# Airworthiness Directives; Turbomeca Arrius 2F Turboshaft Engines
> **Rule** · Final rule. · Published 2007-05-22 · Effective 2007-06-26 · 72 FR 28589
## Document
- **Document number:** E7-9721
- **Category:** airworthiness
- **Manufacturer:** Turbomeca Arrius 2F Turboshaft
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 72 FR 28589
- **Publication date:** 2007-05-22
- **Effective date:** 2007-06-26
- **FAA docket:** Docket No. FAA-2005-22430
## Abstract

The FAA is superseding an existing airworthiness directive (AD) for Turbomeca Arrius 2F turboshaft engines. That AD currently requires removing from service certain serial number (SN) fuel control units (FCUs) or replacing the constant delta pressure (delta P) diaphragm in those FCUs. This AD requires replacing all FCUs not incorporating modification Tf 55 with FCUs that incorporate modification Tf 55. This AD results from the European Aviation Safety Agency (EASA) and Turbomeca expanding the applicability to the full population of FCUs installed on Arrius 2F turboshaft engines. FCUs not incorporating modification Tf 55 are susceptible to having an improperly assembled constant delta P diaphragm. We are issuing this AD to prevent an uncommanded engine in-flight shutdown on a single-engine helicopter, resulting in a forced autorotation landing or an accident.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2007/05/22/E7-9721/airworthiness-directives-turbomeca-arrius-2f-turboshaft-engines)
---
*AI Analytics · CC0 1.0*