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Airworthiness Directives; Eurocopter France Model AS332L2

airworthiness · Rule · Final rule; request for comments. · Published 1999-05-11 · Effective 1999-05-26 · 64 FR 25198

Document

Document number
99-11781
Federal Register citation
64 FR 25198
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
1999-05-11
Effective date
1999-05-26
FAA docket
Docket No. 99-SW-09-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to AS332L2 helicopters. This action requires inspecting each main rotor head drag damper (damper) for a tear, crack, or bonding separation in the elastomer and, if necessary, replacing the damper with an airworthy damper. This amendment is prompted by a report of increased helicopter vibration in flight that was traced to the delamination of the elastomer on a damper. This condition, if not corrected, could result in failure of a damper and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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