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Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal Inc. and Garrett Turbine Engine Co.) TFE731-2 and -3 Series Turbofan Engines

airworthiness · Rule · Final rule. · Published 2005-06-22 · Effective 2005-07-27 · 70 FR 35992

Document

Document number
05-12080
Federal Register citation
70 FR 35992
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Honeywell International Inc. (Formerly AlliedSignal Inc. and Garrett Turbine
Publication date
2005-06-22
Effective date
2005-07-27
FAA docket
Docket No. FAA-2004-18496

Abstract

The FAA is adopting a new airworthiness directive (AD) for Honeywell International Inc. (formerly AlliedSignal Inc. and Garrett Turbine Engine Co.) TFE731-2 and -3 series turbofan engines with certain part numbers (P/Ns) and serial numbers (SNs) of low pressure (LP) 1st and 2nd stage turbine rotor discs initially installed. This AD requires replacement of those LP 1st and 2nd stage turbine rotor discs. This AD results from a report of an uncontained failure of an LP 2nd stage turbine rotor disc that resulted in an in-flight engine shutdown. We are issuing this AD to prevent LP turbine rotor disk separation, which could result in an uncontained engine failure and damage to the airplane.

Source

Authoritative
Federal Register document
Machine
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