# N425JS: Dornier Luftfahrt 328-100, registration cancelled 2008-09-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 22, 2008
- Exported to: Indonesia
- Status when cancelled: Valid registration
- Airframe: [Dornier Luftfahrt 328-100](https://openairdocs.org/model/dornier-luftfahrt-328-100) (registry code 2996100)
- Data sheets: [TCDS A45NM](https://openairdocs.org/tcds/A45NM) (OpenAirDocs)
- Serial number: 3037
- Type of aircraft: Fixed wing multi engine
- Certificate issued: August 26, 2008
- Last registry action: August 26, 2008
- Mode S code: A50F0B
- Owner when cancelled: [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE)
- Location: Cornwall, United Kingdom
- Owner type: Corporation
- The mark today: https://openairdocs.org/aircraft/N425JS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=425JS
- Page: https://openairdocs.org/deregistered/N425JS-2008-09-22

From the FAA registry file of October 27, 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 328-100: https://openairdocs.org/model/dornier-luftfahrt-328-100.md

## Service difficulty reports (53, newest 50)

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

- [SDR VNAA0408002](https://openairdocs.org/sdr/VNAA0408002), Aug 2, 2004: POWER SUPPLY. FAILED. THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY WAS DEAD. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE
- [SDR VNAA0406014](https://openairdocs.org/sdr/VNAA0406014), Jun 21, 2004: DAU. FAILED. ON CLIMBOUT, THE CREW RECEIVED AN ON SIDE BLUE STICK SHAKER CAS MESSAGE. THE AIRCRAFT THEN RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R
- [SDR VNAA0406010](https://openairdocs.org/sdr/VNAA0406010), Jun 14, 2004: DAU. FAILED. DURING CLIMBOUT, THE CREW RECEIVED A RT STICK SHAKER CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 DATA ACQUISITION UNIT IN ACCOR
- [SDR VNAA0403006](https://openairdocs.org/sdr/VNAA0403006), Mar 2, 2004: LIGHT. FAILED. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROW 4 WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE AMBER LIGHT STRIP IN ACCORDANCE WITH DORNIE
- [SDR VNAA0312009](https://openairdocs.org/sdr/VNAA0312009), Dec 17, 2003: PILOT VALVE. FAILED. THE CREW REPORTED RECEIVING A EMERGENCY PARKING BRAKE ACCUMULATOR CAS MESSAGE. MAINTENANCE INSPECTED AND FOUND THE PILOT VALVE STUCK. MAINTENANCE THEN CLEANED A
- [SDR VNAA0312002](https://openairdocs.org/sdr/VNAA0312002), Dec 2, 2003: DAU. FAILED. DURING TAKEOFF, THE CREW RECEIVED A LEFT AND RIGHT HAND SHAKER FAIL AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE DATA ACQUISITION UNIT IN ACCORDA
- [SDR VNAA0306011](https://openairdocs.org/sdr/VNAA0306011), Jun 22, 2003: GENERATOR. FAILED. DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. THE CREW RESET THE SYSTEM AND WAS CLEARED FOR ANOTHER TAKEOFF ATTE
- [SDR VNAA0306012](https://openairdocs.org/sdr/VNAA0306012), Jun 22, 2003: GCU. FAILED. DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND GENERATOR CONTRO
- [SDR VNAA0306013](https://openairdocs.org/sdr/VNAA0306013), Jun 22, 2003: SENSOR. FAILED. DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. THE AIRCRAFT WAS THEN FERRIED TO CAK. MAINTENANCE INSPECTED AND RE
- [SDR VNAA0306002](https://openairdocs.org/sdr/VNAA0306002), Jun 3, 2003: VALVE. FAILED. EN ROUTE, THE CREW RECEIVED A EMERGENCY PARKING BRAKE VALVE ACCUMULATOR LOW CAS MESSAGE IN FLIGHT. THE ACCUMULATOR WAS SERVICED AND THE AIRCRAFT WAS THEN FERRIE
