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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
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