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Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, and 230 Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 2000-02-28 · Effective 2000-03-14 · 65 FR 10385

Document

Document number
00-4371
Federal Register citation
65 FR 10385
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2000-02-28
Effective date
2000-03-14
FAA docket
Docket No. 99-SW-77-AD

Abstract

This amendment adopts a new airworthiness directive (AD) applicable to Bell Helicopter Textron Canada (BHTC) Model 222, 222B, 222U, and 230 helicopters. This action requires inspecting the swashplate assembly drive pin (drive pin) for damage or looseness, torque testing to determine if the interference fit between the drive pin and rotating ring (ring) is adequate, and replacing any unairworthy drive pin. This amendment is prompted by an accident investigation that revealed fatigue failure of a drive pin. The actions specified in this AD are intended to prevent fatigue failure of a drive pin and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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