2002-03-09 R1
FR doc 02-6502 · 67 FR 13089AD 2002-03-09 R1Published 2002-03-21Effective 2002-03-27
Requires a one-time visual inspection for surface finish and a one-time fluorescent penetrant inspection for cracks of certain impellers installed on LTS101 series turboshaft and LTP101 series turboprop engines.
Full official abstract
This amendment revises an existing airworthiness directive (AD), that is applicable to Honeywell International Inc. (formerly AlliedSignal Inc. and Textron Lycoming) LTS101 series turboshaft and LTP101 series turboprop engines. The existing AD will become effective on March 27, 2002, and requires a one-time visual inspection for surface finish and a one-time fluorescent penetrant inspection for cracks of certain impellers installed on LTS101 series turboshaft and LTP101 series turboprop engines. This amendment requires the same inspections, and in addition, allows installation of impellers that pass those inspections. This revision to the existing AD is prompted by an inadvertent omission in the existing AD to include allowance of installation of impellers that pass inspections required by the AD. The actions specified by this AD are intended to prevent impeller failure from cracks in the impeller back face area, which could result in an uncontained engine failure.
More directives for Honeywell LTP101
- AD 2011-08-06 Airworthiness Directives; Honeywell International Inc. LTS101 Series Tur... Effective 2011-05-17
- AD 2009-24-12 Airworthiness Directives; Honeywell International Inc. LTS101 Series Tur... Effective 2010-01-04
- AD 2002-03-09 Airworthiness Directives; Honeywell International Inc. (Formerly AlliedS... Effective 2002-03-27
- AD 2001-25-04 Airworthiness Directives; Honeywell International Inc. Models LTS101-600... Effective 2002-01-23
- AD 2001-22-07 Airworthiness Directives; Honeywell International, Inc. LTP 101 Series T... Effective 2001-11-30
