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Airworthiness Directives; Eurocopter France Model EC120 Helicopters

airworthiness · Rule · Final rule. · Published 2005-05-09 · Effective 2005-06-13 · 70 FR 24304

Document

Document number
05-8951
Federal Register citation
70 FR 24304
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Eurocopter France Model EC120
Publication date
2005-05-09
Effective date
2005-06-13
FAA docket
Docket No. FAA-2005-20289

Abstract

This amendment adopts a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model EC120 helicopters that requires inspecting the tail rotor drive shaft (drive shaft) damper half-clamps (half-clamps) to determine if they are centered on the friction ring, and if not correctly positioned, centering the half-clamps on the friction ring. This amendment is prompted by the discovery of half- clamps that were incorrectly positioned. The actions specified by this AD are intended to detect incorrect positioning of the drive shaft half-clamps, and to prevent interference of the half-clamps with the drive shaft, which could result in scoring on the drive shaft, failure of the drive shaft, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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