# N457PS: 1996 Dornier Luftfahrt 328-100, registration cancelled 2009-03-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 17, 2009
- Status when cancelled: Triennial form not returned
- Airframe: [Dornier Luftfahrt 328-100](https://openairdocs.org/model/dornier-luftfahrt-328-100) (registry code 2996100)
- Engine: [Pratt & Whitney Canada PW119B](https://openairdocs.org/engine/pratt-whitney-canada-pw119b) (registry code 52133)
- Data sheets: [TCDS A45NM](https://openairdocs.org/tcds/A45NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 3048
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: April 24, 1996
- Certificate issued: June 20, 1996
- Last registry action: November 18, 2008
- Mode S code: A58D73
- 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/N457PS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=457PS
- Page: https://openairdocs.org/deregistered/N457PS-2009-03-17

From the FAA registry file of November 3, 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 (49)

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

- [SDR VNAA0308017](https://openairdocs.org/sdr/VNAA0308017), Aug 26, 2003: CONNECTOR. DIRTY. EN ROUTE, THE CREW RECEIVED A LEFT HAND PROP LOW OIL PRESSURE INDICATION AND RETURNED TO TYS. MAINTENANCE INSPECTED AND SERVICED THE LEFT HAND OIL AND CLEANED T
- [SDR VNAA0305023](https://openairdocs.org/sdr/VNAA0305023), May 31, 2003: LIGHT. FAILED. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING STRIP AT ROW 4 AND 5 WAS NOT ILLUMINATING. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND R
- [SDR VNAA0302022](https://openairdocs.org/sdr/VNAA0302022), Feb 24, 2003: STALL WARNING. FAILED. DURING TAKEOFF, THE CREW RECEIVED A PUSHER FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CREW RESET THE PUSHER AND FLIGHT 4140 WAS CLEARED FOR ANOTHER TAKEOFF ATTEM
- [SDR VNAA0211012](https://openairdocs.org/sdr/VNAA0211012), Nov 10, 2002: CONNECTOR. DIRTY. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT 9A WAS NOT WORKING. MAINTENANCE INSPECTED AND CLEANED THE LIGHTING CONNECTOR IN ACCORDANCE WITH DORNIER MAINTEN
- [SDR VNAA0210021](https://openairdocs.org/sdr/VNAA0210021), Oct 19, 2002: FIRE DETECTOR. FAILED. DURING CLIMB, THE CARGO FIRE LIGHT ILLUMINATED ON THE RED WARNING PANEL INTERMITTENTLY. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND RELEASED THE CARGO CO
- [SDR VNAA0209029](https://openairdocs.org/sdr/VNAA0209029), Sep 20, 2002: LIGHT. LOOSE. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 10 TO 12 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND RESECURED THE EMERGENCY FLOOR LIGHTING IN 
- [SDR VNAA0209023](https://openairdocs.org/sdr/VNAA0209023), Sep 16, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROW 9 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGENCY BATTERY IN ACCORDANCE WITH DOR
- [SDR VNAA0209022](https://openairdocs.org/sdr/VNAA0209022), Sep 15, 2002: LIGHT. INOPERATIVE. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING STRIP WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE LIGHTING STRIP IN ACCORDANCE WITH DORNIER
- [SDR VNAA0208044](https://openairdocs.org/sdr/VNAA0208044), Aug 29, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE LAST TWO EMERGENCY FLOOR TRACK LIGHTS WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 4LK EMERGENCY BATTERY IN ACCORDAN
