# Airworthiness Directives; General Electric Company (GE) CF34-1A, CF34-3A, and CF34-3B Series Turbofan Engines
> **Rule** · Final rule. · Published 2009-11-30 · Effective 2010-01-04 · 74 FR 62481
## Document
- **Document number:** E9-28236
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 74 FR 62481
- **Publication date:** 2009-11-30
- **Effective date:** 2010-01-04
- **FAA docket:** Docket No. FAA-2009-0328
## Abstract

The FAA is adopting a new airworthiness directive (AD) for GE CF34-1A, CF34-3A, and CF34-3B series turbofan engines. This AD requires removing from service certain part number (P/N) and serial number (SN) fan blades within compliance times specified in this AD, inspecting the fan blade abradable rub strip on certain engines for wear, inspecting the fan blades on certain engines for cracks, inspecting the aft actuator head hose fitting for correct position, and, if necessary, repositioning the hose fitting. This AD results from a report of an under-cowl fire and a failed fan blade. We are issuing this AD to prevent failure of certain P/N and SN fan blades and aft actuator head hoses, which could result in an under-cowl fire and subsequent damage to the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2009/11/30/E9-28236/airworthiness-directives-general-electric-company-ge-cf34-1a-cf34-3a-and-cf34-3b-series-turbofan)
---
*AI Analytics · CC0 1.0*