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AD FAA-2013-0879

Airworthiness Directives; General Electric Company Turbofan Engines

Summary

We are superseding Airworthiness Directive (AD) 2013-24-17 for General Electric Company (GE) GE90-110B1 and GE90-115B turbofan engines with certain high-pressure compressor (HPC) rotor stage 2-5 spools installed. AD 2013-24-17 required removing these spools from service at times determined by a drawdown plan. This AD retains the same requirements as AD 2013-24-17. This AD also adds additional part number (P/N) HPC spools to the applicability. This AD was prompted by reports of cracking on these additional spools. We are issuing this AD to correct the unsafe condition on these products.

Directive Details

AD Number

FAA-2013-0879

Document Number

2017-06715

Type

Rule

Publication Date

April 6, 2017

Effective Date

April 21, 2017

Affected Manufacturer

General Electric Company Turbofan

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2013-0879

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

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