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AD FAA-2014-0433

Airworthiness Directives; Rolls-Royce plc Turbofan Engines

Summary

We are superseding airworthiness directive (AD) 98-07-07 for all Rolls-Royce plc (RR) RB211-535E4 and RB211-535E4-B turbofan engines. AD 98-07-07 required removing certain part number (P/N) low- pressure (LP) fuel filter-to-high-pressure (HP) fuel pump tube assemblies and installing flexible LP fuel filter-to-HP fuel pump tube assemblies. This AD expands the applicability of AD 98-07-07 to include the RB211-535E4-C-37 turbofan engine and requires removal from service of additional P/N LP fuel filter-to-high-pressure HP fuel pump tube assemblies. This AD was prompted by reports of fuel leaks that have resulted in a number of engine in-flight shutdowns. We are issuing this AD to prevent loss of fuel supply to the engine, which could lead to an in-flight shutdown of one or more engines, loss of thrust control, and damage to the airplane.

Directive Details

AD Number

FAA-2014-0433

Document Number

2014-28189

Type

Rule

Publication Date

December 2, 2014

Effective Date

January 6, 2015

Affected Manufacturer

Rolls-Royce plc Turbofan

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2014-0433

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Rolls-Royce plc Turbofan →

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