N460PS, cancelled Jan 25, 2005
Service difficulty reports · 48
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 = 'N460PS' AND deregistration_id = 'N460PS-2005-01-25' 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.
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 = 'N460PS' AND deregistration_id = 'N460PS-2005-01-25' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR VNAA0310010Control Panel · failedDURING TAKEOFF, THE CREW RECEIVED A LT GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FORSDR VNAA0308022Battery · dischargedTHE CREW REPORTED THAT THE FIRST ROW OF EMERGENCY FLOOR LIGHTING WAS 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 WASSDR VNAA0302027Pressure Switch · failedDURING FLIGHT, THE CREW RECEIVED A RIGHT HAND PROP OIL PRESSURE LOW CAS MESSAGE. ALL OTHER ENGINE INDICATIONS WERE NORMAL AND WITH MAINTENANCE CONTROL, CONCLUDED THERE WAS AN INDICATION PROBLEM. THE CREW REQUESTED PRIORITY HANDLING FROM PHL ATC THEN DIVERTEDSDR VNAA0302021Valve · failedEN ROUTE, THE CREW RECEIVED A EMERGENCY PARKING BRAKE CAS MESSAGE AND DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCSDR VNAA0210004Battery · dischargedTHE CREW REPORTED THAT THE LAST ROW OF EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASSDR VNAA0209034Battery · dischargedTHE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVSDR VNAA0208031Battery · dischargedTHE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 9 TO 12 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK POSITION. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR VNAA0208006Battery · dischargedTHE CREW REPORTED THAT THE EMERGENCY LIGHT AT ROW 11A WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFSDR VNAA0207014Wire · failedDURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND FOUND A TERMINAL WIRE CREATING A LOOSE CONNECTION. MAINTENANCE REPAIRED THE WIRE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OSDR VNAA0207003Control Panel · failedAFTER THE PASSENGERS HAD BEEN BOARDED, HALFWAY THROUGH THE PREFLIGHT BRIEFING SMOKE BEGAN FORMING IN THE CABIN. THE FIRST OFFICER EVACUATED THE PASSENGERS AND THEN THE FLIGHT ATTENDANT. THE APU GENERATOR HAD FAILED, THUS CAUSING THE HX FAN TO NOT OPERATE WHISDR VNAA0206012Connector · dirtyDURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND ENGINE CONTROL UNIT FAIL AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND CLEANED THE ENGINE CONTROL UNIT CANNON PLUG IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND TSDR VNAA0206004Sensor · failedDURING CLIMBOUT, THE CREW RECEIVED A LEFT HAND DC GENERATOR FAIL CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE HALL EFFECT SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCSDR VNAA0201008Lead · frayedDURING CLIMB, THE CREW RECEIVED A RIGHT HAND PROPELLER FAIL MESSAGE AND RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND FOUND A FRAYED PROP DE-ICE LEAD AND REPAIRED IT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL TEST WERE PERFORMED ASDR VNAA0112008Restrictor Valve · failedDURING CLIMBOUT, THE CREW RECEIVED A PACK OVERPRESSURE INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RESTRICTOR FOR THE RIGHT HAND OVERPRESSURE SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00. OPERATIONAL CHECKS WERE PESDR VNAA0109006Windshield · failedAFTER DEPARTING TYS, THE CREW RECEIVED A RIGHT HAND WINDSHIELD HEAT FAIL CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THEN CALLED DISPATCH. DUE TO WEATHER SURROUNDING PHL THE CREW DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RISDR VNAA0109003IndicatorDURING THE TAKE OFF ROLL, THE CREW RECEIVED A LEFT HAND INBOARD BRAKE TEMPERATURE MESSAGE AND ABORTEDTAKE OFF. THE CREW RETURNED TO THE GATE AND MAINTENANCE PERFORMED A MAINTENANCE FUNCTION AND MEL'D THE INDICATOR. THE ACTUAL BRAKE TEMPERATURE WAS 32C. SDR VNAA0107024Switch · out of adjAFTER DEPARTING PIT, THE CREW RECEIVED A GROUND/AIR DOOR OPEN INDICATION ON THE RED WARNING PANEL. FLIGHT 4141 RETURNED TO PIT WHERE MAINTENANCE INSPECTED AND ADJUSTED THE MICROSWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKSSDR VNAA0105021Bleed Valve · failedDURING CLIMBOUT THE CREW RECEIVED A RIGHT HAND BLEED VALVE FAIL CAS MESSAGE. THE CREW CYCLED THE SYSTEM SEVERAL TIMES THEN CALLED MAINTENANCE CONTROL. THE CREW WAS INSTRUCTED TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND LOW PRESSURE BSDR VNAA0105008Smoke · detectedDURING TAXI TO THE RUNWAY, THE FLIGHT ATTENDANT NOTIFIED THE CAPTAIN THERE WAS SMOKE IN THE CABIN. APPROXIMATELY 10 TO 15 SECONDS LATER THE CREW RECEIVED A LAV SMOKE CAS MESSAGE. THE CREW IMMEDIATELY FOLLOWED THE QUICK REFERENCE HANDBOOK AND EVACUATED THE PLSDR VNAA0104008Light · inoperativeDURING DESCENT, FLIGHT 4065 HAD NO LEFT HAND GEAR DOWN INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CONFIRMED THAT THE BULB WAS INOPERABLE. FLIGHT 4065 DID A GO AROUND AND HAD ATC CONFIRM GEAR WAS DOWN. FLIGHT 4065 EXECUTED THE LANDING WITSDR VNAA0104007Battery · overheatedWHILE EN ROUTE FROM PIT TO AZO, THE CREW RECEIVED A BATTERY OVERHEAT INDICATION ON THE RED WARNING PANEL. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CONTACTED MAINTENANCE CONTROL. THE CREW REPORTED THAT THE FLIGHT WOULD DIVERT INTO CAK. WHILE ON APPSDR VNAA0104006Switch · faultyDURING THE TAKEOFF ROLL THE FLIGHT CREW RECEIVED A RIGHT ELECTRONIC ENGINE CONTROL FAIL MESSAGE. THE FLIGHT CREW ABORTED THE TAKEOFF AND EXITED THE RUNWAY WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT CONDITION LEVER MICROSWITCHSDR VNAA0104003Bleed Valve · failedAS THE FLIGHT CREW APPLIED TAKEOFF POWER THE RIGHT ELECTRONIC ENGINE CONTROL UNIT WOULD FAIL. THE FLIGHT CREW EXITED THE RUNWAY WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT ENGINE INTERCOMPRESSOR BLEED VAVLE IN ACCORDANCE WITH DORNIER MAINTSDR VNAA0103003A/C Pack · failedWHILE PARKED AT THE GATE THE FLIGHT CREW REPORTED THE RIGHT ENVIROMENTAL UNIT FAILED AND SMOKE ENTERED THE CABIN. MAINTENANCE INSPECTED AND FERRIED THE AIRCRAFT TO DAY. UPON ARRIVAL IN DAY MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE SDR VNAA0101002Switch · failedDURING THE TAKEOFF ROLL, THE CREW RECEIVED A RIGHT HAND FUEL PRESSURE LOW LIGHT ILLUMINATION AND THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. FLIGHT 4070 WAS CANCELED. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED THE ENGINE SDR VNAA0101001Warning Light · illuminatedDURING THE TAKEOFF ROLL, THE CREW RECEIVED A RIGHT HAND FUEL PRESSURE LOW LIGHT ILLUMINATION AND THE CREW ABORTED TAKEOFF. THE CREW CLEARED THE RUNWAY AND THE LIGHT EXTINGUISHED. THE CREW PERFORMED AN ENGINE RUN WHICH CHECKED GOOD. THE CREW WAS CLEARED FOR SDR VNAA0012015Fan · failedTHE CAPTAIN DECLARED AN EMERGENCY DUE TO SMOKE IN THE CABIN. THE AIRCRAFT WAS EVACUATED ON THE TAXI WAY. THE PASSENGERS WERE PICKED UP BY BUS AND THE AIRCRAFT WAS TOWED BACK TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE RECIRCULATION FAN IN ACCORDANCESDR VNAA0011015Seal · deformedDURING CLIMBOUT THE AIRCRAFT WOULD NOT PRESSURIZE. THE CAPTAIN DECIDED TO RETURN TO PIT. MAINTENANCE INSPECTED AND FOUND THE DOOR SEAL DEFORMED AND THE OUTFLOW VALVE BLOCKING TOOL INSTALLED. MAINTENANCE REMOVED THE BLOCKING TOOL AND REPLACED THE DOOR SEAL ISDR VNAA0011002Light · failedTHE CREW REPORTED THAT THE EMERGENCY LIGHTING FLOOR STRIP WOULD NOT ILLUMINATE. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WSDR VNAA0007002Cowl Door · openAFTER DEPARTURE, THE FLIGHT ATTENDANT NOTIFIED THE CREW THAT THE LEFT HAND ENGINE INBOARD COWLING WAS OPEN. FLIGHT 4083 RETURNED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND SECURED THE COWLING IN ACCORDANCE WITH DORNIER MAINTENANCE SDR VNAA0004021Battery · failedTHE CREW REPORTED THAT THE EMERGENCY LIGHTS AT ROW 7 AND 9 WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERATIONAL CHECKS WERE PERFORMED AND THE ASDR 20000426SH034Fork · wornPITCH CHANGE FORK WAS FOUND WORN BEYOND MANUAL LIMITS BEFORE FIRST OVERHAUL. WEAR ON FORK SLOTS MEASURED 0.010 INCH - 0014 INCH OF ALLOWABLE 0.010 INCH MAXIMUM. (X)SDR VNAA0003015Warning System · activatedTHE FLIGHT CREW RECEIVED A TAKEOFF CONFIGURATION WARNING AS THE TAKEOFF ROLL WAS INITIATED. THE FLIGHT CREW ABORTED THE TAKEOFF AND EXITED THE RUNWAY. THE FLIGHT CREW ADJUSTED THE TRIM LEVERS AND ATTEMPTED ANOTHER TAKEOFF WHICH RESULTED IN A NORMAL DEPARTURESDR VNAA0001011Battery · dischargedTHE CREW FOUND THAT THE EMERGENCY EXIT LIGHTAT THE 9A POSITION DID NOT WORK. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 9A POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFSDR VNAA9910019Governor · failedUPON APPLICATION OF TAKEOFF POWER THE FLIGHT CREW RECEIVED ABNORMAL TORQUE INDICATIONS ON THE RIGHT HAND ENGINE. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REPLACED THE RIGHT HAND PROPELLER OVERSPEED GOVERNOR IN ACCORDANCE WITH DORSDR VNAA9910007Air Dist · odorWHILE AT THE GATE AND AFTER STARTING BOTH ENGINES AND REMOVING GROUND POWER, THE FLIGHT CREW REPORTED A STRONG ELECTRICAL / FIRE SMELL. MAINTENANCE INSPECTED ALL ELECTRICAL COMPONETS OF THE AFFECTED SYSTEMS AND PERFORMED GROUND OPERATIONAL CHECKS WITH NO DISCSDR VNAA9907008Power Supply · failedDURING THE PRE-FLIGHT INSPECTION, A SECTION OF EMERGENCY LIGHTS WERE NOTED TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE 4LK EMERGENCY POWER SUPPLY, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE COMPLETED, AND THSDR VNAA9906004Linkage · disconnectedLEFT PROPELLER RPM AND TORQUE READINGS REMAINED AT 74 PERCENT REGARDLESS OF CONDITION LEVER INPUTS. NOSE WHEEL STEERING WAS ALSO NOTED TO BE INOPERATIVE. THE CREW SHUTDOWN THE LT ENGINE AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND FOUND THE CONTROL SDR VNAA9905013Battery · dischargedDURING THE POST FLIGHT INSPECTION, THE EMERGENCY LIGHTS AT ROWS 4, 5, AND 6 WERE NOTED TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR VNAA9903006Brakes · overheatedTHE AIRCRAFT RETURNED TO THE GATE FOLLOWING A BRAKE TEMPERATURE HIGH WARNING INDICATION. OUTSTATION MAINTENANCE INSPECTED AND CYCLED THE BRAKES, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-00. OPERATIONAL TAXI CHECKS WERE COMPLETED, AND THE AIRCRAFT SDR VNAA9902011Battery · dischargedDURING THE PREFLIGHT INSPECTION, TWO STRIPS OF EMERGENCY FLOOR LIGHTING WERE NOTED TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY PACK AT 5LK POSITION, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERATIONAL CHECKS WESDR VNAA9902010Connector · dirtyTHE LEFT HAND PROPELLER OVERSPEED TEST FAILED TO OPERATE WHEN SELECTED ON THE TAXI PRIOR TO TAKEOFF. MAINTENANCE INSPECTED AND CLEANED THE LEFT HAND PROPELLER OVERSPEED GOVERNOR CANNON PLUG. OPERATIONAL CHECKS WERE COMPLETED, IN ACCORDANCE WITH DORNIER MAINTSDR VNAA9808020Pump · failedON APPROACH, CREW RECEIVED FLAP CONTROL FAIL CAS MESSAGE. REVIEWED CHECKLIST AND PERFORMED 0 DEGREE FLAP LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE MAIN HYDRAULIC PUMP INOPERATIVE. REPLACED PUMP IN ACCORDANCSDR VNAA9807005Deice Boot · wornTHE RIGHT HAND WING SURFACE DE-ICE SYSTEM FAILED, DURING THE TAXI PRIOR TO TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE DEFERRED THE SURFACE DE-ICE SYSTEM PER THE MINUMUM EQUIPMENT LIST, AND THE AIRCRAFT WAS RETURNED TO SERVICE. ON 15 JULY 98, MASDR VNAA9802017Iac · failedDURING THE TAXI FOR TAKEOFF, THE FLIGHT MANAGEMENT SYSTEM WOULD NOT ALIGN WITH THE RUNWAY THAT WAS SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 INTEGRATED AVIONICS COMPUTER IN ACCORDANCE WITH DORNIER MAINTENANCE MASDR VNAA9802014Poteniometer · out of adjustWHEN THE CONDITION LEVERS WERE BROUGHT FORWARD FOR TAKEOFF, A NOSE STEERING FAIL WARNING OCCURRED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE IN AZO INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT INTO CAK. SDR VNAA9611003Autofeather · malfunctionedAUTOFEATHER DID NOT ARM ITSELF DURING TAKEOFF, ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE PERFORMED GROUND RUN AND AUTOFEATHER OPERATIONAL CHECK, NO DEFECTS NOTED. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR VNAA9611001Pseu · failedAFTER TAKEOFF, DURING GEAR RETRACTION. TAKEOFF CONFIGURATION HORN AND GEAR UNSAFE INDICATIONS CAME UP ALONG WITH ERRATIC MESSAGES. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PSEU, OPERATIONAL CHECKED GOOD AN
Back to N460PS, cancelled Jan 25, 2005