Safety record in brief:1 NTSB accident (substantial damage, Nov 2003)5 ADs may apply
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The malfunction of the rotor drive system due to improper maintenance, which resulted in the uncoupling of the drive shaft during takeoff-initial climb. A factor associated with the accident is the undertorqued drive system bolts.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for LAX04TA052)
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 |
|---|---|---|---|
| 2021-04-15 | Vertical Stabilizer, Spar/Rib | Mar 23, 2021 | Airframe (AS 350 B3)Only with: AS350B3 helicopters excluded if Modification 07.3148 embodied in production or Eurocopter AS350 Service Bulletin 55.00.14 (any revision) embodied in service; AS355 models all serial numbers. |
| 2013-23-09 | Eurocopter France Helicopters | Dec 27, 2013 | Airframe (AS 350 B3)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 B3)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 B3)Only with: Sliding door pre-modification (MOD) 073298 or pre-MOD 073308 installed. |
| 2012-25-04 | Eurocopter France Helicopters | May 9, 2013 | Airframe (AS 350 B3)Only with: Modification (MOD) 07 5601 installed (AS350B3e configuration). |
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.