# N460PS: Dornier Luftfahrt 328-100, registration cancelled 2005-01-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 25, 2005
- Exported to: Denmark
- Status when cancelled: Valid registration
- Airframe: [Dornier Luftfahrt 328-100](https://openairdocs.org/model/dornier-luftfahrt-328-100) (registry code 2996100)
- Data sheets: [TCDS A45NM](https://openairdocs.org/tcds/A45NM) (OpenAirDocs)
- Serial number: 3061
- Type of aircraft: Fixed wing multi engine
- Certificate issued: September 9, 1996
- Last registry action: November 6, 2002
- Mode S code: A59AF1
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N460PS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=460PS
- Page: https://openairdocs.org/deregistered/N460PS-2005-01-25

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Dornier Luftfahrt 328-100: https://openairdocs.org/model/dornier-luftfahrt-328-100.md

## Service difficulty reports (48)

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

- [SDR VNAA0310010](https://openairdocs.org/sdr/VNAA0310010), Oct 14, 2003: CONTROL PANEL. FAILED. DURING TAKEOFF, THE CREW RECEIVED A LT GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIE
- [SDR VNAA0308022](https://openairdocs.org/sdr/VNAA0308022), Aug 29, 2003: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE FIRST ROW OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANC
- [SDR VNAA0302027](https://openairdocs.org/sdr/VNAA0302027), Feb 27, 2003: PRESSURE SWITCH. FAILED. DURING FLIGHT, THE CREW RECEIVED A RIGHT HAND PROP OIL PRESSURE LOW CAS MESSAGE. ALL OTHER ENGINE INDICATIONS WERE NORMAL AND WITH MAINTENANCE CONTROL, CONCLUDE
- [SDR VNAA0302021](https://openairdocs.org/sdr/VNAA0302021), Feb 24, 2003: VALVE. FAILED. 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 A
- [SDR VNAA0210004](https://openairdocs.org/sdr/VNAA0210004), Oct 4, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE LAST ROW OF EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGENCY BATTERY IN ACCORDANCE WITH 
- [SDR VNAA0209034](https://openairdocs.org/sdr/VNAA0209034), Sep 24, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAIN
- [SDR VNAA0208031](https://openairdocs.org/sdr/VNAA0208031), Aug 21, 2002: BATTERY. DISCHARGED. 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 POSITIO
- [SDR VNAA0208006](https://openairdocs.org/sdr/VNAA0208006), Aug 5, 2002: BATTERY. DISCHARGED. 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 ACCO
- [SDR VNAA0207014](https://openairdocs.org/sdr/VNAA0207014), Jul 11, 2002: WIRE. FAILED. 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 CO
- [SDR VNAA0207003](https://openairdocs.org/sdr/VNAA0207003), Jul 2, 2002: CONTROL PANEL. FAILED. AFTER THE PASSENGERS HAD BEEN BOARDED, HALFWAY THROUGH THE PREFLIGHT BRIEFING SMOKE BEGAN FORMING IN THE CABIN. THE FIRST OFFICER EVACUATED THE PASSENGERS AND T
- [SDR VNAA0206012](https://openairdocs.org/sdr/VNAA0206012), Jun 20, 2002: CONNECTOR. DIRTY. DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND ENGINE CONTROL UNIT FAIL AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND CLEANED THE ENGINE CONTROL UNIT CANNON PL
- [SDR VNAA0206004](https://openairdocs.org/sdr/VNAA0206004), Jun 6, 2002: SENSOR. FAILED. 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 A
- [SDR VNAA0201008](https://openairdocs.org/sdr/VNAA0201008), Jan 6, 2002: LEAD. FRAYED. 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 REP
- [SDR VNAA0112008](https://openairdocs.org/sdr/VNAA0112008), Dec 7, 2001: RESTRICTOR VALVE. FAILED. DURING CLIMBOUT, THE CREW RECEIVED A PACK OVERPRESSURE INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RESTRICTOR FOR THE RIGHT HAND OVER
- [SDR VNAA0109006](https://openairdocs.org/sdr/VNAA0109006), Sep 10, 2001: WINDSHIELD. FAILED. 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. D
- [SDR VNAA0109003](https://openairdocs.org/sdr/VNAA0109003), Sep 6, 2001: INDICATOR. 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 PER
- [SDR VNAA0107024](https://openairdocs.org/sdr/VNAA0107024), Jul 29, 2001: SWITCH. OUT OF ADJ. 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 A
- [SDR VNAA0105021](https://openairdocs.org/sdr/VNAA0105021), May 28, 2001: BLEED VALVE. FAILED. 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 
- [SDR VNAA0105008](https://openairdocs.org/sdr/VNAA0105008), May 13, 2001: SMOKE. DETECTED. 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 
- [SDR VNAA0104008](https://openairdocs.org/sdr/VNAA0104008), Apr 15, 2001: LIGHT. INOPERATIVE. 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. FL
- [SDR VNAA0104007](https://openairdocs.org/sdr/VNAA0104007), Apr 12, 2001: BATTERY. OVERHEATED. 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 CON
- [SDR VNAA0104006](https://openairdocs.org/sdr/VNAA0104006), Apr 10, 2001: SWITCH. FAULTY. 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 WITHO
- [SDR VNAA0104003](https://openairdocs.org/sdr/VNAA0104003), Apr 5, 2001: BLEED VALVE. FAILED. AS THE FLIGHT CREW APPLIED TAKEOFF POWER THE RIGHT ELECTRONIC ENGINE CONTROL UNIT WOULD FAIL. THE FLIGHT CREW EXITED THE RUNWAY WITHOUT INCIDENT. MAINTENANCE IN
- [SDR VNAA0103003](https://openairdocs.org/sdr/VNAA0103003), Mar 3, 2001: A/C PACK. FAILED. 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
- [SDR VNAA0101002](https://openairdocs.org/sdr/VNAA0101002), Jan 1, 2001: SWITCH. FAILED. 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 
- [SDR VNAA0101001](https://openairdocs.org/sdr/VNAA0101001), Jan 1, 2001: WARNING LIGHT. ILLUMINATED. 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 L
- [SDR VNAA0012015](https://openairdocs.org/sdr/VNAA0012015), Dec 18, 2000: FAN. FAILED. 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 W
- [SDR VNAA0011015](https://openairdocs.org/sdr/VNAA0011015), Nov 16, 2000: SEAL. DEFORMED. 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 
- [SDR VNAA0011002](https://openairdocs.org/sdr/VNAA0011002), Nov 2, 2000: LIGHT. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING FLOOR STRIP WOULD NOT ILLUMINATE. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE EME
- [SDR VNAA0007002](https://openairdocs.org/sdr/VNAA0007002), Jul 3, 2000: COWL DOOR. OPEN. 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 FURTH
- [SDR VNAA0004021](https://openairdocs.org/sdr/VNAA0004021), Apr 20, 2000: BATTERY. FAILED. 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
- [SDR 20000426SH034](https://openairdocs.org/sdr/20000426SH034), Apr 6, 2000: FORK. WORN. 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.
- [SDR VNAA0003015](https://openairdocs.org/sdr/VNAA0003015), Mar 15, 2000: WARNING SYSTEM. ACTIVATED. 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 FLIGH
- [SDR VNAA0001011](https://openairdocs.org/sdr/VNAA0001011), Jan 12, 2000: BATTERY. DISCHARGED. 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 ACCO
- [SDR VNAA9910019](https://openairdocs.org/sdr/VNAA9910019), Oct 27, 1999: GOVERNOR. FAILED. UPON APPLICATION OF TAKEOFF POWER THE FLIGHT CREW RECEIVED ABNORMAL TORQUE INDICATIONS ON THE RIGHT HAND ENGINE. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT. MAINT
