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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
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