N459PS, cancelled Jan 12, 2005

Service difficulty reports · 69

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR VNAA0401006Shim · failedDURING 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 Jan 10, 2004 · N459PS · Dorner DO328100 · Engine Oil System (Airframe Furnished)SDR 2004FA0000038Seal · leakingCAS MISCOMPARE MESSAGE AT 25000 FT. ALSO THE MOISTURE INDICATOR IS PINK. (WO NR 33910)Dec 19, 2003 · N459PS · Dorner DO328100 · Elevator Control SystemSDR VNAA0312003Boot · failedDURING 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 Dec 5, 2003 · N459PS · Dorner DO328100 · Airfoil Anti/De-ice SystemSDR VNAA0310020Power Supply · malfunctionedTHE 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 Oct 28, 2003 · N459PS · Dorner DO328100 · Emergency LightingSDR VNAA0310019Battery · failedTHE 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 WAOct 22, 2003 · N459PS · Dorner DO328100 · Emergency LightingSDR VNAA0308005Indicator · failedDURING 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 Aug 8, 2003 · N459PS · Dorner DO328100 · Weather Radar SystemSDR VNAA0307003Sensor · failedDURING 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.Jul 15, 2003 · N459PS · Dorner DO328100 · Pneumatic Indicating SystemSDR VNAA0305017Bleed Valve · failedDURING 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 DORNIEMay 26, 2003 · N459PS · Dorner DO328100 · Compressor Bleed ValveSDR VNAA0304005Proximity Sensor · failedON 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 MApr 9, 2003 · N459PS · Dorner DO328100 · Landing Gear Position and WarningSDR VNAA0303017A/C Pack · failedDURING 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.Mar 14, 2003 · N459PS · Dorner DO328100 · Cabin Cooling SystemSDR VNAA0302015Power Supply · failedTHE 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 SEFeb 16, 2003 · N459PS · Dorner DO328100 · Lighting SystemSDR VNAA0211029Bleed Valve · failedDURING 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 9Nov 26, 2002 · N459PS · Dorner DO328100 · Pneumatic SystemSDR VNAA0211027Limiter · failedDURING 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.Nov 25, 2002 · N459PS · Dorner DO328100 · Rudder Control SystemSDR VNAA0209030Battery · dischargedTHE 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 Sep 22, 2002 · N459PS · Dorner DO328100 · Emergency LightingSDR VNAA0209016Battery · overheatedAFTER 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 PERFORMEDSep 14, 2002 · N459PS · Dorner DO328100 · Battery/Charger SystemSDR VNAA0209006Battery · dischargedTHE 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 RELEASEDSep 5, 2002 · N459PS · Dorner DO328100 · Emergency LightingSDR VNAA0208027Battery · dischargedTHE 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 WAAug 19, 2002 · N459PS · Dorner DO328100 · Emergency LightingSDR VNAA0204026Generator · failedDURING 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 WEApr 29, 2002 · N459PS · Dorner DO328100 · Electrical Power SystemSDR VNAA0204025Generator · failedDURING 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 GENERATApr 29, 2002 · N459PS · Dorner DO328100 · Electrical Power SystemSDR VNAA0204024Flow Divider · failedSHORTLY 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. PIApr 27, 2002 · N459PS · Dorner DO328100 · Aircraft Fuel SystemSDR VNAA0204017Warning System · malfunctionedDURING 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.Apr 19, 2002 · N459PS · Dorner DO328100 · AC Indicating SystemSDR VNAA0204008SwitchWHILE 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 DApr 13, 2002 · N459PS · Dorner DO328100 · Communications SystemSDR VNAA0204003Controller · malfunctionedFORTY-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 MApr 10, 2002 · N459PS · Dorner DO328100 · Cabin Pressure ControllerSDR VNAA0203036Panel · failedAS 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. OPEMar 21, 2002 · N459PS · Dorner DO328100 · AC Power Distribution SystemSDR VNAA0203035Ecu · failedDURING 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 AMar 21, 