- [SDR VNAA0304019](https://openairdocs.org/sdr/VNAA0304019), Apr 18, 2003: CONTROL PANEL. FAILED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ECU FAIL INDICATION AND ABORTED TAKEOFF. WHILE TAXIING BACK TO THE GATE, THE FLIGHT ATTENDANT REPORTED SMOKE IN TH
- [SDR VNAA0211013](https://openairdocs.org/sdr/VNAA0211013), Nov 11, 2002: POWER SUPPLY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT WORKING AT ROWS 6 TO 9. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH D
- [SDR VNAA0209036](https://openairdocs.org/sdr/VNAA0209036), Sep 26, 2002: LIGHT. LOOSE. THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND RESECURED THE EMERGENCY FLOOR LIGHTING IN ACCORDANCE WITH DORNIER 
- [SDR VNAA0209035](https://openairdocs.org/sdr/VNAA0209035), Sep 26, 2002: LIGHT. LOOSE. THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND RESECURED THE EMERGENCY FLOOR LIGHTING IN ACCORDANCE WITH DORNIER 
- [SDR VNAA0209033](https://openairdocs.org/sdr/VNAA0209033), Sep 23, 2002: LIGHT. LOOSE. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROW 4 TO 6 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND RESECURED THE EMERGENCY FLOOR LIGHTING STRIP I
- [SDR VNAA0209005](https://openairdocs.org/sdr/VNAA0209005), Sep 5, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 4 TO 5 WILL NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH DO
- [SDR VNAA0206015](https://openairdocs.org/sdr/VNAA0206015), Jun 24, 2002: CIRCUIT BREAKER. DURING TAKE OFF, THE CREW RECEIVED A TAKEOFF MISCONFIGURE CAS MESSAGE AND ABORTED TAKE OFF. MAINTENANCE ADVISED THE CREW TO RECYCLE THE IAC CIRCUIT BREAKER AND 
- [SDR VNAA0204021](https://openairdocs.org/sdr/VNAA0204021), Apr 24, 2002: WIRE. FAILED. DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND FOUND A DISCONNECTED WIRE ON THE 1VE PANEL
- [SDR VNAA0204018](https://openairdocs.org/sdr/VNAA0204018), Apr 19, 2002: GENERATOR. FAILED. AFTER DEPARTING SDF, THE LEFT HAND GENERATOR FAILED. THE CAPTAIN RESET THE GENERATOR TWICE AND BOTH TIMES THE GENERATOR WOULD FAIL. FLIGHT 4145 THEN RETURNED TO
- [SDR VNAA0102012](https://openairdocs.org/sdr/VNAA0102012), Feb 20, 2001: CONNECTOR. DIRTY. AFTER TAKING THE RUNWAY THE CREW RECEIVED A RIGHT ENGINE ELECTRONIC CONTROL UNIT FAIL CAS MESSAGE. FLIGHT CREW ABORTED THE TAKEOFF. AFTER THE AIRCRAFT CLEARED T
- [SDR VNAA0102009](https://openairdocs.org/sdr/VNAA0102009), Feb 17, 2001: LANDING GEAR. MALFUNCTIONED. FLIGHT 4189 WAS NOT GETTING THE LANDING GEAR LOCK DOWN INDICATION. THE CREW PERFORMED A MISS APPROACH AND RAN THROUGH THE QUICK REFERENCE HANDBOOK. THE CREW USE
- [SDR VNAA0101027](https://openairdocs.org/sdr/VNAA0101027), Jan 31, 2001: POWER SUPPLY. FAILED. THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLIES WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED BOTH EMERGENCY POWER SUPPLIES IN ACCORDANCE WITH DORNIER 
- [SDR VNAA0101018](https://openairdocs.org/sdr/VNAA0101018), Jan 20, 2001: BRUSH BLOCK. MALFUNCTIONED. DURING THE TAKEOFF ROLL, THE CREW RECEIVED AN AMBER CAS MESSAGE FOR LEFT PROP HEAT FAIL AND A CHIME. FLIGHT 4001 ABORTED TAKE OFF. MAINTENANCE INSPECTED AND CLE
- [SDR VNAA0101003](https://openairdocs.org/sdr/VNAA0101003), Jan 5, 2001: BATTERY. FAILED. THE CREW REPORTED THE THE EMERGENCY LIGHTING WAS NOT ILLUMINATING AROUND THE 4LK LOCATION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK P
