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FAA AD on Rolls-Royce plc RB211-22B series turbofan engines
Washington, Usa - To prevent corrosion-induced cracking of the IP compressor stage 6 to 7 rotor shaft assembly, resulting in an uncontained engine failure and damage to 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-10-AD; Amendment 39-13213; AD 2003-13-12] RIN 2120-AA64 Airworthiness Directives; Rolls-Royce plc RB211-22B Series Turbofan Engines PDF Copy (If Available): Preamble Information AGENCY: Federal...
fra/pec - 47336
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency