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Airworthiness Directives; Eurocopter France Model AS-350B, B1, B2, BA, C, D, D1, and AS 355E, F, F1, F2, and N Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 1998-12-02 · Effective 1998-12-17 · 63 FR 66418

Document

Document number
98-31858
Federal Register citation
63 FR 66418
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
1998-12-02
Effective date
1998-12-17
FAA docket
Docket No. 98-SW-41-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to Eurocopter France Model AS-350B, B1, B2, BA, C, D, D1, and AS 355E, F, F1, F2, and N helicopters. This action requires measuring the tail rotor pitch change control rod (control rod) outboard spherical bearing for radial and axial play. If the play exceeds 0.008-inch, replacing the control rod with an airworthy control rod is required. This amendment is prompted by one accident and one incident. Investigations revealed a broken control rod on the helicopter involved in the accident and a severely worn control rod on the helicopter involved in the incident. This condition, if not corrected, could result in separation of the outboard spherical bearing ball from its outer race, rubbing of the body of the control rod against the tail rotor blade pitch horn clevis, failure of the control rod, and loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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