# Service difficulty reports: N460PS, cancelled Jan 25, 2005 A list on [N460PS, cancelled Jan 25, 2005](https://openairdocs.org/deregistered/N460PS-2005-01-25.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR VNAA0310010](https://openairdocs.org/sdr/VNAA0310010.md): Control Panel · failed · Oct 14, 2003 · N460PS · Dorner DO328100 · Electrical Power System > DURING 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 FOR - [SDR VNAA0308022](https://openairdocs.org/sdr/VNAA0308022.md): Battery · discharged · Aug 29, 2003 · N460PS · Dorner DO328100 · Emergency Lighting > THE 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 WAS - [SDR VNAA0302027](https://openairdocs.org/sdr/VNAA0302027.md): Pressure Switch · failed · Feb 27, 2003 · N460PS · Dorner DO328100 · Propeller Controlling System > DURING 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 DIVERTED - [SDR VNAA0302021](https://openairdocs.org/sdr/VNAA0302021.md): Valve · failed · Feb 24, 2003 · N460PS · Dorner DO328100 · Landing Gear Brake System > EN 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 AIRC - [SDR VNAA0210004](https://openairdocs.org/sdr/VNAA0210004.md): Battery · discharged · Oct 4, 2002 · N460PS · Dorner DO328100 · Emergency Lighting > THE 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 RELEAS - [SDR VNAA0209034](https://openairdocs.org/sdr/VNAA0209034.md): Battery · discharged · Sep 24, 2002 · N460PS · Dorner DO328100 · Emergency Lighting > THE 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 SERV - [SDR VNAA0208031](https://openairdocs.org/sdr/VNAA0208031.md): Battery · discharged · Aug 21, 2002 · N460PS · Dorner DO328100 · Emergency Lighting > THE 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 VNAA0208006](https://openairdocs.org/sdr/VNAA0208006.md): Battery · discharged · Aug 5, 2002 · N460PS · Dorner DO328100 · Emergency Lighting > THE 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 AIRCRAF - [SDR VNAA0207014](https://openairdocs.org/sdr/VNAA0207014.md): Wire · failed · Jul 11, 2002 · N460PS · Dorner DO328100 · Electrical Power System Wiring > DURING 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. O - [SDR VNAA0207003](https://openairdocs.org/sdr/VNAA0207003.md): Control Panel · failed · Jul 2, 2002 · N460PS · Dorner DO328100 · AC Power Distribution System > AFTER 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 WHI - [SDR VNAA0206012](https://openairdocs.org/sdr/VNAA0206012.md): Connector · dirty · Jun 20, 2002 · N460PS · Dorner DO328100 · Fuel Control/Turbine Engines > DURING 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 T - [SDR VNAA0206004](https://openairdocs.org/sdr/VNAA0206004.md): Sensor · failed · Jun 6, 2002 · N460PS · Dorner DO328100 · DC Generating System > DURING 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 AIRC - [SDR VNAA0201008](https://openairdocs.org/sdr/VNAA0201008.md): Lead · frayed · Jan 6, 2002 · N460PS · Dorner DO328100 · Propeller/Rotor Anti-Ice/De-Ice System > DURING 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 A - [SDR VNAA0112008](https://openairdocs.org/sdr/VNAA0112008.md): Restrictor Valve · failed · Dec 7, 2001 · N460PS · Dorner DO328100 · Pneumatic Distribution System > DURING 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 PE - [SDR VNAA0109006](https://openairdocs.org/sdr/VNAA0109006.md): Windshield · failed · Sep 10, 2001 · N460PS · Dorner DO328100 · Window/Windshield System > AFTER 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 RI - [SDR VNAA0109003](https://openairdocs.org/sdr/VNAA0109003.md): Indicator · Sep 6, 2001 · N460PS · Dorner DO328100 · Landing Gear System > DURING 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 VNAA0107024](https://openairdocs.org/sdr/VNAA0107024.md): Switch · out of adj · Jul 29, 2001 · N460PS · Dorner DO328100 · Door Warning System > AFTER 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 CHECKS - [SDR VNAA0105021](https://openairdocs.org/sdr/VNAA0105021.md): Bleed Valve · failed · May 28, 2001 · N460PS · Dorner DO328100 · Pneumatic Distribution System > DURING 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 B - [SDR VNAA0105008](https://openairdocs.org/sdr/VNAA0105008.md): Smoke · detected · May 13, 2001 · N460PS · Dorner DO328100 · Air Distribution System > DURING 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 PL - [SDR VNAA0104008](https://openairdocs.org/sdr/VNAA0104008.md): Light · inoperative · Apr 15, 2001 · N460PS · Dorner DO328100 · Landing Gear Position and Warning > DURING 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 WIT - [SDR VNAA0104007](https://openairdocs.org/sdr/VNAA0104007.md): Battery · overheated · Apr 12, 2001 · N460PS · Dorner DO328100 · Battery/Charger System > WHILE 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 APP - [SDR VNAA0104006](https://openairdocs.org/sdr/VNAA0104006.md): Switch · faulty · Apr 10, 2001 · N460PS · Dorner DO328100 · Power Lever > DURING 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 MICROSWITCH - [SDR VNAA0104003](https://openairdocs.org/sdr/VNAA0104003.md): Bleed Valve · failed · Apr 5, 2001 · N460PS · Dorner DO328100 · Compressor Bleed Valve > AS 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 MAINT - [SDR VNAA0103003](https://openairdocs.org/sdr/VNAA0103003.md): A/C Pack · failed · Mar 3, 2001 · N460PS · Dorner DO328100 · Cabin Cooling System > WHILE 