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AD FAA-2013-0880

Airworthiness Directives; Rolls-Royce plc Turbofan Engines

Summary

We are adopting a new airworthiness directive (AD) for all Rolls-Royce plc (RR) RB211 Trent 553-61, 553A2-61, 556-61, 556A2-61, 556B-61, 556B2-61, 560-61, and 560A2-61 turbofan engines. This AD requires replacement or repair of the low-pressure (LP) compressor fan blade set before reaching a specified number of flight cycles since new (FCSN) or flight cycles since last leading edge profile blade repair (FCSLR). This AD was prompted by reports of erosion of the leading edge profile of the LP compressor blade set contributing to fan blade flutter. We are issuing this AD to prevent failure of the LP compressor blades, which could lead to an uncontained engine failure and damage to the airplane.

Directive Details

AD Number

FAA-2013-0880

Document Number

2013-28178

Type

Rule

Publication Date

November 26, 2013

Effective Date

December 11, 2013

Affected Manufacturer

Rolls-Royce plc Turbofan

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2013-0880

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Rolls-Royce plc Turbofan →

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