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Airworthiness Directives; Eurocopter Deutschland GmbH Model EC135 Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 2008-02-01 · Effective 2008-02-19 · 73 FR 6008

Document

Document number
E8-1702
Federal Register citation
73 FR 6008
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Eurocopter Deutschland GmbH Model EC135
Publication date
2008-02-01
Effective date
2008-02-19
FAA docket
Docket No. FAA-2008-0101

Abstract

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 2007-26-51, which was sent previously to all known U.S. owners and operators of Eurocopter Deutschland GmbH (Eurocopter) Model EC135 helicopters by individual letters. This AD requires, within 5 hours time-in-service (TIS), inspecting the tail rotor control rod (control rod) and adjoining ball pivot and replacing any unairworthy parts before further flight. This amendment is prompted by a report of a fatal accident involving the failure of a control rod. The actions specified by this AD are intended to prevent failure of a control rod and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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