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 VNAA0101002](https://openairdocs.org/sdr/VNAA0101002.md): Switch · failed · Jan 1, 2001 · N460PS · Dorner DO328100 · Fuel Pressure Indicating > DURING 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 VNAA0101001](https://openairdocs.org/sdr/VNAA0101001.md): Warning Light · illuminated · Jan 1, 2001 · N460PS · Dorner DO328100 · Fuel Pressure Indicating > DURING 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 VNAA0012015](https://openairdocs.org/sdr/VNAA0012015.md): Fan · failed · Dec 18, 2000 · N460PS · Dorner DO328100 · Air Distribution Fan > THE 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 ACCORDANCE - [SDR VNAA0011015](https://openairdocs.org/sdr/VNAA0011015.md): Seal · deformed · Nov 16, 2000 · N460PS · Dorner DO328100 · Passenger/Crew Doors > DURING 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 I - [SDR VNAA0011002](https://openairdocs.org/sdr/VNAA0011002.md): Light · failed · Nov 2, 2000 · N460PS · Dorner DO328100 · Emergency Lighting > THE 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 W - [SDR VNAA0007002](https://openairdocs.org/sdr/VNAA0007002.md): Cowl Door · open · Jul 3, 2000 · N460PS · Dorner DO328100 · Engine Cowling System > AFTER 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 VNAA0004021](https://openairdocs.org/sdr/VNAA0004021.md): Battery · failed · Apr 20, 2000 · N460PS · Dorner DO328100 · Emergency Lighting > THE 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 A - [SDR 20000426SH034](https://openairdocs.org/sdr/20000426SH034.md): Fork · worn · Apr 6, 2000 · N460PS · Dorner DO328100 · Propeller Controlling System > PITCH 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 VNAA0003015](https://openairdocs.org/sdr/VNAA0003015.md): Warning System · activated · Mar 15, 2000 · N460PS · Dorner DO328100 · Central Warning > THE 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 DEPARTURE - [SDR VNAA0001011](https://openairdocs.org/sdr/VNAA0001011.md): Battery · discharged · Jan 12, 2000 · N460PS · Dorner DO328100 · Emergency Lighting > THE 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 AIRCRAF - [SDR VNAA9910019](https://openairdocs.org/sdr/VNAA9910019.md): Governor · failed · Oct 27, 1999 · N460PS · Dorner DO328100 · Propeller Governor > UPON 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 DOR - [SDR VNAA9910007](https://openairdocs.org/sdr/VNAA9910007.md): Air Dist · odor · Oct 13, 1999 · N460PS · Dorner DO328100 · Air Distribution System > WHILE 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 DISC - [SDR VNAA9907008](https://openairdocs.org/sdr/VNAA9907008.md): Power Supply · failed · Jul 27, 1999 · N460PS · Dorner DO328100 · Emergency Lighting > DURING 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 TH - [SDR VNAA9906004](https://openairdocs.org/sdr/VNAA9906004.md): Linkage · disconnected · Jun 8, 1999 · N460PS · Dorner DO328100 · Power Lever > LEFT 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 VNAA9905013](https://openairdocs.org/sdr/VNAA9905013.md): Battery · discharged · May 30, 1999 · N460PS · Dorner DO328100 · Emergency Lighting > DURING 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 VNAA9903006](https://openairdocs.org/sdr/VNAA9903006.md): Brakes · overheated · Mar 1, 1999 · N460PS · Dorner DO328100 · Brake > THE 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 VNAA9902011](https://openairdocs.org/sdr/VNAA9902011.md): Battery · discharged · Feb 20, 1999 · N460PS · Dorner DO328100 · Emergency Lighting > DURING 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 WE - [SDR VNAA9902010](https://openairdocs.org/sdr/VNAA9902010.md): Connector · dirty · Feb 17, 1999 · N460PS · Dorner DO328100 · Propeller Controlling System > THE 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 MAINT - [SDR VNAA9808020](https://openairdocs.org/sdr/VNAA9808020.md): Pump · failed · Aug 23, 1998 · N460PS · Dorner DO328100 · Hydraulic Pump (Electric/Engine), Main > ON 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 ACCORDANC - [SDR VNAA9807005](https://openairdocs.org/sdr/VNAA9807005.md): Deice Boot · worn · Jul 14, 1998 · N460PS · Dorner DO328100 · Airfoil Anti/De-ice System > THE 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, MA - [SDR VNAA9802017](https://openairdocs.org/sdr/VNAA9802017.md): Iac · failed · Feb 18, 1998 · N460PS · Dorner DO328100 · Independent Position Determining System > DURING 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 MA - [SDR VNAA9802014](https://openairdocs.org/sdr/VNAA9802014.md): Poteniometer · out of adjust · Feb 12, 1998 · N460PS · Dorner DO328100 · Landing Gear Steering System > WHEN 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 VNAA9611003](https://openairdocs.org/sdr/VNAA9611003.md): Autofeather · malfunctioned · Nov 8, 1996 · N460PS · Dorner DO328100 · Propeller Feathering/Reversing > AUTOFEATHER 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 VNAA9611001](https://openairdocs.org/sdr/VNAA9611001.md): Pseu · failed · Nov 4, 1996 · N460PS · Dorner DO328100 · Landing Gear Position and Warning > AFTER 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 ## 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 = 'N460PS' AND deregistration_id = 'N460PS-2005-01-25' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N460PS-2005-01-25/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.