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Aircraft record

N38MD1989 Eurocopter AS365N3

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 19829 ADs may apply4 service difficulty reports

Registration
Valid
expires Jul 31, 2027
Based in
Salt Lake City, UT
owner city / state
Engine
ARRIEL 2C · 779 hp
Turbomeca
Owners
1
since 2020
NTSB events
None
since 1982
ADs may apply
9
confirm with A&P
Service reports
4
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Bank Of Utah Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Jul 22, 2020
Expires
Jul 31, 2027
Airworthiness
Standard · Transport
Airworthiness date
Oct 24, 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
AS365N3
Year
1989
Serial number
6335
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
14
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Type certificate data sheet
H10EU
Mode S code
A45A08

Engine

Make and model
Turbomeca Arriel 2c
Type
Turbo-shaft
Power
779 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. 2020 – nowBank Of Utah TrusteeSalt Lake City, UT · 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 (9)

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
2021-13-08Fuel Control/ Turbine EnginesAug 19, 2021Engine (ARRIEL 2C)
2021-13-19Airbus HelicoptersAug 17, 2021Airframe (AS365N3)Only with: Except helicopters with Eurocopter MOD 53C17 or MOD 53D02, or Airbus Helicopters MOD 07 53D21 or MOD 07 53D22, installed.
2021-05-08Engine BMEP/ Torque IndicatingApr 15, 2021Engine (ARRIEL 2C)
2016-25-13Safran Helicopter Engines, S.A. (Formerly Turbomeca S.A.) Turboshaft EnginesFeb 3, 2017Engine (ARRIEL 2C)Only with: Engine accessory gearbox (AGB) P/N 0292120650 with a machined front casing installed.
2016-03-02Turbomeca S.A. Turboshaft EnginesMar 15, 2016Engine (ARRIEL 2C)Only with: Engines with modification TU34 or TU34A installed.
Show all 9 ADs
ADSubjectEffectiveApplies to
2015-13-04Turbomeca S.A. Turboshaft EnginesSep 1, 2015Engine (ARRIEL 2C)
2014-12-05Turbomeca S.A. Turboshaft EnginesAug 4, 2014Engine (ARRIEL 2C)
2013-08-17Eurocopter France HelicoptersJun 5, 2013Airframe (AS365N3)
2010-23-02Eurocopter France (Eurocopter) Model SA-365N, SA-365N1, AS-365N2, and AS 365 N3…Nov 22, 2010Airframe (AS365N3)Only with: Horizontal stabilizer P/N 365A13-3030-1901, -1902, -1903, -1904, -1905, -1906, -1908, -1909; 365A13-3036-00, -0001, -0002, -0003; or 365A13-3038-00 installed.

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

Service Difficulty Reports (4)

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 drive · lockwasher · misinstalledSep 21, 2011

    INCORRECT APPLICATION OF LOCKING WASHERS ON ROTOR SHAFT NUT RETAINER LOCK (117-12118-01). INCORRECT APPLICATION OCCURRED DURING INSTALLATION OF REPLACEMENT ROTOR SHAFT. DISCOVERED WHILE PERFORMING MAIN GEARBOX LOWER CASING REPAIR. (REMOVAL OF ROTOR SHAFT REQUIRED). SECURITY OF ROTOR SHAFT RETAINER…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Tail rotor drive · bearing · failedSep 13, 2011

    FAILURE OF INPUT PINION TAPERED ROLLER BEARING OF TAIL ROTOR GEARBOX. FAILURE OCCURRED DURING GROUND RUN AFTER MX. REPLACEMENT OF TAIL ROTOR GEARBOX. TAIL ROTOR GEARBOX INPUT CASING DISCOLORED DUE TO OVERHEATING OF FAILED BEARING. INPUT PINION SEIZED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · valve · leaksOct 19, 1997

    DRAIN VALVE LEAKS AT SEAMS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reports
  • Engine oil · transmitter · defectiveDec 15, 1995

    OIL PRESSURE TRANSMITTER FLUCTUATING AND PEGGING AT 5 BARS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Related aircraft

Show all 8 related aircraft
All 12 registered Eurocopter AS365N3 aircraft

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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