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Aircraft record

N339EV1974 Eurocopter France SA330J

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:1 NTSB accident (substantial damage, Jan 2018)24 ADs may apply2 service difficulty reports

Registration
Valid
expires May 31, 2031
Based in
Cedar City, UT
owner city / state
Engine
TURMO IVC · 1495 hp
Turbomeca
Owners
1
since 2024
NTSB events
1
substantial, 2018
ADs may apply
24
confirm with A&P
Service reports
2
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Southern Utah University
Owner type
Government
City, state
Cedar City, UT
Certificate issued
May 9, 2024
Expires
May 31, 2031
Airworthiness
Standard · Transport
Airworthiness date
Jan 20, 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 data

Airframe

Manufacturer
Eurocopter France
Model
SA330J
Year
1974
Serial number
1285
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
19
Engines
1
Max takeoff weight
12,500 - 19,999 lb
Type certificate data sheet
H4EU
Mode S code
A3B7B6

Engine

Make and model
Turbomeca Turmo Ivc
Type
Turbo-shaft
Power
1495 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. 2024 – nowSouthern Utah UniversityCedar City, UT · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

Jan 26, 2018 · Pacific Ocean

The worn rear bearing of the freewheel unit. Contributing to the accident was the delay in analyzing an oil sample, which would have detected the increase in metal contaminants from the worn bearing.

Damage
Substantial
Injuries
None
Report
ANC18LA020

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC18LA020)

ADs published since 1998 that may apply (24)

