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Airworthiness Directives; Bell Helicopter Textron Inc. Model 205A-1, 205B, 212, 412, and 412CF Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 2000-12-13 · Effective 2000-12-28 · 65 FR 77780

Document

Document number
00-31317
Federal Register citation
65 FR 77780
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2000-12-13
Effective date
2000-12-28
FAA docket
Docket No. 2000-SW-49-AD

Abstract

This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron Inc. (BHTI) Model 205A-1, 205B, 212, 412, and 412CF helicopters. This action requires inspecting the locking washer on each main rotor actuator (actuator) for twisting or damage to the tab and replacing any locking washer that has a twisted or damaged tab. Replacing certain locking washers, regardless of condition, is also required within a specified time period. Installing a certain airworthy locking device on each actuator constitutes terminating action for the requirements of this AD. This amendment is prompted by an incident in which a damaged locking washer allowed the rod end to detach from the collective actuator, causing loss of collective control of the main rotor. The current locking washer is subject to mechanical damage and failure, which allows the actuator piston to unthread itself from its rod end. This condition, if not corrected, could cause loss of control of the main rotor and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
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