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Aircraft record

N277SD2000 Eurocopter EC120B

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

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

Registration
Valid
expires Apr 30, 2029
Based in
Mather, CA
owner city / state
Engine
ARRIUS 2F · 432 hp
Turbomeca
Owners
1
since 2002
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
Registered owner
Sacramento County Sheriffs Office
Owner type
Government
City, state
Mather, CA
Certificate issued
Jan 22, 2002
Expires
Apr 30, 2029
Airworthiness
Experimental · Research and Development
Airworthiness date
Sep 7, 2001

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
2000
Serial number
1134
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
A2C211

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. 2002 – nowSacramento County Sheriffs OfficeMather, CA · current

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.

  • Engine oil · line · mismanufacturedJan 1, 2004

    DURING ROUTINE MAINTENANCE, OIL LINE B-NUT WAS LOOSENED, IT WAS NOTED THAT LINE MOVED AWAY FROM MATING CONNECTOR APPROX .2500 INCH. A SPRING SCALE WAS USED TO PULL THE LINE BACK INTO PLACE, IT REQUIRED 45 LBS OF FORCE TO DO SO. THE MFG WAS CONTACTED, PRINT OF PART WAS OBTAINED AND PART WAS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · control panel · failedJan 17, 2002

    SX 16 NIGHTSUN QUIT OPERATING. FOUND RELAY PANEL INOPERATIVE. REPLACE RELAY ASSEMBLY. PROBABLE CAUSE: RELAY INTERNAL FAILURE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · control panel · inoperativeJan 17, 2002

    SX16 NIGHTSUN QUIT OPERATING. FOUND RELAY PANEL INOPERATIVE, REPLACE RELAY ASSEMBLY. PROBABLE CAUSE: RELAY INTERNAL FAILURE.

    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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