Airworthiness Directives; Turbomeca Arriel 2B Series Turboshaft Engines
airworthiness · Rule · Final rule. · Published 2006-10-19 · Effective 2006-11-24 · 71 FR 61634
Document
Document number
E6-17326
Federal Register citation
71 FR 61634
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Turbomeca Arriel 2B Series Turboshaft
Publication date
2006-10-19
Effective date
2006-11-24
FAA docket
Docket No. FAA-2005-23809
Abstract
The FAA is adopting a new airworthiness directive (AD) for Turbomeca Arriel 2B, 2B1, and 2B1A turboshaft engines. This AD requires visually inspecting the splines of the high-pressure (HP) pump drive gear shaft and coupling shaft assembly for wear. This AD results from reports of uncommanded in-flight shutdowns of engines. We are issuing this AD to detect wear on the splines of the HP pump drive gear shaft and coupling shaft assembly, which could interrupt the fuel flow and cause an uncommanded in-flight shutdown of the engine on a single- engine helicopter. The in-flight shutdown of the engine could result in a forced autorotation landing or accident.