Airworthiness Directives; Bell Helicopter Textron Model 212, 412, and 412EP Helicopters
airworthiness · Rule · Final rule; request for comments. · Published 2005-10-13 · Effective 2005-10-28 · 70 FR 59636
Document
Document number
05-20324
Federal Register citation
70 FR 59636
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2005-10-13
Effective date
2005-10-28
FAA docket
Docket No. FAA-2005-22634
Abstract
This amendment adopts a new airworthiness directive (AD) for the specified Bell Helicopter Textron (Bell) model helicopters modified with Aeronautical Accessories, Inc. (AAI), Supplemental Type Certificate (STC) SH2820SO or that have the affected AAI Parts Manufacturer Approval (PMA) parts installed. This action requires inspecting a certain part-numbered reservoir assembly adapter (adapter) for the counter bore depth (dimension D). If the dimension D of the adapter exceeds .860 inch, before further flight, this AD requires replacing the reservoir assembly and adapter with airworthy parts. This amendment is prompted by a report of a rupture of an adapter during nitrogen charging because of inadequate wall thickness for the operating pressures. The actions specified in this AD are intended to prevent the rupture of an adapter, uncontrolled jetting of pressurized gas from the nitrogen bottle, and subsequent injury to occupants or damage to the helicopter.