WESTWIND HELICOPTERS, INC.

Part 135 operator · designator IAVA

Data confidence: Records are linked by certificate number, aircraft registration, or a name match that a reviewer has confirmed. Each record below shows how it was linked.

Also recorded as: WESTWIND HELICOPTERS, INC., Westwind Helicopters, Westwind Helicopters, Inc.

Accident & enforcement record

Events that happened, regardless of the operator's own reporting. Each links to its public source.

NTSB accidents & incidents

Acc · 2022-10-26 Operator named in NTSB report
BELL 407 (N34BM) Fatal injury Part 135

Operated by Westwind Helicopters INC (per NTSB report)

Source: NTSB case CEN23FA019
Acc · 2017-02-27 Operator named in NTSB report
BELL 407 (N1371) Fatal injury Part 91

Operated by Westwind Helicopters (per NTSB report)

Source: NTSB case CEN17FA112
Inc · 2014-05-30 Operator named in NTSB report
BELL 407 (N1197) None injury Part 135

Operated by Westwind Helicopters (per NTSB report)

Source: NTSB case CEN14IA270

FAA enforcement actions

FAA enforcement records haven't been loaded into GroundCheck yet, so none can be shown — a gap in our data, not evidence of a clean enforcement history.

Maintenance disclosure history

Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal.

10 reports on file.

K · 2021-09-19 Matched by certificate designator
N91WH · ATA 6320

AFTER DEPARTING KPTN ABOUT 15 MINUTES OUT TRANSMISSION LOW PRESSURE LIGHT ILLUMINATED AND TRANSMISSION OIL PRESSURE WAS READING LOW AND ERRATIC. TRANSMISSION OIL TEMPERATURE WAS READING HIGH. PILOT LANDED IN A FIELD. UPON SHUTTING DOWN THERE WAS OIL ON THE SIDE OF AIRCRAFT. MAINTENANCE WAS FLOWN TO THE LOCATION AND DETERMINED THAT THE FREEWHEELING UNIT AFT SUPPORT SEAL HAD MIGRATED PARTIALLY OUT OF THE SEAL BOSS AND WAS LEAKING. AFT SUPPORT ASSEMBLY WAS REPLACED AND TRANSMISSION SERVICEABILITY CHECK PERFORMED WITH NO DEFECTS NOTED.

Source: SDR IAVA91WH91921 · FAA SDRS
O · 2020-07-31 Matched by certificate designator
N34BM · ATA 6510

DURING 100 HOUR LUBRICATION OF TAIL ROTOR DRIVE SHAFT SPLINES THE #3 TAIL ROTOR DRIVE SHAFT WAS FOUND CRACKED AT ONE ATTACHMENT EAR. TOTAL TIME OF PART IS UNKNOW AS IT IS AN ON CONDITION PART.

Source: SDR IAVA202008040001 · FAA SDRS
O · 2019-10-16 Matched by certificate designator
N170AM · ATA 5302

CRACK ON UPPER TAIL BOOM SKIN AT STATION 172 FROM 3RD RIVET FORWARD OF CASTING ON SKIN SPLICE SEAM TO 4TH RIVET AT TAIL ROTOR GEARBOX CASTING ATTACHMENT RIVET LINE.

Source: SDR IAVA2019101600001 · FAA SDRS
O · 2019-07-29 Matched by certificate designator
N177AL · ATA 5320

DURING POST FLIGHT INSPECTION FOUND CRACK IN ROOF. LEFT AFT CORNER FROM RIVET HOLE WHERE ROOF ATTACHES TO ROLL OVER BULKHEAD. CRACK WAS VERIFIED BY DYE PENETRANT. DURING REMOVAL OF ROOF FOUND CORROSION ON RIGHT HAND AFT CORNER.

Source: SDR IAVA2019072900001 · FAA SDRS
O · 2017-03-27 Matched by certificate designator
N20WH · ATA 7240

OUTER COMBUSTION CASE HAS A CRACK ABOUT 270 DEGREES AROUND FUEL NOZZLE BOSS.

