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AD FAA-2017-1117

Airworthiness Directives; Rolls-Royce plc Turbofan Engines

Resumen

We are superseding airworthiness directive (AD) 2014-24-08 for all Rolls-Royce plc (RR) RB211-535E4-37, RB211-535E4-B-37, and RB211- 535E4-C-37 turbofan engines with certain low-pressure (LP) fuel filter- to-high-pressure (HP) fuel pump tube assemblies, or HP fuel pump-to- fuel flow governor (FFG) or FFG-to-HP pump inlet overspill return tube assemblies and flanged adaptor, installed. AD 2014-24-08 required replacing certain LP fuel filter-to-HP fuel pump tube assemblies. This AD retains the requirement in AD 2014-24-08 to remove the LP fuel filter-to-HP fuel pump tube, adds new compliance thresholds, and requires installation of new HP fuel pump-to-FFG and FFG-to-HP pump inlet overspill return tube assemblies and flanged adaptor. This AD was prompted by fuel leaks that have occurred at the flanged joints of the HP fuel pump-to-FFG tube assembly and FFG-to-HP pump inlet overspill return tube assembly. We are issuing this AD to correct the unsafe condition on these products.

Detalles de la directiva

Número de AD

FAA-2017-1117

Número de documento

2017-26572

Tipo

Rule

Fecha de publicación

December 11, 2017

Fecha de entrada en vigor

January 16, 2018

Fabricante afectado

Rolls-Royce plc Turbofan

Criticidad

routine

Emergencia

No

Docket ID

Docket No. FAA-2017-1117

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

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