# Airworthiness Directives; Eurocopter Deutschland GmbH Model EC135 Helicopters
> **Rule** · Final rule; request for comments. · Published 2009-05-28 · Effective 2009-06-12 · 74 FR 25394
## Document
- **Document number:** E9-12319
- **Category:** airworthiness
- **Manufacturer:** Eurocopter Deutschland GmbH Model EC135
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 74 FR 25394
- **Publication date:** 2009-05-28
- **Effective date:** 2009-06-12
- **FAA docket:** Docket No. FAA-2009-0482
## Abstract

We are adopting a new airworthiness directive (AD) for Eurocopter Deutschland GmbH (Eurocopter) Model EC135 helicopters. This AD results from a report of abnormal main rotor blade vibrations on a Eurocopter Model EC135 helicopter. This AD also results from mandatory continuing airworthiness information (MCAI) issued by the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community. The MCAI states that an operator reported unusual vibrations during the start phase of the main rotor blade on one helicopter. The vibrations stopped after the application of torque. Subsequent maintenance personnel found that six of the eight attachment screws of the lower hub-shaft bearing support were loose. This condition was discovered in two additional helicopters. Loose screws in the bearing support, if not detected and corrected, could result in abnormal main rotor blade vibrations and subsequent damage to the main transmission.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2009/05/28/E9-12319/airworthiness-directives-eurocopter-deutschland-gmbh-model-ec135-helicopters)
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