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importantRule

AD FAA-2008-0101

Airworthiness Directives; Eurocopter Deutschland GmbH Model EC135 Helicopters

Summary

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.

Directive Details

AD Number

FAA-2008-0101

Document Number

E8-1702

Type

Rule

Publication Date

February 1, 2008

Effective Date

February 19, 2008

Affected Manufacturer

Eurocopter Deutschland GmbH Model EC135

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2008-0101

Topics

Air transportationAircraftAviation safetySafety

Official Documents

View all ADs for Eurocopter Deutschland GmbH Model EC135 →

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