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Airworthiness Directives; Eurocopter France Model SA-365N1, AS- 365N2, and SA-366G1 Helicopters

airworthiness · Rule · Final rule. · Published 1998-05-07 · Effective 1998-06-11 · 63 FR 25158

Document

Document number
98-12114
Federal Register citation
63 FR 25158
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1998-05-07
Effective date
1998-06-11
FAA docket
Docket No. 97-SW-49-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to Eurocopter France (Eurocopter) Model SA-365N1, AS-365N2, and SA-366G1 helicopters, that requires initial and repetitive inspections of the tail rotor blade Kevlar tie-bar (Kevlar tie-bar) for cracks or delaminations. This amendment is prompted by a report of delamination of a Kevlar tie-bar. The actions specified by this AD are intended to detect cracks that could lead to delamination of the Kevlar tie-bar, loss of tail rotor control, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
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