# N424JS: 1995 Dornier Luftfahrt 328-100, registration cancelled 2013-11-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 13, 2013 - Status when cancelled: Registration expired, pending cancellation - 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: 3033 - Year built: 1995 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: March 3, 1995 - Certificate issued: October 2, 2007 - Last registry action: October 2, 2007 - Mode S code: A50B54 - Owner when cancelled: [Ada USA Inc](https://openairdocs.org/faa-owner/ADA%20USA%20INC) - Location: [Doral, FL](https://openairdocs.org/faa-place/FL/Doral) - Owner type: Corporation - Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N424JS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=424JS - Page: https://openairdocs.org/deregistered/N424JS-2013-11-13 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 (75, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR VNAA0408015](https://openairdocs.org/sdr/VNAA0408015), Aug 29, 2004: GCU. FAILED. DURING TAKEOFF, THE CREW RECEIVED A LT GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE LT GENERATOR CONROL UNIT IN ACCORDA - [SDR VNAA0408012](https://openairdocs.org/sdr/VNAA0408012), Aug 19, 2004: CIRCUIT BREAKER. TRIPPED. DURING CLIMBOUT, THE CREW RECEIVED AN ELEVATOR ASYMMETRY CAS MESSAGE THEN FLIGHT 2540 RETURNED TO PIT. MAINTENANCE INSPECTED AND FOUND THE RIGHT HAND TRIM CIRCU - [SDR VNAA0401017](https://openairdocs.org/sdr/VNAA0401017), Jan 31, 2004: COMPUTER. FAILED. DURING FLIGHT, THE CREW RECEIVED A TAKEOFF CONFIGURATION WARNING INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 IAC IN ACCORDANCE W - [SDR VNAA0312005](https://openairdocs.org/sdr/VNAA0312005), Dec 9, 2003: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERIES IN ACCORDANCE WITH DORNIER MAINTENANCE - [SDR VNAA0309004](https://openairdocs.org/sdr/VNAA0309004), Sep 7, 2003: GENERATOR. FAILED. DURING TAKEOFF, THE CREW RECEIVED A NR 1 DC GENERATOR FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CREW THEN RESET THE GENERATOR AND WAS CLEARED FOR ANOTHER TAKEOF - [SDR VNAA0309005](https://openairdocs.org/sdr/VNAA0309005), Aug 8, 2003: BPCU. FAILED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL AND DISPLAYS 3, 4, AND 5 FAILED AND THE CREW ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED TH - [SDR VNAA0307001](https://openairdocs.org/sdr/VNAA0307001), Jul 9, 2003: CONNECTOR. FAILED. THE CREW RECEIVED AN INDICATION THAT THE LEFT HAND PROP WAS ONLY PRODUCING 36 NP. THE FLIGHT THEN RETURNED TO EVV. OUTSTATION MAINTENANCE INSPECTED AND CLEANED - [SDR VNAA0306006](https://openairdocs.org/sdr/VNAA0306006), Jun 12, 2003: CONTROLLER. FAILED. DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE AIRCRAFT WAS THEN FERRIED TO CAK. MAINTENANCE INSPECTED AND RE - [SDR VNAA0305015](https://openairdocs.org/sdr/VNAA0305015), May 21, 2003: GASKET. LOOSE. DURING THE CLIMBOUT, THE CREW HEARD A BANGING NOISE ON THE FUSELAGE AND RETURNED TO DAY. MAINTENANCE INSPECTED AND FOUND A PIECE OF WEATHER STRIPPING LOOSE AT T - [SDR VNAA0301020](https://openairdocs.org/sdr/VNAA0301020), Jan 20, 2003: REGULATOR. FAILED. DURING CLIMBOUT, THE CREW RECEIVED AN ELEVATOR TRIM FAIL INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WERE INSTRUCTED TO DIVERT TO DAY AND LAN - [SDR VNAA0212039](https://openairdocs.org/sdr/VNAA0212039), Dec 31, 2002: PSEU. FAILED. DURING