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AD FAA-2018-0314

Airworthiness Directives; Rolls-Royce plc Turbofan Engines

Summary

We are adopting a new airworthiness directive (AD) for all Rolls-Royce plc (RR) Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, and Trent 1000-L2 turbofan engines. This AD requires initial and repetitive inspections of the intermediate-pressure compressor (IPC) stage 1 rotor blades, IPC stage 2 rotor blades, and IPC shaft stage 2 dovetail posts, and removing any cracked parts from service. This AD was prompted by IPC blade separations resulting in engine failures. We are issuing this AD to address the unsafe condition on these products.

Directive Details

AD Number

FAA-2018-0314

Document Number

2018-08602

Type

Rule

Publication Date

April 24, 2018

Effective Date

April 24, 2018

Affected Manufacturer

Rolls-Royce plc Turbofan

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2018-0314

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

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