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FAA AD on Rolls-Royce plc RB211 Trent 800 series turbofan engines
Washington, Usa - To prevent stage 5 and 6 disc crack initiation and propagation leading to uncontained disc 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. 2003-NE-03-AD; Amendment 39-13249; AD 2003-15-06] RIN 2120-AA64 Airworthiness Directives; Rolls-Royce plc RB211 Trent 800 Series Turbofan Engines PDF Copy (If Available): Preamble Information AGENCY:...
fra/pec - 48601
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency