# Service difficulty reports: N426JS, cancelled May 21, 2009

A list on [N426JS, cancelled May 21, 2009](https://openairdocs.org/deregistered/N426JS-2009-05-21.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 · 81 reports

- [SDR VNAA0407001](https://openairdocs.org/sdr/VNAA0407001.md): Sensor · failed · Jul 4, 2004 · N426JS · Dorner DO328100 · Stall Warning System
  > DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA AND PUSHER FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE VISUALLY INSPECTED THE SYSTEM AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. THE SYSTEM WAS RESET AND THE
- [SDR VNAA0406012](https://openairdocs.org/sdr/VNAA0406012.md): Gcu · failed · Jun 16, 2004 · N426JS · Dorner DO328100 · DC Generating System
  > DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL INDICATION AND ABORTED TAKEOFF. ON TAXI BACK, THE CREW RECEIVED A DC GENERATOR FAIL CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE GENERATOR CONTROL UNIT IN ACCORDANCE WITH DORNIER M
- [SDR VNAA0406011](https://openairdocs.org/sdr/VNAA0406011.md): Warning Light · illuminated · Jun 15, 2004 · N426JS · Dorner DO328100 · Stall Warning System
  > DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND STICK SHAKER PUSHER ON SIDE FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE SHAKER PUSHER RESET ITSELF AND FLIGHT 2417 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 2417 THEN DEPARTED WITH NO FURTHER INCIDENTS.
- [SDR VNAA0405011](https://openairdocs.org/sdr/VNAA0405011.md): Control Unit · failed · May 18, 2004 · N426JS · Dorner DO328100 · Fire Detection
  > THE CREW REPORTED THAT A FIRE SQUIB WAS FAILING TO TEST. MAINTENANCE INSPECTED AND REPLACED THE FIRE WARNING CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA0403014](https://openairdocs.org/sdr/VNAA0403014.md): Sensor · failed · Mar 26, 2004 · N426JS · Dorner DO328100 · Stall Warning System
  > DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA AND PUSHER FAIL THEN ABORTED TAKEOFF. AS THE AIRCRAFT PULLED OFF OF THE RUNWAY IT CORRECTED ITSELF, THE CREW REPORTED VERY WINDY CONDITIONS. THE AIRCRAFT WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPAR
- [SDR VNAA0401003](https://openairdocs.org/sdr/VNAA0401003.md): Sensor · failed · Jan 8, 2004 · N426JS · Dorner DO328100 · Stall Warning System
  > DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA FAIL INDICATION AND ABORTED TAKEOFF. FLIGHT 2463 THEN RETURNED TO THE GATE TO HAVE MAINTENANCE REST THE AOA VANE LEVEL. FLIGHT 2463 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER IN
- [SDR VNAA0310012](https://openairdocs.org/sdr/VNAA0310012.md): Control Unit · failed · Oct 19, 2003 · N426JS · Dorner DO328100 · Fire Detection
  > THE CREW REPORTED RECEIVING A APU FIRE LOOP FAIL AND A FALSE FIRE INDICATION. MAINTENANCE INSPECTED AND REPLACED THE FIRE DETECTION CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RE
- [SDR VNAA0310004](https://openairdocs.org/sdr/VNAA0310004.md): Line · failed · Oct 4, 2003 · N426JS · Dorner DO328100 · Air Intake Anti/De-Ice System
  > DURING FLIGHT, THE CREW RECEIVED A RIGHT HAND ENGINE INTAKE DE-ICE FAIL INDICATION AND RETURNED TO PHL. MAINTENANCE INSPECTED AND REPLACED THE INTAKE LINE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCR
- [SDR VNAA0309009](https://openairdocs.org/sdr/VNAA0309009.md): Dau · failed · Sep 14, 2003 · N426JS · Dorner DO328100 · Central Computers
  > THE CREW REPORTED A LT PUSHER FAIL CASS MESSAGE. AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED LT DATA ACQUISION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND AIRCRAFT WAS RELEASED T
- [SDR VNAA0308002](https://openairdocs.org/sdr/VNAA0308002.md): Fuse · blown · Aug 4, 2003 · N426JS · Dorner DO328100 · External Power System
  > WITH THE EXTERNAL POWER HOOKED UP, SMOKE ENTERED THE FLIGHT DECK AND THE PASSENGERS WERE DEPLANED. MAINTENANCE INSPECTED AND REPLACED BOTH FUSES IN THE GROUND POWER SYSTEM IN ACCORDANCE WITH DORNIER MAINTENANCE MANAUL 24-00-00, BUT GROUND POWER WAS STILL INOP
- [SDR VNAA0304002](https://openairdocs.org/sdr/VNAA0304002.md): Brake · failed · Apr 6, 2003 · N426JS · Dorner DO328100 · Landing Gear Brake System
  > THE CREW REPORTED THAT THE CAPTAIN'S BRAKES HIT THE STOP WITHOUT ANY BRAKING ACTION TAKING PLACE. MAINTENANCE INSPECTED AND BLED THE BRAKES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASE
- [SDR VNAA0303034](https://openairdocs.org/sdr/VNAA0303034.md): Dau · failed · Mar 30, 2003 · N426JS · Dorner DO328100 · Propeller/Rotor Anti-Ice/De-Ice System
  > AFTER TAKEOFF THE RIGHT PROPELLER HEAT FAILED. THE FLIGHT CREW RETURNED TO THE FIELD. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE RIGHT DATA ACQUISTION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-42-00. OPERATIONAL CHECKS WERE COMPLETED AND
- [SDR VNAA0303032](https://openairdocs.org/sdr/VNAA0303032.md): Valve · failed · Mar 29, 2003 · N426JS · Dorner DO328100 · Cabin Cooling System
  > DURING TAKEOFF CREW REPORTED AOA, SHAKER AND PUSHER FAIL. MESSAGE CLEARED AFTER EXITING RUNWAY. THEN CREW REPORTED LT PACK WOULD NOT COOL IN EITHER MODE. AIRCRAFT WAS FERRIED TO DAY WHERE THE LT TEMP CONTROL VALVE WAS REPLACED IN ACCORDANCE WITH MAINTENANCE
- [SDR VNAA0302026](https://openairdocs.org/sdr/VNAA0302026.md): Brush Block · failed · Feb 27, 2003 · N426JS · Dorner DO328100 · Propeller/Rotor Anti-Ice/De-Ice System
  > DURING CRUISE, THE RIGHT HAND PROP HEAT FAILED. DUE TO LIGHT SNOW AT THE DESTINATION, FLIGHT 4050 DIVERTED TO DAY. MAINTENANCE INSPECTED AND FOUND THE BRUSHBLOCK TO BE OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE BRUSHBLOCK IN ACCORDANCE WITH DORNIER MAINTEN
- [SDR VNAA0301027](https://openairdocs.org/sdr/VNAA0301027.md): Proximity Switch · out of adjust · Jan 24, 2003 · N426JS · Dorner DO328100 · Door Warning System
  > EN ROUTE, THE MASTER CAUTION LIGHT ILLUMINATED AND THE PRESSURE CHECKED GOOD. THE CREW DESCENDED AND SLOWED TO 150 KIAS. AT FL180 THE LIGHT EXTINGUISHED. UPON ARRIVAL AT DCA, MAINTENANCE INSPECTED AND ADJUSTED THE OVER CENTER PROXI SWITCH CLEARANCE IN ACCOR
- [SDR VNAA0301018](https://openairdocs.org/sdr/VNAA0301018.md): Proximity Switch · failed · Jan 18, 2003 · N426JS · Dorner DO328100 · Door Warning System
  > EN ROUTE, THE CREW RECEIVED A OPEN DOOR INDICATION ON THE RED WARNING PANEL FOR THE PASSENGER DOOR. THERE WAS NO LOSS OF PRESSURE AND THE DOOR WAS SECURE. FLIGHT 4195 THEN DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE 8MC OVER THE CENTER PROXIMITY
- [SDR VNAA0212030](https://openairdocs.org/sdr/VNAA0212030.md): Warning System · malfunctioned · Dec 25, 2002 · N426JS · Dorner DO328100 · Stall Warning System
  > AFTER THE POWER LEVERS WERE ADVANCED, THE CREW RECEIVED A ANGLE OF ATTACK FAIL MESSAGE AND ABORTED TAKEOFF. THE MESSAGE EXTINGUISHED BY ITSELF AND FLIGHT 4172 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4172 THEN DEPARTED WITH NO FURTHER INCIDENTS.
- [SDR VNAA0211016](https://openairdocs.org/sdr/VNAA0211016.md): Stall Warning · malfunctioned · Nov 14, 2002 · N426JS · Dorner DO328100 · Stall Warning System
  > DURING TAKEOFF, THE CREW RECEIVED AN AOA SENSOR FAIL CAWS MESSAGE AND ABORTED TAKEOFF. AFTER CLEARING THE RUNWAY THE MESSAGE CLEARED AND FLIGHT 4165 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4165 THEN DEPARTED WITH NO FURTHER INCIDENTS.
- [SDR VNAA0210025](https://openairdocs.org/sdr/VNAA0210025.md): Sensor · out of adjust · Oct 23, 2002 · N426JS · Dorner DO328100 · Door Warning System
  > EN ROUTE AT 27,000 FEET, THE CREW RECEIVED A DOORS LIGHT ON THE RED WARNING PANEL. THERE WAS NO CHANGE IN THE PRESSURIZATION. THE CREW DESCENDED TO 15,000 FEET AND THE LIGHT EXTINGUISHED. UPON ARRIVAL AT PIT, MAINTENANCE INSPECTED AND ADJUSTED THE OVER THE
- [SDR VNAA0208021](https://openairdocs.org/sdr/VNAA0208021.md): Panel · malfunctioned · Aug 13, 2002 · N426JS · Dorner DO328100 · AC Power Distribution System
  > DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE P
- [SDR VNAA0207008](https://openairdocs.org/sdr/VNAA0207008.md): Power Supply · failed · Jul 9, 2002 · N426JS · Dorner DO328100 · Lighting System
  > THE CREW REPORTED THAT THE FORWARD EMERGENCY POWER SUPPLY WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR
- [SDR VNAA0207004](https://openairdocs.org/sdr/VNAA0207004.md): Warning System · malfunctioned · Jul 5, 2002 · N426JS · Dorner DO328100 · Central Warning
  > DURING TAKEOFF, THE CREW RECEIVED A CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. AFTER EXITING THE RUNWAY, THE SYSTEM RESET ITSELF AND THE MESSAGE EXTINGUISHED. FLIGHT 4159 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS
- [SDR VNAA0203024](https://openairdocs.org/sdr/VNAA0203024.md): Stall Warning · malfunctioned · Mar 16, 2002 · N426JS · Dorner DO328100 · Stall Warning System
  > THE FLIGHT WAS ON THE TAKEOFF ROLL WHEN THE FLIGHT CREW RECEIVED A STALL PUSHER FAIL WARNING MESSAGE ON THE EICAS DISPLAY. THE FLIGHT CREW ABORTED THE TAKEOFF AND EXITED THE RUNWAY. ONCE CLEARING THE RUNWAY THE WARNING MESSAGE CLEARED ITSELF WITH NO ACTION F
- [SDR VNAA0202015](https://openairdocs.org/sdr/VNAA0202015.md): Engine · failed · Feb 13, 2002 · N426JS · Dorner DO328100 · Powerplant System
  > AFTER BEING CLEAR FOR A VISUAL APPROACH, THE CREW REPORTED ENTERING AN AREA OF MODERATE TURBULENCE. THERE WAS A SINGLE JOLT, NOBODY SUSTAIN ANY SERIOUS INJURIES. THE LEFT HAND ENGINE WAS REPORTED TO SHUT DOWN DURING THE EVENT. WITHOUT SUFFICIENT TIME FOR A
- [SDR VNAA0201017](https://openairdocs.org/sdr/VNAA0201017.md): Stick Shaker · malfunctioned · Jan 21, 2002 · N426JS · Dorner DO328100 · Stall Warning System
  > DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND SHAKER FAIL MESSAGE AND ABORTED TAKEOFF. THE MESSAGE CLEARED AND MAINTENANCE CONTROL CLEARED FLIGHT 4050 FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4050 THEN DEPARTED WITH NO FURTHER INCIDENTS.
- [SDR VNAA0111002](https://openairdocs.org/sdr/VNAA0111002.md): Warning System · malfunctioned · Nov 2, 2001 · N426JS · Dorner DO328100 · Stall Warning System
  > AT THE BEGINNING OF THE TAKEOFF ROLL, THE CREW RECEIVED A PUSHER CAS MESSAGE AND ABORTED TAKEOFF. AFTER CLEARING THE RUNWAY THE MESSAGES CLEARED. THE CREW AND MAINTENANCE FELT THE STRONG WINDS HAD CAUSED THESE INDICATIONS AND FLIGHT 4032 WAS CLEARED FOR ANOT
- [SDR VNAA0110020](https://openairdocs.org/sdr/VNAA0110020.md): Warning System · malfunctioned · Oct 26, 2001 · N426JS · Dorner DO328100 · Stall Warning System
  > DURING TAKEOFF, THE CREW RECEIVED A PUSHER FAIL AND AOA CAS MESSAGES AND ABORTED TAKEOFF. THE MESSAGES WENT OUT ALMOST IMMEDIATELY AND THE CREW ATTEMPTED ANOTHER TAKEOFF. FLIGHT 4052 THEN DEPARTED WITH NO FURTHER INCIDENTS.
- [SDR VNAA0110011](https://openairdocs.org/sdr/VNAA0110011.md): Stall Warning · malfunctioned · Oct 16, 2001 · N426JS · Dorner DO328100 · Stall Warning System
  > DURING THE TAKEOFF ROLL, THE CREW RECEIVED AN ANGLE OF ATTACK CHIME AND FAILURE. ABORTED THE TAKEOFF. AS FLIGHT 4138 CLEARED THE RUNWAY THE MESSAGE CLEARED. THE CREW CONTACTED MAINTENANCE CONTROL AND WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4138 THE
- [SDR VNAA0109012](https://openairdocs.org/sdr/VNAA0109012.md): Starter Gen · failed · Sep 20, 2001 · N426JS · Dorner DO328100 · Starter-Generator
  > AT APPROXIMATELY 60 KNOTS THE CREW RECEIVED A LEFT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE STARTER GENERATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIR
- [SDR VNAA0108008](https://openairdocs.org/sdr/VNAA0108008.md): Valve · failed · Aug 15, 2001 · N426JS · Dorner DO328100 · Landing Gear System
  > ON APPROACH TO AZO, THE GEAR WAS SELECTED DOWN AND THE CREW RECEIVED NO GEAR INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND MANUALLY LOWERED THE GEAR. THE MAIN GEAR WAS GREEN BUT THE NOSE SHOWED IN TRANSIT. THE CREW DID A FLY BY TO ENSURE GE
- [SDR VNAA0108003](https://openairdocs.org/sdr/VNAA0108003.md): Warning System · malfunctioned · Aug 6, 2001 · N426JS · Dorner DO328100 · Central Warning
  > DURING THE TAKEOFF ROLL, THE CREW RECEIVED A TAKEOFF CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. THE CREW RESET THE SYSTEM AND ATTEMPTED ANOTHER TAKEOFF. FLIGHT 4156 DEPARTED WITH NO FURTHER INCIDENTS.
- [SDR VNAA0107013](https://openairdocs.org/sdr/VNAA0107013.md): Warning System · malfunctioned · Jul 9, 2001 · N426JS · Dorner DO328100 · Central Warning
  > DURING THE TAKEOFF ROLL, THE CREW RECEIVED A ENGINE MISCOMPARE CAS MESSAGE. THE CREW ABORTED TAKEOFF AND EXITED THE RUNWAY. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE MESSAGE CLEARED. FLIGHT 4043 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPAR
- [SDR VNAA0105004](https://openairdocs.org/sdr/VNAA0105004.md): Metering Valve · failed · May 8, 2001 · N426JS · Dorner DO328100 · Landing Gear Brake System
  > FLIGHT 4097 WAS TAXIING AND THE FIRST OFFICER'S LEFT HAND BRAKE WAS INEFFECTIVE AND THE CREW RETURNED TO THE GATE. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND BLED THE BRAKE METERING UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00
- [SDR VNAA0103019](https://openairdocs.org/sdr/VNAA0103019.md): Window · cracked · Mar 31, 2001 · N426JS · Dorner DO328100 · Flight Compartment Windows
  > DURING CLIMBOUT THE FLIGHT CREW REPORTED THAT THE FIRST OFFICERS SIDE WINDOW HAD CRACKED. THE FLIGHT CREW RETURNED TO THE FIELD AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE SIDE WINDOW IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 56-10-00. OPER
- [SDR VNAA0012030](https://openairdocs.org/sdr/VNAA0012030.md): Warning System · failed · Dec 30, 2000 · N426JS · Dorner DO328100 · Airfoil Anti/De-ice System
  > AFTER 10 MINUTES INTO THE FLIGHT, THE CREW RECEIVED AN AIRFOIL DEICE FAIL CAS MESSAGE. DISPATCH ADVISED THE CREW TO RETURN TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED THE VERTICAL LEADING EDGE ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-0
- [SDR VNAA0012025](https://openairdocs.org/sdr/VNAA0012025.md): Apu · failed · Dec 26, 2000 · N426JS · Dorner DO328100 · APU Oil System
  > FLIGHT 4145 WAS EVACUATED AT THE GATE DUE TO SMOKE IN CABIN. OUTSTATION MAINTENANCE INSPECTED AND FOUND THE AUXILIARY POWER UNIT WAS BURNING OIL. THE AUXILIARY UNIT WAS DEFERRED AND FLIGHT 4145 DEPARTED WITH A 103 MINUTE DELAY.
