# N328JS: 1995 Dornier Luftfahrt 328-100, registration cancelled 2008-11-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 26, 2008 - Exported to: Indonesia - Status when cancelled: Valid registration - 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: 3030 - Year built: 1995 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Special flight permit - Airworthiness date: July 21, 2008 - Certificate issued: October 9, 2007 - Last registry action: October 9, 2007 - Mode S code: A38CE1 - Owner when cancelled: [Comtran International Inc](https://openairdocs.org/faa-owner/COMTRAN%20INTERNATIONAL%20INC) - Location: [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio) - Owner type: Corporation - Owner's area on the map: 29.5387° N, 98.4913° W: Placed by OpenAirDocs at the center of ZIP code 78216, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N328JS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=328JS - Page: https://openairdocs.org/deregistered/N328JS-2008-11-26 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 (62, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR VNAA0308008](https://openairdocs.org/sdr/VNAA0308008), Aug 13, 2003: SMOKE DETECTOR. FAILED. THE CREW REPORTED THAT THE LAV SMOKE DETECTOR WAS INOP. MAINTENANCE THEN DEFERRED THE LAV SMOKE DETECTOR, 26-3 CODE C. - [SDR VNAA0307008](https://openairdocs.org/sdr/VNAA0307008), Jul 24, 2003: WARNING SYSTEM. MALFUNCTIONED. ON APPROACH TO PHL AT 6000 FEET AND 20 MILES WEST THE FLIGHT CREW RECEIVED A TCAS RA. THE FLIGHT CREW INIATED A DESCENT TO 5400 FEET WHERE THE TCAS RA ALERT CLE - [SDR VNAA0303007](https://openairdocs.org/sdr/VNAA0303007), Mar 6, 2003: DAU. FAILED. AFTER DEPARTING FROM DCA, THE CREW RECEIVED A WEIGHT ON WHEELS CAS MESSAGE AND ASSOCIATED PROXI SYSTEM FAIL CAS MESSAGES. FLIGHT 4031 WAS INSTRUCTED TO DIVERT T - [SDR VNAA0303002](https://openairdocs.org/sdr/VNAA0303002), Mar 3, 2003: SWITCH. FAILED. AFTER DEPARTING PIT, THE CREW ADVISED MAINTENANCE CONTROL OF A LEFT HAND PACK FAIL INDICATION. MAINTENANCE CONTROL ADVISED THE CREW TO RETURN TO PIT. MAINTENANC - [SDR VNAA0302020](https://openairdocs.org/sdr/VNAA0302020), Feb 23, 2003: A/C PACK. FAILED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND PACK OVERHEAT CAS MESSAGE AND ABORTED TAKEOFF. THE SYSTEM RESET ITSELF AND FLIGHT 4021 WAS CLEARED FOR ANOTHER TAK - [SDR VNAA0302005](https://openairdocs.org/sdr/VNAA0302005), Feb 9, 2003: WIRE HARNESS. FAILED. ON APPROACH, CREW LOWERED GEAR AND FAILED TO RECEIVE A GREEN DOWN & LOCKED INDICATION. CREW ABORTED LANDING. CREW MANUALLY LOWERED GEAR, CREW RECEIVED ALL GREEN - [SDR VNAA0211001](https://openairdocs.org/sdr/VNAA0211001), Nov 1, 2002: CONNECTOR. DIRTY. DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE AND ABORTED TAKEOFF. UPON RETURNING TO THE GATE, MAINTENANCE INSPECTED AND CLEANED THE - [SDR VNAA0209008](https://openairdocs.org/sdr/VNAA0209008), Sep 7, 2002: BRAKE. DURING TAKE OFF, THE CREW RECEIVED A HIGH BRAKE TEMPERATURE INDICATION AND ABORTED TAKE OFF. THE CREW TAXIED OFF THE RUNWAY AND WAITED FOR THE BRAKE TEMPERATUES - [SDR VNAA0208009](https://openairdocs.org/sdr/VNAA0208009), Aug 7, 2002: CONTROL UNIT. FAILED. DURING DESCENT, THE CAPTAIN REPORTED LOSING THE TRANSPONDER, RADIO MANAGEMENT UNITS 1 AND 2, FLIGHT MANAGEMENT SYSTEM, TCAS, AUTOMATIC DIRECTION FINDER, AND LOC - [SDR VNAA0202010](https://openairdocs.org/sdr/VNAA0202010), Feb 9, 2002: DAU. FAILED. DURING CLIMBOUT, THE CREW RECEIVED A NR 2 FAULT WARNING COMPUTER FAIL INDICATION AND RETURNED TO PIT. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE INSPECTED AND - [SDR VNAA0201001](https://openairdocs.org/sdr/VNAA0201001), Jan 1, 2002: A/C PACK. MALFUNCTIONED. AS THE CREW BEGAN TO APPLY POWER, THE CREW RECEIVED A RIGHT HAND PACK CAS MESSAGE AND ABORTED TAKEOFF. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND RESET - [SDR VNAA0112014](https://openairdocs.org/sdr/VNAA0112014), Dec 20, 2001: SENSOR. WHILE ENROUTE TO AZO,FLIGHT 4169 RECEIVED A LEFT HAND ENGINE HIGH OIL PRESSURE INDICATION, FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO TOL. MAINTENANC - [SDR VNAA0112015](https://openairdocs.org/sdr/VNAA0112015), Dec 20, 2001: LEAD. FAILED. DURING CLIMBOUT FROM PIT, THE CREW RECEIVED A LEFT HAND PROP HEAT FAIL MESSAGE AND RETURNED TO THE PIT. MAINTENANCE INSPECTED AND REPLACED TWO PROPELLER HEAT LE - [SDR VNAA0112010](https://openairdocs.org/sdr/VNAA0112010), Dec 12, 2001: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 7 TO 9 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION - [SDR VNAA0111006](https://openairdocs.org/sdr/VNAA0111006), Nov 13, 2001: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 6, 7, AND 8 WERE NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE W - [SDR VNAA0105003](https://openairdocs.org/sdr/VNAA0105003), May 6, 2001: WARNING SYSTEM. ACTIVATED. AT THE OUTER MARKER THE CREW ATTEMPTED TO LOWER THE LANDING GEAR AND RECEIVED A NOSE WHEEL STEERING POWER-UP FAIL CAS MESSAGE. THE CREW NOTIFIED THE TOWER AND P - [SDR VNAA0104017](https://openairdocs.org/sdr/VNAA0104017), Apr 25, 2001: SIGN. LOOSE. THE CREW REPORTED THAT THE EMERGENCY SIGN AT ROW 11A WAS MISSING A SCREW AND IS LOOSE. MAINTENANCE INSPECTED AND RESURED THE SIGN IN ACCORDANCE WITH DORNIER MAI - [SDR VNAA0102017](https://openairdocs.org/sdr/VNAA0102017), Feb 25, 2001: DUCT. FAILED. DURING FLIGHT THE LEFT ENGINE INLET DEICE AND LEFT OUTBOARD WING DEICE FAILED. THE FLIGHT DIVERTED TO PIT WHERE HIGH WINDS AND TURBULENCE CAUSED A MISSED APPROA - [SDR VNAA0101009](https://openairdocs.org/sdr/VNAA0101009), Jan 12, 2001: CONNECTOR. SHORTED. THIRTY MINUTES INTO THE FLIGHT, THE FLIGHT ATTENDANT INFORMED THE CAPTAIN THAT THERE WAS A ELECTRICAL SMELL IN THE GALLEY. THE FIRST OFFICER WENT BACK AND CONFI - [SDR VNAA0012024](https://openairdocs.org/sdr/VNAA0012024), Dec 25, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY TRACK LIGHTING AT ROW 9 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH D - [SDR VNAA0012014](https://openairdocs.org/sdr/VNAA0012014), Dec 17, 2000: BOOT. MISSING. DURING CLIMB OUT, THE SYSTEM PAGE SHOWED THAT THE RIGHT HAND DE-ICE BOOT WAS FAILING. THE FIRST OFFICER LOOKED AND SEEN SOME OF THE BOOT WAS MISSING. THE WEATHE - [SDR VNAA0011025](https://openairdocs.org/sdr/VNAA0011025), Nov 25, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHT WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE - [SDR VNAA0011019](https://openairdocs.org/sdr/VNAA0011019), Nov 19, 2000: WIRE. BROKEN. AFTER TAKE OFF, FLIGHT 4042 HAD A PROP HEAT FAIL CAS MESSAGE. DUE TO WEATHER AT THE DESTINATION, FLIGHT 4042 RETURNED TO PIT. MAINTENANCE INSPECTED AND REPAIRED - [SDR VNAA0009023](https://openairdocs.org/sdr/VNAA0009023), Sep 