Airworthiness Directive

AD 2001-22-07 66 FR 54119 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-26967
Amendment
39-12486
Published
2001-10-26
Effective
2001-11-30
Models covered
1
Last live check
2026-10-02
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AD

2001-22-07

FR doc 01-26967 · 66 FR 54119

AD 2001-22-07Published 2001-10-26Effective 2001-11-30

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 a new life limitation and removal of rigid tube fuel manifold assemblies and replacement with serviceable assemblies.

Full official abstract

This amendment adopts a new airworthiness directive (AD), that is applicable to certain Honeywell International, Inc. (formerly AlliedSignal, Inc. and Textron Lycoming) LTP 101 series turboprop and LTS101 series turboshaft engines. This amendment requires a new life limitation and removal of rigid tube fuel manifold assemblies and replacement with serviceable assemblies. This amendment is prompted by reports of cracking and fuel leakage of rigid tube fuel manifolds. The actions specified by this AD are intended to prevent engine fuel leakage due to low-cycle fatigue (LCF) cracking of the rigid tube fuel manifold, which could result in an in-flight fire.

More directives for Honeywell LTP101

  1. AD 2011-08-06 Airworthiness Directives; Honeywell International Inc. LTS101 Series Tur... 2011-04-12
  2. AD 2009-24-12 Airworthiness Directives; Honeywell International Inc. LTS101 Series Tur... 2009-11-30
  3. AD 2002-03-09 R1 Airworthiness Directives; Honeywell International Inc. (formerly AlliedS... 2002-03-21
  4. AD 2002-03-09 Airworthiness Directives; Honeywell International Inc. (Formerly AlliedS... 2002-02-20
  5. AD 2001-25-04 Airworthiness Directives; Honeywell International Inc. Models LTS101-600... 2001-12-19

All Honeywell LTP101 directives

Applies to 1 model in our index