# N441JS: 1995 Dornier Luftfahrt 328-100, registration cancelled 2006-02-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 7, 2006
- Exported to: Germany
- 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: 3059
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: November 6, 1995
- Certificate issued: February 12, 1996
- Last registry action: November 15, 2005
- Mode S code: A54F2D
- 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/N441JS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=441JS
- Page: https://openairdocs.org/deregistered/N441JS-2006-02-07

From the FAA registry file of October 28, 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 VNAA0408009](https://openairdocs.org/sdr/VNAA0408009), Aug 16, 2004: PROXIMITY SENSOR. OUT OF ADJUST. DURING FLIGHT, THE DOORS LIGHT ON THE RED WARNING PANEL CAME ON. THE CREW THEN DIVERTED TO ELM. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE THEN ADJUSTED 
- [SDR VNAA0407009](https://openairdocs.org/sdr/VNAA0407009), Jul 31, 2004: SMOKE DETECTOR. FAILED. THE CREW REPORTED RECEIVING A LAV SMOKE MESSAGE. MAINTENANCE CONTROL DEFERRED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH MEL 26-3 CODE-C. THE MEL WAS CLEARED BY 
- [SDR VNAA0406007](https://openairdocs.org/sdr/VNAA0406007), Jun 13, 2004: POWER SUPPLY. FAILED. THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLIES FAILED TO TEST. MAINTENANCE HAD THE CREW RUN THE ENGINES FOR 10 MINUTES AND PERFORM AN OPERATIONAL CHECK IN 
- [SDR VNAA0405004](https://openairdocs.org/sdr/VNAA0405004), May 3, 2004: DOOR. OPEN. AFTER TAKEOFF, THE MAIN CABIN DOOR OPENED, AND FLIGHT 2447 RETURNED TO ABE, AIRCRAFT N441JS WAS THEN FERRIED TO CAK. THIS IS CURRENTLY STILL UNDER INVESTIGATION
- [SDR VNAA0403009](https://openairdocs.org/sdr/VNAA0403009), Mar 9, 2004: FITTING. FAILED. DURING FLIGHT, THE LEFT HAND ENGINE TORQUE WAS FLUCUATING AND FLIGHT 2434 RETURNED TO DAY. MAINTENEANCE INSPECTED AND FOUND A P-3 LINE FITTING LOOSE THEN TIGHTE
- [SDR VNAA0401008](https://openairdocs.org/sdr/VNAA0401008), Jan 19, 2004: TERMINAL. LOOSE. DURING FLIGHT, THE CREW RECEIVED A LT PROPELLER HEAT FAIL BOTH MODES AND RETURNED TO PIT. MAINTENANCE CLEANED SLIP RING AND TIGHTENED TERMINAL ENDS ON BRUSH BLO
- [SDR VNAA0308014](https://openairdocs.org/sdr/VNAA0308014), Aug 21, 2003: PROBE. FAILED. DURING FLIGHT, THE CREW RECEIVED A TAT HEAT FAIL CAS MESSAGE AND RETURNED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE TAT PROBE IN ACCORDANCE WITH DORNIER MA
- [SDR VNAA0305004](https://openairdocs.org/sdr/VNAA0305004), May 2, 2003: HMU. FAILED. AT 13,000, THE CREW BEGAN GETTING A LEFT HAND ENGINE SURGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CONTACTED MAINTENANCE CONTROL. THE CREW THEN DIVE
- [SDR VNAA0212035](https://openairdocs.org/sdr/VNAA0212035), Dec 28, 2002: FAN. FAILED. THE CREW REPORTED A BURNING SMELL IN THE COCKPIT AREA. THEN THE AVIONICS FAN FAILED. MAINTENANCE INSPECTED THE AVIONICS FAN AND FOUND IT DID FAIL. MAINTENANCE C
- [SDR VNAA0212034](https://openairdocs.org/sdr/VNAA0212034), Dec 26, 2002: VALVE. FAILED. EN ROUTE, THE CREW RECEIVED A PARKING BRAKE ACCUMULATOR PRESSURE LOW CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO ROC. THE AIRCRA
- [SDR VNAA0212014](https://openairdocs.org/sdr/VNAA0212014), Dec 9, 2002: PSEU. FAILED. THE CREW RECEIVED A PROXY SYSTEM AMBER CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUA
- [SDR VNAA0212005](https://openairdocs.org/sdr/VNAA0212005), Dec 4, 2002: SCREW. WHILE ENROUTE TO EVV, THE CREW RECEIVED A CAPTAIN'S WINDSHIELD HEAT FAIL CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND CLEANED THE WINDSHIELD SCREW
- [SDR VNAA0212006](https://openairdocs.org/sdr/VNAA0212006), Dec 4, 2002: WINDSHIELD. DURING THE CLIMB OUT, THE CREW RECEIVED A CAPTAIN'S WINDSHIELD HEAT FAIL AND RETURNED TO PIT. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE WILL REPLACE THE
- [SDR VNAA0211002](https://openairdocs.org/sdr/VNAA0211002), Nov 1, 2002: SHIM. JUST PRIOR TO DESCENDING, THE CREW RECEIVED A HIGH OIL PRESSURE INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND FEATHERED THE PROP WHILE PASSING 
- [SDR VNAA0210029](https://openairdocs.org/sdr/VNAA0210029), Oct 30, 2002: PROXIMITY SENSOR. DIRTY. EN ROUTE TO EVV AT 18,000 FEET, THE CREW RECEIVED A DOORS INDICATION ON THE RED WARNING PANEL AND DESCENDED TO 10,000 FEET AND THE LIGHT EXTINGUISHED. FLIGHT 40
- [SDR VNAA0209007](https://openairdocs.org/sdr/VNAA0209007), Sep 5, 2002: BLADE. OUT OF ADJUST. DURING CLIMBOUT, THE CREW REPORTED THAT THE LEFT HAND FUEL SHUT OFF VALVE IS CLOSED AND THERE WAS A TORQUE SPLIT OF 5 PERCENT. THE CREW ELECTED TO RETURN TO YOW
- [SDR VNAA0207032](https://openairdocs.org/sdr/VNAA0207032), Jul 22, 2002: CLAMP. FAILED. THE CREW REPORTED A HOT SMELL IN THE CABIN APPROXIMATELY UNDER THE PACK AREA. MAINTENANCE INSPECTED AND FOUND A LOOSE CLAMP AROUND THE HOT AIR DUCT. MAINTENANCE
- [SDR VNAA0204007](https://openairdocs.org/sdr/VNAA0204007), Apr 13, 2002: LAMP. AFTER SELECTING GEAR DOWN, THE CREW RECEIVED NO NOSE GEAR DOWN AND LOCK INDICATION. A LAMP TEST THEN INDICATED THAT THERE WAS A BURNED OUT LIGHT. AS A PRECAUTIO
- [SDR VNAA0110009](https://openairdocs.org/sdr/VNAA0110009), Oct 14, 2001: BOOT. FAILED. DURING CLIMBOUT, THE LEFT HAND INBOARD DE-ICE BOOT FAILED AND FLIGHT 4075 RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE LEADING EDGE ASSEMBLY IN ACCOR
- [SDR VNAA0105015](https://openairdocs.org/sdr/VNAA0105015), May 24, 2001: CONTROL VALVE. FAILED. AFTER DEPARTURE, THE CREW RECEIVED A AIRFOIL DE-ICE SYSTEM FAIL. THE CAPTAIN CONTACTED MAINTENANCE CONTROL AND WAS INSTRUCTED TO DIVERT TO CAK. FLIGHT 4135 DIVE
- [SDR VNAA0009005](https://openairdocs.org/sdr/VNAA0009005), Sep 11, 2000: APU. ODOR. AS FLIGHT 4169 DEPARTED THE CREW SMELLED AN UNUSUAL ODOR IN THE COCKPIT AND BECAME LIGHT HEADED. THE CREW IMMEDIATELY RETURNED TO THE FIELD AND PROCEEDED TO THE
- [SDR VNAA0008008](https://openairdocs.org/sdr/VNAA0008008), Aug 10, 2000: SENSOR. FAILED. AFTER DEPARTURE THE CREW WAS GETTING A LEFT HAND BLEED VALVE FAIL MESSAGE. AFTER A MAINTENANCE CALL AND DIFFERENT PROCEDURES, MAINTENANCE CONTROL ADVISED THE CR
- [SDR VNAA0006009](https://openairdocs.org/sdr/VNAA0006009), Jun 21, 2000: BATTERY. FAILED. THE FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHTING AT THE 5 LK POSITION WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 5 LK 
- [SDR VNAA0005010](https://openairdocs.org/sdr/VNAA0005010), May 16, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING IN ROW 6 WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 5LK POSITION IN ACC
- [SDR VNAA0004007](https://openairdocs.org/sdr/VNAA0004007), Apr 5, 2000: WARNING LIGHT. ILLUMINATED. DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION WARNING INDICATION. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND ATTEMPTED ANOTHER DEPARTURE. 
