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AD FAA-2015-7491

Airworthiness Directives; General Electric Company Turbofan Engines

Summary

We are superseding Airworthiness Directive (AD) 2016-13-05 for all General Electric Company (GE) GE90-76B, GE90-77B, GE90-85B, GE90- 90B, and GE90-94B turbofan engines. AD 2016-13-05 required eddy current inspection (ECI) of the high-pressure compressor (HPC) stage 8-10 spool at each shop visit for all affected engines and ECI or ultrasonic inspection (USI) for certain affected engines. This new AD requires initial and repetitive on-wing USIs of the HPC stage 8-10 spool for certain engines prior to shop visit and ECI of all affected engines at each shop visit. This AD was prompted by analysis that the risk of the failure of an HPC stage 8-10 spool was excessive without repetitive USI prior to shop visit. We are issuing this AD to correct the unsafe condition on these products.

Directive Details

AD Number

FAA-2015-7491

Document Number

2017-07476

Type

Rule

Publication Date

April 14, 2017

Effective Date

May 19, 2017

Affected Manufacturer

General Electric Company Turbofan

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2015-7491

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for General Electric Company Turbofan →

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