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Airworthiness Directives; Turbomeca S.A. Arrius 2 B1, 2 B1A, 2 B1A-1, and 2 B2 Turboshaft Engines

airworthiness · Rule · Final rule; request for comments. · Published 2005-06-14 · Effective 2005-06-29 · 70 FR 34334

Document

Document number
05-11611
Federal Register citation
70 FR 34334
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2005-06-14
Effective date
2005-06-29
FAA docket
Docket No. FAA-2005-21443

Abstract

The FAA is adopting a new airworthiness directive (AD) for Turbomeca S.A. Arrius 2 B1, 2 B1A, 2 B1A-1, and 2 B2 turboshaft engines. This AD requires replacing the software in the Engine Electronic Control Unit (EECU). This AD results from a report of simultaneous loss of automatic control of both engines of a Eurocopter Deutschland EC 135 helicopter, during flight. We are issuing this AD to prevent simultaneous loss of automatic control of both engines and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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