Airworthiness Directive

AD 2001-17-15 66 FR 44945 Active

Federal Aviation Administration · 14 CFR part 39

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

FR document
01-21220
Amendment
39-12406
Published
2001-08-27
Effective
2001-10-01
Models covered
1

Last live check: 2026-08-19

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AD

2001-17-15

FR doc 01-21220 · 66 FR 44945

AD 2001-17-15Published 2001-08-27Effective 2001-10-01

Supersedes 95-09-02

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

Full official abstract

This amendment supersedes an existing airworthiness directive (AD), AD 95-09-02, that applies to Honeywell International Inc. (formerly AlliedSignal Inc. and Textron Lycoming Inc.) LTS101 series turboshaft and LTP101 series turboprop engines. That AD superseded priority letter AD 94-19-01 and currently requires initial and repetitive inspections of the engine fuel pump internal drive splines for wear and replacement of engine fuel pumps that exhibit wear beyond specified limits.This amendment requires a reduction in inspection intervals for the engine fuel pump internal drive splines. This amendment is prompted by a report from the engine manufacturer that 13 percent of the pumps installed on aircraft that were returned from the field for the required 900-hour interval inspection revealed excessive internal drive spline wear. The actions specified by this AD are intended to prevent worn splines in fuel pumps which could cause 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

Applies to 1 model in our index