendment 39-16048; AD 2009-21-09] RIN 2120-AA64 Airworthiness Directives; Rolls-Royce plc RB211...

fra/pec - 1110417

AVIONEWS - World Aeronautical Press Agency
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