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AD FAA-2015-6823

Airworthiness Directives; General Electric Company Turbofan Engines

Summary

We are adopting a new airworthiness directive (AD) for all General Electric Company (GE) GE90-76B, -77B, -85B, -90B, and -94B turbofan engines. This AD requires performing an eddy current inspection (ECI) or ultrasonic inspection (USI) of the high-pressure compressor (HPC) stage 8-10 spool and removing from service those parts that fail inspection. This AD was prompted by an uncontained failure of the HPC stage 8-10 spool, leading to an airplane fire. We are issuing this AD to prevent failure of the HPC stage 8-10 spool, uncontained rotor release, damage to the engine, and damage to the airplane.

Directive Details

AD Number

FAA-2015-6823

Document Number

2015-33075

Type

Rule

Publication Date

January 12, 2016

Effective Date

January 27, 2016

Affected Manufacturer

General Electric Company Turbofan

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2015-6823

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

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AD FAA-2015-6823 — Airworthiness Directives; General Electric Company Turbofan Engines