- [SDR VNAA0006008](https://openairdocs.org/sdr/VNAA0006008), Jun 21, 2000: BLEED VALVE. FAILED. DURING TAKE OFF, THE CREW RECEIVED AN ELECTRONIC CONTROL UNIT FAIL CAS MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND CLEANED THE INTER BLEED VALVE IN 
- [SDR VNAA0005008](https://openairdocs.org/sdr/VNAA0005008), May 8, 2000: SENSOR. MALFUNCTIONED. DURING THE TAKEOFF ROLL, THE CREW RECEIVED A AOA HEAT FAIL CAS MESSAGE. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. OUTSTATION MAINTENANCE FOUND THE AOA 
- [SDR VNAA0002014](https://openairdocs.org/sdr/VNAA0002014), Feb 19, 2000: WARNING SYSTEM. ACTIVATED. FLIGHT 9467 - ABORTED TAKE OFF AFTER RECEIVING A LEFT AND RIGHT LOW FUEL PRESSURE CAS MESSAGE WHEN CROSS FEEDING. WHILE TAXIING, THE MESSAGE CLEARED, THE CREW T
- [SDR VNAA0001018](https://openairdocs.org/sdr/VNAA0001018), Jan 22, 2000: SENSOR. FAILED. DURING APPROACH, THE CREW RECEIVED NO GEAR EXTENSION INDICATION. THE CREW DECLARED AN EMERGENCY AND REQUESTED A FLY BY TO ENSURE THAT THE NOSE GEAR WAS EXTENDED
- [SDR VNAA0001010](https://openairdocs.org/sdr/VNAA0001010), Jan 10, 2000: BATTERY. DISCHARGED. THE CREW FOUND THAT THE EMERGENCY LIGHTS AT THE 6LK POSITION WERE NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION IN A
- [SDR VNAA9911021](https://openairdocs.org/sdr/VNAA9911021), Nov 25, 1999: BATTERY. DISCHARGED. THE FLIGHT CREW FOUND EMERGENCY LIGHTS 4, 5, 6, AND 7 NOT WORKING. THE AIRCRAFT WAS FERRIED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT 
- [SDR VNAA9910017](https://openairdocs.org/sdr/VNAA9910017), Oct 26, 1999: BATTERY. DISCHARGED. THE FLIGHT CREW REPORTED THE EMERGENCY LIGHTS AT 7 THROUGH 9 WOULD NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE EMERGENCY BATTERY AT THE 7LK POSITION IN
- [SDR VNAA9909010](https://openairdocs.org/sdr/VNAA9909010), Sep 29, 1999: PANEL. LEAKING. ON CLIMB-OUT, THE FLIGHT CREW REPORTED A RUDDER LIMITED FAIL CAS MESSAGE ABOVE 160 KTS. THEY ALSO EXPERIENCED A CABIN PRESSURIZATION WARNING ABOVE 10000 FT. THE
- [SDR VNAA9907006](https://openairdocs.org/sdr/VNAA9907006), Jul 18, 1999: METERING UNIT. FAILED. CREW REPORTED, DURING TAXI BRAKES PULSATED SO STRONGLY AFTER LANDING THAT THEY WERE USELESS IN STOPPING THE AIRCRAFT. MAINTENANCE INSPECTED AND REPLACED THE BRA
- [SDR VNAA9906007](https://openairdocs.org/sdr/VNAA9906007), Jun 28, 1999: BATTERY. DISCHARGED. THE 3RD SET OF EMERGENCY FLOOR LIGHTING INOP. REMOVED AND REPLACED 6LK EMERGENCY BATTERY.
- [SDR VNAA9901025](https://openairdocs.org/sdr/VNAA9901025), Jan 23, 1999: CONNECTOR. DIRTY. THE LEFT PROPELLER MOVED TO THE FEATHER POSITION WHEN POWER LEVERS WERE ADVANCED TO FLIGHT IDLE. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE CLEAN
- [SDR VNAA9812008](https://openairdocs.org/sdr/VNAA9812008), Dec 13, 1998: PCU. FAILED. DURING THE TAXI FOR TAKEOFF, THE LEFT HAND ENGINE WAS REPORTED TO HAVE AN UNCOMMANDED INCREASE IN RPM. ALSO, THE ENGINE WAS OVER TORQUED AND WAS SHUT DOWN BY TH
- [SDR VNAA9810023](https://openairdocs.org/sdr/VNAA9810023), Oct 28, 1998: POWER LEVER. LACK OF LUBE. DURING THE TAKEOFF, THE LEFT HAND ENGINE POWER CONTROL LEVER WOULD NOT ADVANCE ABOVE FLIGHT IDLE, WHEN SELECTED BY THE CREW. THE AIRCRAFT ABORTED THE TAKEOFF, A
- [SDR VNAA9810020](https://openairdocs.org/sdr/VNAA9810020), Oct 22, 1998: PROBE. FAILED. DURING THE TAXI PRIOR TO TAKEOFF, A TOTAL AIR TEMPERATURE PROBE FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE FOR REPAIR. MAINTENANCE INSP
