# Proposed AD FAA-2010-0891: Eurocopter France Models SA330F, SA330G, and SA330J Helicopters

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2011-03-02
- Products: Eurocopter France
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: September 13, 2010, 75 FR 55492
- Comments due: October 28, 2010
- Became: [AD 2011-03-02](https://openairdocs.org/ad/2011-03-02)
- Docket: FAA-2010-0891 (https://www.regulations.gov/docket/FAA-2010-0891, where comments are filed)
- Project: 2009-SW-055-AD
- FR document: 2010-22775
- Official PDF: https://openairdocs.org/files/sha256/27/6a/276a787bfd0c472cb801fd72fbda37130c6b4a2d3379f913431ddf984cf1a263 (from https://www.govinfo.gov/content/pkg/FR-2010-09-13/pdf/2010-22775.pdf)
- Federal Register: https://www.federalregister.gov/documents/2010/09/13/2010-22775/airworthiness-directives-eurocopter-france-models-sa330f-sa330g-and-sa330j-helicopters
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5BB9ACA4669BE41C862579C300707CA0.0001
- Page: https://openairdocs.org/proposed/FAA-2010-0891

## Summary

We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

While adjusting the position of the pedal unit on a SA 330 helicopter, the copilot set the position beyond the end limit (``tall pilot'' position). This resulted in the separation of the pedal adjustment system and the pedals rocking forward. After investigation, it was determined that the Loctite bond on the ``tall pilot'' stop nut was damaged, most likely due to aging of the adhesive. The nut came loose and could no longer perform its stop function. The threaded rod of the adjustment system separated from the system. The separation of the adjustment system, if not corrected, could result in the loss of control of the pedal units, causing the helicopter to begin rotating.

The proposed AD would require actions that are intended to address the unsafe condition described in the MCAI.

## Notices in this docket

- Sep 13, 2010: Notice of proposed rulemaking (NPRM). (first notice), FR document 2010-22775, comments due Oct 28, 2010 (https://www.federalregister.gov/documents/2010/09/13/2010-22775/airworthiness-directives-eurocopter-france-models-sa330f-sa330g-and-sa330j-helicopters)

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