# N434JS: 1995 Dornier Luftfahrt 328-100, registration cancelled 2006-04-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 6, 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: 3051 - Year built: 1995 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: August 8, 1995 - Certificate issued: August 9, 1995 - Last registry action: November 15, 2005 - Mode S code: A532D3 - 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/N434JS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=434JS - Page: https://openairdocs.org/deregistered/N434JS-2006-04-06 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 (71, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR VNAA0406001](https://openairdocs.org/sdr/VNAA0406001), Jun 2, 2004: HANDLE. FAILED. AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT GO UP AND THE CREW RETURNED TO CAK. MAINTENANACE INSPECTED AND REPLACED THE GEAR RETRACT CIRCUIT BREAKER IN ACCORDANCE - [SDR VNAA0405012](https://openairdocs.org/sdr/VNAA0405012), May 22, 2004: SMOKE DETECTOR. FAILED. THE CREW REPORTED GETTING A LAV SMOKE FAIL CAS MESSAGE. MAINTENANCE DEFERRED THE LAV SMOKE DETECTION SYSTEM WITH THE CREW PER 26-3 CODE C. - [SDR VNAA0403012](https://openairdocs.org/sdr/VNAA0403012), Mar 20, 2004: VALVE. FAILED. DURING FLIGHT, THE RIGHT HAND ENGINE ITT INDICATED 100 DEGREES HOTTER THAN THE LEFT HAND ENGINE AND THE CREW RETURNED TO DCA. MAINTENANCE INSPECTED AND REPLACED - [SDR VNAA0403007](https://openairdocs.org/sdr/VNAA0403007), Mar 3, 2004: PANEL. FAILED. THE CREW REPORTED SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHE - [SDR VNAA0403008](https://openairdocs.org/sdr/VNAA0403008), Mar 3, 2004: DISPLAY. FAILED. THE CREW REPORTED THAT A PRIMARY FUNCTION DISPLAY HAD FADED IN AND OUT TWICE. FLIGHT 2466 THEN DIVERTED TO CAK. MAINTENANCE INSPECTED AND REPLACED THE PRIMARY D - [SDR VNAA0403005](https://openairdocs.org/sdr/VNAA0403005), Mar 2, 2004: LIGHT. FAILED. THE CREW REPORTED THAT THE ROW 8 EMERGENCY FLOOR LIGHTING WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE AMBER LIGHT STRIP IN ACCORDANCE WITH DORNIER M - [SDR VNAA0312012](https://openairdocs.org/sdr/VNAA0312012), Dec 20, 2003: BLEED VALVE. FAILED. DURING TAKEOFF, THE LEFT BLEED VALVE FAILED TO CLOSE WITH THE APU ON AND THE CREW ABORTED TAKEOFF. THE CREW THEN PERFORMED CHECK OF THE SYSTEM WITH THE APU BLEE - [SDR VNAA0310008](https://openairdocs.org/sdr/VNAA0310008), Oct 9, 2003: ROD. OUT OF ADJUST. DURING CLIMBOUT, THE CREW RECEIVED A PASSENGER DOOR UNLOCK INDICATION AND RETURNED TO PHL. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND ADJUS - [SDR VNAA0310007](https://openairdocs.org/sdr/VNAA0310007), Oct 8, 2003: BOLT. FAILED. DURING CLIMBOUT, THE CREW RECEIVED A PASSENGER DOOR UNLOCK INDICATION AND RETURNED TO DAY. MAINTENANCE INSPECTED AND ADJUSTED THE OVERCENTER SWITCH AND SHOOT BO - [SDR VNAA0308018](https://openairdocs.org/sdr/VNAA0308018), Aug 26, 2003: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIE - [SDR VNAA0309007](https://openairdocs.org/sdr/VNAA0309007), Aug 8, 2003: SENSOR. FAILED. THE CREW REPORTED RECEIVING A RIGHT HAND SHAKER ON SIDE CAS MESSAGE AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE ANGLE OF ATTACK SENSOR IN A - [SDR VNAA0304021](https://openairdocs.org/sdr/VNAA0304021), Apr 22, 2003: POWER SUPPLY. FAILED. THE CREW REPORTED THAT THE 5LK EMERGENCY LIGHT POWER SUPPLY WAS BAD. