# N432JS: 1995 Dornier Luftfahrt DO 328-100, registration cancelled 2009-09-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 15, 2009
- Exported to: Indonesia
- Status when cancelled: Valid registration
- Airframe: [Dornier Luftfahrt DO 328-100](https://openairdocs.org/model/dornier-luftfahrt-do-328-100) (registry code 2996000)
- Engine: [Pratt & Whitney Canada PW119B](https://openairdocs.org/engine/pratt-whitney-canada-pw119b) (registry code 52133)
- Data sheets: [TCDS A45NM](https://openairdocs.org/tcds/A45NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 3045
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: June 28, 1995
- Certificate issued: February 21, 2008
- Last registry action: February 21, 2008
- Mode S code: A52B65
- Owner when cancelled: [Comtran International Inc](https://openairdocs.org/faa-owner/COMTRAN%20INTERNATIONAL%20INC)
- Location: [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio)
- Owner type: Corporation
- Owner's area on the map: 29.5387° N, 98.4913° W: Placed by OpenAirDocs at the center of ZIP code 78216, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N432JS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=432JS
- Page: https://openairdocs.org/deregistered/N432JS-2009-09-15

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Dornier Luftfahrt DO 328-100: https://openairdocs.org/model/dornier-luftfahrt-do-328-100.md

## Service difficulty reports (55, newest 50)

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

- [SDR VNAA0402013](https://openairdocs.org/sdr/VNAA0402013), Feb 29, 2004: LIGHT. FAILED. THE CREW REPORTED THAT THE FIRST STRIP OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND RESECURED THE EMERGENCY FLOOR LIGHT STRIP CON
- [SDR VNAA0401001](https://openairdocs.org/sdr/VNAA0401001), Jan 2, 2004: POWER SUPPLY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING WILL NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANC
- [SDR VNAA0312013](https://openairdocs.org/sdr/VNAA0312013), Dec 21, 2003: SMOKE. DETECTED. THE CREW RECEIVED A LAV SMOKE FAIL INDICATION. THE CREW CYCLED THE CIRCUIT BREAKER AND THE MESSAGE CLEARED, THERE WAS NO EVIDENCE OF SMOKE. THE AIRCRAFT WAS THE
- [SDR VNAA0307010](https://openairdocs.org/sdr/VNAA0307010), Jul 31, 2003: CONTROL UNIT. FAILED. WHILE EN ROUTE FROM PHL TO GSP CREW REPORTED RADAR INOPERATIVE. CREW DIVERTED TO PIT WHERE MAINTENANCE REPLACED THE RADAR UNIT. AIRCRAFT DEPARTED WITH NO OTHER 
- [SDR VNAA0306016](https://openairdocs.org/sdr/VNAA0306016), Jun 29, 2003: CONTROL PANEL. FAILED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKEOFF. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLAC
- [SDR VNAA0303021](https://openairdocs.org/sdr/VNAA0303021), Mar 17, 2003: SEAL. FAILED. DURING CLIMB OUT, THE CREW HEARD A THUMPING NOISE FROM THE UPPER RIGHT SIDE OF THE AIRCRAFT AND RETURNED TO DAY. MAINTENANCE INSPECTED AND TRIMMED THE UPPER FUS
- [SDR VNAA0302012](https://openairdocs.org/sdr/VNAA0302012), Feb 14, 2003: CONNECTOR. FAILED. EN ROUTE, THE CREW RECEIVED A FUEL ASYMMETRY CAS MESSAGE AND DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE COAX CONNECTOR ON THE REFUEL PANEL IN ACCOR
- [SDR VNAA0302011](https://openairdocs.org/sdr/VNAA0302011), Feb 13, 2003: TRANSFER PUMP. FAILED. ENROUTE, THE CREW NOTICED A FUEL IMBALANCE AND HAD A LEFT HAND FEEDER TANK LOW CAS MESSAGE AND FUEL ASSYMETRY CAS MESSAGE THEN DIVERTED TO BDL. ON FINAL THE MES
- [SDR VNAA0301029](https://openairdocs.org/sdr/VNAA0301029), Jan 26, 2003: GCU. FAILED. DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL CAS MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND GENERATOR CON
- [SDR VNAA0301028](https://openairdocs.org/sdr/VNAA0301028), Jan 26, 2003: BPCU. FAILED. DURING TAKE OFF, THE CREW PUSHED THE THROTTLES FORWARD AND RECEIVED A RIGHT HAND DC GENERATOR FAILED MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND REP
- [SDR VNAA0301005](https://openairdocs.org/sdr/VNAA0301005), Jan 6, 2003: CONNECTOR. DIRTY. EN ROUTE TO TYS, THE CREW RECEIVED A FUEL FEEDER TANK LOW CAS MESSAGE. THE CREW CALLED MAINTENANCE CONTROL AND THE DECISION WAS MADE TO DIVERT TO ROA. OUTSTATIO
- [SDR VNAA0212027](https://openairdocs.org/sdr/VNAA0212027), Dec 21, 2002: PANEL. MALFUNCTIONED. DURING FLIGHT THE CREW RECEIVED A LEFT HAND FEEDER LOW CAS MESSAGE AND DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE REFUEL/DEFUEL PANEL IN ACCORDANCE
- [SDR VNAA0210015](https://openairdocs.org/sdr/VNAA0210015), Oct 15, 2002: WARNING SYSTEM. ACTIVATED. DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. THE CREW EXITED THE RUNWAY AND RECONFIGURED THE AIRCRAFT AND WAS CLEA
- [SDR VNAA0210007](https://openairdocs.org/sdr/VNAA0210007), Oct 10, 2002: WARNING SYSTEM. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION MESSAGE AND ABORTED TAKEOFF. WHEN EXITING THE RUNWAY, THE MESSAGE CLEARED. FLIGHT 4140 WAS THEN CLEARE
- [SDR VNAA0209018](https://openairdocs.org/sdr/VNAA0209018), Sep 15, 2002: CIRCUIT BREAKER. TRIPPED. FLIGHT 4056 WAS ON THE RUNWAY READY FOR TAKEOFF AND RECEIVED A LEFT HAND PACK OVERHEAT MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND RESET THE L2 CIRCU
- [SDR VNAA0203014](https://openairdocs.org/sdr/VNAA0203014), Mar 9, 2002: OIL SYSTEM. LOW. APPROXIMATELY 10 TO 15 MILES NORTH OF TRI-CITYS THE CREW RECEIVED A LOW OIL PRESSURE CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CALLED MAIN
- [SDR VNAA0112005](https://openairdocs.org/sdr/VNAA0112005), Dec 6, 2001: UPLOCK. FAILED. UPON GEAR RETRACTION, THE CREW RECEIVED A LEFT HAND GEAR NOT LOCKED INDICATION RADIOED MAINTENANCE CONTROL AND RETURNED TO DAY. MAINTENANCE INSPECTED AND REPLAC
