airworthiness · Rule · Final rule. · Published 2009-06-29 · Effective 2009-08-03 · 74 FR 30917
Document
Document number
E9-15099
Federal Register citation
74 FR 30917
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Turbomeca S.A. Arrius 2F Turboshaft
Publication date
2009-06-29
Effective date
2009-08-03
FAA docket
Docket No. FAA-2005-22039
Abstract
The FAA is superseding an existing airworthiness directive (AD) for Turbomeca S.A. Arrius 2F turboshaft engines that have not incorporated Turbomeca Modification Tf75. That AD currently requires replacing the O-ring on the check valve piston in the lubrication unit at repetitive intervals. This AD requires the same repetitive replacements and would require incorporating Modification Tf75 as terminating action to the repetitive O-ring replacements. Modification Tf75 replaces the check valve piston with a piston design not requiring an O-ring. This AD results from the European Aviation Safety Agency (EASA) and Turbomeca S.A. mandating the incorporation of Modification Tf75. We are issuing this AD to prevent an uncommanded in-flight shutdown of the engine, which could result in a forced autorotation landing and damage to the helicopter.