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Airworthiness Directives; Honeywell International Inc. TPE331-3, -5, -6, -8, -10, and -11 Series Turboprop and TSE331-3 Series Turboshaft Engines

airworthiness · Rule · Final rule. · Published 2002-12-16 · Effective 2003-01-21 · 67 FR 76981

Document

Document number
02-31172
Federal Register citation
67 FR 76981
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2002-12-16
Effective date
2003-01-21
FAA docket
Docket No. 2001-NE-11-AD

Abstract

This amendment adopts a new airworthiness directive (AD), that is applicable to Honeywell International Inc. (formerly AlliedSignal Inc., Garrett Turbine Engine Company and AiResearch Manufacturing Company of Arizona) TPE331-3, -5, -6, -8, -10, and -11 series turboprop and TSE331-3 series turboshaft engines. This amendment requires removing weld repaired first stage compressor impellers from service. This amendment is prompted by an uncontained TPE331-11U turboprop engine failure and an in-flight shutdown due to the separation of the first stage Ti 6-4 compressor impeller. The actions specified by this AD are intended to prevent uncontained engine failures, in-flight shutdowns, and secondary damage.

Source

Authoritative
Federal Register document
Machine
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