- [SDR VNAA0004023](https://openairdocs.org/sdr/VNAA0004023), Mar 27, 2000: BLEED VALVE. MALFUNCTIONED. THE RIGHT HAND HIGH PRESSURE VALVE HAD BEEN PREVIOUSLY ON THE MEL LIST. DURING CLIMBOUT THE CABIN ALTITUDE STARTED TO CLIMB. THE CREW REFERRED TO THE QUICK REFE
- [SDR VNAA0003026](https://openairdocs.org/sdr/VNAA0003026), Mar 25, 2000: SHUTOFF VALVE. FAILED. THE RIGHT HAND MAIN DUCT PRESSURE REDUCING SHUTOFF VALVE FAILED IN THE CLOSED POSITION. MAINTENANCE INSPECTED AND REPLACED THE MAIN DUCT PRESSURE REDUCING SHUTO
- [SDR VNAA0002004](https://openairdocs.org/sdr/VNAA0002004), Feb 3, 2000: HORN ASSY. FAILED. WHILE CLIMBING THROUGH 11,000 FEET, THE CREW RECEIVED A RIGHT HAND ELEVATOR HORN HEAT FAIL CAS MESSAGE. THE CREW TRIED TWICE TO RESET THE CIRCUIT BREAKER BUT WO
- [SDR VNAA9911012](https://openairdocs.org/sdr/VNAA9911012), Nov 15, 1999: BLEED VALVE. FAILED. THE FLIGHT CREW RECEIVED A LEFT HAND LOW PRESSURE BLEED VALVE FAIL CAS MESSAGE DURING THE TAKEOFF ROLL. WHILE TALKING TO MAINTENANCE CONTROL THE CAS MESSAGE CLE
- [SDR VNAA9911001](https://openairdocs.org/sdr/VNAA9911001), Nov 1, 1999: PCU. FAILED. WHILE PREPARING TO TAXI, FLIGHT 4097 COULD NOT GET THE RIGHT HAND PROPELLER OUT OF FEATHER. MAINTENANCE INSPECTED AND REPLACED THE PROPELLER CONTROL UNIT IN ACC
- [SDR VNAA9905010](https://openairdocs.org/sdr/VNAA9905010), May 26, 1999: CONTROL BOX. INOPERATIVE. THE LANDING GEAR FAILED TO INDICATE DOWN AND LOCKED WHEN SELECTED ON FINAL APPROACH. THE CREW FOLLOWED QRH PROCEDURES AND DECLARED AN EMERGENCY. THE AIRCRAFT MA
- [SDR VNAA9812021](https://openairdocs.org/sdr/VNAA9812021), Dec 22, 1998: POWER SUPPLY. FAILED. THE EMERGENCY LIGHTS AT 9DF AND 7DF WERE NOTED TO BE INOPERATIVE, DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE POWER SUPPLY AT THE 5L
- [SDR VNAA9812016](https://openairdocs.org/sdr/VNAA9812016), Dec 22, 1998: CONNECTOR. DIRTY. DURING TAXI, THE LEFT HAND PROPELLER OVERSPEED TEST FAILED TO OPERATE WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND CLEANED THE OV
- [SDR VNAA9810003](https://openairdocs.org/sdr/VNAA9810003), Oct 5, 1998: PCU. FAILED. THE LEFT PROPELLER FAILED TO UNFEATHER WHEN SELECTED, DURING THE PUSHBACK FOR DEPARTURE. THE AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLAC
- [SDR VNAA9808024](https://openairdocs.org/sdr/VNAA9808024), Aug 24, 1998: DEICE BOOT. DEFECTIVE. DURING TAXI FOR TAKEOFF, CREW RECEIVED AIRFRAME DEICE FAIL MESSAGE. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED AIRCRAFT AND DEFERRED RT MIDDLE WING DEICE 
- [SDR VNAA9807007](https://openairdocs.org/sdr/VNAA9807007), Jul 16, 1998: CONTROL PANEL. FAILED. DURING THE TAXI PRIOR TO TAKEOFF, A PITOT HEAT FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE ICE S
- [SDR VNAA9806013](https://openairdocs.org/sdr/VNAA9806013), Jun 24, 1998: VALVE. FAILED. A CROSSBLEED WARNING MESSAGE OCCURED DURING THE TAXI FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE CROSSBLEED VALVE, IN
- [SDR VNAA9803026](https://openairdocs.org/sdr/VNAA9803026), Mar 24, 1998: CONNECTOR. DIRTY. THE RIGHT HAND PROPELLER OVERSPEED TEST FAILED WHEN SELECTED, DURING TAXI CHECKS. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED, CLEANED A
- [SDR VNAA9712020](https://openairdocs.org/sdr/VNAA9712020), Dec 31, 1997: CONTROL UNIT. TRIPPED. DURING TAXI, CREW RECEIVED FLAP CONTROL FAIL INDICATION. CREW RETURNED TO GATE. MAINTENANCE RESET FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT APPROVED F
