← FAA Federal Register actions

Airworthiness Directives; Eurocopter France Model EC130 B4 Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 2006-06-12 · Effective 2006-07-27 · 71 FR 33598

Document

Document number
06-5241
Federal Register citation
71 FR 33598
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Eurocopter France Model EC130 B4
Publication date
2006-06-12
Effective date
2006-07-27
FAA docket
Docket No. FAA-2006-24807

Abstract

This amendment adopts a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model EC130 B4 helicopters. This action requires inspecting the throttle twist grip (twist grip) assembly for any foreign body (chip or debris), any rotating micro-switch, and any micro-switch roller that does not move freely. If any unairworthy condition is found, this action requires that it be corrected before further flight. This amendment is prompted by two reports of a twist grip assembly jamming in the "IDLE" position. The actions specified in this AD are intended to detect and prevent jamming of the twist grip assembly, which, if present, could keep the engine from operating above idle speed and result in subsequent loss of control of the engine power of the helicopter.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown