# Service difficulty reports: N425JS, cancelled Sep 22, 2008 A list on [N425JS, cancelled Sep 22, 2008](https://openairdocs.org/deregistered/N425JS-2008-09-22.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 53 reports - [SDR VNAA0408002](https://openairdocs.org/sdr/VNAA0408002.md): Power Supply · failed · Aug 2, 2004 · N425JS · Dorner DO328100 · Emergency Lighting > THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY WAS DEAD. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. - [SDR VNAA0406014](https://openairdocs.org/sdr/VNAA0406014.md): Dau · failed · Jun 21, 2004 · N425JS · Dorner DO328100 · Stall Warning System > 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, REMOVED, AND REPLACED THE NR 2 DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL - [SDR VNAA0406010](https://openairdocs.org/sdr/VNAA0406010.md): Dau · failed · Jun 14, 2004 · N425JS · Dorner DO328100 · Stall Warning System > 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 ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT - [SDR VNAA0403006](https://openairdocs.org/sdr/VNAA0403006.md): Light · failed · Mar 2, 2004 · N425JS · Dorner DO328100 · Emergency Lighting > 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 DORNIER MAITNENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR - [SDR VNAA0312009](https://openairdocs.org/sdr/VNAA0312009.md): Pilot Valve · failed · Dec 17, 2003 · N425JS · Dorner DO328100 · Landing Gear Retraction/Extension System > THE CREW REPORTED RECEIVING A EMERGENCY PARKING BRAKE ACCUMULATOR CAS MESSAGE. MAINTENANCE INSPECTED AND FOUND THE PILOT VALVE STUCK. MAINTENANCE THEN CLEANED AND LUBED THE PILOT VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHE - [SDR VNAA0312002](https://openairdocs.org/sdr/VNAA0312002.md): Dau · failed · Dec 2, 2003 · N425JS · Dorner DO328100 · Central Computers > DURING TAKEOFF, THE CREW RECEIVED A LEFT AND RIGHT HAND SHAKER FAIL AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT W - [SDR VNAA0306011](https://openairdocs.org/sdr/VNAA0306011.md): Generator · failed · Jun 22, 2003 · N425JS · Dorner DO328100 · AC Generation System > 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 ATTEMPT. - [SDR VNAA0306012](https://openairdocs.org/sdr/VNAA0306012.md): Gcu · failed · Jun 22, 2003 · N425JS · Dorner DO328100 · DC Generating System > DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND GENERATOR CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED A - [SDR VNAA0306013](https://openairdocs.org/sdr/VNAA0306013.md): Sensor · failed · Jun 22, 2003 · N425JS · Dorner DO328100 · DC Indicating System > DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. THE AIRCRAFT WAS THEN FERRIED TO CAK. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND HALL EFFECT SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. - [SDR VNAA0306002](https://openairdocs.org/sdr/VNAA0306002.md): Valve · failed · Jun 3, 2003 · N425JS · Dorner DO328100 · Master Cylinder/Brake Valve > 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 FERRIED TO PIT. MAINTENANCE THEN INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE - [SDR VNAA0304019](https://openairdocs.org/sdr/VNAA0304019.md): Control Panel · failed · Apr 18, 2003 · N425JS · Dorner DO328100 · AC Power Distribution System > 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 THE CABIN AND THE CREW EVACUATED THE AIRCRAFT. THE CREW THEN TAXIIED THE AIRCRAFT BACK TO THE GATE. - [SDR VNAA0211013](https://openairdocs.org/sdr/VNAA0211013.md): Power Supply · failed · Nov 11, 2002 · N425JS · Dorner DO328100 · Lighting System > 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 DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASE - [SDR VNAA0209036](https://openairdocs.org/sdr/VNAA0209036.md): Light · loose · Sep 26, 2002 · N425JS · Dorner DO328100 · Emergency Lighting > THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND RESECURED THE EMERGENCY FLOOR LIGHTING IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR S - [SDR VNAA0209035](https://openairdocs.org/sdr/VNAA0209035.md): Light · loose · Sep 26, 2002 · N425JS · Dorner DO328100 · Emergency Lighting > THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND RESECURED THE EMERGENCY FLOOR LIGHTING IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR S - [SDR VNAA0209033](https://openairdocs.org/sdr/VNAA0209033.md): Light · loose · Sep 23, 2002 · N425JS · Dorner DO328100 · Emergency Lighting > 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 IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE - [SDR VNAA0209005](https://openairdocs.org/sdr/VNAA0209005.md): Battery · discharged · Sep 5, 2002 · N425JS · Dorner DO328100 · Emergency Lighting > 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 DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED - [SDR VNAA0206015](https://openairdocs.org/sdr/VNAA0206015.md): Circuit Breaker · Jun 24, 2002 · N425JS · Dorner DO328100 · Flight Control System > 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 THE MESSAGE CLEARED. FLIGHT 4182 WAS THEN CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND DEPARTED WITHO - [SDR VNAA0204021](https://openairdocs.org/sdr/VNAA0204021.md): Wire · failed · Apr 24, 2002 · N425JS · Dorner DO328100 · Electrical Power System > 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. MAINTENANCE CONNECTED THE WIRE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIO - [SDR VNAA0204018](https://openairdocs.org/sdr/VNAA0204018.md): Generator · failed · Apr 19, 2002 · N425JS · Dorner DO328100 · Electrical Power System > 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 SDF. OUTSTATION MAINTENANCE INSPECTED AND SWAPPED GENERATOR CONTROL UNITS FROM SIDE TO SIDE IN A - [SDR VNAA0102012](https://openairdocs.org/sdr/VNAA0102012.md): Connector · dirty · Feb 20, 2001 · N425JS · Dorner DO328100 · Compressor Bleed Valve > 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 THE RUNWAY THE FLIGHT CREW RESET THE ELECTRONIC CONTROL UNIT AND ANOTHER TAKEOFF ATTEMPT WAS MADE A - [SDR VNAA0102009](https://openairdocs.org/sdr/VNAA0102009.md): Landing Gear · malfunctioned · Feb 17, 2001 · N425JS · Dorner DO328100 · Landing Gear Retraction/Extension System > 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 USED THE EMERGENCY HYDRAULIC SYSTEM TO PUMP THE GEAR DOWN AND GOT A GEAR DOWN AND LOCKED INDICATION. - [SDR VNAA0101027](https://openairdocs.org/sdr/VNAA0101027.md): Power Supply · failed · Jan 31, 2001 · N425JS · Dorner DO328100 · Emergency Lighting > THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLIES WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED BOTH EMERGENCY POWER SUPPLIES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR S - [SDR VNAA0101018](https://openairdocs.org/sdr/VNAA0101018.md): Brush Block · malfunctioned · Jan 20, 2001 · N425JS · Dorner DO328100 · Propeller/Rotor Anti-Ice/De-Ice System > 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 CLEANED THE BRUSH BLOCK AND SLIP RING IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERAT - [SDR VNAA0101003](https://openairdocs.org/sdr/VNAA0101003.md): Battery · failed · Jan 5, 2001 · N425JS · Dorner DO328100 · Emergency Lighting > THE CREW REPORTED THE THE EMERGENCY LIGHTING WAS NOT ILLUMINATING AROUND THE 4LK LOCATION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED - [SDR VNAA0006008](https://openairdocs.org/sdr/VNAA0006008.md): Bleed Valve · failed · Jun 21, 2000 · N425JS · Dorner DO328100 · Compressor Bleed Valve > 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 ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 75-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIR - [SDR VNAA0005008](https://openairdocs.org/sdr/VNAA0005008.md): Sensor · malfunctioned · May 8, 2000 · N425JS · Dorner DO328100 · Attitude and Direction Data System > 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 SENSORS MISALIGNED. OUTSTATION MAINTENANCE ALIGNED THE SENSORS IN ACCORDANCE WITH DORNIER MAINTEN - [SDR VNAA0002014](https://openairdocs.org/sdr/VNAA0002014.md): Warning System · activated · Feb 19, 2000 · N425JS · Dorner DO328100 · Central Warning > 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 THEN ATTEMPTED ANOTHER TAKEOFF. FLIGHT 9467 DEPARTED WITHOUT FURTHER INCIDENT. - [SDR VNAA0001018](https://openairdocs.org/sdr/VNAA0001018.md): Sensor · failed · Jan 22, 2000 · N425JS · Dorner DO328100 · Landing Gear Position and Warning > 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. THE NOSE GEAR WAS EXTENDED AND THE AIRCRAFT LANDED WITHOUT AN INCIDENT. MAINTENANCE INSPECTED A - [SDR VNAA0001010](https://openairdocs.org/sdr/VNAA0001010.md): Battery · discharged · Jan 10, 2000 · N425JS · Dorner DO328100 · Emergency Lighting > 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 ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRC - [SDR VNAA9911021](https://openairdocs.org/sdr/VNAA9911021.md): Battery · discharged · Nov 25, 1999 · N425JS · Dorner DO328100 · Emergency Lighting > 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 THE 6LK LOCATION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE - [SDR VNAA9910017](https://openairdocs.org/sdr/VNAA9910017.md): Battery · discharged · Oct 26, 1999 · N425JS · Dorner DO328100 · Emergency Lighting > 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 ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE COMPLETED AND THE AI - [SDR VNAA9909010](https://openairdocs.org/sdr/VNAA9909010.md): Panel · leaking · Sep 29, 1999 · N425JS · Dorner DO328100 · Fuselage Miscellaneous Structure > 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 FLIGHT CREW RETURNED TO THE FIELD AND A NORMAL LANDING WAS PERFORMED. MAINTENANCE INSPECTED THE - [SDR VNAA9907006](https://openairdocs.org/sdr/VNAA9907006.md): Metering Unit · failed · Jul 18, 1999 · N425JS · Dorner DO328100 · Landing Gear Brake System > CREW REPORTED, DURING TAXI BRAKES PULSATED SO STRONGLY AFTER LANDING THAT THEY WERE USELESS IN STOPPING THE AIRCRAFT. MAINTENANCE INSPECTED AND REPLACED THE BRAKE METERING UNIT. OPERATION CHECKS FAILED AND THE BRAKE METERING UNIT HAD TO BE REPLACED AGAIN. B - [SDR VNAA9906007](https://openairdocs.org/sdr/VNAA9906007.md): Battery · discharged · Jun 28, 1999 · N425JS · Dorner DO328100 · Emergency Lighting > THE 3RD SET OF EMERGENCY FLOOR LIGHTING INOP. REMOVED AND REPLACED 6LK EMERGENCY BATTERY. - [SDR VNAA9901025](https://openairdocs.org/sdr/VNAA9901025.md): Connector · dirty · Jan 23, 1999 · N425JS · Dorner DO328100 · Propeller Controlling System > THE LEFT PROPELLER MOVED TO THE FEATHER POSITION WHEN POWER LEVERS WERE ADVANCED TO FLIGHT IDLE. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE CLEANED THE LT ENGINE SENSOR HARNESS CONNECTORS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-21-00, - [SDR VNAA9812008](https://openairdocs.org/sdr/VNAA9812008.md): Pcu · failed · Dec 13, 1998 · N425JS · Dorner DO328100 · Propeller Controlling System > 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 THE CREW. THE AIRCRAFT THEN RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND - [SDR VNAA9810023](https://openairdocs.org/sdr/VNAA9810023.md): Power Lever · lack of lube · Oct 28, 1998 · N425JS · Dorner DO328100 · Power Lever > 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, AND RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED, CLEANED AND LUBRICATED, THE LEFT HAND P - [SDR VNAA9810020](https://openairdocs.org/sdr/VNAA9810020.md): Probe · failed · Oct 22, 1998 · N425JS · Dorner DO328100 · Outside Air Temperature Indicator/Sensor > DURING THE TAXI PRIOR TO TAKEOFF, A TOTAL AIR TEMPERATURE PROBE FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE FOR REPAIR. MAINTENANCE INSPECTED AND REPLACED THE TOTAL AIR TEMPERATURE PROBE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL - [SDR VNAA9808025](https://openairdocs.org/sdr/VNAA9808025.md): Valve · defective · Aug 25, 1998 · N425JS · Dorner DO328100 · Landing Gear Brake System > DURING CLIMB, CREW RECEIVED EMERGENCY PARKING BRAKE ACCUMULATOR CAS MESSAGE. CREW CONSULTED CHECK LIST WHICH REQUIRES LANDING AT NEAREST AVAILABLE AIRPORT. AIRCRAFT RETURNED TO CAK AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND TH - [SDR VNAA9808017](https://openairdocs.org/sdr/VNAA9808017.md): Exhaust · dented · Aug 18, 1998 · N425JS · Dorner DO328100 · APU Exhaust System > 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 THE AIRCRAFT AS IT TAXIED BY. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLA - [SDR VNAA9808014](https://openairdocs.org/sdr/VNAA9808014.md): Connector · loose · Aug 16, 1998 · N425JS · Dorner DO328100 · Fire Detection > A RIGHT HAND ENGINE FIRE DETECT WARNING LIGHT ILLUMINATED, DURING THE TAXI FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND RESECURED THE RIGHT HAND ENGINE FIRE LOOP SENSOR WIRE CANNON PLUG, IN ACCORDANCE WITH DORNIER MAINTENANCE MAN - [SDR VNAA9802007](https://openairdocs.org/sdr/VNAA9802007.md): Harness · failed · Feb 8, 1998 · N425JS · Dorner DO328100 · Landing Gear Position and Warning > AFTER TAKEOFF, A PROXY FAIL WARNING MESSAGE ILLUMINATED DURING GEAR RETRACTION. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED, WITHOUT ANY FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPLACED THE LEFT DOWN LOCK SWITCH HARNESS IN ACCORDANCE WITH DORNIER MAINT - [SDR VNAA9801006](https://openairdocs.org/sdr/VNAA9801006.md): Tat Probe · defective · Jan 9, 1998 · N425JS · Dorner DO328100 · Outside Air Temperature Indicator/Sensor > 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 PROBE WAS REPLACED IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-10-00. OPERATIONAL CHECK GOOD A - [SDR VNAA9712016](https://openairdocs.org/sdr/VNAA9712016.md): Aoa Sensor · defective · Dec 25, 1997 · N425JS · Dorner DO328100 · Stall Warning System > 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 SYSTEM. AIRCRAFT WAS REPOSITIONED TO PIT. WHEN AIRCRAFT ARRIVED IN PIT, CREW REPORTED THAT THE RT - [SDR VNAA9711020](https://openairdocs.org/sdr/VNAA9711020.md): Timer · failed · Nov 30, 1997 · N425JS · Dorner DO328100 · Propeller/Rotor Anti-Ice/De-Ice System > 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. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND PROPELLER DE-ICE TIMER IN ACCORDANCE WITH DORNIER - [SDR VNAA9706007](https://openairdocs.org/sdr/VNAA9706007.md): Seal · worn · Jun 24, 1997 · N425JS · Dorner DO328100 · Starter-Generator > 60 MINUTES INTO FLIGHT, RT ENGINE OIL PRESSURE WENT AMBER. 20 MINUTES LATER OIL PRESSURE DROPPED AND RED WARNING PANEL ILLUMINATED. CHECKLIST COMPLETED AND ENGINE WAS SHUT DOWN. LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT STARTER SHAFT - [SDR VNAA9705002](https://openairdocs.org/sdr/VNAA9705002.md): Flow Contl Vlv · failed · May 2, 1997 · N425JS · Dorner DO328100 · Air Intake Anti/De-Ice System > AFTER TAKEOFF, THE RIGHT ENGINE INTAKE DE-ICE FAILED. RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT INTAKE EJECTOR FLOW CONTROL VALVE, OPERATIONAL CHECKED GOOD. - [SDR VNAA9606004](https://openairdocs.org/sdr/VNAA9606004.md): Exhaust Nozzle · defective · Jun 8, 1996 · N425JS · Dorner DO328100 · Engine Collector/Tailpipe/Nozzle > 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 MX IT WAS DISCOVERED THAT THE MOUNT FLANGE ON THE EXHAUST NOZZLE HAD FAILED ALLOWING HOT EXHAUST - [SDR VNAA9600002](https://openairdocs.org/sdr/VNAA9600002.md): Computer · defective · Mar 17, 1996 · N425JS · Dorner DO328100 · Flight Management Computing Hardware System > 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 MM 34.41.00. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR 96ZZZX455](https://openairdocs.org/sdr/96ZZZX455.md): Fuel Filter · dirty · Jan 8, 1996 · N425JS · Dorner DO328100 · Engine Fuel Distribution > 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 FILTER IMPENDING BYPASS INDICATION. AIRCRAFT RETURNED TO PIT, LANDED WITHOUT FURTHER INCIDENT. PIT MAI Next page: https://openairdocs.org/deregistered/N425JS-2008-09-22/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N425JS' AND deregistration_id = 'N425JS-2008-09-22' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N425JS-2008-09-22/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.