# Service difficulty reports: N459PS, cancelled Jan 12, 2005

A list on [N459PS, cancelled Jan 12, 2005](https://openairdocs.org/deregistered/N459PS-2005-01-12.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 · 69 reports

- [SDR VNAA0401006](https://openairdocs.org/sdr/VNAA0401006.md): Shim · failed · Jan 10, 2004 · N459PS · Dorner DO328100 · Engine Oil System (Airframe Furnished)
  > DURING FLIGHT, THE CREW RECEIVED A LEFT HAND OIL PRESSURE HIGH INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REMOVED A SHIM FROM THE LEFT HAND OIL PRESSURE REGULATOR IN ACCORDANCE WITH DOENIER MAINTENANCE MANUAL 79-00-00. OPERATIONAL CHECKS WERE
- [SDR 2004FA0000038](https://openairdocs.org/sdr/2004FA0000038.md): Seal · leaking · Dec 19, 2003 · N459PS · Dorner DO328100 · Elevator Control System
  > CAS MISCOMPARE MESSAGE AT 25000 FT. ALSO THE MOISTURE INDICATOR IS PINK. (WO NR 33910)
- [SDR VNAA0312003](https://openairdocs.org/sdr/VNAA0312003.md): Boot · failed · Dec 5, 2003 · N459PS · Dorner DO328100 · Airfoil Anti/De-ice System
  > DURING FLIGHT, THE CREW RECEIVED A LEFT HAND MIDDLE LEADING EDGE BOOT FAILING IN ALL MODES AND DIVERTED TO DAY. MAINTENANCE INSPECTED AND PATCHED THE LEFT HAND MIDDLE LEADING EDGE DE-ICE BOOT IN ACCORDANCE WITH SMP. OPERATIONAL CHECKS WERE PERFORMED AND THE
- [SDR VNAA0310020](https://openairdocs.org/sdr/VNAA0310020.md): Power Supply · malfunctioned · Oct 28, 2003 · N459PS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT ON ENGINE START THE EMERGENCY LIGHTS ROW 7, 8, & 9 GO OUT. MAINTENANCE SWAPPED POWER SUPPLIES 6LK & 7LK. OPERATION OF THE SYSTEM WAS CHECKED IN ACCORDANCE WITH DORNIER MANUAL 33-00-00 AND NO FAULTS FOUND. THE AIRCRAFT WAS RELEASED TO
- [SDR VNAA0310019](https://openairdocs.org/sdr/VNAA0310019.md): Battery · failed · Oct 22, 2003 · N459PS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 5-10 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WA
- [SDR VNAA0308005](https://openairdocs.org/sdr/VNAA0308005.md): Indicator · failed · Aug 8, 2003 · N459PS · Dorner DO328100 · Weather Radar System
  > DURING FLIGHT, THE WEATHER RADAR FAILED INTERMITTENTLY AND THE CREW RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE WEATHER RADAR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED
- [SDR VNAA0307003](https://openairdocs.org/sdr/VNAA0307003.md): Sensor · failed · Jul 15, 2003 · N459PS · Dorner DO328100 · Pneumatic Indicating System
  > DURING CRUISE FLIGHT THE FLIGHT CREW EXPERIENCED STATIC ON BOTH VHF RADIOS AND A FAILING LEFT HIGH PRESSURE BLEED VALVE. AFTER CONFERING WITH MAINTENANCE CONTROL THE CREW DIVERTED TO DAYTON. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT.
- [SDR VNAA0305017](https://openairdocs.org/sdr/VNAA0305017.md): Bleed Valve · failed · May 26, 2003 · N459PS · Dorner DO328100 · Compressor Bleed Valve
  > DURING CLIMB OUT FROM PIT, THE CREW REPORTED THE RIGHT HAND HIGH PRESSURE BLEED VALVE FAILED AND THEN HAD A POWER LEVER SPLIT AND RETURNED TO PIT. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE THEN TRIMMED THE RIGHT HAND ENGINE IN ACCORDANCE WITH DORNIE
- [SDR VNAA0304005](https://openairdocs.org/sdr/VNAA0304005.md): Proximity Sensor · failed · Apr 9, 2003 · N459PS · Dorner DO328100 · Landing Gear Position and Warning
  > ON APPROACH, THE CREW RECEIVED A PROXI SYSTEM FAIL INDICATION AND PERFORMED A GO-AROUND. ON THE SECOND APPROACH, THE LANDING WAS NORMAL AND FLIGHT 4009 LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE THEN INSPECTED THE PROXI SYSTEM IN ACCORDANCE WITH DORNIER M
- [SDR VNAA0303017](https://openairdocs.org/sdr/VNAA0303017.md): A/C Pack · failed · Mar 14, 2003 · N459PS · Dorner DO328100 · Cabin Cooling System
  > DURING TAKEOFF, THE RIGHT HAND PACK FAILED AND THE CREW ABORTED TAKEOFF. THE CREW THEN RESET THE SYSTEM AND WERE CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4019 THEN DEPARTED WITH NO FURTHER INCIDENTS.
- [SDR VNAA0302015](https://openairdocs.org/sdr/VNAA0302015.md): Power Supply · failed · Feb 16, 2003 · N459PS · Dorner DO328100 · Lighting System
  > THE CREW REPORTED THE EMERGENCY AND BACK UP BATTERIES FAIL TO TEST. MAINTENANCE INSPECTED AND REPLACED BOTH EMERGENCY POWER SUPPLIES IN ACCORDANCE WITH DONIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SE
- [SDR VNAA0211029](https://openairdocs.org/sdr/VNAA0211029.md): Bleed Valve · failed · Nov 26, 2002 · N459PS · Dorner DO328100 · Pneumatic System
  > DURING TAKE OFF, THE CREW RECEIVED A BLEED SHUT OFF VALVE CAS MESSAGE AND ABORTED TAKE OFF. AFTER THE AIRCRAFT CLEARED THE RUNWAY, THE CREW CYCLED THE BLEED VALVE AND THE MESSAGE CLEARED. FLIGHT 9424 WAS THEN CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND FLIGHT 9
- [SDR VNAA0211027](https://openairdocs.org/sdr/VNAA0211027.md): Limiter · failed · Nov 25, 2002 · N459PS · Dorner DO328100 · Rudder Control System
  > DURING CLIMB OUT, THE CREW RECEIVED A RUDDER NOT LIMITED ABOVE 165 KNOTS MESSAGE AND RETURNED TO RIC. THE TOWER DECLARED AN EMERGENCY AND FLIGHT 4084 LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE DEFERRED THE RUDDER LIMITER, 27-4 C.
- [SDR VNAA0209030](https://openairdocs.org/sdr/VNAA0209030.md): Battery · discharged · Sep 22, 2002 · N459PS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 7 TO 9 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT
- [SDR VNAA0209016](https://openairdocs.org/sdr/VNAA0209016.md): Battery · overheated · Sep 14, 2002 · N459PS · Dorner DO328100 · Battery/Charger System
  > AFTER TAKEOFF, THE CREW RECEIVED A NR 2 MAIN BATTERY OVERHEAT CAS MESSAGE AND RETURNED TO BNA. MAINTENANCE WAS DISPATCHED, INSPECTED, AND REPLACED THE NR 2 MAIN BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED
- [SDR VNAA0209006](https://openairdocs.org/sdr/VNAA0209006.md): Battery · discharged · Sep 5, 2002 · N459PS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 6 TO 9 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 VNAA0208027](https://openairdocs.org/sdr/VNAA0208027.md): Battery · discharged · Aug 19, 2002 · N459PS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT THE ROW 6 TO 9 OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WA
- [SDR VNAA0204026](https://openairdocs.org/sdr/VNAA0204026.md): Generator · failed · Apr 29, 2002 · N459PS · Dorner DO328100 · Electrical Power System
  > DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND GENERATOR AND BUS POWER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WE
- [SDR VNAA0204025](https://openairdocs.org/sdr/VNAA0204025.md): Generator · failed · Apr 29, 2002 · N459PS · Dorner DO328100 · Electrical Power System
  > DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKE OFF. THE CREW RESET THE GENERATOR AND IT CONTINUED TO WORK DURING THE TAXI BACK TO THE GATE. MAINTENANCE CONTROL HAD OUTSTATION MAINTENANCE INSPECT THE RIGHT HAND GENERAT
- [SDR VNAA0204024](https://openairdocs.org/sdr/VNAA0204024.md): Flow Divider · failed · Apr 27, 2002 · N459PS · Dorner DO328100 · Aircraft Fuel System
  > SHORTLY AFTER TAKE OFF, THE CREW HAD A POWER SPLIT AND THE LEFT HAND ENGINE FUEL SHOWED 500 POUNDS PER HOUR MORE THAN THE RIGHT HAND. THE CREW NOTICED A FLUID OFF THE LEFT HAND ENGINE, DECLARED AN EMERGENCY, AND RETURNED TO PWM WITH NO FURTHER INCIDENTS. PI
- [SDR VNAA0204017](https://openairdocs.org/sdr/VNAA0204017.md): Warning System · malfunctioned · Apr 19, 2002 · N459PS · Dorner DO328100 · AC Indicating System
  > DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKEOFF. AFTER LEAVING THE RUNWAY, THE CREW RESET THE GENERATOR AND ATTEMPTED ANOTHER TAKEOFF. FLIGHT 4018 THEN DEPARTED WITH NO FURTHER INCIDENTS.
- [SDR VNAA0204008](https://openairdocs.org/sdr/VNAA0204008.md): Switch · Apr 13, 2002 · N459PS · Dorner DO328100 · Communications System
  > WHILE ENROUTE, THE CREW CALLED MAINTENANCE CONTROL AND STATED THE FIRST OFFICER'S MICROPHONE'S PUSH TO TALK SWITCH WAS NOT WORKING. FLIGHT 4169 DIVERTED TO CAK WHO HAD THE PART IN STOCK. MAINTENANCE THEN INSPECTED AND REPLACED THE SWITCH IN ACCORDANCE WITH D
- [SDR VNAA0204003](https://openairdocs.org/sdr/VNAA0204003.md): Controller · malfunctioned · Apr 10, 2002 · N459PS · Dorner DO328100 · Cabin Pressure Controller
  > FORTY-FIVE MINUTES OUT OF DCA, THE CREW RECEIVED A CABIN ALTITUDE PRESSURE WARNING INDICATION. THE PRESSURIZATION WAS UNCONTROLLABLE. THE CREW DECLARED AN EMERGENCY, FOLLOWED THE QUICK REFERENCE HANDBOOK, AND DESCENDED TO 10,000 FEET. THE CREW SWITCHED TO M
- [SDR VNAA0203036](https://openairdocs.org/sdr/VNAA0203036.md): Panel · failed · Mar 21, 2002 · N459PS · Dorner DO328100 · AC Power Distribution System
  > AS THE AIRCRAFT WAS IN ROTATION, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL MESSAGE. THE CREW TOOK OFF AND CIRCLED THE FIELD AND LANDED. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPE
- [SDR VNAA0203035](https://openairdocs.org/sdr/VNAA0203035.md): Ecu · failed · Mar 21, 2002 · N459PS · Dorner DO328100 · Engine Fuel and Control
  > DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL INDICATION AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND REPLACED THE BUS POWER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED A
- [SDR VNAA0203034](https://openairdocs.org/sdr/VNAA0203034.md): Iru · malfunctioned · Mar 21, 2002 · N459PS · Dorner DO328100 · Inertial Guidance System
  > AS THE CREW ADVANCED THE POWER LEVERS, THE INERTIAL REFERENCE SYSTEM'S AUXILIARY SYSTEM FAILED AND THE CREW ABORTED TAKEOFF. THE FLIGHT THEN RETURNED TO THE GATE. MAINTENANCE ADVISED THE CREW TO TURN OFF ALL POWER AND ALLOW THE SYSTEM TO RESET. WHEN THE CRE
- [SDR VNAA0203033](https://openairdocs.org/sdr/VNAA0203033.md): Ecu · Mar 21, 2002 · N459PS · Dorner DO328100 · Electrical Power System
  > DURING TAKE OFF, THE CREW RECEIVED A ECU FAIL CAS MESSAGE AND ABORTED TAKE OFF. THE AIRCRAFT CLEARED THE RUNWAY AND THE MESSAGE CLEARED BY ITSELF. THE CREW ATTEMPTED ANOTHER TAKE OFF AND DEPARTED WITH NO FURTHER INCIDENTS.
- [SDR VNAA0203032](https://openairdocs.org/sdr/VNAA0203032.md): Connector · dirty · Mar 20, 2002 · N459PS · Dorner DO328100 · Fuel Control/Turbine Engines
  > DURING TAKEOFF THE FLIGHT CREW RECEIVED A LEFT ENGINE ELECTRONIC CONTROL UNIT FAIL WARNING MESSAGE. AFTER ABORTING THE TAKEOFF A LEFT GENERATOR FAIL AND RIGHT HX FAN FAIL MESSAGE ALSO ILLUMINATED. THE FLIGHT CREW NOTED A MIST IN THE CABIN WHICH DISSIPATED A
- [SDR VNAA0112020](https://openairdocs.org/sdr/VNAA0112020.md): Door · failed · Dec 28, 2001 · N459PS · Dorner DO328100 · Doors
  > WHILE IN CRUISE, THE CREW RECEIVED A RED WARNING PANEL DOOR LIGHT. THE SYSTEMS PAGE SHOWED IT WAS THEMAIN CABIN DOOR. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO TRI. OUTSTATION MAINTENANCE FOUND NO DEFECTS SO THE AIRCRAFT WAS FERRIED T
- [SDR VNAA0111011](https://openairdocs.org/sdr/VNAA0111011.md): Generator · failed · Nov 28, 2001 · N459PS · Dorner DO328100 · Electrical Power System
  > DURING TAKE OFF, THE CREW RECEIVED A DECREASE IN TORQUE INDICATION AND ABORTED TAKE OFF. WHILE PULLING ONTO THE TAXI WAY, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND GENERATOR IN ACCORDANCE WITH DORN
- [SDR VNAA0110021](https://openairdocs.org/sdr/VNAA0110021.md): Pseu · failed · Oct 29, 2001 · N459PS · Dorner DO328100 · Indicating/Recording System
  > 25 MINUTES AFTER DEPARTING PIT, THE CREW RECEIVED A PROXI SYSTEM FAIL INDICATION. THE CREW CONTACTED MAINTENANCE CONTROL AND WERE ADVISED TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PSEU UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-0
- [SDR VNAA0108010](https://openairdocs.org/sdr/VNAA0108010.md): Valve · failed · Aug 18, 2001 · N459PS · Dorner DO328100 · Air Conditioning System
  > WHILE CLIMBING OUT FROM PIT, THE CREW NOTICED THE CABIN TEMPERATURE WAS 95 DEGREES. THE CREW TRIED THE TEMPERATURE CONTROL VALVE IN BOTH MANUAL AND AUTO MODES WITH NO EFFECT. THE CREW DECIDED TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE TEMPERAT
- [SDR VNAA0108007](https://openairdocs.org/sdr/VNAA0108007.md): Brake · Aug 13, 2001 · N459PS · Dorner DO328100 · Navigation System
  > DURING THE TAKE OFF ROLL, THE CREW RECEIVED A HIGH BRAKE TEMPERATURE CAS MESSAGE. THE CREW ABORTED TAKE OFF AND EXITTED THE RUNWAY AND ALLOWED THE BRAKES TO COOL. FLIGHT 4092 WAS CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS.
- [SDR VNAA0108006](https://openairdocs.org/sdr/VNAA0108006.md): Warning System · malfunctioned · Aug 13, 2001 · N459PS · Dorner DO328100 · Air Collision Avoidance System
  > DURING THE TAKEOFF ROLL, THE CREW RECEIVED A TCAS FAIL MESSAGE. THE CREW ABORTED TAKEOFF AND WHILE EXITING THE RUNWAY THE MESSAGE CLEARED. FLIGHT 4092 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT.
- [SDR VNAA0106001](https://openairdocs.org/sdr/VNAA0106001.md): A/C Pack · failed · Jun 4, 2001 · N459PS · Dorner DO328100 · Cabin Cooling System
  > THE CREW REPORTED A ELECTRIC BURNING SMELL. MAINTENANCE INSPECTED AND REPLACED THE COLD AIR UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA0103011](https://openairdocs.org/sdr/VNAA0103011.md): Stick Shaker · failed · Mar 12, 2001 · N459PS · Dorner DO328100 · Stall Warning System
  > AFTER THE FLIGHT CREW PERFORMED THE STALL STICK PUSHER TEST THE ELEVATOR CONTROL WOULD NOT MOVE PAST NEUTRAL FROM THE NOSE DOWN POSITION. MAINTENANCE INSPECTED AND FOUND THE STICK PUSHER ENGAGED. MAINTENANCE DISCONNECTED AND SECURED THE STICK PUSHER UNIT FO
- [SDR VNAA0012027](https://openairdocs.org/sdr/VNAA0012027.md): Power Supply · failed · Dec 27, 2000 · N459PS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY WILL NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE FORWARD SUPPLY, FERRIED THE AIRCRAFT TO CVG AND REPLACED THE AFT SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL TESTS WERE PER
- [SDR VNAA0011001](https://openairdocs.org/sdr/VNAA0011001.md): Bleed Valve · failed · Nov 2, 2000 · N459PS · Dorner DO328100 · Compressor Bleed Valve
  > WHILE ON THE ACTIVE RUNWAY, FLIGHT 4098 RECEIVED A BLEED SHUT OFF VALVE FAIL CAS MESSAGE. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND LOW PRESSURE BLEED VALVE I
- [SDR VNAA0010018](https://openairdocs.org/sdr/VNAA0010018.md): Sensor · failed · Oct 28, 2000 · N459PS · Dorner DO328100 · Stall Warning System
  > DURING TAKEOFF, THE CREW RECEIVED A RIGHT SHAKER FAIL, RIGHT PUSHER FAIL, AND A RIGHT ANGLE OF ATTACK FAIL. THE CREW ABORTED TAKEOFF. WHEN FLIGHT 4135 CLEARED THE RUNWAY, THE MESSAGES CLEARED. THE CREW CONTACTED MAINTENANCE CONTROL AND WERE CLEARED FOR ANO
- [SDR VNAA0010009](https://openairdocs.org/sdr/VNAA0010009.md): Bleed Valve · failed · Oct 10, 2000 · N459PS · Dorner DO328100 · Compressor Bleed Valve
  > FLIGHT 4147 WAS EN ROUTE AND DEVELOPED A RIGHT HAND TORQUE PROBLEM. THE CREW CONTACTED MAINTENANCE CONTROL AND DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE INTERCOMPRESSION BLEED VALVE IN ACCORDANCE WITH 71-00-0
- [SDR VNAA0009024](https://openairdocs.org/sdr/VNAA0009024.md): Warning System · activated · Sep 28, 2000 · N459PS · Dorner DO328100 · Central Warning
  > DURING TAKEOFF, THE CREW RECEIVED A PUSHER FAIL CAS MESSAGE. FLIGHT 4132 ABORTED TAKEOFF. AFTER THE AIRCRAFT CLEARED THE RUNWAY AND THE CREW DID A SYSTEMS CHECK AND GROUND POWER RUN THERE WAS NO MESSAGES AND THE AIRCRAFT WAS RELEASED FOR ANOTHER TAKEOFF ATTE
- [SDR VNAA0009022](https://openairdocs.org/sdr/VNAA0009022.md): Receiver · failed · Sep 23, 2000 · N459PS · Dorner DO328100 · Visual Omnirange (VOR) System
  > FLIGHT 4135 PIT TO SBN DECLARED AN EMERGENCY DUE TO THE CREW HAVING TO DEVIATE FROM THE OPERATIONS SPECIFICATIONS. THE AIRCRAFT HAD A LOCALIZER RECEIVER FAIL AND BOTH RECEIVERS WERE ERRATIC. THE ADF ON THIS AIRCRAFT WAS DEFFERRED. THE CREW COULD NOT USE THE
- [SDR VNAA0009020](https://openairdocs.org/sdr/VNAA0009020.md): Control Valve · failed · Sep 22, 2000 · N459PS · Dorner DO328100 · Airfoil Anti/De-ice System
  > FLIGHT 4060 WAS EN ROUTE TO CAE AND HAD AN AIRFOIL DE-ICE FAIL. FLIGHT 4060 WAS IN ICING CONDITIONS AND WAS INSTRUCTED TO RETURN TO PIT FOR MAINTENANCE. MAINTENANCE INSPECTED AND REPLACED THE EJECTOR FLOW CONTROL VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE
- [SDR VNAA0009010](https://openairdocs.org/sdr/VNAA0009010.md): Warning System · activated · Sep 14, 2000 · N459PS · Dorner DO328100 · Central Warning
  > THE CREW ABORTED TAKEOFF DUE TO A PUSHER FAIL CAS MESSAGE. UPON CLEARING THE RUNWAY THE MESSAGE CLEARED AND FLIGHT 4145 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4145 DEPARTED WITHOUT ANY FURTHER INCIDENT.