- [SDR VNAA0208038](https://openairdocs.org/sdr/VNAA0208038), Aug 24, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY BATTERY AT THE 4LK POSITION NEEDS REPLACED. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK POSITION IN
- [SDR VNAA0207044](https://openairdocs.org/sdr/VNAA0207044), Jul 29, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 4 AND 5 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE 
- [SDR VNAA0207023](https://openairdocs.org/sdr/VNAA0207023), Jul 17, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 4 AND 5 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AND POWER SU
- [SDR VNAA0207018](https://openairdocs.org/sdr/VNAA0207018), Jul 13, 2002: DOOR. MALFUNCTIONED. AFTER TAKEOFF, THE CREW EXPERIENCED A VIBRATION IN THE NOSE SECTION OF THE AIRCRAFT. A GEAR DOOR WAS OBSERVED BY GROUND PERSONNEL AS REMAINING OPEN WHEN THE GEA
- [SDR VNAA0205017](https://openairdocs.org/sdr/VNAA0205017), May 27, 2002: WIRE. LOOSE. THE CREW REPORTED THAT THE EMERGENCY LIGHTING STRIP AT ROWS 4, 5 AND 6 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND SECURED THE WIRING CONNECTION IN ACCORDAN
- [SDR VNAA0204019](https://openairdocs.org/sdr/VNAA0204019), Apr 20, 2002: POWER SUPPLY. FAILED. THE AIRCRAFT HAD THE EMERGENCY BATTERY CHANGED PRIOR TO FLIGHT 4189. HOWEVER, ON THE TAXI FROM THE GATE THE EMERGENCY LIGHTING AT ROWS 3 AND 4 DIDN'T ILLUMINATE
- [SDR VNAA0204011](https://openairdocs.org/sdr/VNAA0204011), Apr 16, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING IN ROWS 4 AND 5 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 5LK POSITIO
- [SDR VNAA0203011](https://openairdocs.org/sdr/VNAA0203011), Mar 9, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 3, 4, AND 5 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDA
- [SDR VNAA0201019](https://openairdocs.org/sdr/VNAA0201019), Jan 24, 2002: PANEL. FAILED. DURING TAKEOFF, THE FUEL QUANTITY FAILED AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE REFUELING PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANU
- [SDR VNAA0201012](https://openairdocs.org/sdr/VNAA0201012), Jan 12, 2002: WINDSHIELD. CRACKED. DURING CRUISE, FIRST OFFICER ADVISED THE RIGHT HAND WINDSHIELD CRACKED. LANDED AT THE FIRST SUITABLE AIRPORT. DID NOT DECLARE AN EMERGENCY. LANDED WITHOUT ANY I
- [SDR VNAA0112016](https://openairdocs.org/sdr/VNAA0112016), Dec 21, 2001: BATTERY. FAILED. THE CREW RECEIVED A NUMBER 2 BATTERY OVERHEAT MESSAGE AND RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND REPLACED THE MAIN BATTERY IN ACCORDANCE WITH DORNIER 
- [SDR VNAA0110013](https://openairdocs.org/sdr/VNAA0110013), Oct 17, 2001: BATTERY PACK. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION IN ACCORDANCE W
- [SDR VNAA0106010](https://openairdocs.org/sdr/VNAA0106010), Jun 11, 2001: DETECTOR. FAILED. DURING CLIMB OUT OF PIT, THE CREW RECEIVED A RED WARNING PANEL INDICATION OF A CARGO FIRE. THE CREW WENT THROUGH THE QUICK REFERENCE PROCEDURES AND RETURNED TO 
- [SDR VNAA0104019](https://openairdocs.org/sdr/VNAA0104019), Apr 27, 2001: TIRE. BLOWN. AS THE FLIGHT ACHIEVED V1, THE CREW FELT A VIBRATION. THE FLIGHT ATTENDANT REPORTED THAT A PASSENGER HEARD A LOUD BANG FROM UNDER THE AIRCRAFT. THE CREW CALLED 
- [SDR VNAA0103017](https://openairdocs.org/sdr/VNAA0103017), Mar 30, 2001: LIGHT. INOPERATIVE. THE FLIGHT CREW REPORTED THAT THE EMERGENCY FLOOR PATHWAY LIGHT WOULD NOT ILLUMINATE ADJACENT TO THE CABIN SEAT ROW 7 POSITION. MAINTENANCE REPLACED THE FLOOR P
