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Airworthiness Directives; Honeywell International Inc. TPE331 Series Turboprop, and TSE331-3U Model Turboshaft Engines

airworthiness · Rule · Final rule. · Published 2006-07-05 · Effective 2006-08-09 · 71 FR 38054

Document

Document number
06-5929
Federal Register citation
71 FR 38054
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2006-07-05
Effective date
2006-08-09
FAA docket
Docket No. FAA-2006-23704

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Honeywell International Inc. TPE331 series turboprop, and TSE331-3U model turboshaft engines. This AD requires implementing a new flight cycle counting method for first, second, and third-stage turbine rotors used in aircraft that make multiple takeoffs and landings without an engine shutdown, and removing turbine rotors from service that have reached or exceeded their cycle life limits. This new flight cycle counting method requires determining total equivalent cycles accrued. This AD results from several reports of uncontained turbine rotor separation on engines used in special-use operations. We are issuing this AD to prevent uncontained failure of the turbine rotor due to low-cycle-fatigue (LCF), and damage to the aircraft.

Source

Authoritative
Federal Register document
Machine
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