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Aircraft record

N300EV1975 Eurocopter SA 330J

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply7 service difficulty reports

Registration
Valid
expires Apr 30, 2030
Based in
Swainsboro, GA
owner city / state
Engine
TURMO IVC · 1495 hp
Turbomeca
Owners
1
since 2023
NTSB events
None
since 1982
ADs may apply
1
confirm with A&P
Service reports
7
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Aeroxs INC
Owner type
Corporation
City, state
Swainsboro, GA
Certificate issued
Apr 6, 2023
Expires
Apr 30, 2030
Airworthiness
Standard · Transport
Airworthiness date
Feb 18, 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
SA 330J
Year
1975
Serial number
1301
Aircraft type
Rotorcraft
Category
Land
Certification
Not Type Certificated
Seats
19
Engines
1
Max takeoff weight
12,500 - 19,999 lb
Mode S code
A31FCA

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. 2023 – nowAeroxs INCSwainsboro, GA · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

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

ADs published since 1998 that may apply (1)

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
99-07-07Eurocopter France Model SA 330J HelicoptersApr 12, 1999Airframe (SA 330J)Only with: Main rotor head sleeves P/N 330A31.1376.00 through .05 or 30A31.1376.12 through .17 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 (7)

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 · compressor · stalledFeb 27, 2016

    DURING THE LAST FLIGHT OF THE DAY, THE ACFT WAS DESCENDING WITH 7.5% PITCH. AS SOON AS PITCH WAS PULLED IN, NR 1 ENG WENT INTO COMPRESSOR STALL WITH A TEMP OF 780F. A LOWER PITCH SETTING OF 8% WAS SET & PULLED IN POWER WITH THE SAME RESULT. ENG FLIGHT IDLES MATCHED WITHIN 1%. ENG GND IDLES MATCHED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · fuel filter · cloggedMay 27, 2015

    DURING THE FIRST TAKEOFF FROM THE SHIP AS SOON AS THE ACFT CAME OFF THE DECK, THE RT LOW PRESS FILTER CLOGGED LIGHT ILLUMINATED AS THE HELICOPTER WAS TRANSITIONING TO A HOVER. WHILE IN A HOVER THE FILTER CLOGGED LIGHT FLICKERED ON & OFF, THE PILOTS REQUESTED PERMISSION TO LAND BACK ON THE SHIP.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · structure · corrodedMar 5, 2015

    DURING P4 AGEING INSPECTION, SIGNIFICANT CORROSION WAS FOUND ON EXTRUSION AT FRAME 2480 UNDER PILOTS SEATS IAW SRM 53-12 PG 13 FIG 7 ITEM 24.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reports
  • Fuselage · beam · corrodedMar 5, 2015

    DURING P4 AGEING INSPECTION, SIGNIFICANT CORROSION WAS FOUND BELOW MAIN GEARBOX LT BEAM A-38. IAW SRM 53-13 PG 77 & 78 ITEM 6.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · beam · corrodedMar 5, 2015

    DURING P4 AGEING INSPECTION, SIGNIFICANT CORROSION WAS FOUND ON LT & RT BEAMS AT THE HOOK WELL AREA IAW SRM 53-12 PG 35E FIG 18A ITEMS 21 & 22.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · angle · corrodedMar 5, 2015

    DURING P4 AGEING INSPECTION, SIGNIFICANT CORROSION WAS FOUND ON UPPER LT FUSELAGE ANGLE IAW 53-12 PG 32 & E3 FIG 17 ITEM 26.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · pump · seizedSep 11, 2014

    UPON LEAVING PORT AFTER AN EXTENDED PERIOD, 30 DAYS, WAS SCHEDULED FOR AN EXERCISE FLIGHT, AFTER LONG IN PORT PERIOD & PILOT TRAINING. ACFT HAD BEEN FLYING WITH NO ISSUES FOR APPROX 45 MINUTES WHEN PILOTS SCHEDULED FUEL TRANSFER. WHEN FUEL TRANSFER SWITCH WAS SELECTED THE CORRESPONDING CB POPPED.…

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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