Resumen
We are rescinding an airworthiness directive (AD) for RRD BR700-715A1-30, BR700-715B1-30, and BR700-715C1-30 turbofan engines. The existing AD resulted from the need to reduce the published life limits of high-pressure (HP) turbine stage 1 discs, part numbers (P/Ns) BRH20130 and BRH20131, and HP turbine stage 2 discs, P/Ns BRH19423 and BRH19427. We are rescinding the existing AD because RRD has revised the approved published life limits of these parts to the same or higher limits as originally certified.
Detalles de la directiva
Número de AD
FAA-2008-0224
Número de documento
2012-15961
Tipo
Rule
Fecha de publicación
July 2, 2012
Fecha de entrada en vigor
August 6, 2012
Fabricante afectado
Rolls-Royce Deutschland Ltd & Co KG (RRD) Turbofan
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2008-0224
Temas
Documentos oficiales
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