N330KW1976 S N I A S SA330J
This N-number isn't registered right now. Below is its last known registration, canceled Dec 6, 2019.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched10 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Ep Aviation LLC
- Owner type
- LLC
- City, state
- Wood Dale, IL
- Certificate issued
- Nov 25, 2019
- Canceled
- Dec 6, 2019
- Airworthiness
- Standard · Transport
- Airworthiness date
- Mar 5, 2003
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 dataAirframe
- Manufacturer
- S N I A S
- Model
- SA330J
- Year
- 1976
- Serial number
- 1418
- Aircraft type
- Rotorcraft
- Category
- Land
- Certification
- Type Certificated
- Seats
- 19
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Type certificate data sheet
- H4EU
- Mode S code
- A396C5
Engine
- Make and model
- Turbomeca Turmo Iv Ser
- Type
- Turbo-shaft
- Power
- 1170 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2019Ep Aviation LLCWood Dale, IL
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (0)
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.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (10)
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.
- Fuselage · reinforcement · crackedOct 5, 2018
CRACKS WERE DISCOVERED IN THE MGB ATTACH REINFORCEMENT AT FRAME 3855. THE MAXIMUM CRACK LENGTH IS APPROXIMATELY 3.0 INCHES IN THE VERTICAL LEG OF THE FITTING. REF SRM TABLE 11, FIGURE 17, ITEM 18 P/N 330A-22-9701-22. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRENTLY IN WORK. ONCE THE REPAIR IS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floorbeam · corrodedOct 1, 2018
WHILE PERFORMING A P2 INSPECTION, CORROSION WAS DISCOVERED ON THE FLOORBEAM END CAP IN TWO LOCATIONS AT FRAME 5295. THE CORROSION REMOVAL RESULTED IN A MAXIMUM MATERIAL LOSS IN THE PRIMARY STRUCTURE OF 0.035 INCHES IN DEPTH. TECHNICAL DATA PACKAGE PR2018023 WAS CREATED TO PROVIDE GUIDANCE FOR…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · bracket · corrodedJul 28, 2016
DURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Main rotor · bracket · corrodedJul 28, 2016
DURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · bracket · corrodedJul 28, 2016
DURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · bracket · corrodedJul 28, 2016
DURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · corrodedJun 18, 2016
DURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE MAIN FRAME OF STRUCTURE AT JACK SUPPORT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · corrodedJun 18, 2016
DURING AN AGING INSPECTION, AREAS OF CORROSION WERE FOUND ON THE LT DECK ANGLE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bracket · corrodedJun 18, 2016
DURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE UPPER ANGLE BRACKET.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · corrodedJun 18, 2016
DURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE UPPER ANGLE FORWARD AND REAR.
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