Resumen
We are adopting a new airworthiness directive (AD) for all Rolls-Royce plc (RR) Trent 1000-A, 1000-C, 1000-D, 1000-E, 1000-G, and 1000-H turbofan engines. This AD requires removing engine electronic controller (EEC) software earlier than standard MB6.15 and replacing with a software standard eligible for installation. This AD was prompted by a finding that an intermediate pressure (IP) shaft failure may not be detected by EEC software earlier than standard MB6.15. We are issuing this AD to detect IP shaft failure and prevent IP compressor turbine burst, uncontained engine failure, and damage to the airplane.
Detalles de la directiva
Número de AD
FAA-2014-0705
Número de documento
2014-25739
Tipo
Rule
Fecha de publicación
October 30, 2014
Fecha de entrada en vigor
November 14, 2014
Fabricante afectado
Rolls-Royce plc Turbofan
Criticidad
important
Emergencia
No
Docket ID
Docket No. FAA-2014-0705
Temas
Documentos oficiales
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