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Emergency ADRule

AD FAA-2007-0157

Airworthiness Directives; Turbomeca Makila 1A and 1A1 Turboshaft Engines

Summary

The FAA is superseding an existing airworthiness directive (AD) for Turbomeca Makila 1A, 1A1, and 1A2 turboshaft engines. That AD currently requires replacing certain digital electronic control units (DECUs) and electronic control units (ECUs) with modified DECUs and ECUs. This AD applies only to Makila 1A and 1A1 turboshaft engines, and requires replacing the selector-comparator board in the ECU with a board incorporating Turbomeca modification TU 250. This AD results from recent unexplained reversions of the ECU to the 65% N1 back-up mode. We are issuing this AD to prevent dual-engine continued operation at 65% N1 after reversion of the ECU to the 65% N1 back-up mode due to temporary loss of N2 speed signal, which could lead to inability to continue safe flight, emergency autorotation landing, or an accident.

Directive Details

AD Number

FAA-2007-0157

Document Number

E8-8083

Type

Rule

Publication Date

April 16, 2008

Effective Date

May 21, 2008

Affected Manufacturer

Turbomeca Makila 1A and 1A1 Turboshaft

Criticality

critical

Emergency

Yes

Docket ID

Docket No. FAA-2007-0157

Topics

Air transportationAircraftAviation safetySafety

Official Documents

View all ADs for Turbomeca Makila 1A and 1A1 Turboshaft →

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