This N-number isn't registered right now. Below is its last known registration, canceled May 9, 2013.
Safety record in brief:1 NTSB accident (substantial damage, May 2006)8 ADs may apply4 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.
The pilot's loss of control for undetermined reasons.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DFW06LA118)
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 |
|---|---|---|---|
| 2015-10-07 | Turbomeca S.A. Turboshaft Engines | Jun 12, 2015 | Engine (ARRIUS 2F) |
| 2013-11-09 | Turbomeca S.A. Turboshaft Engines | Jul 5, 2013 | Engine (ARRIUS 2F) |
| 2012-07-09 | Turbomeca S.A. Turboshaft Engines | May 24, 2012 | Engine (ARRIUS 2F)Only with: Right-hand (RH) rear half-wall, P/N 0319 99 824 0, installed. |
| 2009-14-01 | Turbomeca S.A. Arrius 2F Turboshaft Engines | Aug 3, 2009 | Engine (ARRIUS 2F)Only with: Engines that have not incorporated modification Tf75. |
| 2008-13-27 | Turbomeca S.A. Arrius 2F Turboshaft Engines | Aug 6, 2008 | Engine (ARRIUS 2F)Only with: Engines that have not incorporated Turbomeca Modification Tf 12A. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2007-11-06 | Turbomeca Arrius 2F Turboshaft Engines | Jun 26, 2007 | Engine (ARRIUS 2F)Only with: Engines with fuel control units (FCUs) not incorporating modification Tf 55. |
| 2005-17-15 | Turbomeca Arrius 2F Turboshaft Engines | Sep 12, 2005 | Engine (ARRIUS 2F) |
| 2005-17-17 | Turbomeca S.A. Arrius 2F Turboshaft Engines | Sep 12, 2005 | Engine (ARRIUS 2F) |
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.
DURING PREFLIGHT FOUND 5 SEPARATED, DEBONDED AREAS ON WINDOWS AND A CRACK IN THE WINDSHIELD. INSPECTION BY MAINT REVEALED THE NR 8 TAIL ROTOR DRIVE SHAFT HAD FAILED. A WO WAS OPENED FOR REPAIR OF THIS AC. REMOVED AND REPLACED PILOTS WINDSHIELD. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.WEAR PLATE DEBONDED / REPLACED WITH NEW OR SERVICEABLE BY FIELD MAINTENANCE.
From FAA Service Difficulty Reports; matched by N-number and serial number.FOUND WEAR PLATE DEBONDED. ASSY. REPLACED BY FIELD MAINT.
From FAA Service Difficulty Reports; matched by N-number and serial number.FLIGHT CONTROL TEFLON BUSHINGS WORN. MFG HAS NO REPLACMENT PROCEDURE.
From FAA Service Difficulty Reports; matched by N-number and serial number.