# Airworthiness Directives; General Electric Company CF34 Series Turbofan Engines
> **Rule** · Final rule; request for comments. · Published 2001-05-16 · Effective 2001-05-31 · 66 FR 27017
## Document
- **Document number:** 01-12006
- **Category:** airworthiness
- **Manufacturer:** General Electric Company CF34 Series Turbofan
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 66 FR 27017
- **Publication date:** 2001-05-16
- **Effective date:** 2001-05-31
- **FAA docket:** Docket No. 2000-NE-42-AD
## Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Company (GE) CF34-1A, -3A, -3A1, - 3A2, -3B, and -3B1 turbofan engines. This action requires a one-time inspection, and if necessary replacement of certain fan disks for electrical arc-out indications, and assigns a reduction in the life limit of certain fan disks. This amendment is prompted by a report of a crack that was found during a visual inspection as part of routine engine maintenance. The actions specified in this AD are intended to prevent rupture of the fan disk due to cracks that initiate at an electrical arc-out, which could result in an uncontained failure of the engine.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2001/05/16/01-12006/airworthiness-directives-general-electric-company-cf34-series-turbofan-engines)
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