# Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal Inc. and Garrett Turbine Engine Co.) TFE731-2 and -3 Series Turbofan Engines
> **Rule** · Final rule. · Published 2005-06-22 · Effective 2005-07-27 · 70 FR 35992
## Document
- **Document number:** 05-12080
- **Category:** airworthiness
- **Manufacturer:** Honeywell International Inc. (Formerly AlliedSignal Inc. and Garrett Turbine
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 70 FR 35992
- **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
- [Federal Register document](https://www.federalregister.gov/documents/2005/06/22/05-12080/airworthiness-directives-honeywell-international-inc-formerly-alliedsignal-inc-and-garrett-turbine)
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