# Airworthiness Directives; General Electric Company (GE) CF6-80A Series Turbofan Engines
> **Rule** · Final rule. · Published 2009-04-13 · Effective 2009-05-18 · 74 FR 16754
## Document
- **Document number:** E9-8263
- **Category:** airworthiness
- **Manufacturer:** General Electric Company (GE) CF6-80A Series Turbofan
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 74 FR 16754
- **Publication date:** 2009-04-13
- **Effective date:** 2009-05-18
- **FAA docket:** Docket No. FAA-2008-0827
## Abstract

The FAA is adopting a new airworthiness directive (AD) for GE CF6-80A series turbofan engines with certain stage 1 high-pressure turbine (HPT) rotor disks, installed. This AD requires removal from service of those stage 1 HPT rotor disks within 30 days after the effective date of the AD. This AD results from the FAA learning that those disks are susceptible to cracks developing at the aft chamfer of the blade dovetail slots. We are issuing this AD to prevent cracks developing at the aft chamfer of the blade dovetail slots that could propagate to a failure of the disk and cause an uncontained engine failure and damage to the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2009/04/13/E9-8263/airworthiness-directives-general-electric-company-ge-cf6-80a-series-turbofan-engines)
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