N425AM2011 Eurocopter EC 130 B4
Safety record in brief:No NTSB accidents or incidents since 198213 ADs may apply9 service difficulty reports
Registration
FAA Aircraft Registry · Oct 19, 2026- Registered owner
- First-Citizens Bank & Trust Co
- Owner type
- Corporation
- City, state
- Morristown, NJ
- Certificate issued
- Jan 24, 2023
- Expires
- Jan 31, 2030
- Airworthiness
- Standard · Normal
- Airworthiness date
- Apr 16, 2012
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
- EC 130 B4
- Year
- 2011
- Serial number
- 7264
- Aircraft type
- Rotorcraft
- Category
- Land
- Certification
- Type Certificated
- Seats
- 6
- Engines
- 1
- Max takeoff weight
- 12,500 - 19,999 lb
- Type certificate data sheet
- H9EU
- Mode S code
- A50E3E
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- 2023 – nowFirst-Citizens Bank & Trust CoMorristown, NJ · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (13)
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 |
|---|---|---|---|
| 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. |
| 2012-18-18 | Turbomeca S.A. Turboshaft Engines | Oct 24, 2012 | Engine (ARRIEL 2B1)Only with: Engines not modified by TU166 modification. |
Show all 13 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2012-03-11 | Turbomeca S.A. Turboshaft Engines | Mar 20, 2012 | Engine (ARRIEL 2B1) |
| 2011-06-07 | Eurocopter France (Eurocopter) Model EC130 B4 Helicopters | Apr 6, 2011 | Airframe (EC 130 B4)Only with: Flotation gear unit "1G" (1G unit), P/N 350A63256300, installed. |
| 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 (9)
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.
- Air conditioning and pressurization · unknown · odorSep 10, 2024
DURING CLIMB OUT MED CREW ADVISED THEY DETECTED AN ELECTRICAL ODOR COMING FROM THE OXYGEN QTY DISPLAY PANEL, NO VISIBLE SMOKE OR HEAT DETECTED FROM PANEL. PERFORMED INSPECTION OF WIRES ON BACK PANEL, MGB COMPARTMENT AND ENGINE. PERFORMED GROUND RUN, NO DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Navigation · pitot tube · cloggedJun 17, 2023
G500 AIRSPEED INDICATION WAS LAGGING BEHIND PERCEIVED AIRSPEED ON CLIMB OUT FROM AIRPORT REPOSITIONING TO BASE. ONCE AT TRAFFIC PATTERN ALTITUDE, BEGAN TO TRY AND DIAGNOSE WHAT THE G500 AIRSPEED INDICATION WAS SHOWING. IT MAXED OUT AT 50KIAS AT WHAT I PERCEIVED TO BE CRUISE AIRSPEED, CRUISE POWER…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Air conditioning and pressurization · hose · unknownMay 8, 2023
AFTER TAKE OFF WITH AIR CONDITIONING FAN ON AND DEMIST 1 TURN OPEN COCKPIT HAD BURNING SMELL AND SMOKE HAZE. AIRCRAFT RETURNED TO DEPARTURE LOCATION WITHOUT INCIDENT. INSPECTED HEAT AND DEMIST DIFFUSERS FOR DEBRIS WITH NONE FOUND. HEAT AND DEMIST VALVES OPERATE NORMAL WITH NO LEAKS UNDER BELLY.…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 9 reportsShow fewer reports
- Fuselage · deck plate · elongatedJun 3, 2020
HAS AN ELONGATED HOLE ON THE RT SIDE OF THE TRANSMISSION DECK THAT IS UTILIZED IN THE AFT AC EVAPORATOR PN EC130-6204-2 INSTALLATION DWG EC130-622 AS THE MOST INBOARD AFT HOLE UTILIZING AN AN3-4A BOLT. AT THE HOLES WIDEST POINT IT MEASURES AT .35 BY .26. THE HOLE IS LOCATED APPROXIMATELY STA 3382…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · chafedMay 20, 2020
CHAFES TO THE AFT FUSELAGE AFT FRAME (PN: 350A21-1242.20). THE CHAFES ARE FOUND ON THE FREE EDGES OF THE INBOARD STIFFENING FLANGES ON THE LH AND RH SIDES OF THE FRAME. THE LH SIDE CHAFES WERE MEASURED TO BE 7MM X 12MM (0.276” X 0.472”) AND 0.014” DEEP; AND THE OTHER CHAFE MEASURED TO BE 3MM X 3MM…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bulkhead · crackedMay 13, 2020
CRACK DAMAGE WAS NOTED ON THE 22 DEGREE BULKHEAD WEB
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · doubler · crackedFeb 26, 2018
DURING A PREFLIGHT AIRWORTHINESS CHECK, FOUND CRACK IN THE UPPER AFT CORNER OF DOUBLER AROUND THE OPENING OF THE BATTERY COMPARTMENT IN THE TAILBOOM. CRACK MEASURED 1 3/8 INCHES IN LENGTH
From FAA Service Difficulty Reports; matched by N-number and serial number. - Tail rotor drive · mount · crackedOct 14, 2017
CRACK FOUND ON THE NR 1 TAIL ROTOR DRIVE SHAFT BEARING MOUNT BRACKET, FOUND DURING A SHCEDULED MAINTENANCE BEARING CHANGE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · search light · inoperativeJan 31, 2014
THE PILOT REPORTED THAT HE & THE MEDICAL CREW WERE ON CLIMB OUT JUST FOLLOWING A REFUEL OF THE ACFT WHEN THEY EXPERIENCED AN ELEC SMELL COME THROUGH THE CABIN. THE PILOT IMMEDIATELY PERFORMED AN EMERGENCY LANDING INTO A VACANT PARKING LOT. THE MECHANIC DID A THOROUGH INSPECTION OF THE ACFT TO…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026