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Airworthiness Directives; General Electric Company Turbofan Engines

airworthiness · Rule · Final rule. · Published 2017-12-19 · Effective 2018-01-23 · 82 FR 60106

Document

Document number
2017-27248
Federal Register citation
82 FR 60106
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
General Electric Company Turbofan
Publication date
2017-12-19
Effective date
2018-01-23
FAA docket
Docket No. FAA-2017-0660

Abstract

We are adopting a new airworthiness directive (AD) for certain General Electric Company (GE) GEnx-1B64/P2, -1B67/P2, -1B70/P2, -1B70/ 75/P2, -1B70C/P2, and -1B74/75/P2 turbofan engines. This AD was prompted by a report of the failure of the high-pressure turbine (HPT) stage 1 blade retainer and subsequent in-flight shutdown of the engine. This AD requires inspection of the HPT stage 1 blade retainer. We are issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
Machine
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