# Airworthiness Directives; General Electric Company Turbofan Engines
> **Rule** · Final rule. · Published 2014-10-23 · Effective 2014-11-28 · 79 FR 63307
## Document
- **Document number:** 2014-24697
- **Category:** airworthiness
- **Manufacturer:** General Electric Company Turbofan
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 79 FR 63307
- **Publication date:** 2014-10-23
- **Effective date:** 2014-11-28
- **FAA docket:** Docket No. FAA-2007-28413
## Abstract

We are superseding airworthiness directives (ADs) 90-26-01, 91-20-02, and 2009-05-02 for all General Electric Company (GE) CF6-80C2 and CF6-80E1 series turbofan engines. This AD retains the requirements of those ADs and requires removal of additional fuel manifold part numbers (P/Ns), additional repetitive inspections, replacement as required of certain fuel manifold P/Ns and tube (block) clamps, and replacement of loop clamps. This AD was prompted by a report of an under-cowl fire caused by a manifold high-pressure fuel leak, and several additional reports of fuel leaks. We are issuing this AD to prevent failure of the fuel manifold, which could lead to uncontrolled engine fire, engine damage, and damage to the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2014/10/23/2014-24697/airworthiness-directives-general-electric-company-turbofan-engines)
---
*AI Analytics · CC0 1.0*