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Airworthiness Directives; Eurocopter France Model EC130 B4 Helicopters

airworthiness · Rule · Final rule. · Published 2008-03-24 · Effective 2008-04-28 · 73 FR 15395

Document

Document number
E8-5494
Federal Register citation
73 FR 15395
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Eurocopter France Model EC130 B4
Publication date
2008-03-24
Effective date
2008-04-28
FAA docket
Docket No. FAA-2007-28229

Abstract

This amendment adopts a new airworthiness directive (AD) for the specified Eurocopter France (Eurocopter) Model EC 130 B4 helicopters, with certain twist grip assemblies installed, that requires inspecting the pilot and co-pilot collective levers for proper bonding between the twist grip drive tubes and the control pinions and if debonding is present, replacing the collective levers before further flight. This amendment is prompted by one incident in which the engine remained at idle speed although the twist grip had been turned to the flight position. The actions specified by this AD are intended to detect debonding between the twist grip drive tubes and the control pinions on the pilot and co-pilot collective levers to prevent loss of cockpit throttle control of the engine, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
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