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Airworthiness Directive

AD 96-12-27 61 FR 31007 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-15383
Amendment
39-9668
Published
1996-06-19
Effective
1996-08-19
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/96-12-27 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

96-12-27

FR doc 96-15383 · 61 FR 31007

AD 96-12-27Published 1996-06-19Effective 1996-08-19

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 removal from service of suspect disks for a one-time inspection of the disk tenon area of the gas generator turbine disk.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to AlliedSignal Inc. (formerly Textron Lycoming) LTS 101 series turboshaft and LTP 101 series turboprop engines, that requires removal from service of suspect disks for a one-time inspection of the disk tenon area of the gas generator turbine disk. This amendment is prompted by a report of a gas generator turbine disk tenon failure. The actions specified by this AD are intended to prevent total loss of engine power, inflight engine shutdown, and possible damage to the aircraft.

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All Honeywell LTP101 directives

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Applies to 1 model in our index