Airworthiness Directive

AD 98-04-15 63 FR 9732 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-3798
Amendment
39-10327
Published
1998-02-26
Effective
1998-04-27
Models covered
1
Last live check
2026-10-01
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AD

98-04-15

FR doc 98-3798 · 63 FR 9732

AD 98-04-15Published 1998-02-26Effective 1998-04-27

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires replacement or radiographic inspection, and replacement, if necessary, of certain third stage turbine stators with serviceable parts.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to AlliedSignal Inc., (formerly Garrett Engine Division, Garrett Turbine Engine Company and AiResearch Manufacturing Company of Arizona) TPE331 series turboprop and TSE331 turboshaft engines, that requires replacement or radiographic inspection, and replacement, if necessary, of certain third stage turbine stators with serviceable parts. This amendment is prompted by a report of an outer band weld that cracked subsequent to a radiographic inspection required by a previous AD. The actions specified by this AD are intended to prevent third stage turbine wheel separation due to thermal fatigue cracking and shifting of the third stage turbine stator, which could contact the third stage turbine wheel and result in an uncontained engine failure and damage to the aircraft.

More directives for Honeywell TPE331

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  5. AD 2016-21-07 Airworthiness Directives; Honeywell International Inc. Turboprop Engines 2016-10-24

All Honeywell TPE331 directives

Applies to 1 model in our index