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AD FAA-2016-2701

Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

Summary

We are adopting a new airworthiness directive (AD) for certain Turbomeca S.A. Makila 2A and 2A1 turboshaft engines. This AD requires tightening the nut attaching the swivel union to the engine power turbine module M04. This AD was prompted by two occurrences of commanded in-flight shutdown following low oil pressure warning. We are issuing this AD to prevent loosening of the nut and oil leakage from the low-pressure oil system, which could lead to in-flight shutdown of the engine and forced landing.

Directive Details

AD Number

FAA-2016-2701

Document Number

2016-06372

Type

Rule

Publication Date

March 22, 2016

Effective Date

April 6, 2016

Affected Manufacturer

Turbomeca S.A. Turboshaft

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2016-2701

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

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AD FAA-2016-2701 — Airworthiness Directives; Turbomeca S.A. Turboshaft Engines