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
2021-09-14Airbus Helicopters (Type Certificate Previously Held by Eurocopter France) HelicoptersJun 22, 2021Airframe (SA330J)Only with: MGB oil cooling fan rotor shaft bearings (rear and front) P/N 704A33651114 (MP/N 205FFTX74K6-G33) or P/N 704A33651268 (MP/N 594918) installed.
2020-19-02Airbus HelicoptersOct 7, 2020Airframe (SA330J)Only with: Tail rotor blade P/N 330A12-0005-(all dash numbers) or 330A12-0006-(all dash numbers) installed.
2020-16-09Airbus Helicopters (Type Certificate Previously Held by Eurocopter France) HelicoptersSep 10, 2020Airframe (SA330J)Only with: MGB input flexible coupling flange assembly P/N 330A-32937401 installed and modified per MOD 0752416 and MOD 0752419, excluding assemblies inspected per Working Card 65.32.601 since new or MGB overhaul, or installed on an MGB overhauled after April 1, 2015 and not replaced since.
2014-05-11Airbus Helicopters (Type Certificate Previously Held by Eurocopter France) (Airbus…Apr 15, 2014Airframe (SA330J)Only with: Tail rotor control turnbuckle P/N 330A27-5031-20 installed.
2014-05-15Airbus Helicopters (Type Certificate Previously Held by Eurocopter France) (Airbus…Apr 15, 2014Airframe (SA330J)Only with: Hoist beam P/N 330A87-2345-00, -01, -02, -03, -04, -05, or -06 installed with a single or double hoist plate (AS332 models) or a single hoist plate (SA330J).
Show all 24 ADs
ADSubjectEffectiveApplies to
2012-18-08Eurocopter France HelicoptersOct 24, 2012Airframe (SA330J)
2010-23-23Eurocopter France (ECF) Model SA330F, G, and J; and AS332C, L, L1, and L2 HelicoptersDec 22, 2010Airframe (SA330J)
2009-22-10Eurocopter France (ECF) Model AS332C, AS332L, AS332L1, AS332L2, SA330F, SA330G, and…Dec 29, 2009Airframe (SA330J)Only with: Main rotor blade de-icing system distributor retaining clamp P/N 225000-18454 or P/N D18454 installed.
2003-14-12Eurocopter France Model SA330F, G, and J; AS332C, L, and L1; SA341G; SA342J; AS350B, BA…Aug 25, 2003Airframe (SA330J)
2002-25-01Eurocopter France Model AS332C, AS332L, AS332L1, SA330F, SA330G, and SA330J HelicoptersJan 22, 2003Airframe (SA330J)Only with: Tail rotor pitch change rod and bearing, part number 330A33-9903-20, installed.
2002-20-03Eurocopter France Model AS332C, L, L1, and L2; AS350B, BA, B1, B2, B3, and D; AS355E, F…Nov 6, 2002Airframe (SA330J)Only with: Metal ferry fuel tank P/N 330A 871310.00, .01, .02, .03, or .04 installed (AS332, AS350, AS355, AS365, SA330, SA360, SA365 models), or tank P/N 3160S 7375020 or 3160S 7375020-1 installed (SA.316B/C, SA.319B).
2002-18-05Eurocopter France Model SA330F, SA330G, SA330J, AS332C, AS332L, and AS332L1 HelicoptersOct 21, 2002Airframe (SA330J)Only with: Tail rotor blade de-icing rotating collector P/N APCL 110-265-201 installed.
2002-18-06Eurocopter France Model AS332C, L, L1, and Model SA330F, G, and J HelicoptersOct 21, 2002Airframe (SA330J)Only with: Tail rotor gearbox P/N 332A33-0001, 330A33-0000, or 330A33-0011 (all dash numbers, AS332 models) or P/N 330A33-9109 (all dash numbers, SA330 models) installed.
2002-15-08Eurocopter France Model EC120B, EC 155B, SA330F, SA330G, SA330J, AS332C, AS332L…Sep 6, 2002Airframe (SA330J)Only with: SIREN load release unit (cargo hook) P/N AS21-5-1 through AS21-5-7 with cargo hook serial number less than 415 installed.
2002-12-14Eurocopter France Model SA330F, G, J, and AS332C, L, and L1 HelicoptersJul 8, 2002Airframe (SA330J)Only with: Multi-Purpose Air Intake (MPAI) installed; SA330J not modified by MOD 0723672 (SB 30.16) or MOD 0725920 (SB 30.17); AS332C, L, L1 not modified by MOD 0725885 (SB 30.00.44) or MOD 0725974 and MOD 0725998 (SB 30.00.46).
2000-10-05Eurocopter France Model SE.3160, SA.316B, SA.316C, SA.319B, SA330F, SA330G, SA330J…Jun 29, 2000Airframe (SA330J)Only with: Emergency flotation gear nitrogen cylinder P/N ARZ 74921 with inflation head P/N 74929 that has no S/N or S/N lower than 12000, or has union nut P/N 75441 or 75834 installed.
2000-06-05Eurocopter France Model SA330F, SA330G, SA330J, AS332C, AS332L, AS332L1, and AS332L2Apr 10, 2000Airframe (SA330J)
99-07-07Eurocopter France Model SA 330J HelicoptersApr 12, 1999Airframe (SA330J)Only with: Main rotor head sleeves P/N 330A31.1376.00 through .05 or 30A31.1376.12 through .17 installed.
99-07-02Eurocopter France Model AS 332C, L, L1, and L2 Helicopters and Model SA 330F, G, and J…Apr 7, 1999Airframe (SA330J)Only with: For SA 330F, G, and J only: main rotor blades P/N 330A11-0020, 330A11-0022, or 330A11-0027 (all dash numbers) installed.
98-23-09Eurocopter France Model SA 330F, G, and J HelicoptersDec 15, 1998Airframe (SA330J)Only with: Tail rotor head assembly P/N 330 A 33 0000 (all dash numbers) or 330 A 33 0001 (all dash numbers) installed.
98-23-03Eurocopter France Model SA 330F, G, and J HelicoptersDec 10, 1998Airframe (SA330J)Only with: Tail rotor electrical bonding braids P/N 332A031.1276.00 installed, not modified in accordance with AMS 332A07-66-003 or AMS 33207-66-072.
98-13-40Eurocopter France Model SA 330F, G, and J HelicoptersJul 31, 1998Airframe (SA330J)
98-12-16Eurocopter France Model SA 330F, G, and J HelicoptersJul 14, 1998Airframe (SA330J)
98-08-13Eurocopter France Model SA 330F, G, and J, and AS 332C, L, L1, and L2 HelicoptersApr 27, 1998Airframe (SA330J)Only with: Tail rotor head pitch change spider arm P/N 330A330104.20 or .21, or 332A330039.20 or .21 installed (SA 330 models); P/N 332A330039.20 or .21 installed (AS 332 models).

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

Service Difficulty Reports (2)

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.

  • Equipment and furnishings · hook · brokenMar 29, 2018

    WHILE FLYING, THE PILOTS FELT A BUMP IN THE AIRCRAFT AND LOOKED DOWN USING THE CARGO MIRRORS TO SEE THE LOAD IMPACT THE WATER. INSPECTION OF THE HOOK SYSTEM WAS DONE AND WAS FOUND TO BE BROKEN, INTERNAL STEEL CABLE STILL INTACT, ALLOWING FOR THE HOOK TO BE MANUALLY ACTUATED AND OPENING THE HOOK AS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Tail rotor drive · drive shaft · shearedJan 26, 2018

    AFTER THE FLIGHT HAD BEEN COMPLETED AND THE AIRCRAFT WAS BACK ON THE SHIP AND CHOCKED AND CHAINED THE CREW PROCEEDED TO PERFORM THE FRESH WATER RINSE OF THE ENGINES. WITH THE #2 ENGINE AT FLIGHT IDLE AND THE #1 ENGINE AT GROUND IDLE THE FOR THE ENGINE RINSE THE PILOTS HEARD WHAT THEY THOUGHT WAS A…

    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

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