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AD FAA-2008-0071

Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, 230, and 430 Helicopters

Summary

This amendment supersedes an existing airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) helicopters, that currently requires certain checks and inspections of the tail rotor blades. If a crack is found, the existing AD requires replacing the tail rotor blade (blade) with an airworthy blade before further flight. This amendment requires the same checks and inspections of the blades until they are required to be replaced and removes certain serial numbered and specifically coded blades from the applicability of the AD. This amendment is prompted by the approved rework of certain blades and two newly redesigned blades, which, if installed, constitute terminating action for the inspection requirements. The actions specified by this AD are intended to detect a crack in a blade, and to prevent loss of a blade and subsequent loss of control of the helicopter.

Directive Details

AD Number

FAA-2008-0071

Document Number

2010-11071

Type

Rule

Publication Date

June 11, 2010

Effective Date

July 16, 2010

Affected Manufacturer

Bell Helicopter Textron Canada Model 222, 222B, 222U, 230, and 430

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2008-0071

Topics

Air transportationAircraftAviation safetySafety

Official Documents

View all ADs for Bell Helicopter Textron Canada Model 222, 222B, 222U, 230, and 430 →

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