26, 2000: BATTERY. INOPERATIVE. THE CREW REPORTED THAT THE EMERGENCY LIGHTING ABOVE SEAT 9A WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK POSITION I - [SDR VNAA0009014](https://openairdocs.org/sdr/VNAA0009014), Sep 18, 2000: BLEED VALVE. FAILED. DURING CRUISE, FLIGHT 4082 HAD A CROSS BLEED VALVE FAIL IN THE OPEN POSITION. THE CREW ATTEMPTED TO TROUBLESHOOT THE PROBLEM IN FLIGHT THEN ELECTED TO RETURN TO - [SDR VNAA0009016](https://openairdocs.org/sdr/VNAA0009016), Sep 18, 2000: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE LAVATORY AND GALLEY EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE W - [SDR VNAA0008013](https://openairdocs.org/sdr/VNAA0008013), Aug 19, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK POSITION IN ACCORDANCE - [SDR VNAA0007009](https://openairdocs.org/sdr/VNAA0007009), Jul 13, 2000: RELAY. FAILED. DURING TAKEOFF, THE CREW RECEIVED A MAIN HYDRAULIC PUMP FAIL CAS MESSAGE. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. THE AIRCRAFT WAS FERRIED TO CAK WHE - [SDR VNAA0006001](https://openairdocs.org/sdr/VNAA0006001), Jun 2, 2000: BATTERY. FAILED. THE FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHTING AT THE 7LK POSITION WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7 - [SDR VNAA0005005](https://openairdocs.org/sdr/VNAA0005005), May 4, 2000: DOOR. LOOSE. DURING CLIMBOUT, THE CREW FELT A VIBRATION WHICH INCREASE AS SPEED INCREASED. THE CREW CONTACTED AIR TRAFFIC CONTROL AND REQUESTED TO RETURN TO THE FIELD. FLIGH - [SDR VNAA0004026](https://openairdocs.org/sdr/VNAA0004026), Apr 30, 2000: WARNING SYSTEM. ACTIVATED. DURING TAKEOFF, THE CREW RECEIVED AN ENGINE MISCOMPARE MESSAGE. THE CAS MESSAGE CLEARED AFTER CLEARING THE RUNWAY. THE CREW CONFERRED WITH MAINTENANCE CONTROL A - [SDR VNAA0004018](https://openairdocs.org/sdr/VNAA0004018), Apr 15, 2000: STICK SHAKER. FAILED. THE CREW RECEIVED A RIGHT HAND AOA AND RIGHT HAND SHAKER FAIL CAS MESSAGES ON CLIMB OUT. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CALLED MAINTENANCE C - [SDR VNAA0004011](https://openairdocs.org/sdr/VNAA0004011), Apr 5, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTS AT ROWS 8 THROUGH 9 AND THE EXIT SIGN WERE NOT WORKING. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANC - [SDR VNAA0003027](https://openairdocs.org/sdr/VNAA0003027), Mar 27, 2000: PROPELLER. LIGHTNING STRIKE. WHILE ON DESCENT INTO PIT, THE AIRCRAFT WAS STRUCK BY LIGHTNING. THE FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A LIGHTNING STRIKE INSP - [SDR VNAA9912006](https://openairdocs.org/sdr/VNAA9912006), Dec 8, 1999: POWER LEVER. FAILED. DURING THE TAKEOFF ROLL, THE CREW ADVANCED THE POWER LEVERS BUT THEY FAILED TO FULLY RELEASE. THE CREW ABORTED TAKEOFF AND PROCEEDED TO CHECK THE SYSTEM. AFTER - [SDR VNAA9911016](https://openairdocs.org/sdr/VNAA9911016), Nov 20, 1999: SENSOR. FAILED. DURING FLIGHT, WITH GEAR UP THE CREW RECEIVED THREE RED AND THREE GREEN INDICATIONS INTERMITTENTLY. MAINTENANCE INSPECTED AND REPLACED THE PROXIMITY SENSOR ELEC - [SDR VNAA9908010](https://openairdocs.org/sdr/VNAA9908010), Aug 30, 1999: CONTROL CABLE. BENT. FLIGHT CREW REPORTED LEFT ENGINE CONDITION LEVER DIFFICULT TO OPERATE. MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FERRY FLIGHT TO CAK. THE LEFT HAND CONDIT - [SDR VNAA9908009](https://openairdocs.org/sdr/VNAA9908009), Aug 27, 1999: FRICTION LOCK. STUCK. FLIGHT CREW REPORTED CONDITION LEVER VERY HARD TO MOVE AND FRICTION KNOB STUCK. MAINTENANCE INSPECTED AND LOOSENED THE FRICTION KNOB, IN ACCORDANCE WITH DORNIER - [SDR VNAA9906005](https://openairdocs.org/sdr/VNAA9906005), Jun 21, 1999: METERING UNIT. FAILED. ANTISKID FAILED ON TAXI OUT. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED BRAKE METERING UNIT. - [SDR VNAA9906008](https://openairdocs.org/sdr/VNAA9906008), Jun 16, 1999: FAN. FAILED. DURING ENGINE SHUT DOWN, SMOKE WAS NOTED IN THE COCKPIT. MAINTENANCE INSPECTED AND DEFERRED THE GROUND COOLING FAN IN ACCORDANCE WITH THE MINIMUM EQUIPMENT LIST - [SDR VNAA9903014](https://openairdocs.org/sdr/VNAA9903014), Mar 14, 1999: SWITCH. FAILED. DURING CRUISE FLIGHT, A PROXI SYSTEM FAIL WARNING MESSAGE WAS NOTED BY THE CREW. AN EMERGENCY WAS NOT DECLARED, BUT THE CREW REQUESTED EMERGENCY EQUIPMENT UPON - [SDR VNAA9903010](https://openairdocs.org/sdr/VNAA9903010), Feb 23, 1999: POWER SUPPLY. FAILED. DURING THE PREFLIGHT INSPECTION, THE EMERGENCY LIGHTS AT ROWS FOUR AND SIX WERE NOTED TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY - [SDR VNAA9902009](https://openairdocs.org/sdr/VNAA9902009), Feb 16, 1999: DISPLAY UNIT. FAILED. THE NUMBER ONE DISPLAY UNIT FAILED AFTER PUSHBACK. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NUMBER ONE DISPLAY UNIT, IN ACCORDA - [SDR VNAA9901019](https://openairdocs.org/sdr/VNAA9901019), Jan 20, 1999: BATTERY. DISCHARGED. THE EMERGENCY LIGHTS AT ROWS FOUR THROUGH SIX WERE NOTED TO BE INOPERATIVE DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIG - [SDR VNAA9812019](https://openairdocs.org/sdr/VNAA9812019), Dec 28, 1998: BATTERY. DISCHARGED. DURING THE PREFLIGHT INSPECTION, EMERGENCY LIGHTS WERE NOTED TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE BATTERY PACK AT POSITION 5LK. OPERATIONAL - [SDR VNAA9811012](https://openairdocs.org/sdr/VNAA9811012), Nov 11, 1998: HYD FLUID. REQD SERVICE. A-HYDRAULIC QUANTITY LOW WARNING MESSAGE ILLUMINATED, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND SERVICED THE - [SDR VNAA9807013](https://openairdocs.org/sdr/VNAA9807013), Jul 29, 1998: ACTUATOR. FAILED. WHEN THE LANDING GEAR WAS SELECTED DOWN DURING APPROACH, THE RT MAIN GEAR UNLOCK LIGHT REMAINED ILLUMINATED. THE ACFT CLIMBED TO 8000 FT AND MADE ANOTHER ATTEMP - [SDR VNAA9806005](https://openairdocs.org/sdr/VNAA9806005), Jun 6, 1998: ENGINE. BIRD STRIKE. WHILE INBOUND TO PIT, THE AIRCRAFT WAS STRUCK BY A BIRD ON THE RIGHT HAND ENGINE NACELLE. THE FLIGHT CONTINUED TO PIT, AND LANDED WITHOUT ANY INCIDENT. MAINTENA - [SDR VNAA9805011](https://openairdocs.org/sdr/VNAA9805011), May 20, 1998: CIRCUIT BREAKER. TRIPPED. THE AIRCRAFT RETURNED TO THE GATE AFTER RECEIVING AN ANGLE OF ATTACK, AND SHAKER FAIL WARNING MESSAGES. MAINTENANCE INSPECTED AND FOUND THE RIGHT HAND ANGLE OF - [SDR VNAA9804015](https://openairdocs.org/sdr/VNAA9804015), Apr 17, 1998: AOA SENSOR. FAILED. DURING TAXI FOR TAKEOFF, A STICK PUSHER AND ANGLE OF ATTACK FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTE All 62: https://openairdocs.org/deregistered/N328JS-2008-11-26/reports.md ## Other aircraft with N328JS - [Registered now](https://openairdocs.org/aircraft/N328JS): DJI AGRAS T50, S/N 63YBLAQ0020047 --- 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.