Safety record in brief:1 NTSB accident (substantial damage, Apr 2000)8 ADs may apply
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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.
Failure of the manufacturer to ensure proper quality control of the ignition solenoid housing chamfer area, which allowed for insufficient clamping forces between the ignition solenoid housing and T-fitting, and the eventual separation of the T-fitting, loss of fuel, and loss of engine power.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX00LA167)
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.