- [SDR VNAA9707005](https://openairdocs.org/sdr/VNAA9707005), Jul 20, 1997: SMOKE DETECTOR. ACTIVATED. SHORTLY AFTER TAKEOFF, THE CREW NOTED LAV SMOKE WARNING ILLUMINATED. CREW ALSO BELIEVED TO HAVE SMELLED A SLIGHT ODOR IN THE AIRCRAFT AT THAT TIME. THE AIRCRAFT
- [SDR VNAA9707004](https://openairdocs.org/sdr/VNAA9707004), Jul 20, 1997: OVERTEMP SWITCH. DEFECTIVE. DURING TAKEOFF ROLL, RT ECS OVERHEAT CAS MESSAGE ILLUMINATED. ABORTED T/O AND RETURNED TO GATE. INSPECTED SYSTEM AND DEFERRED RT AIR CYCLE MACHINE IN ACCORDANCE
- [SDR VNAA9703005](https://openairdocs.org/sdr/VNAA9703005), Mar 18, 1997: BRUSH BLOCK. FAILED. LEFT PROP HEAT CAS MESSAGE ILLUMINATED AFTER PROP HEAT WAS SELECTED ON. AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE REMOVED AND REPLACED THE LEFT PROP DE-ICE BR
- [SDR VNAA9703003](https://openairdocs.org/sdr/VNAA9703003), Mar 10, 1997: RETRACT MECH. MALFUNCTIONED. LOUD NOISE COMING FROM NOSE GEAR AREA WHEN GEAR WAS RETRACTED, GOES AWAY WHEN GEAR IS EXTENDED. RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE FOUN
- [SDR VNAA9701002](https://openairdocs.org/sdr/VNAA9701002), Jan 3, 1997: DAU. FAILED. ENCOUNTERED LOSS OF DAU NR 1, DAU NR 2 AND ADC. THIS RESULTED IN THE LOSS OF THE PRIMARY FLIGHT INSTRUMENTATION AND ENGINE INSTUMENTATION. ALSO, LOSS OF FMS. NO
- [SDR VNAA9606008](https://openairdocs.org/sdr/VNAA9606008), Jun 17, 1996: BULB. FAILED. ON APPROACH AFTER SELECTING GEAR DOWN, THE CREW REPORTED LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. CREW SHOT A MISSED APPROACH WHILE THE FIRST OF
- [SDR VNAA9600013](https://openairdocs.org/sdr/VNAA9600013), Apr 6, 1996: CONTROL UNIT. MALFUNCTIONED. PIT - FLT 4169 - DURING TAKEOFF ROLL, THE CREW WAS ALERTED BY A C.A.S. MESSAGE THAT BRAKES WERE HOT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. PIT MX RE-RA
- [SDR 96ZZZX2117](https://openairdocs.org/sdr/96ZZZX2117), Mar 7, 1996: WARNING LIGHT. ILLUMINATED. FLT 4165 - CREW REPORTED THE CARGO DOOR WARNING LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT RETURNED TO AZO, LANDED 400 POUNDS OVERWEIGHT. AIRCRAFT WAS FERRIED WH
- [SDR 96ZZZX2116](https://openairdocs.org/sdr/96ZZZX2116), Feb 3, 1996: DEICE BOOT. DEFECTIVE. BLD/IAD - FLT 4126 - EN ROUTE, CREW REPORTED A PROBLEM WITH THE LEFT ENGINE INLET DEICE BOOT. THEY WERE ALERTED BY AN AMBER CAS MESSAGE DEICE BOOT FAIL. AIRCRAF

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB NYC04IA116](https://openairdocs.org/ntsb/NYC04IA116), May 3, 2004: Dornier DO-328-100 (N441JS), Allentown, PA, incident, no damage. Probable cause: The opening of the main cabin door after takeoff, for undetermined reasons.

## 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 20040503019809I](https://openairdocs.org/incident/20040503019809I), May 3, 2004: Dorner DO328100 (N441JS), Allentown, PA, Minor damage. (-23) On takeoff, cabin door came completely open. Flight attendant reached across aisle to passengers in seats 1D and 1F for assistance. Allegheny commuter…
- [Incident 20000203002599I](https://openairdocs.org/incident/20000203002599I), Feb 3, 2000: Dorner DO328100 (N441JS), Pittsburgh, PA. On February 3, 2000, at 1022EA, a DO-328, s/n 3059, registered as N441JS, operated by "vnaa" (psa airlines) as flight 4003 returned to Pittsburgh, PA (pit) sue…

## Other aircraft with N441JS

- [Cancelled 2022-11-05](https://openairdocs.org/deregistered/N441JS-2022-11-05): Jack Sharp ZODIAC 601-HD, S/N 6-8916. Registration expired, pending cancellation. Owner: [Sharp Jack D](https://openairdocs.org/faa-owner/SHARP%20JACK%20D), [Prineville, OR](https://openairdocs.org/faa-place/OR/Prineville)

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