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AD FAA-2016-6990

Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

Summary

We are adopting a new airworthiness directive (AD) for certain Turbomeca S.A. Arriel 1, 1A, 1A1, 1A2, 1B, 1B2, 1C, 1C1, 1C2, 1D, 1D1, 1E, 1E2, 1K1, 1S, and 1S1 turboshaft engines. This AD requires removing the centrifugal impeller and replacing with a part eligible for installation. This AD was prompted by an anomaly that occurred during the grinding operation required by modification TU376, which increases the clearance between the rear curvic coupling of the centrifugal impeller and the fuel injection manifold. We are issuing this AD to prevent failure of the centrifugal impeller, uncontained centrifugal impeller release, damage to the engine, and damage to the helicopter.

Directive Details

AD Number

FAA-2016-6990

Document Number

2016-26184

Type

Rule

Publication Date

November 1, 2016

Effective Date

December 6, 2016

Affected Manufacturer

Turbomeca S.A. Turboshaft

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2016-6990

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

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