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AD FAA-2008-0490

Airworthiness Directives; Bell Helicopter Textron Model 204B, 205A, 205A-1, 205B, 210, 212, 412, 412CF, and 412EP Helicopters

Summary

This amendment adopts a new airworthiness directive (AD) for the specified Bell Helicopter Textron (Bell) model helicopters. This action requires certain checks and inspections of each tail rotor blade assembly (T/R blade) at specified intervals and repairing or replacing, as applicable, any unairworthy T/R blade. This amendment is prompted by three failures of a T/R blade occurring during flight and a recent incident of a cracked T/R blade discovered during a scheduled visual inspection. The actions specified in this AD are intended to detect damage to a T/R blade that could lead to cracking of a T/R blade and subsequent loss of control of the helicopter.

Directive Details

AD Number

FAA-2008-0490

Document Number

E8-9790

Type

Rule

Publication Date

May 6, 2008

Effective Date

May 21, 2008

Affected Manufacturer

Bell Helicopter Textron Model 204B, 205A, 205A-1, 205B, 210, 212, 412, 412CF, and 412EP

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2008-0490

Topics

Air transportationAircraftAviation safetySafety

Official Documents

View all ADs for Bell Helicopter Textron Model 204B, 205A, 205A-1, 205B, 210, 212, 412, 412CF, and 412EP →

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