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Airworthiness Directive

AD 95-09-02 60 FR 20189 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires initial and repetitive inspections for wear of the engine fuel pump internal drive splines, and replacement of engine fuel pumps that exhibit wear beyond specified limits.

Superseded by AD 2001-17-15Federal Register (opens in a new tab)

FR document
95-10134
Published
1995-04-25
Effective
1995-05-10
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/95-09-02 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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AD

95-09-02

FR doc 95-10134 · 60 FR 20189

AD 95-09-02Published 1995-04-25Effective 1995-05-10

Superseded by 2001-17-15

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 initial and repetitive inspections for wear of the engine fuel pump internal drive splines, and replacement of engine fuel pumps that exhibit wear beyond specified limits.

Supersedes an earlier directive that is not in our index. See the official text.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to AlliedSignal Engines (formerly Textron Lycoming) LTS101 series turboshaft and LTP101 series turboprop engines. This action supersedes priority letter AD 94-19-01 that currently requires initial and repetitive inspections for wear of the engine fuel pump internal drive splines, and replacement of engine fuel pumps that exhibit wear beyond specified limits. This action clarifies the original requirements of the current AD by providing additional information to emphasize that the AD only applies to engines installed on single-engine aircraft and to emphasize that removed fuel pumps must be returned to the manufacturer for inspection. In addition, this action defines a serviceable part. This amendment is prompted by requests to clarify interpretations of the current priority letter AD. The actions specified by this AD are intended to prevent engine fuel pump failure, which can result in total engine power loss and possible loss of the aircraft.

More directives for Honeywell LTP101

  1. AD 2011-08-06 Airworthiness Directives; Honeywell International Inc. LTS101 Series Tur... Effective 2011-05-17
  2. AD 2009-24-12 Airworthiness Directives; Honeywell International Inc. LTS101 Series Tur... Effective 2010-01-04
  3. AD 2002-03-09 R1 Airworthiness Directives; Honeywell International Inc. (formerly AlliedS... Effective 2002-03-27
  4. AD 2002-03-09 Airworthiness Directives; Honeywell International Inc. (Formerly AlliedS... Effective 2002-03-27
  5. AD 2001-25-04 Airworthiness Directives; Honeywell International Inc. Models LTS101-600... Effective 2002-01-23

All Honeywell LTP101 directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 95-09-02 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index