2002 · N459PS · Dorner DO328100 · Engine Fuel and ControlSDR VNAA0203034Iru · malfunctionedAS 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 CREMar 21, 2002 · N459PS · Dorner DO328100 · Inertial Guidance SystemSDR VNAA0203033EcuDURING 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.Mar 21, 2002 · N459PS · Dorner DO328100 · Electrical Power SystemSDR VNAA0203032Connector · dirtyDURING 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 AMar 20, 2002 · N459PS · Dorner DO328100 · Fuel Control/Turbine EnginesSDR VNAA0112020Door · failedWHILE 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 TDec 28, 2001 · N459PS · Dorner DO328100 · DoorsSDR VNAA0111011Generator · failedDURING 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 DORNNov 28, 2001 · N459PS · Dorner DO328100 · Electrical Power SystemSDR VNAA0110021Pseu · failed25 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 31-00-0Oct 29, 2001 · N459PS · Dorner DO328100 · Indicating/Recording SystemSDR VNAA0108010Valve · failedWHILE 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 TEMPERATAug 18, 2001 · N459PS · Dorner DO328100 · Air Conditioning SystemSDR VNAA0108007BrakeDURING 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.Aug 13, 2001 · N459PS · Dorner DO328100 · Navigation SystemSDR VNAA0108006Warning System · malfunctionedDURING 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.Aug 13, 2001 · N459PS · Dorner DO328100 · Air Collision Avoidance SystemSDR VNAA0106001A/C Pack · failedTHE 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.Jun 4, 2001 · N459PS · Dorner DO328100 · Cabin Cooling SystemSDR VNAA0103011Stick Shaker · failedAFTER 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 FOMar 12, 2001 · N459PS · Dorner DO328100 · Stall Warning SystemSDR VNAA0012027Power Supply · failedTHE 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 PERDec 27, 2000 · N459PS · Dorner DO328100 · Emergency LightingSDR VNAA0011001Bleed Valve · failedWHILE 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 INov 2, 2000 · N459PS · Dorner DO328100 · Compressor Bleed ValveSDR VNAA0010018Sensor · failedDURING 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 ANOOct 28, 2000 · N459PS · Dorner DO328100 · Stall Warning SystemSDR VNAA0010009Bleed Valve · failedFLIGHT 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 71-00-0Oct 10, 2000 · N459PS · Dorner DO328100 · Compressor Bleed ValveSDR VNAA0009024Warning System · activatedDURING 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 ATTESep 28, 2000 · N459PS · Dorner DO328100 · Central WarningSDR VNAA0009022Receiver · failedFLIGHT 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 THESep 23, 2000 · N459PS · Dorner DO328100 · Visual Omnirange (VOR) SystemSDR VNAA0009020Control Valve · failedFLIGHT 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 Sep 22, 2000 · N459PS · Dorner DO328100 · Airfoil Anti/De-ice SystemSDR VNAA0009010Warning System · activatedTHE 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.Sep 14, 2000 · N459PS · Dorner DO328100 · Central WarningSDR VNAA0009007Bulb · failedTHE 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.Sep 12, 2000 · N459PS · Dorner DO328100 · Emergency LightingSDR VNAA0007004Bulb · failedWHILE 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 APJul 6, 2000 · N459PS · Dorner DO328100 · Landing Gear Position and WarningSDR VNAA0006013Warning System · false activationTHE 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, TJun 24, 2000 · N459PS · Dorner DO328100 · Central WarningSDR VNAA0004022Stick Shaker · failedDURING 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 ANApr 23, 2000 · N459PS · Dorner DO328100 · Altimeter, Barometric/EncoderSDR VNAA0004002Door · damagedDURING 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 INSPEApr 2, 2000 · N459PS · Dorner DO328100 · Emergency ExitsSDR VNAA9912010Ecu · failedDURING 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 MAINTENANDec 9, 1999 · N459PS · Dorner DO328100 · Fuel Control/Turbine Engines
Back to N459PS, cancelled Jan 12, 2005