- [SDR VNAA0103014](https://openairdocs.org/sdr/VNAA0103014), Mar 16, 2001: LIGHT. INOPERATIVE. THE FLIGHT CREW REPORTED THAT THE EMERGENCY FLOOR PATH LIGHTING ADJACENT TO SEAT ROW 10 WOULD NOT OPERATE. MAINTENANCE INSPECTED AND FERRIED THE AIRCRAFT TO PIT
- [SDR VNAA0103013](https://openairdocs.org/sdr/VNAA0103013), Mar 15, 2001: BATTERY. DISCHARGED. CREW REPORTED EMERGENCY LIGHTS BETWEEN ROWS 3 AND 5 WERE NOT WORKING. MAINTENANCE REPLACED EMERGENCY BATTERY AT 5LK IN ACCORDANCE WITH MAINTENANCE MANUAL 33-50-
- [SDR VNAA0103005](https://openairdocs.org/sdr/VNAA0103005), Mar 3, 2001: WIRE. DAMAGED. THE FLIGHT CREW FOUND THE SERVICE DOOR EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE REPAIRED THE EXIT LIGHT WIRE
- [SDR VNAA0102002](https://openairdocs.org/sdr/VNAA0102002), Feb 6, 2001: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROW FOUR WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 5LK POSITION IN 
- [SDR VNAA0012029](https://openairdocs.org/sdr/VNAA0012029), Dec 29, 2000: BOOT. FAILED. AFTER 10 MINUTES INTO THE FLIGHT, THE CREW RECEIVED A AIRFOIL DEICE FAIL CAS MESSAGE. DISPATCH ADVISED THE CREW TO RETURN TO DAY WHERE MAINTENANCE INSPECTED AND
- [SDR VNAA0011030](https://openairdocs.org/sdr/VNAA0011030), Nov 30, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE EMER
- [SDR VNAA0011026](https://openairdocs.org/sdr/VNAA0011026), Nov 25, 2000: BLEED VALVE. FAILED. WHILE LINED UP FOR TAKE OFF THE CREW RECEIVED A RIGHT HAND AND LEFT HAND PACK FAIL CAS MESSAGE. THE CREW CLEARED THE RUNWAY AND CONTACTED MAINTENANCE CONTROL. M
- [SDR VNAA0009012](https://openairdocs.org/sdr/VNAA0009012), Sep 15, 2000: VALVE. FAILED. FLIGHT 4191 WAS IN ICING CONDITIONS AND HAD THE RIGHT HAND INBOARD DE-ICE BOOT FAIL. FLIGHT 4191 RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND REPLACED THE E
- [SDR VNAA0009003](https://openairdocs.org/sdr/VNAA0009003), Sep 7, 2000: WARNING SYSTEM. ACTIVATED. DURING TAKEOFF, A RIGHT HAND CAS MESSAGE APPEARED. THE CREW ABORTED THE TAKEOFF. THE CREW RESET THE CIRCUIT BREAKER AND THE MESSAGE CLEARED. THE CREW ATTEMPTED 
- [SDR VNAA0004017](https://openairdocs.org/sdr/VNAA0004017), Apr 13, 2000: BATTERY. INOPERATIVE. THE CREW REPORTED THAT THE EMERGENCY SIGN AND FLOOR LIGHTS AT ROW 11A WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK 
- [SDR VNAA0003016](https://openairdocs.org/sdr/VNAA0003016), Mar 16, 2000: DEICE SYSTEM. FAILED. WHILE CLIMBING OUT OF PIT EN ROUTE TO SBN, THE CREW RECEIVED AN AIRFOIL DE-ICE FAIL MESSAGE. THE CREW CONTACTED MAINTENANCE CONTROL AND WERE INSTRUCTED TO DIVER
- [SDR VNAA0001006](https://openairdocs.org/sdr/VNAA0001006), Jan 6, 2000: BLEED VALVE. FAILED. DURING TAKEOFF, THE LEFT HIGH PRESSURE BLEED VALVE FAILED. THE CREW ABORTED TAKEOFF. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED TH
- [SDR VNAA0001004](https://openairdocs.org/sdr/VNAA0001004), Jan 5, 2000: ECU. FAILED. DURING TAKEOFF, THE CREW RECEIVED A ELECTRONIC ENGINE CONTROL UNIT FAIL CAS MESSAGE. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE CONTROL HAD 
- [SDR VNAA9912014](https://openairdocs.org/sdr/VNAA9912014), Dec 29, 1999: DEICE SYSTEM. FAILED. DURING TAKEOFF, THE CREW RECEIVED A LEFT ENGINE INTAKE DE-ICE FAIL CAS MESSAGE. THE CREW ABORTED TAKEOFF AND CLEARED THE RUNWAY. THE CREW COULD VISUALLY VERIFY 