- [SDR VNAA0009007](https://openairdocs.org/sdr/VNAA0009007.md): Bulb · failed · Sep 12, 2000 · N459PS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY LIGHT IN THE LAVATORY WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE BULB IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA0007004](https://openairdocs.org/sdr/VNAA0007004.md): Bulb · failed · Jul 6, 2000 · N459PS · Dorner DO328100 · Landing Gear Position and Warning
  > WHILE ON APPROACH AFTER EXTENDING THE GEAR, THE CREW RECEIVED TWO OUT OF THREE GREEN LIGHTS. AFTER CONTACTING MAINTENANCE CONTROL IT WAS AGREED IT WAS AN INDICATION PROBLEM, THE LIGHT WAS OUT. THE AIRCRAFT WAS FLOWN TO WHEELING THEN CAME BACK TO SHOOT THE AP
- [SDR VNAA0006013](https://openairdocs.org/sdr/VNAA0006013.md): Warning System · false activation · Jun 24, 2000 · N459PS · Dorner DO328100 · Central Warning
  > THE CREW RECEIVED A MOMENTARY RT STICK SHAKER FAIL CAS MESSAGE AND ABORTED THE TAKE OFF, EXITED THE RUNWAY, AND CONTACTED MAINTENANCE CONTROL AND WAS ADVISED IF THE MESSAGE DID NOT STAY ON OR COME BACK, CONTINUE THE FLIGHT. THE CREW RE-ENTERED THE RUNWAY, T
- [SDR VNAA0004022](https://openairdocs.org/sdr/VNAA0004022.md): Stick Shaker · failed · Apr 23, 2000 · N459PS · Dorner DO328100 · Altimeter, Barometric/Encoder
  > DURING THE TAKEOFF ROLL, FLIGHT 4088 EXPERIENCED A AOA MISCOMPARE, AOA FAIL, AND RIGHT HAND PUSHER FAIL CAS MESSAGES. THE CREW ABORTED TAKEOFF AND THE MESSAGES HAD CLEARED BEFORE THEY WERE OFF THE RUNWAY. THE CREW CONTACTED DISPATCH AND STATION OPERATIONS AN
- [SDR VNAA0004002](https://openairdocs.org/sdr/VNAA0004002.md): Door · damaged · Apr 2, 2000 · N459PS · Dorner DO328100 · Emergency Exits
  > DURING PREFLIGHT, THE CREW NOTICED THAT THE EMERGENCY DOOR AT THE 1 D & F SEAT POSITION HAD APPEARED TO HAVE BEEN TAMPERED WITH FROM THE OUTSIDE. THE CREW CONTINUED THE PREFLIGHT AND FOUND NOTHING ELSE OUT OF PLACE OR SUSPICIOUS. OUTSTATION MAINTENANCE INSPE
- [SDR VNAA9912010](https://openairdocs.org/sdr/VNAA9912010.md): Ecu · failed · Dec 9, 1999 · N459PS · Dorner DO328100 · Fuel Control/Turbine Engines
  > DURING TAKEOFF, THE RIGHT ELECTRONIC ENGINE CONTROL UNIT FAILED. THE CREW ABORTED TAKEOFF AND CLEARED THE RUNWAY. MAINTENANCE INSPECTED AND CLEANED THE ELECTRONIC ENGINE CONTROL UNIT AND INTERCOMP BLEED VALVE CANNON PLUGS IN ACCORDANCE WITH DORNIER MAINTENAN

Next page: https://openairdocs.org/deregistered/N459PS-2005-01-12/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 = 'N459PS' AND deregistration_id = 'N459PS-2005-01-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N459PS-2005-01-12/reports

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