- [SDR VNAA0012009](https://openairdocs.org/sdr/VNAA0012009.md): Chip Detector · failed · Dec 9, 2000 · N426JS · Dorner DO328100 · Engine Oil Indicating System
  > AFTER DEPARTURE, THE CREW RECEIVED A LEFT HAND ENGINE CHIP DETECTOR LIGHT. MAINTENANCE CONTROL AND DISPATCH HAD FLIGHT 4012 RETURN TO DAY FOR MAINTENANCE. MAINTENANCE INSPECTED AND FOUND FUSS ON THE CHIP DETECTOR. MAINTENANCE CLEANED THE CHIP DETECTOR IN AC
- [SDR VNAA0010003](https://openairdocs.org/sdr/VNAA0010003.md): Brake Assy · malfunctioned · Oct 3, 2000 · N426JS · Dorner DO328100 · Landing Gear Brake System
  > THE CREW REPORTED THAT THE FIRST OFFICER''S RIGHT HAND BRAKE PEDAL WENT TO THE FLOOR WITHOUT A RESPONSE FROM THE BRAKE SYSTEM. MAINTENANCE INSPECTED AND BLED THE BRAKE SYSTEM IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-00. OPERATIONAL CHECKS WERE PER
- [SDR VNAA0007015](https://openairdocs.org/sdr/VNAA0007015.md): Computer · failed · Jul 26, 2000 · N426JS · Dorner DO328100 · Landing Gear Position and Warning
  > THE CREW REPORTED A SERIES OF PROXI FAIL MESSAGES. AFTER FOLLOWING THE QRH AND CHECKING THE CIRCUIT BREAKERS, THE CREW SELECTED THE GEAR HANDLE DOWN AND RECEIVED NO RESPONSE FROM THE GEAR. THE CREW DECLARED AN EMERGENCY, HAND PUMPED THE GEAR DOWN AND LANDED
- [SDR VNAA0007010](https://openairdocs.org/sdr/VNAA0007010.md): Brake · failed · Jul 13, 2000 · N426JS · Dorner DO328100 · Brake
  > AFTER BEING PUSHED BACK FROM THE GATE, THE CAPTAIN NOTICE THE BRAKES WERE INOPERATIVE. THE CREW RETURNED TO THE GATE. MAINTENANCE INSPECTED AND BLED THE BRAKES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-00. OPERATIONAL CHECKS WERE PERFORMED AND THE
- [SDR VNAA0005003](https://openairdocs.org/sdr/VNAA0005003.md): Control Box · failed · May 3, 2000 · N426JS · Dorner DO328100 · Brake Anti-Skid Section
  > THE CREW REPORTED THAT THE BRAKES WERE COMPLETELY INEFFECTIVE WHILE TAXIING. FLIGHT 4102 RETURNED TO THE GATE WHERE MAINTENANCE BLED THE BRAKES AND REPLACED THE ANTI-SKID CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS
- [SDR VNAA0004014](https://openairdocs.org/sdr/VNAA0004014.md): Brake · failed · Apr 8, 2000 · N426JS · Dorner DO328100 · Brake
  > AFTER DEPARTING THE GATE, THE CREW DISCOVERED THAT THE FIRST OFFICERS BRAKES WERE INEFFECTIVE. THE CREW RETURNED TO THE GATE WHERE MAINTENANCE, AFTER ARRIVING FROM PIT, INSPECTED AND BLED THE BRAKES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-00. OPE
- [SDR VNAA0004012](https://openairdocs.org/sdr/VNAA0004012.md): Pcu · failed · Apr 6, 2000 · N426JS · Dorner DO328100 · Propeller Synchronizer Section
  > WHILE CLIMBING THROUGH FLT 020, THE CREW RECEIVED AN INTERMITTENT RIGHT HAND PROPELLER LOW OIL PRESSURE CAS MESSAGE. REACHING FLT 100 THE MESSAGE REMAINED CONSTANT, THE CREW DECIDED TO RETURN TO THE FIELD. THE AIRCRAFT WAS FERRIED TO AKRON WHERE MAINTENANCE