- [SDR VNAA9808025](https://openairdocs.org/sdr/VNAA9808025), Aug 25, 1998: VALVE. DEFECTIVE. DURING CLIMB, CREW RECEIVED EMERGENCY PARKING BRAKE ACCUMULATOR CAS MESSAGE. CREW CONSULTED CHECK LIST WHICH REQUIRES LANDING AT NEAREST AVAILABLE AIRPORT. AIRC
- [SDR VNAA9808017](https://openairdocs.org/sdr/VNAA9808017), Aug 18, 1998: EXHAUST. DENTED. DURING THE TAXI FOR TAKEOFF, THE AIRCRAFT WAS STRUCK BY A FREE ROLLING WORK STAND ON WHEELS. THE TOWER REPORTED THAT IT LOOKED AS IF AN ENGINE STAND ROLLED INTO
- [SDR VNAA9808014](https://openairdocs.org/sdr/VNAA9808014), Aug 16, 1998: CONNECTOR. LOOSE. A RIGHT HAND ENGINE FIRE DETECT WARNING LIGHT ILLUMINATED, DURING THE TAXI FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND RESECURED T
- [SDR VNAA9802007](https://openairdocs.org/sdr/VNAA9802007), Feb 8, 1998: HARNESS. FAILED. AFTER TAKEOFF, A PROXY FAIL WARNING MESSAGE ILLUMINATED DURING GEAR RETRACTION. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED, WITHOUT ANY FURTHER PROBLEMS. MAI
- [SDR VNAA9801006](https://openairdocs.org/sdr/VNAA9801006), Jan 9, 1998: TAT PROBE. DEFECTIVE. DURING TAXI, THE CREW RECEIVED A TAT HEAT FAIL MESSAGE. CREW RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE TAT PROBE DEFECTIVE. TAT PRO
- [SDR VNAA9712016](https://openairdocs.org/sdr/VNAA9712016), Dec 25, 1997: AOA SENSOR. DEFECTIVE. DURING TAXI, THE CREW RECEIVED A STICK PUSHER FAIL CAS MESSAGE. AIRCRAFT RETURNED TO THE GATE AND CONTACTED MAINTENANCE CONTROL. DEFERRED THE RT STICK SHAKER SY
- [SDR VNAA9711020](https://openairdocs.org/sdr/VNAA9711020), Nov 30, 1997: TIMER. FAILED. DURING CLIMBOUT, THE CREW NOTED A RIGHT HAND PROPELLER HEAT FAIL WARNING MESSAGE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT ANY FURTHER INCIDENT. MA
- [SDR VNAA9706007](https://openairdocs.org/sdr/VNAA9706007), Jun 24, 1997: SEAL. WORN. 60 MINUTES INTO FLIGHT, RT ENGINE OIL PRESSURE WENT AMBER. 20 MINUTES LATER OIL PRESSURE DROPPED AND RED WARNING PANEL ILLUMINATED. CHECKLIST COMPLETED AND ENGI
- [SDR VNAA9705002](https://openairdocs.org/sdr/VNAA9705002), May 2, 1997: FLOW CONTL VLV. FAILED. AFTER TAKEOFF, THE RIGHT ENGINE INTAKE DE-ICE FAILED. RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT INTAKE EJECTOR FLO
- [SDR VNAA9606004](https://openairdocs.org/sdr/VNAA9606004), Jun 8, 1996: EXHAUST NOZZLE. DEFECTIVE. CREW REPORTED, A RIGHT HAND ENGINE INLET DE-ICE FAILURE ON APPROACH TO PIT. AIRCRAFT CONTINUED ON AND LANDED WITHOUT INCIDENT. UPON FURTHER INVESTIGATION BY PIT
- [SDR VNAA9600002](https://openairdocs.org/sdr/VNAA9600002), Mar 17, 1996: COMPUTER. DEFECTIVE. PIT - FLT 4077 - FMS DEAD RECKONING MODE ILLUMINATED ON THE ANNUNICATION PANEL. CREW ELECTED TO RETURN TO PIT. PIT MX REPLACED THE NR 1 NAVIGATION COMPUTER IAW 
- [SDR 96ZZZX455](https://openairdocs.org/sdr/96ZZZX455), Jan 8, 1996: FUEL FILTER. DIRTY. FLT 4194 - DURING CRUISE, THE FLIGHT CREW WAS ALERTED BY AN AMBER FUEL FILTER BYPASS CAS MESSAGE. EICAS FUEL SYSTEM PAGE INDICATED THE LEFT ENGINE HP FUEL FILTE

All 53: https://openairdocs.org/deregistered/N425JS-2008-09-22/reports.md

## FAA accident and incident reports (1)

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 19980818036689I](https://openairdocs.org/incident/19980818036689I), Aug 18, 1998: Dorner DO328100 (N425JS), Pittsburgh, PA, Minor damage. (-5) Aircraft was hit on the tail cone by a portable maintenance stand that blew across the ramp in gusty winds. Damage to the aircrafts' tail cone was minor.…

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