This N-number isn't registered right now. Below is its last known registration, canceled Jan 7, 2014.
Safety record in brief:1 NTSB accident (destroyed damage, May 2008)4 ADs may apply2 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
Loss of engine power during approach for landing due to a fatigue fracture of a power turbine blade.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for SEA08MA136)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2011-23-13 | Honeywell International Inc. Turboshaft Engines | Nov 29, 2011 | Engine (LTS101-600A-3)Only with: Power turbine governor (PTG) model AL-AB1, P/N 4-301-289-03, 4-301-289-05, 4-301-289-09, 4-301-101-16, or 4-301-101-18 installed, marked with compliance symbol N or P, or with no compliance symbol, on the PTG identification plate. |
| 2011-08-06 | Honeywell International Inc. LTS101 Series Turboshaft Engines and LTP101 Series… | May 17, 2011 | Engine (LTS101-600A-3)Only with: Power turbine rotor P/N 4-141-290-01, -02, -03, -05, -06, -11, -12, -13, -14, or -16 installed. |
| 2009-24-12 | Honeywell International Inc. LTS101 Series Turboshaft and LTP101 Series Turboprop Engines | Jan 4, 2010 | Engine (LTS101-600A-3)Only with: Engines with certain gas generator turbine discs, P/N 4-111-015-14, installed. |
| 2001-22-07 | Honeywell International, Inc. LTP 101 Series Turboprop and LTS101 Series Turboshaft… | Nov 30, 2001 | Engine (LTS101-600A-3)Only with: Rigid tube fuel manifolds P/N 4-301-042-02, -04, -05, -06, 4-301-236-01, -02, -03, -04, 4-301-286-01, -02, or 4-301-376-01 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
GEAR REJECTED AT INTERMOUNTAIN TURBINE FOR PITTING AND UNABLE TO ESTABLISH PROPER STATIC GEAR PATTERN REPLACED ASSY. WITH EXCHANGE
From FAA Service Difficulty Reports; matched by N-number and serial number.REJECTED BY NAMPA VALLEY HELICOPTERS DUE TO PITTING AND UNABLE TO ESTABLISH STATIC GEAR PATTERN REPLACED WITH EXCHANGE ASSY.
From FAA Service Difficulty Reports; matched by N-number and serial number.