Airworthiness Directives; Sicma Aero Seat; Third Occupant Seat Assemblies, 133 Series
airworthiness · Rule · Final rule. · Published 2006-12-15 · Effective 2007-01-19 · 71 FR 75411
Document
Document number
E6-21186
Federal Register citation
71 FR 75411
Type
Rule
Action
Final rule.
Category
airworthiness
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.