- [SDR 20000413SH058](https://openairdocs.org/sdr/20000413SH058.md): Plate · cracked · Apr 4, 2000 · N426JS · Dorner DO328100 · Propeller Blade Section
  > DURING SEARCH INSPECTION, 4 EACH C-6066-1 PRELOAD PLATES WERE FOUND CRACKED. ONE EACH PRELOAD PLATE WAS CRACKED IN SUCH A MANNER THAT IT BROKE DURING INSPECTION. TIME SINCE LAST INSPECTION: 2,160:30 HOURS. (X)
- [SDR VNAA0003023](https://openairdocs.org/sdr/VNAA0003023.md): Brake · failed · Mar 24, 2000 · N426JS · Dorner DO328100 · Brake
  > THE FLIGHT CREW REPORTED THAT THE FIRST OFFICER''S BRAKES WERE NOT RESPONDING WHEN APPLIED. MAINTENANCE INSPECTED THE AIRCRAFT AND FERRIED THE AIRCRAFT TO PIT. THE FERRY FLIGHT WAS MADE WITHOUT INCIDENT. MAINTENANCE THEN BLED THE FIRST OFFICER''S BRAKES IN
- [SDR VNAA0003005](https://openairdocs.org/sdr/VNAA0003005.md): Bleed Valve · failed · Mar 6, 2000 · N426JS · Dorner DO328100 · Compressor Bleed Valve
  > DURING THE TAKEOFF ROLL, FLIGHT 4087, RECEIVED A RIGHT PACK OVER PRESSURE WARNING. THE FLIGHT CREW ABORTED THE TAKEOFF AND EXITED THE RUNWAY. THE WARNING MESSAGE HAD CLEARED AND ANOTHER TAKEOFF WAS ATTEMPTED WITH A RIGHT PACK OVER PRESSURE WARNING RESULTING
- [SDR VNAA9911009](https://openairdocs.org/sdr/VNAA9911009.md): Nl Probe · failed · Nov 12, 1999 · N426JS · Dorner DO328100 · Engine RPM Indicating System
  > DURING CLIMBOUT, THE FLIGHT CREW RECEIVED A CAS MESSAGE INDICATING AN ENGINE MISCOMPARE. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NL PROBE SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 77-14-0
- [SDR VNAA9910022](https://openairdocs.org/sdr/VNAA9910022.md): Brake Sys · reqd service · Oct 31, 1999 · N426JS · Dorner DO328100 · Landing Gear Brake System
  > DURING TAXI, THE FLIGHT CREW REPORTED THE FIRST OFFICERS' LEFT HAND BRAKE PEDAL HAD NO RESPONSE WHEN ACTIVATED. AIRCRAFT WAS FERRIED TO PIT. MAINTENANCE INSPECTED AND BLED THE FIRST OFFICERS' BRAKE SYSTEMS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-
- [SDR VNAA9903016](https://openairdocs.org/sdr/VNAA9903016.md): Fan · failed · Mar 17, 1999 · N426JS · Dorner DO328100 · Air Distribution Fan
  > DURING CLIMB AFTER TAKEOFF, THE CREW SMELLED AND NOTED SMOKE IN THE COCKPIT. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND FOUND THE FORWARD RECIRC FAN TO BE INOPERATIVE. MAINTENANCE DEFERRED THE FORWARD RECIRC
- [SDR VNAA9812004](https://openairdocs.org/sdr/VNAA9812004.md): Connector · damaged · Dec 6, 1998 · N426JS · Dorner DO328100 · Pitot/Static Anti-Ice System
  > A NR 1 PITOT HEAT FAIL WARNING MESSAGE ILLUMINATED, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT. THE FERRY FLIGHT WAS COMPLETED WITHOUT ANY PROBLEMS

Next page: https://openairdocs.org/deregistered/N426JS-2009-05-21/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 = 'N426JS' AND deregistration_id = 'N426JS-2009-05-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N426JS-2009-05-21/reports

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