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MA - [SDR VNAA0304016](https://openairdocs.org/sdr/VNAA0304016), Apr 18, 2003: SMOKE. DETECTED. THE CREW REPORTED SMOKE IN THE COCKPIT OVERHEAD PANEL OR LIGHT ON APU START. OUTSTATION MAINTENANCE INSPECTED THE APU AND FOUND NO DEFECTS, INSPECTED THE OVERHE - [SDR VNAA0303027](https://openairdocs.org/sdr/VNAA0303027), Mar 24, 2003: CONNECTOR. DISCONNECTED. THE CREW REPORTED THE EMERGENCY FLOOR LIGHTS AT ROWS 4-6 WERE INOPERTIVE. MAINTENANCE RESECURED LIGHT STRIP CONNECTION AND PERFORMED OPERATIONAL CHECK IN ACCORD - [SDR VNAA0303015](https://openairdocs.org/sdr/VNAA0303015), Mar 12, 2003: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 4 TO 6 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDA - [SDR VNAA0303001](https://openairdocs.org/sdr/VNAA0303001), Mar 2, 2003: FAN. FAILED. THE CREW REPORTED A LEFT HAND HX FAN FAIL, THEN A LEFT HAND PACK OVERHEAT, AND THEN A LAV SMOKE CAS MESSAGE. THE CREW WITH MAINTENANCE CONTROL MEL'D THE LEFT HA - [SDR VNAA0302007](https://openairdocs.org/sdr/VNAA0302007), Feb 10, 2003: WARNING LIGHT. FALSE INDICATION. THE CREW RECEIVED A LAV SMOKE CAS MESSAGE, THERE WAS NO LAV FIRE. MAINTENANCE CONTROL DEFERRED THE LAV FIRE EXTINGUISH SYSTEM IN ACCORDANCE WITH MEL 26-3 C. - [SDR VNAA0210012](https://openairdocs.org/sdr/VNAA0210012), Oct 13, 2002: LIGHT. INOPERATIVE. THE CREW REPORTED THAT THE EMERGENCY LIGHTING STRIP AT ROW 9A WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE LIGHTING STRIP AT ROW 9A IN ACCORDANC - [SDR VNAA0208032](https://openairdocs.org/sdr/VNAA0208032), Aug 21, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT THE REAR EXIT SIGN WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK PO - [SDR VNAA0207045](https://openairdocs.org/sdr/VNAA0207045), Jul 30, 2002: FLIGHT DIR. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A FLIGHT DIRECTOR FAIL IN THE HORIZONTAL MODE AND ABORTED TAKEOFF. ON THE TAXI WAY THE CREW CALLED MAINTENANCE CONTROL AND RES - [SDR VNAA0111013](https://openairdocs.org/sdr/VNAA0111013), Nov 30, 2001: AILERON. JAMMED. AILERONS MOMENTARILY JAMMED IN FLIGHT. JERKED FREE AND CONTROLS REMAINED STIFF. FLIGHT 4064 RETURNEDTO PIT. MAINTENANCE VISUALLY INSPECTED AILERON CONTROL CABLE - [SDR VNAA0111008](https://openairdocs.org/sdr/VNAA0111008), Nov 18, 2001: SWITCH. FAILED. AFTER DEPARTING PHL, THE CREW RECEIVED A PACK FAIL AND OVER PRESSURE INDICATION. MAINTENANCE CONTROL AND DISPATCH DECIDED THAT FLIGHT 4062 SHOULD DIVERT TO CAK. - [SDR VNAA0107025](https://openairdocs.org/sdr/VNAA0107025), Jul 30, 2001: COMPUTER. FAILED. DURING THE TAKE OFF ROLL, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL CAS MESSAGE. THE CREW ABORTED TAKE OFF. WHEN EXITTING THE RUNWAY THE COMPUTER RESET - [SDR VNAA0107012](https://openairdocs.org/sdr/VNAA0107012), Jul 8, 2001: VALVE. FAILED. DURING TAXI THE CREW RECEIVED A EMERGENCY PARKING BRAKE ACCUMULATOR FAIL CAS MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND FOLLOWED THE PROCEDUR - [SDR VNAA0107010](https://openairdocs.org/sdr/VNAA0107010), Jul 8, 2001: CONTROLLER. MALFUNCTIONED. DURING CLIMBOUT THE CABIN FAILED TO PRESSURIZE AND MAINTENANCE DECIDED TO MEL THE PRESSURIZATION. DUE TO FUEL CONSIDERATION AT THE LOWER ALTITUDE FLIGHT 4021 DI - [SDR VNAA0107007](https://openairdocs.org/sdr/VNAA0107007), Jul 4, 2001: PSU. MALFUNCTIONED. FLIGHT 4012 WAS APPROXIMATELY 50 NM NE OF LEX AND THE FLIGHT ATTENDANT NOTIFIED THE CREW OF A BURNING SMELL IN THE CABIN. THE CAPTAIN VERIFIED THE SMELL. THE CA - [SDR VNAA0106019](https://openairdocs.org/sdr/VNAA0106019), Jun 26, 2001: PANEL. FAILED. DURING CLIMB, AT 4200MSL, THE CREW HEARD A NOISE AND DETERMINED THERE WAS A PROBLEM WITH THE PRESSURIZATION SYSTEM. THE CREW CONTACTED MAINTENANCE CONTROL AND W - [SDR VNAA0105020](https://openairdocs.org/sdr/VNAA0105020), May 28, 2001: BLEED VALVE. FAILED. DURING CLIMBOUT THE RIGHT HAND PACK FAILED. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK THEN HAD A DUAL PACK OVERPRESSURE FAIL CAS MESSAGE. THE CREW DECIDED - [SDR VNAA0103010](https://openairdocs.org/sdr/VNAA0103010), Mar 10, 2001: HARNESS. DEFECTIVE. AFTER TAKING THE RUNWAY FLIGHT 4168 RECEIVED A PROXIMITY SYSTEM FAIL WARNING MESSAGE. THE FLIGHT CREW THEN CLEARED THE RUNWAY. MAINTENANCE INSPECTED THE AIRCRAF - [SDR VNAA0103001](https://openairdocs.org/sdr/VNAA0103001), Mar 3, 2001: DOOR. NOT SEATED. DURING CLIMBOUT THE AIRCRAFT WOULD NOT PRESSURIZE. THE FLIGHT CREW RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND RESEATED THE AVIONICS BAY MAINTENANCE HATCH - [SDR VNAA0102019](https://openairdocs.org/sdr/VNAA0102019), Feb 7, 2001: WARNING SYSTEM. ACTIVATED. AS THE AIRCRAFT WAS TAXIING ON TO THE RUNWAY RECEIVED A PACK FAIL CAS MESSAGE. THE CREW ADVISED TOWER OF NEED TO EXIT THE RUNWAY. THE CREW WENT THRU THE QRH AND - [SDR VNAA0101023](https://openairdocs.org/sdr/VNAA0101023), Jan 25, 2001: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE NOT ILLUMINATING AT ROWS 4 THROUGH 6. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 5LK POSIT - [SDR VNAA0012026](https://openairdocs.org/sdr/VNAA0012026), Dec 26, 2000: HYDRO MECH UNIT. FAILED. FLIGHT 4070 ABORTED TAKEOFF AFTER POWER LEVERS WERE ADVANCED AND THE LEFT HAND ENGINE OVER TORQUED. MAINTENANCE INSPECTED AND REPLACED THE PROPELLER HYDRAULIC U - [SDR VNAA0012007](https://openairdocs.org/sdr/VNAA0012007), Dec 8, 2000: BRUSH BLOCK. DAMAGED. ENROUTE FROM PIT TO AZO, THE CREW RECEIVED A LEFT HAND PROPELLER HEAT FAIL CAS MESSAGE. FLIGHT 4169 DIVERTED TO DAY WHERE MAINTENANCE OHMED THE DE-ICE BOOTS AND - [SDR VNAA0011024](https://openairdocs.org/sdr/VNAA0011024), Nov 25, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHT BY THE FLIGHT ATTENDANT'S SEAT WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCO - [SDR VNAA0010013](https://openairdocs.org/sdr/VNAA0010013), Oct 18, 2000: BATTERY. DISCHARGED. FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY, OPS CHECK GOOD. - [SDR VNAA0009004](https://openairdocs.org/sdr/VNAA0009004), Sep 11, 2000: SEAL. OUT OF ADJ. FLIGHT 4155 OBSERVED A CABIN DIFFERENTIAL POUNDS PER SQUARE INCH OF .23 AT FLIGHT LEVEL 110 AND THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT 4155 DIVERTED INTO PIT - [SDR VNAA0009001](https://openairdocs.org/sdr/VNAA0009001), Sep 1, 2000: CONTROL PANEL. FAILED. FLIGHT 4171 RETURNED TO THE FIELD IN PITTSBURGH DUE TO NO PRESSURIZATION IN AUTO OR MANUAL MODE. MAINTENANCE INSPECTED AND REPLACED THE PRESSURE CONTROL PANEL I - [SDR VNAA0006004](https://openairdocs.org/sdr/VNAA0006004), Jun 13, 2000: PUMP. FAILED. AT THE START OF THE TAKEOFF ROLL, THE CREW RECEIVED A HYDRAULIC MAIN TEMPERATURE HIGH MESSAGE. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANC - [SDR VNAA0004010](https://openairdocs.org/sdr/VNAA0004010), Apr 5, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHTS AT ROWS 7 THROUGH 9 WERE NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION I - [SDR VNAA0003019](https://openairdocs.org/sdr/VNAA0003019), Mar 17, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE AT THE 6LK POSITION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WIT - [SDR VNAA0002016](https://openairdocs.org/sdr/VNAA0002016), Feb 20, 2000: BATTERY. INOPERATIVE. THE CREW NOTICED THAT EMERGENCY LIGHTS AT ROW SEVEN THROUGH NINE WERE NOT OPERATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH - [SDR VNAA0001009](https://openairdocs.org/sdr/VNAA0001009), Jan 8, 2000: RESISTOR. FAILED. EN ROUTE THE CREW NOTICED ELECTRICAL BURNING FUMES IN THE COCKPIT. THE F/A NOTED ELECTRICAL BURNING FUMES IN ROWS 1 AND 2. THE CREW DECLARED AN EMERGENCY AND DI - [SDR VNAA9912007](https://openairdocs.org/sdr/VNAA9912007), Dec 9, 1999: BATTERY. DISCHARGED. THE FLIGHT CREW FOUND THE EMERGENCY LIGHTS 7, 8, AND 9 NOT WORKING. THE AIRCRAFT WAS FERRIED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT - [SDR VNAA9911007](https://openairdocs.org/sdr/VNAA9911007), Nov 10, 1999: BATTERY. DISCHARGED. THE FLIGHT CREW FOUND THE EMERGENCY LIGHT AT SEAT 7A DID NOT WORK. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE L03 POSITION IN ACCORDANCE WI - [SDR VNAA9910009](https://openairdocs.org/sdr/VNAA9910009), Oct 16, 1999: BATTERY. DISCHARGED. THE FLIGHT CREW FOUND THE EMERGENCY EXIT LIGHT AT SEAT 9A WAS NOT WORKING. MAINTENANCE REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION IN ACCORDANCE WITH THE - [SDR VNAA9910001](https://openairdocs.org/sdr/VNAA9910001), Oct 3, 1999: BATTERY PACK. DISCHARGED. A SECTION OF EMERGENCY FLOOR LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY PACK IN ACCORDANCE WITH DORNIER - [SDR VNAA9908003](https://openairdocs.org/sdr/VNAA9908003), Aug 5, 1999: FIRE WARNING. ACTIVATED. THE AIRCRAFT RETURNED TO THE GATE FOR AN INTERMITTANT LAV FIRE WARNING INDICATION. MAINTENANCE INSPECTED AND REPLACED THE LAV FIRE BOTTLE, IN ACCORDANCE WITH DO - [SDR VNAA9902002](https://openairdocs.org/sdr/VNAA9902002), Feb 6, 1999: CONTROL PANEL. FAILED. THE AIRCRAFT RETURNED TO THE GATE FOLLOWING A CPCS MISCOMPARE WARNING MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE PRESSURIZATION CONTROL PANEL, IN ACCORDANC - [SDR VNAA9809027](https://openairdocs.org/sdr/VNAA9809027), Sep 30, 1998: SPRING. LOOSE. THE AIRCRAFT RETURNED TO THE GATE, DUE TO THE FIRST OFFICERS SEAT VERTICAL ADJUSTMENT FUNCTION BEING INOPERATIVE. MAINTENANCE INSPECTED AND RE-SECURED THE VERTI All 71: https://openairdocs.org/deregistered/N434JS-2006-04-06/reports.md ## FAA accident and incident reports (3) 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 20011029030759I](https://openairdocs.org/incident/20011029030759I), Oct 29, 2001: Dorner DO328100 (N434JS), Pittsburgh, PA. (-23) Psa (vnaa) flight 4189 reported a hydraulic problem and landed at kpit at 1833E on 10/29/01 without incident. The pilot discrepancy was an amber proxy… - [Incident 19980822036699I](https://openairdocs.org/incident/19980822036699I), Aug 22, 1998: Dorner DO328100 (N434JS), Pittsburgh, PA. (-5) Crew received a main hydraulic pump fail message and standby hydraulic system failure on eicas. The crew followed checklist and lowered landing gear.… - [Incident 19970527017539I](https://openairdocs.org/incident/19970527017539I), May 27, 1997: Dorner DO328100 (N434JS), Akron, OH. Narrative: a & p mechanic, terry s. hunsdorf (certificate no. 278722631) while accomplishing a high speed maintenance taxi check, permitted the aircraft to… --- 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.