Safety record in brief:1 NTSB accident (substantial damage, Jun 2016)8 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.
The pilot's decision to exit the helicopter with the engine and rotors turning and the selection of unsuitable terrain for a landing, which resulted in a roll over.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for GAA16CA318)
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.
FIXED BUSHING FROM SCISSOR LINK DISBONDED & SEIZED ON REMOVABLE CARBIDE BUSHING.
From FAA Service Difficulty Reports; matched by N-number and serial number.ENGINE CHIP LIGHT IN CRUISE FLIGHT. INSPECTED BOTH MAGNETIC PLUGS FOR FOREIGN MATERIAL, NONE WAS NOTED. INSPECTED AND TESTED MAGNETIC PLUG HEADS IAW 79-38-00-750-801, INSPECTION AND OPS CHECKS WERE GOOD. REMOVED AND REPLACED ENGINE OIL AND RETURN FILTER IAW 79-24-05-901-801-A01. OPS AND LEAK…
From FAA Service Difficulty Reports; matched by N-number and serial number.