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FAA AD on Rolls-Royce plc. RB211-535 turbofan engines
Washington, Usa - To prevent LP turbine stage 2 disc failure, which could result in an uncontained engine failure and possible loss of the airplane
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Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-16-AD; Amendment 39-13290; AD 2003-17-15] RIN 2120-AA64 Airworthiness Directives; Rolls-Royce plc. RB211-535 Turbofan Engines PDF Copy (If Available): Preamble Information AGENCY: Federal Aviation...
fra/pec - 52214
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency