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Airworthiness Directives; General Electric Company Turbofan Engines

airworthiness · Rule · Final rule. · Published 2012-01-23 · Effective 2012-02-27 · 77 FR 3088

Document

Document number
2012-1132
Federal Register citation
77 FR 3088
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
General Electric Company Turbofan
Publication date
2012-01-23
Effective date
2012-02-27
FAA docket
Docket No. FAA-2011-0599

Abstract

We are adopting a new airworthiness directive (AD) for General Electric Company (GE) CF34-10E series turbofan engines. This AD was prompted by a report of heavy wear found on the seating surface of the center vent duct (CVD) (commonly referred to as center vent tube) support ring and on the inside diameter of the fan drive shaft at the mating location. This AD requires removing from service all CVD support assemblies and any fan drive shaft on the affected engines if wear is found on either the CVD support ring or the fan drive shaft. We are issuing this AD to prevent fan drive shaft failure, leading to uncontained engine failure and damage to the airplane.

Source

Authoritative
Federal Register document
Machine
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