Resumen
We are adopting a new airworthiness directive (AD) for certain Rolls-Royce plc (RR) RB211 Trent 768-60, 772-60, and 772B-60 turbofan engines. This AD requires modification of the engine by removing an electronic engine control (EEC) incorporating EEC software standard A14 or earlier and installing an EEC eligible for installation. This AD was prompted by an uncontained multiple turbine blade failure on an RR RB211 Trent 772B turbofan engine. We are issuing this AD to prevent failure of the intermediate-pressure (IP) turbine disk drive arm or burst of the high-pressure turbine disk, which could lead to uncontained engine failure and damage to the airplane.
Detalles de la directiva
Número de AD
FAA-2013-0876
Número de documento
2014-16184
Tipo
Rule
Fecha de publicación
July 11, 2014
Fecha de entrada en vigor
August 15, 2014
Fabricante afectado
Rolls-Royce plc Turbofan
Criticidad
important
Emergencia
No
Docket ID
Docket No. FAA-2013-0876
Temas
Documentos oficiales
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