Airworthiness Directives; Turbomeca Makila 1A and 1A1 Turboshaft Engines
airworthiness · Rule · Final rule. · Published 2008-04-16 · Effective 2008-05-21 · 73 FR 20525
Document
Document number
E8-8083
Federal Register citation
73 FR 20525
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Turbomeca Makila 1A and 1A1 Turboshaft
Publication date
2008-04-16
Effective date
2008-05-21
FAA docket
Docket No. FAA-2007-0157
Abstract
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.