TAKE OFF, THE AIRCRAFT STARTED PULLING TO THE LEFT AT 70 KNOTS AND THE CREW ABORTED TAKE OFF. MAINTENANCE INSPECTED AND REPLACED THE TORQUE LINKS, PSEU, - [SDR VNAA0212037](https://openairdocs.org/sdr/VNAA0212037), Dec 30, 2002: POTENTIOMETER. FAILED. WHEN THE CONDITION LEVERS WERE ADVANCED FOR TAKE OFF, THE AIRCRAFT JUMPED TO THE LEFT, WHEN BROUGHT BACK, JUMPED BACK TO THE RIGHT. THE CREW THEN ABORTED TAKE O - [SDR VNAA0211005](https://openairdocs.org/sdr/VNAA0211005), Nov 6, 2002: RELAY. FAILED. DURING CLIMB, THE CREW ADVISED DISPATCH THAT THE NORMAL ELEVATOR TRIM WOULD NOT WORK IN THE NOSE DOWN DIRECTION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK - [SDR VNAA0210024](https://openairdocs.org/sdr/VNAA0210024), Oct 23, 2002: RELAY. FAILED. DURING THE CLIMB, THE CREW REPORTED A MAIN ELEVATOR TRIM FAIL. THE CREW ENGAGED THE STANDBY TRIM AND HAD NO FURTHER PROBLEMS. AFTER ARRIVAL IN PIT, MAINTENANCE - [SDR VNAA0209031](https://openairdocs.org/sdr/VNAA0209031), Sep 22, 2002: GENERATOR. FAILED. DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND DC GENERATOR FAIL CAS MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND CLEANED THE GENERATOR CANNON PLUG A - [SDR VNAA0208039](https://openairdocs.org/sdr/VNAA0208039), Aug 25, 2002: WIRE. FAILED. THE CREW REPORTED THAT THE 9A EMERGENCY FLOOR LIGHT STRIP WAS LOOSE AND INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED A WIRE ON THE LIGHT STRIP AND RESECURED - [SDR VNAA0204015](https://openairdocs.org/sdr/VNAA0204015), Apr 19, 2002: ECU. FAILED. DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL CAS MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND CLEANED THE INTERCOMP BLEED - [SDR VNAA0204014](https://openairdocs.org/sdr/VNAA0204014), Apr 19, 2002: ECU. FAILED. DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL CAS MESSAGE AND ABORTED TAKE OFF. AS THE AIRCRAFT CLEARED THE RUNWAY THE MESSAGE EXTINGU - [SDR VNAA0203016](https://openairdocs.org/sdr/VNAA0203016), Mar 11, 2002: BRAKE. FAILED. DURING TAKE OFF THE CREW RECEIVED A LEFT HAND INBOARD BRAKE OVERHEAT INDICATION AND ABORTED TAKE OFF. THE CREW CALLED MAINTENANCE CONTROL AND DEFFERRED THE BRAK - [SDR VNAA0201016](https://openairdocs.org/sdr/VNAA0201016), Jan 20, 2002: ECU. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ELECTRONIC CONTROL UNIT FAIL MESSAGE AND ABORTED TAKEOFF. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND RESET - [SDR VNAA0201011](https://openairdocs.org/sdr/VNAA0201011), Jan 10, 2002: CONNECTOR. DIRTY. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ELECTRONIC CONTROL UNIT FAIL CAS MESSAGE AND ABORTED TAKEOFF. OUTSTATION MAINTENANCE CLEANED THE LEFT HAND ELECTRO - [SDR VNAA0201010](https://openairdocs.org/sdr/VNAA0201010), Jan 9, 2002: CONNECTOR. DIRTY. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ELECTRONIC CONTROL UNIT FAIL CAS MESSAGE AND ABORTED TAKEOFF. OUTSTATION MAINTENANCE CLEANED THE LEFT HAND ELECTRO - [SDR VNAA0201009](https://openairdocs.org/sdr/VNAA0201009), Jan 7, 2002: ALTERNATOR. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ELECTRONIC CONTROL UNIT AND LEFT HAND ALTERNATOR FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE MESSAGE CLEARED AS FLIG - [SDR VNAA0112017](https://openairdocs.org/sdr/VNAA0112017), Dec 23, 2001: BLEED VALVE. FAILED. DURING TAKE OFF THE CREW RECEIVED A BLEED VALVE SHUTOFF FAIL MESSAGE AND ABORTED TAKE OFF. THE CREW CALLED MAINTENANCE CONTROL AND RESET THE SYSTEM. FLIGHT 4062 - [SDR VNAA0110001](https://openairdocs.org/sdr/VNAA0110001), Oct 3, 2001: WIRE. CHAFED. DURING TAXI, THE CREW RECEIVED AN INTERMITTENT CARGO FIRE CAS MESSAGE AND FIRE WARNING ON THE RED WARNING PANEL. FLIGHT 4019 RETURNED TO THE GATE. MAINTENANCE I - [SDR VNAA0109018](https://openairdocs.org/sdr/VNAA0109018), Sep 26, 2001: DAU. FAILED. THE CREW REPORTED THAT THE CARGO SMOKE AND FIRE DETECT LIGHTS WERE INTERMITTENTLY COMING ON. MAINTENANCE INSPECTED AND REPLACED THE NUMBER 2 DATA ACQUISITION UN - [SDR VNAA0109014](https://openairdocs.org/sdr/VNAA0109014), Sep 24, 2001: CONTROL BOX. FAILED. THE CARGO FAIL CAS MESSAGE AND THE RED CARGO FIRE BUTTON CAME ON INTERMITTENTLY. MAINTENANCE INSPECTED AND REPLACED THE DIMMER BOX IN ACCORDANCE WITH DORNIER MA - [SDR VNAA0107005](https://openairdocs.org/sdr/VNAA0107005), Jul 4, 2001: RADAR. FAILED. FLIGHT 4075 WAS CLIMBING THROUGH 15,000 FEET AND THE WEATHER RADAR BEGAN TO MALFUNCTION. THE CREW CONTACTED DISPATCH AND WAS ADVISED TO RETURN TO PIT. MAINTENAN - [SDR VNAA0106017](https://openairdocs.org/sdr/VNAA0106017), Jun 23, 2001: VALVE. FAILED. ON CLIMB OUT OF PIT THE RIGHT LOW PRESSURE BLEED VALVE FAILED. AIRCRAFT RETURNED TO PIT AND MAINTENANCE REPLACED THE VALVE AND OPERATIONAL CHECK GOOD - [SDR VNAA0105007](https://openairdocs.org/sdr/VNAA0105007), May 11, 2001: TIRE. FLAT. WHILE TAXIING FROM THE RUNWAY AFTER LANDING, THE CREW NOTICED A VIBRATION WHICH WAS GETTING STRONGER. THE CREW STOPPED THE AIRCRAFT AND THE CAPTAIN GOT OUT AND - [SDR VNAA0104020](https://openairdocs.org/sdr/VNAA0104020), Apr 30, 2001: LIGHT. INOPERATIVE. DURING LANDING, AT THE OUTER MARKER THE CREW LOWERED THE GEAR BUT DID NOT RECEIVE THREE GREEN GEAR INDICATIONS. THE CREW EXECUTED A GO-AROUND, REFERENCED THE QU - [SDR VNAA0101020](https://openairdocs.org/sdr/VNAA0101020), Jan 22, 2001: RECORDER. MALFUNCTIONED. DURING THE TAKEOFF ROLL, THE CREW RECEIVED A FLIGHT DATA RECORDER FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CREW CLEARED THE RUNWAY AND RESET THE FLIGHT DATA RE - [SDR VNAA0101019](https://openairdocs.org/sdr/VNAA0101019), Jan 21, 2001: EEC. MALFUNCTIONED. DURING THE TAKEOFF ROLL, THE CREW RECEIVED A CAS MESSAGE FOR LEFT HAND ELECTRONIC CONTROL UNIT FAIL. FLIGHT 4135 ABORTED TAKEOFF. AFTER THE AIRCRAFT CLEARED THE - [SDR VNAA0012028](https://openairdocs.org/sdr/VNAA0012028), Dec 29, 2000: FAN. FAILED. FLIGHT 4020, WHILE EN ROUTE FROM EVV TO PIT, DIVERTED TO CVG DUE TO SMOKE IN COCKPIT AND CABIN. MAINTENANCE TROUBLESHOT AND DISCOVERED THE AVIONICS FAN WAS FAIL - [SDR VNAA0011022](https://openairdocs.org/sdr/VNAA0011022), Nov 23, 2000: SENSOR. FAILED. THE CREW RECEIVED A LEFT HAND PUSHER AND SHAKER FAIL CAS MESSAGE. MAINTENANCE CONTROL HAD THE CREW CYCLE A CIRCUIT BREAKER BUT THAT DID NOT FIX THE PROBLEM. MAI - [SDR VNAA0010001](https://openairdocs.org/sdr/VNAA0010001), Oct 2, 2000: KNOB. STUCK. AFTER THE AIRCRAFT TOOK THE RUNWAY, THE FIRST OFFICE NOTICED HIS RUDDER PEDALS WOULD NOT RESPOND. THE CREW DECIDED TO ABORT THE TAKEOFF AND RETURN TO THE GATE. - [SDR VNAA0008010](https://openairdocs.org/sdr/VNAA0008010), Aug 13, 2000: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY AFT TRACK LIGHTING WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK POSITION. OPER - [SDR VNAA0005013](https://openairdocs.org/sdr/VNAA0005013), May 