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Airworthiness Directives; Turbomeca Arriel 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2, 1K1, 1S, and 1S1 Turboshaft Engines

airworthiness · Rule · Final rule; request for comments. · Published 2009-12-28 · Effective 2010-01-12 · 74 FR 68510

Document

Document number
E9-29985
Federal Register citation
74 FR 68510
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2009-12-28
Effective date
2010-01-12
FAA docket
Docket No. FAA-2009-0544

Abstract

The FAA is superseding an existing airworthiness directive (AD) for Turbomeca Arriel 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2, 1K1, 1S, and 1S1 turboshaft engines. That AD currently requires initial and repetitive visual inspections of certain reduction gearboxes (module M05) for oil leakage, repair if leaking, and repair of all affected modules as optional terminating action to the repetitive inspections. This AD requires the same actions, but adds five more serial numbers of the reduction gearboxes (module M05) that are affected, and adds an alternative optional terminating action to the repetitive visual inspections. This AD results from Turbomeca identifying five additional reduction gearboxes (module M05) affected, and adding an alternative optional terminating action to the repetitive visual inspections. We are issuing this AD to prevent uncommanded in- flight engine shutdown, possible engine fire, and an emergency autorotation landing.

Source

Authoritative
Federal Register document
Machine
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