- [SDR VNAA0112004](https://openairdocs.org/sdr/VNAA0112004), Dec 5, 2001: SENSOR. AT 100 FEET AGL THE CREW RETRACTED THE GEAR AND THE LEFT HAND GEAR INDICATION REMAINED IN TRANSIT. THE CREW CALLED MAINTENANCE CONTROL AND STATED THAT WHEN EXTE
- [SDR VNAA0111015](https://openairdocs.org/sdr/VNAA0111015), Nov 30, 2001: APU. WHILE ADDING POWER DURING TAKE OFF, THE CABIN FILLED WITH SMOKE AND THE CREW ABORTED TAKE OFF. THE CREW ENSURED ALL PASSENGERS WERE FIT TO RETURN TO THE GATE. A
- [SDR VNAA0110015](https://openairdocs.org/sdr/VNAA0110015), Oct 23, 2001: BATTERY. DISCHARGED. THE CREW REPORTED THE EMERGENCY LIGHTING AT ROWS 7 THROUGH 9 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION 
- [SDR VNAA0110005](https://openairdocs.org/sdr/VNAA0110005), Oct 9, 2001: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS EIGHT AND NINE WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDAN
- [SDR VNAA0109005](https://openairdocs.org/sdr/VNAA0109005), Sep 8, 2001: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION IN ACCORDANCE W
- [SDR VNAA0108019](https://openairdocs.org/sdr/VNAA0108019), Aug 28, 2001: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION IN ACCORDANCE 
- [SDR VNAA0107011](https://openairdocs.org/sdr/VNAA0107011), Jul 8, 2001: WARNING SYSTEM. ACTIVATED. AFTER APPLYING POWER FOR TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION CAS AND ELEVATOR TRIM CAS MESSAGE. THE CREW ABORTED TAKEOFF AND EXITED THE RUNWAY. T
- [SDR VNAA0102006](https://openairdocs.org/sdr/VNAA0102006), Feb 11, 2001: POWER SUPPLY. FAILED. THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY UNITS WOULD NOT TEST. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED BOTH EMERGENCY 
- [SDR VNAA0101005](https://openairdocs.org/sdr/VNAA0101005), Jan 5, 2001: WINDOW. CRACKED. DURING CLIMBOUT, AT 6000 FEET THE CREW NOTICED THAT THE RIGHT HAND SIDE WINDOW HAD CRACKED. THE CREW NOTIFIED ATC AND RETURNED TO PIT FOR MAINTENANCE. MAINTENAN
- [SDR VNAA0007001](https://openairdocs.org/sdr/VNAA0007001), Jul 2, 2000: BRAKE ASSY. OVERHEATED. THE CREW ABORTED TAKEOFF DUE TO BOTH INBOARD AND OUTBOARD BRAKES BEING HOT. THE CREW TAXIED OFF THE RUNWAY AND WAITED FOR THE BRAKES TO COOL OFF. AFTER THE BRAK
- [SDR VNAA0004001](https://openairdocs.org/sdr/VNAA0004001), Apr 1, 2000: ECU. FAILED. AFTER DEPARTING DCA EN ROUTE TO BTV, THE CREW EXPERIENCED A RIGHT HAND ELECTRONIC CONTROL UNIT FAILURE. IT RESET AND OCCURRED TWO MORE TIMES. THE THIRD TIME THE
- [SDR VNAA0002011](https://openairdocs.org/sdr/VNAA0002011), Feb 11, 2000: LEVER. FAILED. WHILE ON APPROACH, THE CREW EXTENDED THE LANDING GEAR BUT DID NOT RECEIVE A GEAR DOWN INDICATION. THE CREW DECLARED AN EMERGENCY AND LEVELED OFF AT 100 FEET SO 
- [SDR VNAA0002001](https://openairdocs.org/sdr/VNAA0002001), Feb 1, 2000: CONTROL VALVE. FAILED. DURING CRUISE, THE CREW RECEIVED A RIGHT INBOARD DE-ICE BOOT IS FAILING MESSAGE. THE CREW RETURNED TO PITTSBURGH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANC
- [SDR VNAA0001020](https://openairdocs.org/sdr/VNAA0001020), Jan 25, 2000: DOOR. DISLODGED. DURING CLIMB-OUT, AIRCRAFT WOULD NOT PRESSURIZE IN EITHER MANUAL OR AUTO MODE. MAINTENANCE CONTROL HAD THE AIRCRAFT RETURN TO THE FIELD. MAINTENANCE INSPECTED A
- [SDR VNAA0001012](https://openairdocs.org/sdr/VNAA0001012), Jan 16, 2000: BATTERY. DISCHARGED. THE CREW FOUND THAT THE EMERGENCY EXIT LIGHT AT THE 11A POSITION DID NOT WORK. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 9A POSITION IN AC
- [SDR VNAA9912017](https://openairdocs.org/sdr/VNAA9912017), Dec 30, 1999: BATTERY. DISCHARGED. THE CREW NOTICED THAT THE EMERGENCY FLOOR LIGHTING WAS NOT WORKING AT THE 7LK POSITION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK POSI
- [SDR VNAA9912001](https://openairdocs.org/sdr/VNAA9912001), Dec 5, 1999: DOOR. UNLATCHED. DURING CLIMB, THE FLIGHT CREW FELT A VIBRATION ON THE LEFT SIDE. THE CREW TURNED ON THE WING LIGHT AND NOTICED THE LEFT ENGINE OUTBOARD COWLING FLAPPING IN FLIG
- [SDR VNAA9911005](https://openairdocs.org/sdr/VNAA9911005), Nov 4, 1999: BATTERY. DISCHARGED. THE FLIGHT CREW FOUND THE EMERGENCY EXIT SIGN LIGHT AT SEAT 11A WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK POSITION IN
- [SDR VNAA9910016](https://openairdocs.org/sdr/VNAA9910016), Oct 25, 1999: ENGINE. BIRD STRIKE. ON PREFLIGHT INSPECTION THE FLIGHT CREW FOUND BIRD REMAINS ON THE LT PROPELLER AND THE LT ENGINE INTAKE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO EXTERNA
