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Airworthiness Directives; Eurocopter France Model AS-350B, B1, B2, B3, BA, and D Helicopters, and Model AS 355E, F, F1, F2 and N Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 1999-04-23 · Effective 1999-05-10 · 64 FR 19881

Document

Document number
99-10053
Federal Register citation
64 FR 19881
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
1999-04-23
Effective date
1999-05-10
FAA docket
Docket No. 98-SW-44-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to Eurocopter France Model AS-350B, B1, B2, B3, BA, and D helicopters, and Model AS 355E, F, F1, F2 and N helicopters. This action requires inspecting the tail rotor spider plate bearing (bearing) for the proper bearing rotational torque, axial play, and for any brinelling of the bearing. This amendment is prompted by service difficulty reports citing the need to prematurely replace bearings due to wear, and by two in-flight incidents of increased tail rotor vibration levels due to bearing wear. This condition, if not corrected, could result in seizure of the bearing, loss of tail rotor control and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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