- [SDR VNAA9910007](https://openairdocs.org/sdr/VNAA9910007), Oct 13, 1999: AIR DIST. ODOR. WHILE AT THE GATE AND AFTER STARTING BOTH ENGINES AND REMOVING GROUND POWER, THE FLIGHT CREW REPORTED A STRONG ELECTRICAL / FIRE SMELL. MAINTENANCE INSPECTED AL
- [SDR VNAA9907008](https://openairdocs.org/sdr/VNAA9907008), Jul 27, 1999: POWER SUPPLY. FAILED. DURING THE PRE-FLIGHT INSPECTION, A SECTION OF EMERGENCY LIGHTS WERE NOTED TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE 4LK EMERGENCY POWER SUPPLY,
- [SDR VNAA9906004](https://openairdocs.org/sdr/VNAA9906004), Jun 8, 1999: LINKAGE. DISCONNECTED. 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 CR
- [SDR VNAA9905013](https://openairdocs.org/sdr/VNAA9905013), May 30, 1999: BATTERY. DISCHARGED. 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 L
- [SDR VNAA9903006](https://openairdocs.org/sdr/VNAA9903006), Mar 1, 1999: BRAKES. OVERHEATED. THE AIRCRAFT RETURNED TO THE GATE FOLLOWING A BRAKE TEMPERATURE HIGH WARNING INDICATION. OUTSTATION MAINTENANCE INSPECTED AND CYCLED THE BRAKES, IN ACCORDANCE W
- [SDR VNAA9902011](https://openairdocs.org/sdr/VNAA9902011), Feb 20, 1999: BATTERY. DISCHARGED. DURING THE PREFLIGHT INSPECTION, TWO STRIPS OF EMERGENCY FLOOR LIGHTING WERE NOTED TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY P
- [SDR VNAA9902010](https://openairdocs.org/sdr/VNAA9902010), Feb 17, 1999: CONNECTOR. DIRTY. 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 O
- [SDR VNAA9808020](https://openairdocs.org/sdr/VNAA9808020), Aug 23, 1998: PUMP. FAILED. ON APPROACH, CREW RECEIVED FLAP CONTROL FAIL CAS MESSAGE. REVIEWED CHECKLIST AND PERFORMED 0 DEGREE FLAP LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE 
- [SDR VNAA9807005](https://openairdocs.org/sdr/VNAA9807005), Jul 14, 1998: DEICE BOOT. WORN. 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 S
- [SDR VNAA9802017](https://openairdocs.org/sdr/VNAA9802017), Feb 18, 1998: IAC. FAILED. 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 INSP
- [SDR VNAA9802014](https://openairdocs.org/sdr/VNAA9802014), Feb 12, 1998: POTENIOMETER. OUT OF ADJUST. 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
- [SDR VNAA9611003](https://openairdocs.org/sdr/VNAA9611003), Nov 8, 1996: AUTOFEATHER. MALFUNCTIONED. AUTOFEATHER DID NOT ARM ITSELF DURING TAKEOFF, ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE PERFORMED GROUND RUN AND AUTOFEATHER OPERATIONAL CHECK, NO DEFE
- [SDR VNAA9611001](https://openairdocs.org/sdr/VNAA9611001), Nov 4, 1996: PSEU. FAILED. AFTER TAKEOFF, DURING GEAR RETRACTION. TAKEOFF CONFIGURATION HORN AND GEAR UNSAFE INDICATIONS CAME UP ALONG WITH ERRATIC MESSAGES. DECLARED EMERGENCY AND LANDED

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20001218022559I](https://openairdocs.org/incident/20001218022559I), Dec 18, 2000: Dorner DO328100 (N460PS), Pittsburgh, PA. (-23) On 12/18/00 at 14:35 e during taxi for departure at pit on taxiway f, the crew of psa flight 4085 a dornier D328 N460PS evacuated crew and passengers due…
- [Incident 20000103039579I](https://openairdocs.org/incident/20000103039579I), Jan 3, 2000: Dorner DO328100 (N460PS), Pittsburgh, PA. (-23)On approach to r/w 28L at pit. The aircraft's hydraulic system temperature indicator showed a high temperature and the hydraulic system pressure showed a…

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