# Airworthiness Directives; Eurocopter France Model EC 155B, EC155B1, SA-365N, SA-365N1, AS-365N2, and AS 365 N3 Helicopters
> **Rule** · Final rule. · Published 2005-06-24 · Effective 2005-07-29 · 70 FR 36482
## Document
- **Document number:** 05-12418
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 70 FR 36482
- **Publication date:** 2005-06-24
- **Effective date:** 2005-07-29
- **FAA docket:** Docket No. FAA-2005-20512
## Abstract

This amendment supersedes an existing airworthiness directive (AD) for Eurocopter France (Eurocopter) Model EC 155B, SA-365N and N1, AS-365N2, and AS 365 N3 helicopters. That AD currently requires inspecting the hydraulic brake hose (hose) for crazing, pinching, distortion, or leaks at the torque link hinge and replacing the hose, if necessary. That AD also requires inspecting the hose and the emergency flotation gear pipe to ensure adequate clearance, and adjusting the landing gear leg, if necessary. This amendment requires the same actions as the existing AD and adds another model helicopter to the applicability. This amendment is prompted by notification by the manufacturer and the European Authority that another affected model helicopter, the Model EC155B1, may have the same unsafe condition and should be added to the existing AD. The actions specified by this AD are intended to prevent failure of a hose, resulting in failure of hydraulic pressure to the brakes on the affected landing gear wheel, and subsequent loss of control of the helicopter during a run-on landing.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2005/06/24/05-12418/airworthiness-directives-eurocopter-france-model-ec-155b-ec155b1-sa-365n-sa-365n1-as-365n2-and-as)
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