Source: SDR IAVA201704050001 · FAA SDRS
E · 2015-10-23 Matched by certificate designator
N297CA · ATA 7230

INITIATED A NORMAL TAKEOFF TO THE SOUTH FROM TB-45. APPROXIMATELY 3-5 SECONDS AFTER INITIATION, A LOUD BANG WAS HEARD WITH ACCOMPANING AIRFRAME SHUTTER. ABORTED TAKE OFF. SECOND BANG AND SHUTTER FOLLOWED AS ACFT SETTLED TO THE GROUND.

Source: SDR IAVA2016F00016 · FAA SDRS
O · 2014-06-05 Matched by certificate designator
N461RA · ATA 7250

RIGHT HAND ELBOW LEAKING AIR IN WELD AREA WHERE FLANGE ATTACHES TO COMBUSTION CASE.

Source: SDR IAVA2014061100002 · FAA SDRS
J · 2014-05-30 Matched by certificate designator
N1197 · ATA 7250

OUTER COMBUSTION CASE CRACKED ON THE RT SIDE UNDER WIRE REINFORCEMENT PATCH.

Source: SDR IAVA201406110001 · FAA SDRS
O · 2011-09-14 Matched by certificate designator
N377RS · ATA 5302

PILOT REPORTED THAT THERE WAS A VIBRATION IN THE ACFT. INVESTIGATION FOUND THE RIVETS WORKING AT TAILBOOM TO TAIL ROTOR GEARBOX CASTING MOUNT. FURTHER INVESTIGATION FOUND A CRACK IN THE TAIL BOOM AT THE 11:00 POSITION, APPROX 1.5 INCHES LONG AT THE ROW OF RIVETS ATTACHING THE TAIL ROTOR GEARBOX CASTING TO THE TAILBOOM. AN EVENT 4 INSPECTION HAD BEEN COMPLIED WITH 64 HOURS PRIOR WITH NO DEFECTS NOTED. THE LAST BALANCE AT EVENT 1 INSPECTION 163.6 HRS PRIOR WITH NO DEFECTS NOTED. AN EVENT 5 INSPECTION HAD BEEN ACCOMPLISHED 17.7 HOURS PRIOR AND NO DEFECTS NOTED. THE TAIL ROTOR WAS REMOVED AND A STATIC BALANCED PERFORMED. THE STATIC BALANCE WAS FOUND TO BE OUT OF TOLERANCE. UPON FURTHER INVESTIGATION THE TAIL ROTOR TRUNNION WAS FOUND TO HAVE SHIFTED . 065.

Source: SDR IAVA201109140001 · FAA SDRS
O · 1996-01-29 Matched by certificate designator
N7266K · ATA 3340

ANTI-COLLISION LIGHT LENS CAME UNGLUED AT SEAMS. REPLACED LENS.

Source: SDR 96ZZZX995 · FAA SDRS

Linked aircraft

N-numberMake / modelYearStatusLink basis
N1170BELL HELICOPTER TEXTRON CANADA 4072001Valid RegistrationMatched by certificate designator
N1197DJI AGRAS T100Valid RegistrationOperator named in NTSB report
N131WMBELL 206-L42005Valid RegistrationMatched by certificate designator
N1371Operator named in NTSB report
N1416BELL 407Valid RegistrationMatched by certificate designator
N2297EBELL 206B1982Valid RegistrationMatched by certificate designator
N34BMBELL 4071998Valid RegistrationOperator named in NTSB report
N34BMBELL 4071998Valid RegistrationMatched by certificate designator
N35LBELL 4072000Valid RegistrationMatched by certificate designator
N377RSBELL 4072003Valid RegistrationMatched by certificate designator
N7266KSIKORSKY S-76A1985Valid RegistrationMatched by certificate designator
N751HCBELL 4071998Valid RegistrationMatched by certificate designator
N82MMBELL HELICOPTER TEXTRON CANADA 4071996Valid RegistrationMatched by certificate designator
N851HCBELL 4071997Valid RegistrationMatched by certificate designator
N91WHBELL 4071998Valid RegistrationMatched by certificate designator