# Airworthiness Directives; Eurocopter France Model AS332C, L, L1, and L2 Helicopters
> **Rule** · Final rule. · Published 2003-12-01 · Effective 2004-01-05 · 68 FR 67018
## Document
- **Document number:** 03-29224
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 68 FR 67018
- **Publication date:** 2003-12-01
- **Effective date:** 2004-01-05
- **FAA docket:** Docket No. 2001-SW-07-AD
## Abstract

This amendment adopts a new airworthiness directive (AD) for the specified Eurocopter France (Eurocopter) model helicopters that requires inspecting the cockpit pedal unit (pedal unit) adjustment lever (lever) for a crack at specified time intervals by a dye- penetrant inspection and replacing any cracked lever with an airworthy lever before further flight. Modifying the pedal unit is also required and is a terminating action for the requirements of this AD. This amendment is prompted by cracks detected in the lever that creates an unsafe condition. The actions specified by this AD are intended to prevent failure of the lever, loss of access to the brake pedals on the ground or loss of yaw control in flight, and subsequent loss of control of the helicopter.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2003/12/01/03-29224/airworthiness-directives-eurocopter-france-model-as332c-l-l1-and-l2-helicopters)
---
*AI Analytics · CC0 1.0*