N104LN2006 Eurocopter AS 350 B3
Safety record in brief:No NTSB accidents or incidents since 198217 ADs may apply5 service difficulty reports
Registration
FAA Aircraft Registry · Oct 18, 2026- Registered owner
- Pathfinder Leasing LLC
- Owner type
- LLC
- City, state
- Anchorage, AK
- Certificate issued
- Jul 5, 2024
- Expires
- Jul 31, 2031
- Airworthiness
- Standard · Normal
- Airworthiness date
- Jul 12, 2006
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Eurocopter
- Model
- AS 350 B3
- Year
- 2006
- Serial number
- 4094
- Aircraft type
- Rotorcraft
- Category
- Land
- Certification
- Type Certificated
- Seats
- 6
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Type certificate data sheet
- H9EU
- Mode S code
- A01497
Engine
- Make and model
- Turbomeca Arriel 2b1
- Type
- Turbo-shaft
- Power
- 747 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2024 – nowPathfinder Leasing LLCAnchorage, AK · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (17)
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. |
| 2016-25-13 | Safran Helicopter Engines, S.A. (Formerly Turbomeca S.A.) Turboshaft Engines | Feb 3, 2017 | Engine (ARRIEL 2B1)Only with: Engine accessory gearbox (AGB) P/N 0292120650 with a machined front casing installed. |
| 2015-13-04 | Turbomeca S.A. Turboshaft Engines | Sep 1, 2015 | Engine (ARRIEL 2B1) |
| 2014-12-05 | Turbomeca S.A. Turboshaft Engines | Aug 4, 2014 | Engine (ARRIEL 2B1) |
| 2014-07-06 | Turbomeca S.A. Turboshaft Engines | May 15, 2014 | Engine (ARRIEL 2B1)Only with: Engines that do not have modification TU157 incorporated. |
Show all 17 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 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). |
| 2012-18-18 | Turbomeca S.A. Turboshaft Engines | Oct 24, 2012 | Engine (ARRIEL 2B1)Only with: Engines not modified by TU166 modification. |
| 2012-03-11 | Turbomeca S.A. Turboshaft Engines | Mar 20, 2012 | Engine (ARRIEL 2B1) |
| 2009-09-03 | Turbomeca S.A. Arriel 2B and 2B1 Turboshaft Engines | Jun 1, 2009 | Engine (ARRIEL 2B1) |
| 2009-08-08 | Turbomeca Arriel 1B, 1D, 1D1, 2B, and 2B1 Turboshaft Engines | Apr 29, 2009 | Engine (ARRIEL 2B1)Serial numbers per Figure 1 of Turbomeca Alert MSB No. A292 72 0827, Version A (Arriel 1B/1D/1D1) and Figure 1 of Turbomeca Alert MSB No. A292 72 2833, Version A (Arriel 2B/2B1), both dated March 20, 2009. Only with: Engines with power turbine modules M04 installed, as listed by SN in the referenced service bulletins. |
| 2009-01-11 | Turbomeca Arriel 2B and 2B1 Turboshaft Engines | Feb 27, 2009 | Engine (ARRIEL 2B1) |
| 2007-19-09 | Turbomeca Arriel 2B1 Turboshaft Engines | Oct 3, 2007 | Engine (ARRIEL 2B1) |
| 2007-10-06 | Turbomeca Arriel 2B1 Turboshaft Engines | May 29, 2007 | Engine (ARRIEL 2B1) |
| 2005-25-13 | Turbomeca Arriel 2B and 2B1 Turboshaft Engines | Dec 28, 2005 | Engine (ARRIEL 2B1)Only with: Engines without modification TU22 incorporated. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (5)
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.
- Fuselage · deck plate · chafedApr 16, 2020
CHAFING ON THE MAIN GEAR BOX - DECK JUST FORWARD OF DRAIN HOLE. X 4240 , Z 1759, YL 80. THE DEPTH OF THE CHAFE IS 0.010” LENGTH OF 10MM AND WIDTH OF 10MM. THE CHAFE IS ONLY 10MM FWD OF DRAIN HOLE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · deck plate · chafedApr 15, 2020
THE TRANSMISSION DECK SKIN HAS CHAFING DAMAGE. THE CHAFE LOCATION IS LOCATED ON THE UPPER SIDE OF THE TRANSMISSION DECK SKIN
From FAA Service Difficulty Reports; matched by N-number and serial number. - Indicating and recording systems · light · failedDec 10, 2016
ENROUTE, CLOCK LIGHT BLINKED OFF AND ON THREE TIMES ACCOMPANIED BY LOUD STATIC IN HEADSET, THEN STAYED DARK. SMELLED STRONG ELECTRICAL ODOR. ABORTED FLIGHT AND DIVERTED. LANDED UNEVENTFULLY. MECHANIC ARRIVED AND DISCONNECTED WIRE TO CLOCK LIGHT,
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Rotor flight controls · pitch rod · leakingAug 3, 2012
TEFLON MATERIAL VISIBLE AND COMING OUT AROUND TOP AND BOTTOM CIRCUMFERENCE OF SPHERICAL BEARING OF TAIL ROTOR PITCH CHANGE LINK. DEFECT FOUND DURING ROUTINE AIRWORTHINESS CHECK. MANDATORY REPLACEMENT OF TAIL ROTOR PITCH CHANGE LINK BEFORE FURTHER FLIGHT IAW AD 2011.22.05, PARA (B).
From FAA Service Difficulty Reports; matched by N-number and serial number. - Electrical power · starter gen · disintegratedAug 12, 2008
GENERATOR LIGHT ILLUMINATED JUST AFTER TAKE OFF FOR AN NVG TRAINING FLIGHT, WITH AN ELECTRICAL BURNING/OZONE ODOR IN THE COCKPIT. THE PILOT RETURNED TO BASE AND LANDED WITHOUT FURTHER INCIDENT. ELECTRICAL ODOR DISPERSED BEFORE LANDING. UPON INSPECTION OF THE STARTER/GENERATOR, MAINTENANCE FOUND…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026