# Airworthiness Directives; Sicma Aero Seat; Third Occupant Seat Assemblies, 133 Series
> **Rule** · Final rule. · Published 2006-12-15 · Effective 2007-01-19 · 71 FR 75411
## Document
- **Document number:** E6-21186
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 71 FR 75411
- **Publication date:** 2006-12-15
- **Effective date:** 2007-01-19
- **FAA docket:** Docket No. FAA-2005-22959
## Abstract

The FAA is adopting a new airworthiness directive (AD) for Sicma Aero Seat third occupant seat assemblies, 133 series. This AD requires visually inspecting the installation of the two headrest bushings and installing Mecanindus pins to secure the bushings. This AD results from Sicma's determination that missing or incorrectly secured bushings could loosen and cause disengagement of the headrest from the seat during a high-energy stop of the airplane, possibly injuring the seat occupant. We are issuing this AD to prevent disengagement of the headrest from the seat during a high-energy stop of the airplane that could injure the seat occupant.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2006/12/15/E6-21186/airworthiness-directives-sicma-aero-seat-third-occupant-seat-assemblies-133-series)
---
*AI Analytics · CC0 1.0*