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AD FAA-2013-0575

Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

Summary

We are adopting a new airworthiness directive (AD) for all Turbomeca S.A. ASTAZOU XIV B and XIV H engines. This AD was prompted by reports of cracks on the 2nd-stage turbine disk. This AD requires replacement of the 2nd-stage turbine disk. We are issuing this AD to prevent disk cracking, uncontained 2nd-stage turbine blade release, damage to the engine, and damage to the helicopter.

Directive Details

AD Number

FAA-2013-0575

Document Number

2014-00166

Type

Rule

Publication Date

January 10, 2014

Effective Date

February 14, 2014

Affected Manufacturer

Turbomeca S.A. Turboshaft

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2013-0575

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

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AD FAA-2013-0575 — Airworthiness Directives; Turbomeca S.A. Turboshaft Engines