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Airworthiness Directives; Turbomeca Arriel 1B, 1D, 1D1, and 1S1 Turboshaft Engines

airworthiness · Rule · Final rule; request for comments. · Published 2006-01-24 · Effective 2006-02-28 · 71 FR 3754

Document

Document number
06-522
Federal Register citation
71 FR 3754
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2006-01-24
Effective date
2006-02-28
FAA docket
Docket No. FAA-2005-21242

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Turbomeca Arriel 1B, 1D, 1D1, and 1S1 turboshaft engines. This AD requires initial and repetitive position checks of the gas generator 2nd stage turbine blades on all Turbomeca Arriel 1B, 1D, 1D1, and 1S1 turboshaft engines, and initial and repetitive replacements of 2nd stage turbines on 1B, 1D, and 1D1 engines only. This AD results from reports of the release of gas generator 2nd stage turbine blades while in service, with full containment of debris. We are issuing this AD to prevent inflight engine shutdown and subsequent forced autorotation landing or accident.

Source

Authoritative
Federal Register document
Machine
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