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Airworthiness Directives; Rolls-Royce Limited, Aero Division-Bristol, S.N.E.C.M.A. Olympus 593 Mk. 610-14-28 Turbofan Engines

airworthiness · Rule · Final rule; request for comments. · Published 2001-07-10 · Effective 2001-08-09 · 66 FR 35896

Document

Document number
01-16926
Federal Register citation
66 FR 35896
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2001-07-10
Effective date
2001-08-09
FAA docket
Docket No. 2000-NE-07-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to Rolls-Royce Limited, Aero Division-Bristol, S.N.E.C.M.A. (RR) Olympus 593 Mk. 610-14-28 turbofan engines. This action requires replacement of the low-oil pressure (LOP) switch. This amendment is prompted by a report of the failure of the low pressure (LP) and high pressure (HP) rotor thrust bearings due to oil starvation that was caused by the loss of the LOP switch function and resulted in a delayed engine shutdown. The actions specified in this AD are intended to prevent the failure of the LOP switch to indicate an LOP event, which could contribute to uncontained engine failure due to oil starvation in the thrust bearings.

Source

Authoritative
Federal Register document
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