This N-number isn't registered right now. Below is its last known registration, canceled May 6, 2013.
Safety record in brief:1 NTSB accident (substantial damage, Sep 2011)8 ADs may apply
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.
Upslope wind conditions while the helicopter was operating at ground idle, which resulted in the helicopter rollover. Contributing to the accident was the lack of manufacturer data regarding the effect of upslope wind conditions on helicopter ground idle operations.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC11LA108)
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 |
|---|---|---|---|
| 2013-23-09 | Eurocopter France Helicopters | Dec 27, 2013 | Airframe (AS 350 BA)Only with: Helicopters with sliding doors installed, except those with modification AL.4262. |
| 2013-21-01 | Eurocopter France (Eurocopter) Helicopters | Oct 25, 2013 | Airframe (AS 350 BA)Only with: Tail rotor hub pitch horn assembly P/N 350A121368.01, .02, .03, or .04, with pitch horn P/N 350A121368.XX, installed. |
| 2013-08-19 | Eurocopter France Helicopters | Jun 5, 2013 | Airframe (AS 350 BA)Only with: Sliding door pre-modification (MOD) 073298 or pre-MOD 073308 installed. |
| 2011-23-13 | Honeywell International Inc. Turboshaft Engines | Nov 29, 2011 | Engine (LTS101-600A3A)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 (LTS101-600A3A)Only with: Power turbine rotor P/N 4-141-290-01, -02, -03, -05, -06, -11, -12, -13, -14, or -16 installed. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2010-11-51 | Eurocopter France (Eurocopter) Model AS350B, BA, B1, B2, C, D, and D1 Helicopters and… | Sep 2, 2010 | Airframe (AS 350 BA)Only with: Tail gearbox control lever P/N 350A33-1058-00, -01, -02, or -03 not marked with an "X" near the P/N installed. |
| 2009-24-12 | Honeywell International Inc. LTS101 Series Turboshaft and LTP101 Series Turboprop Engines | Jan 4, 2010 | Engine (LTS101-600A3A)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 (LTS101-600A3A)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.
No Service Difficulty Reports found for this airframe since 1995.