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Airworthiness Directives; Eurocopter France Model SA-366G1 Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 1998-03-20 · Effective 1998-04-06 · 63 FR 13514

Document

Document number
98-7248
Federal Register citation
63 FR 13514
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Eurocopter France Model SA-366G1
Publication date
1998-03-20
Effective date
1998-04-06
FAA docket
Docket No. 97-SW-31-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to Eurocopter France Model SA-366G1 helicopters. This action requires initial and repetitive inspections of the tail rotor blade Kevlar tie-bar (Kevlar tie-bar) for delaminations. This amendment is prompted by a report of delamination of a Kevlar tie-bar. The actions specified in this AD are intended to detect delaminations of the Kevlar tie-bar, that could result in loss of anti-torque function and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
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