N38662005 Eurocopter AS 350 B3
This N-number isn't registered right now. Below is its last known registration, canceled May 11, 2021.
Safety record in brief:No NTSB accidents or incidents since 198217 ADs may apply5 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Individual owner
- City, state
- Boulder City, NV
- Canceled
- May 11, 2021
- Airworthiness
- Standard · Normal
- Airworthiness date
- Mar 7, 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
- 2005
- Serial number
- 4012
- 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
- A474BE
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- 1980Individual ownerChicago, IL · different airframe: Turner Tweety Bird S/N 222-9
- until 2021Individual ownerBoulder City, NV
- until 1940Individual ownerdifferent airframe: Waco Gxe S/N 977-A
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 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 · support frame · chafedFeb 10, 2016
THE TRANSMISSION SUPPORT FRAME, PN 350A21-1041-143 HAS CHAFING DAMAGE ON THE LOWER FLANGE, FROM AN UNSECURED CABLE, PN 704A34-1302-23. PN 350A38-1040-20 ATTACHES TO PN 350A21-1041-143.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · fire detector · intermittentNov 4, 2014
INTERMITTENT FIRE LIGHT ON FINAL APPROACH. PILOT REPORTED THAT AS HE WAS LANDING THE FIRE LIGHT WOULD FLICKER. AT NO TIME DID THE LIGHT COME ON & STAY ON.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · line · leakingMar 18, 2013
PILOT FOUND HYD HOSE LEAKING ON LANDING, REPLACED HYD HOSE. LEAK CHECKED GOOD. AFTER 1+44 HR FLIGHT ON 03/18/2013 FOUND FLUID ON NEW HOSE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Main rotor · sensor · defectiveJul 23, 2011
PILOT REPORTED A LOSS OF NR INDICATION DURING FLIGHT. PILOT ELECTED TO MAKE A PRECAUTINARY LANDING. TECH WAS DISPATCHED BUT DUE TO THE LOCATION AND SECURITY OF THE ACFT, ELECTED TO HAVE THE ACFT TRANSPORTED TO THE MX FACILITY FOR FURTHER TROUBLESHOOTING. THE TECH REMOVED THE NR SENSOR AND VERIFIED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine controls · potentiometer · out of adjustApr 30, 2011
AMBER GOV LIGHT WAS DETECTED PRIOR TO ACFT LANDING AT BASE. TECH DOWNLOADED VEMD FAIL CODE OF 120 FOR YAW POTENTIOMETER. FOUND YAW POTENTIOMETER SEETINGS ON THE HIGH SIDE OF 53.5 PERCENT. ADJUSTED POTENTIOMETER TO 52.5, AND PERFORMED OPS CHECKS WITH NO DEFECTS NOTED. ALL WORK WAS PERFORMED IAW…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026