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Aircraft record

N378HS2009 Eurocopter EC120B

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jan 21, 2022.

Safety record in brief:No NTSB accidents or incidents since 19828 ADs may apply3 service difficulty reports

Registration
Deregistered
Last based in
Grand Prairie, TX
owner city / state
Engine
ARRIUS 2F · 432 hp
Turbomeca
Owners
1
on record
NTSB events
None
since 1982
ADs may apply
8
confirm with A&P
Service reports
3
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Airbus Helicopters INC
Owner type
Non Citizen Corporation
City, state
Grand Prairie, TX
Canceled
Jan 21, 2022
Airworthiness
Standard · Normal
Airworthiness date
Jan 22, 2009

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 data

Airframe

Manufacturer
Eurocopter
Model
EC120B
Year
2009
Serial number
1566
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
5
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
R0001RD
Mode S code
A45243

Engine

Make and model
Turbomeca Arrius 2f
Type
Turbo-shaft
Power
432 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. until 2022Airbus Helicopters INCGrand Prairie, TX

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (8)

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.

ADSubjectEffectiveApplies to
2015-10-07Turbomeca S.A. Turboshaft EnginesJun 12, 2015Engine (ARRIUS 2F)
2013-11-09Turbomeca S.A. Turboshaft EnginesJul 5, 2013Engine (ARRIUS 2F)
2012-07-09Turbomeca S.A. Turboshaft EnginesMay 24, 2012Engine (ARRIUS 2F)Only with: Right-hand (RH) rear half-wall, P/N 0319 99 824 0, installed.
2009-14-01Turbomeca S.A. Arrius 2F Turboshaft EnginesAug 3, 2009Engine (ARRIUS 2F)Only with: Engines that have not incorporated modification Tf75.
2008-13-27Turbomeca S.A. Arrius 2F Turboshaft EnginesAug 6, 2008Engine (ARRIUS 2F)Only with: Engines that have not incorporated Turbomeca Modification Tf 12A.
Show all 8 ADs
ADSubjectEffectiveApplies to
2007-11-06Turbomeca Arrius 2F Turboshaft EnginesJun 26, 2007Engine (ARRIUS 2F)Only with: Engines with fuel control units (FCUs) not incorporating modification Tf 55.
2005-17-15Turbomeca Arrius 2F Turboshaft EnginesSep 12, 2005Engine (ARRIUS 2F)
2005-17-17Turbomeca S.A. Arrius 2F Turboshaft EnginesSep 12, 2005Engine (ARRIUS 2F)

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (3)

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.

  • Main rotor · scissor link · debondedOct 28, 2013

    SCISSOR LINK FIXED BUSHING DISBONDED FROM SCISSOR LINK, INNER ROTATING, SLIP BUSHING SEIZED IN OUTER STATIONARY BUSHING.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · chafedMay 3, 2011

    DURING THE INSTALLATION OF THE TAILBOOM THAT HAD BEEN REPAIRED FOR CRACKING IN THE LT FWD VOR ANTENNA MOUNT THE MECHANIC NOTED CHAFING ALONG THE BOTTOM OF THE INNER TAILBOOM SKIN UNDER THE WIRE HARNESSES. IN SOME CASES IT HAD PENETRATED THE COMPOSITE MATERIAL AND INTO THE HONEYCOMB. MFG ISSUED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedMar 14, 2011

    DURING THE QC FINAL INSP PHASE OF A 100 HR INSP THE INSPECTOR NOTED A CRACK EXTENDING LONGITUDINALLY FWD AND AFT FROM THE LT FWD NAV/VOR ANTENNA MOUNT. PHOTO`S AND INFOR SENT TO MFG FOR DETERMINATION. MFG SUGGEST REMOVAL AND REPAIR BY MFG. BELIEVE PART TO BE WEAK IN THISE MOUNTING AREAS AND…

    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

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