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Airworthiness Directives; General Electric Company Turbofan Engines

airworthiness · Rule · Final rule. · Published 2016-06-24 · Effective 2016-07-29 · 81 FR 41208

Document

Document number
2016-14474
Federal Register citation
81 FR 41208
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
General Electric Company Turbofan
Publication date
2016-06-24
Effective date
2016-07-29
FAA docket
Docket No. FAA-2015-7491

Abstract

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

Source

Authoritative
Federal Register document
Machine
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