- [SDR VNAA9911017](https://openairdocs.org/sdr/VNAA9911017), Nov 21, 1999: VALVE. FAILED. DURING FLIGHT, THE LEFT HAND PACK TEMPERATURE WAS UNCONTROLLABLE AND CAUSED SMOKE TO ENTER THE FLIGHT DECK. THE CREW TURNED THE LEFT HAND PACK OFF AND THE SMOKE
- [SDR VNAA9908006](https://openairdocs.org/sdr/VNAA9908006), Aug 17, 1999: PANEL. FAILED. TESTING THE EMERGENCY LIGHTS WAS REPORTED AS INTEMITTANT FROM THE CREW. MAINTENANCE INSPECTED AND REPLACED THE FLIGHT ATTENDANT PANEL, IN ACCORDANCE WITH DORNIE
- [SDR VNAA9811025](https://openairdocs.org/sdr/VNAA9811025), Nov 29, 1998: PCU. FAILED. THE RIGHT HAND PROPELLER FAILED TO COME OUT OF FEATHER WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND PROPE
- [SDR VNAA9810008](https://openairdocs.org/sdr/VNAA9810008), Oct 8, 1998: SKIN. BIRD STRIKE. DURING THE DESCENT, THE AIRCRAFT WAS STRUCK BY A BIRD ON THE FUSELAGE, BELOW THE LEFT HAND FORWARD WINDSCREEN. THE AIRCRAFT CONTINUED THE DESCENT INTO PIT AND L
- [SDR VNAA9809021](https://openairdocs.org/sdr/VNAA9809021), Sep 25, 1998: SENSOR. FAILED. DURING THE TAXI FOR TAKEOFF, THE CREW NOTED A LEFT ENGINE ELECTRONIC CONTROL UNIT (ECU) FAIL WARNING MESSAGE. THE AIRCRAFT RETURNED TO THE GATE. PSA MAINTENANCE
- [SDR VNAA9809010](https://openairdocs.org/sdr/VNAA9809010), Sep 11, 1998: SENSOR. FAILED. DURING THE TAXI FOR TAKEOFF, AN ECU FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND ENGINE
- [SDR VNAA9808026](https://openairdocs.org/sdr/VNAA9808026), Aug 28, 1998: TRIM WARNING. ACTIVATED. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE, FOLLOWING A TAKEOFF CONFIG FAIL WARNING MESSAGE. THE CREW SUSPECTED THAT AN UNCOMMANDED ELEVATOR TRIM CHA
- [SDR VNAA9803010](https://openairdocs.org/sdr/VNAA9803010), Mar 10, 1998: PITOT HEAT. FAILED. DURING THE TAXI OUT FOR TAKEOFF, A STANDBY PITOT HEAT FAIL WARNING MESSAGE WAS DISPLAYED. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AN
- [SDR VNAA9703007](https://openairdocs.org/sdr/VNAA9703007), Mar 25, 1997: INTAKE BOOT. DAMAGED. ON CLIMBOUT, THE LEFT ENGINE DE-ICE FAILED WHEN SELECTED ON. RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IN
- [SDR VNAA9609001](https://openairdocs.org/sdr/VNAA9609001), Sep 3, 1996: CONTROL PANEL. DEFECTIVE. ON CLIMBOUT, PILOT WAS UNABLE TO CONTROL CABIN ALTITUDE. AFTER LEVELING OFF AT 10,000, CABIN CONTINUED TO CLIMB. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. 
- [SDR VNAA9600032](https://openairdocs.org/sdr/VNAA9600032), May 13, 1996: TORQUE SENSOR. DEFECTIVE. ON THE TAKEOFF ROLL, LT ENGINE TORQUE INDICATION WAS NOT AT THE MINIMUM LEVEL FOR TAKEOFF. CREW ABORTED THE TAKEOFF AND RETURNED TO THE TAXIWAY. CONDUCTED A POW

## 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 20010611010319I](https://openairdocs.org/incident/20010611010319I), Jun 11, 2001: Dorner DO328100 (N457PS), Pittsburgh, PA. (-23)On June 11, 2001, a DO-328-100, s/n 3048, registered as N457PS and operated as vnaa flight #4076 departed pit when the crew received a cargo firered…
- [Incident 20010427007099I](https://openairdocs.org/incident/20010427007099I), Apr 27, 2001: Dorner DO328100 (N457PS), Pittsburgh, PA, Minor damage. (-23)On April 27, 2001, a DO-328-100, s/n 3028, registered as N457PS and being operated as vnaa flight 4022, had a tire blow out on take off from "pit". The…

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