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N330KW

Cancelled 2019
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Deregistered aircraft · 1976 S N I A S SA330J · Turbomeca TURMO IV series

Open in FAA registry

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Cancelled
December 6, 2019
Exported to
Romania
Status when cancelled
Valid registration
Serial number
1418
Year built
1976
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, transport
Airworthiness date
March 5, 2003
Certificate issued
November 25, 2019
Last registry action
November 25, 2019
Mode S code
A396C5
Owner when cancelled
Ep Aviation LLC
Location
Wood Dale, IL
Owner type
LLC
Airframe modelS N I A S SA330JTCDS H4EU · ADs, bulletins and aircraft registered nowEngine modelTurbomeca TURMO IV seriesTCDS E10EU · Turbo-shaft

From the FAA registry file of October 31, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

NTSB investigations · 1

Matched to this aircraft by N330KW and the event date: up to this one’s cancellation.

NTSB SEA07LA068Accident · No injuriesLimited investigationFinal reportLakeview, ORThe dual student's failure to extend the landing gear during a simulated single-engine forced landing, and the flight instructor's failure to take remedial action to keep the aircraft from touching the runway surface without the landing gear extended.Feb 28, 2007 · Substantial damage

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N330KW and the event date: up to this one’s cancellation.

Accident 20070228002709APractice Training Manuevers · Lakeview, OR(-23) On 2-28-07 pilot examiner, [privacy data omitted] was giving training and instructional flights to 2 other pilots in N330KW, a SA-330-J puma (with a retractable landing gear) helicopter for single engine emergency landings, when he failed to extend the…Feb 28, 2007 · Minor damage

Service difficulty reports · 10

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 39LA201810085176Reinforcement · crackedCRACKS 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 CUROct 5, 2018 · N330KW · Snias SA330J · Fuselage Main, FrameSDR 39LA201810051175Floorbeam · corrodedWHILE 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 WAOct 1, 2018 · N330KW · Snias SA330J · Fuselage Main, Floor BeamSDR 39LA20160728164Bracket · corrodedDURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.Jul 28, 2016 · N330KW · Snias SA330J · Main Rotor BladesSDR 39LA20160728163Bracket · corrodedDURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.Jul 28, 2016 · N330KW · Snias SA330J · Main Rotor BladesSDR 39LA20160728162Bracket · corrodedDURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.Jul 28, 2016 · N330KW · Snias SA330J · Main Rotor BladesSDR 39LA20160728161Bracket · corrodedDURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.Jul 28, 2016 · N330KW · Snias SA330J · Main Rotor BladesSDR 39LA20160618160Angle · corrodedDURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE UPPER ANGLE FORWARD AND REAR.Jun 18, 2016 · N330KW · Snias SA330J · Fuselage Miscellaneous StructureSDR 39LA20160618159Bracket · corrodedDURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE UPPER ANGLE BRACKET.Jun 18, 2016 · N330KW · Snias SA330J · Fuselage Miscellaneous StructureSDR 39LA20160618158Angle · corrodedDURING AN AGING INSPECTION, AREAS OF CORROSION WERE FOUND ON THE LT DECK ANGLE.Jun 18, 2016 · N330KW · Snias SA330J · Fuselage Miscellaneous StructureSDR 39LA20160618157Angle · corrodedDURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE MAIN FRAME OF STRUCTURE AT JACK SUPPORT.Jun 18, 2016 · N330KW · Snias SA330J · Fuselage Miscellaneous Structure