- [SDR VNAA9909002](https://openairdocs.org/sdr/VNAA9909002), Sep 11, 1999: BATTERY. DISCHARGED. THE CABIN EMERGENCY LIGHTS FROM ROWS 7 TO 10 AND THE LT EMERGENCY EXIT SIGN WERE FOUND TO OPERATE INTERMITTENTLY BY THE FLIGHT CREW. MAINTENANCE INSPECTED AND R
- [SDR VNAA9909001](https://openairdocs.org/sdr/VNAA9909001), Sep 2, 1999: CONNECTOR. LOOSE. AFTER TAKEOFF FROM PIT,THE RIGHT ENGINE OIL TEMPERATURE INDICATION WENT TO 120 DEGREES AND THEN THE DISPLAY WENT BLANK ON THE EICAS DISPLAY. THE AIRCRAFT RETURN
- [SDR VNAA9905008](https://openairdocs.org/sdr/VNAA9905008), May 24, 1999: BULB. FAILED. THE LEFT MAIN GEAR GREEN INDICATION LAMPS WERE NOTED TO BE INOPERATIVE, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENAN
- [SDR VNAA9902004](https://openairdocs.org/sdr/VNAA9902004), Feb 9, 1999: WINDOW. CRACKED. WHILE EN ROUTE TO BTV, THE RIGHT HAND SIDE WINDOW OUTER PANE CRACKED. THE AIRCRAFT DIVERTED TO PIT AND LANDED SAFELY. PIT MAINTENANCE INSPECTED AND REPLACED THE
- [SDR VNAA9901020](https://openairdocs.org/sdr/VNAA9901020), Jan 20, 1999: BATTERY. DISCHARGED. THE EMERGENCY LIGHTS AT THE MIDDLE SECTION OF THE AIRCRAFT WERE NOTED TO BE INOPERATIVE, DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE
- [SDR VNAA9901017](https://openairdocs.org/sdr/VNAA9901017), Jan 18, 1999: BATTERY. DISCHARGED. DURING THE PREFLIGHT INSPECTION, EMERGENCY LIGHTS AT ROWS THREE AND SIX WERE NOTED TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTE
- [SDR VNAA9901021](https://openairdocs.org/sdr/VNAA9901021), Jan 14, 1999: SWITCH. DIRTY. AFTER DEPARTURE, A RIGHT HAND MAIN LANDING GEAR UNLOCK INDICATION ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY. OUTSTATION MAINTENANCE INSP
- [SDR VNAA9812010](https://openairdocs.org/sdr/VNAA9812010), Dec 20, 1998: BATTERY. DISCHARGED. SEVERAL EMERGENCY LIGHTS WERE NOTED TO BE INOPERATIVE DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED EMERGENCY BATTERY PACK 7LK, IN ACCORDA
- [SDR VNAA9812003](https://openairdocs.org/sdr/VNAA9812003), Dec 2, 1998: CONTROL UNIT. FAILED. THE AIRCRAFT RETURNED TO THE GATE AFTER RECEIVING A NOSE STEERING FAIL WARNING INDICATION. MAINTENANCE INSPECTED AND REPLACED THE NOSE STEERING CONTROL UNIT, IN
- [SDR VNAA9810021](https://openairdocs.org/sdr/VNAA9810021), Oct 24, 1998: BULB. FAILED. WHEN LANDING GEAR WAS SELECTED DOWN DURING THE APPROACH INTO PIT, THE LEFT HAND MAIN LANDING GEAR GREEN LAMP FAILED TO ILLUMINATE. THE CREW BEGAN PROCEDURE TO R
- [SDR VNAA9809015](https://openairdocs.org/sdr/VNAA9809015), Sep 17, 1998: WINDSHIELD. BIRDSTRIKE. DURING THE CLIMBOUT, THE AIRCRAFT WAS STRUCK BY A BIRD ON THE COCKPIT RIGHT SIDE WINDSHIELD. THE AIRCRAFT CONTINUED TO CLE AND EXECUTED A NORMAL LANDING. OUTSTA
- [SDR VNAA9804027](https://openairdocs.org/sdr/VNAA9804027), Apr 30, 1998: STRUCTURE. BIRD STRIKE. UPON LANDING,THE CREW NOTIFIED MAINTENANCE CONTROL THAT THEY MAY HAVE ENCOUNTERED A BIRD STRIKE. OUTSTATION MAINTENANCE INSPECTED THE AIRCRAFT FOR DAMAGE IN ACC
- [SDR VNAA9804021](https://openairdocs.org/sdr/VNAA9804021), Apr 17, 1998: AOA SENSOR. FAILED. DURING TAXI PRIOR TO TAKEOFF, A STICK PUSHER FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND APPROVED 
- [SDR VNAA9803016](https://openairdocs.org/sdr/VNAA9803016), Mar 14, 1998: PANEL. FAILED. WHEN ELECTRICAL POWER WAS APPLIED TO THE AIRCRAFT, THE CREW NOTICED A TRICKLE OF SMOKE COMING FROM THE FLIGHT GUIDANCE CONTROL PANEL. THE CREW REMOVED ELECTRICA

All 55: https://openairdocs.org/deregistered/N432JS-2009-09-15/reports.md

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20010105000059I](https://openairdocs.org/incident/20010105000059I), Jan 5, 2001: Dorner DO328100 (N432JS), Pittsburgh, PA. (-23) Psa flight 4018 departed pit on 1-5-01, at 6000 feet the captain noticed the crack in the co-pilots window, reduced cabin pressure and returned to pit.…
- [Incident 19991205035569I](https://openairdocs.org/incident/19991205035569I), Dec 5, 1999: Dorner DO328100 (N432JS), Pittsburgh, PA, Minor damage. (-23) On December 5, 1999, at 2248E, a DO-328, s/n 3045, registered as N432JS operating as vnaa flight 4064, returned to land at pit runway 28L after reporting…

## Other aircraft with N432JS

- [Registered now](https://openairdocs.org/aircraft/N432JS): Bell Helicopter Textron Canada 407, S/N 54320, built 2011

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