26, 2000: EJECTOR VALVE. FAILED. WHILE EN ROUTE, THE CREW EXPERIENCED AN AIRFOIL DE-ICE FAIL ON THE TAIL IN FAST AND SLOW MODES. MAINTENANCE ADVISED THE CREW TO RETURN TO PIT DUE TO ICING CONDI - [SDR VNAA0005002](https://openairdocs.org/sdr/VNAA0005002), May 2, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHT STRIP AT ROW 9A WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION IN - [SDR VNAA0004009](https://openairdocs.org/sdr/VNAA0004009), Apr 5, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN AT ROW 9A WAS NOT WORKING. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY - [SDR VNAA0001019](https://openairdocs.org/sdr/VNAA0001019), Jan 24, 2000: STRUCTURE. DAMAGED. DURING TAKEOFF, FLT 9469 EXPERIENCED SUDDEN DECELERATION DUE TO HITTING HARD SLUSH, FOLLOWED BY A DOOR AND AHARS CAS MESSAGES. THE CREW THEN ABORTED TAKEOFF. MA - [SDR VNAA9912016](https://openairdocs.org/sdr/VNAA9912016), Dec 30, 1999: BOLT. FAILED. WHILE EN ROUTE, THE FLIGHT CREW RECEIVED A RED WARNING PANEL DOORS ALERT AND A MAIN CABIN DOOR CAS MESSAGE. MAINTENANCE CONTROL INSTRUCTED THE CREW TO RETURN TO - [SDR VNAA9907005](https://openairdocs.org/sdr/VNAA9907005), Jul 12, 1999: METERING UNIT. FAILED. THE CREW REPORTED THE AIRCRAFT BRAKES WERE PULSATING AND WOULD NOT STOP THE AIRCRAFT ADEQUATELY. MAINTENANCE INSPECTED AND REPLACED THE BRAKE METERING UNIT, IN - [SDR VNAA9903001](https://openairdocs.org/sdr/VNAA9903001), Mar 1, 1999: HUB. CRACKED. DURING THE INSPECTION FOR HARTZELL ALERT SERVICE BULLETIN HD-ASB-61-021, A SUSPECTED CRACK WAS NOTED ON THE RIGHT HAND PROPELLER HUB. MAINTENANCE REPLACED THE P - [SDR VNAA9901024](https://openairdocs.org/sdr/VNAA9901024), Jan 27, 1999: AHRS. FAILED. THE AIRCRAFT RETURNED TO THE FIELD AFTER RECEIVING A FLIGHT DIRECTOR, FLIGHT GUIDANCE AND A LEFT ATTITUDE FAIL WARNING MESSAGES. MAINTENANCE INSPECTED AND REPLA - [SDR VNAA9901014](https://openairdocs.org/sdr/VNAA9901014), Jan 14, 1999: POWER LEVER. LACK OF LUBE. THE LEFT HAND POWER LEVER FAILED TO ADVANCE ABOVE FLIGHT IDLE WHEN SELECTED DURING THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GA - [SDR VNAA9901011](https://openairdocs.org/sdr/VNAA9901011), Jan 13, 1999: SENSOR. DIRTY. THE AIRCRAFT RETURNED TO THE GATE FOLLOWING A CARGO DOOR WARNING MESSAGE. MAINTENANCE INSPECTED AND CLEANED THE DOOR SENSORS, IN ACCORDANCE WITH DORNIER MAINTEN - [SDR VNAA9812007](https://openairdocs.org/sdr/VNAA9812007), Dec 10, 1998: BLEED VALVE. FAILED. THE AIRCRAFT RETURNED TO THE GATE AFTER A LEFT HAND BLEED FAIL WARNING MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND LOW PRESSURE BLEED VALVE, IN AC - [SDR VNAA9811021](https://openairdocs.org/sdr/VNAA9811021), Nov 21, 1998: PCU. FAILED. THE RIGHT HAND PROPELLER FAILED TO COME OUT OF THE FEATHER POSITION, WHEN SELECTED. DURING THE ATTEMPT TO GET THE PROPELLER OUT OF FEATHER, THE RIGHT ENGINE WAS - [SDR VNAA9811014](https://openairdocs.org/sdr/VNAA9811014), Nov 15, 1998: VALVE. FAILED. A LEFT HAND AIR CONDITIONING PACK OVERHEAT WARNING MESSAGE ILLUMINATED, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENAN All 75: https://openairdocs.org/deregistered/N424JS-2013-11-13/reports.md ## Other aircraft with N424JS - [Registered now](https://openairdocs.org/aircraft/N424JS): Gulfstream Aerospace G-IV, S/N 1444, built 2001 --- 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.