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Airworthiness Directives; Turbomeca S.A. Arrius 2 B1, 2 B1A, 2 B1A 1, and 2 K1 Turboshaft Engines

airworthiness · Rule · Final rule. · Published 2003-09-17 · Effective 2003-10-22 · 68 FR 54327

Document

Document number
03-23673
Federal Register citation
68 FR 54327
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2003-09-17
Effective date
2003-10-22
FAA docket
Docket No. 2003-NE-05-AD

Abstract

The FAA is adopting a new airworthiness directive (AD) for Turbomeca S.A. Arrius 2 B1, 2 B1A, 2 B1A 1, and 2 K1 turboshaft engines. This AD requires replacement of the gas generator high pressure (HP) turbine disk before further flight after the engine has accumulated 5 minutes of operating time at the 2\1/2\ minute one engine inoperative (OEI) power rating. This amendment is prompted by a failure of an HP turbine blade during accelerated aging simulation tests performed by the manufacturer on an Arrius 2 B1A engine. We are issuing this AD to prevent engine failure of the only operating engine while experiencing an OEI condition.

Source

Authoritative
Federal Register document
Machine
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