# N426JS: 1995 Dornier Luftfahrt 328-100, registration cancelled 2009-05-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 21, 2009 - 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: 3038 - Year built: 1995 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: April 21, 1995 - Certificate issued: January 11, 2008 - Last registry action: January 11, 2008 - Mode S code: A512C2 - 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/N426JS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=426JS - Page: https://openairdocs.org/deregistered/N426JS-2009-05-21 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 (81, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR VNAA0407001](https://openairdocs.org/sdr/VNAA0407001), Jul 4, 2004: SENSOR. FAILED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA AND PUSHER FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE VISUALLY INSPECTED THE SYSTEM AND PERFORMED OPERAT - [SDR VNAA0406012](https://openairdocs.org/sdr/VNAA0406012), Jun 16, 2004: GCU. FAILED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL INDICATION AND ABORTED TAKEOFF. ON TAXI BACK, THE CREW RECEIVED A DC GENERATOR FAIL CAS M - [SDR VNAA0406011](https://openairdocs.org/sdr/VNAA0406011), Jun 15, 2004: WARNING LIGHT. ILLUMINATED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND STICK SHAKER PUSHER ON SIDE FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE SHAKER PUSHER RESET ITSELF AND FLIGHT 2417 W - [SDR VNAA0405011](https://openairdocs.org/sdr/VNAA0405011), May 18, 2004: CONTROL UNIT. FAILED. THE CREW REPORTED THAT A FIRE SQUIB WAS FAILING TO TEST. MAINTENANCE INSPECTED AND REPLACED THE FIRE WARNING CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE - [SDR VNAA0403014](https://openairdocs.org/sdr/VNAA0403014), Mar 26, 2004: SENSOR. FAILED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA AND PUSHER FAIL THEN ABORTED TAKEOFF. AS THE AIRCRAFT PULLED OFF OF THE RUNWAY IT CORRECTED ITSELF, THE CREW R - [SDR VNAA0401003](https://openairdocs.org/sdr/VNAA0401003), Jan 8, 2004: SENSOR. FAILED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA FAIL INDICATION AND ABORTED TAKEOFF. FLIGHT 2463 THEN RETURNED TO THE GATE TO HAVE MAINTENANCE REST THE AOA VA - [SDR VNAA0310012](https://openairdocs.org/sdr/VNAA0310012), Oct 19, 2003: CONTROL UNIT. FAILED. THE CREW REPORTED RECEIVING A APU FIRE LOOP FAIL AND A FALSE FIRE INDICATION. MAINTENANCE INSPECTED AND REPLACED THE FIRE DETECTION CONTROL UNIT IN ACCORDANCE W - [SDR VNAA0310004](https://openairdocs.org/sdr/VNAA0310004), Oct 4, 2003: LINE. FAILED. DURING FLIGHT, THE CREW RECEIVED A RIGHT HAND ENGINE INTAKE DE-ICE FAIL INDICATION AND RETURNED TO PHL. MAINTENANCE INSPECTED AND REPLACED THE INTAKE LINE IN AC - [SDR VNAA0309009](https://openairdocs.org/sdr/VNAA0309009), Sep 14, 2003: DAU. FAILED. THE CREW REPORTED A LT PUSHER FAIL CASS MESSAGE. AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED LT DATA ACQUISION UNIT IN ACCORDANCE WITH - [SDR VNAA0308002](https://openairdocs.org/sdr/VNAA0308002), Aug 4, 2003: FUSE. BLOWN. WITH THE EXTERNAL POWER HOOKED UP, SMOKE ENTERED THE FLIGHT DECK AND THE PASSENGERS WERE DEPLANED. MAINTENANCE INSPECTED AND REPLACED BOTH FUSES IN THE GROUND P - [SDR VNAA0304002](https://openairdocs.org/sdr/VNAA0304002), Apr 6, 2003: BRAKE. FAILED. THE CREW REPORTED THAT THE CAPTAIN'S BRAKES HIT THE STOP WITHOUT ANY BRAKING ACTION TAKING PLACE. MAINTENANCE INSPECTED AND BLED THE BRAKES IN ACCORDANCE WITH D - [SDR VNAA0303034](https://openairdocs.org/sdr/VNAA0303034), Mar 30, 2003: DAU. FAILED. AFTER TAKEOFF THE RIGHT PROPELLER HEAT FAILED. THE FLIGHT CREW RETURNED TO THE FIELD. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE RIGHT DATA ACQUISTION UN - [SDR VNAA0303032](https://openairdocs.org/sdr/VNAA0303032), Mar 29, 2003: VALVE. FAILED. DURING TAKEOFF CREW REPORTED AOA, SHAKER AND PUSHER FAIL. MESSAGE CLEARED AFTER EXITING RUNWAY. THEN CREW REPORTED LT PACK WOULD NOT COOL IN EITHER MODE. AIRCRA - [SDR VNAA0302026](https://openairdocs.org/sdr/VNAA0302026), Feb 27, 2003: BRUSH BLOCK. FAILED. DURING CRUISE, THE RIGHT HAND PROP HEAT FAILED. DUE TO LIGHT SNOW AT THE DESTINATION, FLIGHT 4050 DIVERTED TO DAY. MAINTENANCE INSPECTED AND FOUND THE BRUSHBLOC - [SDR VNAA0301027](https://openairdocs.org/sdr/VNAA0301027), Jan 24, 2003: PROXIMITY SWITCH. OUT OF ADJUST. EN ROUTE, THE MASTER CAUTION LIGHT ILLUMINATED AND THE PRESSURE CHECKED GOOD. THE CREW DESCENDED AND SLOWED TO 150 KIAS. AT FL180 THE LIGHT EXTINGUISHED. UPON A - [SDR VNAA0301018](https://openairdocs.org/sdr/VNAA0301018), Jan 18, 2003: PROXIMITY SWITCH. FAILED. EN ROUTE, THE CREW RECEIVED A OPEN DOOR INDICATION ON THE RED WARNING PANEL FOR THE PASSENGER DOOR. THERE WAS NO LOSS OF PRESSURE AND THE DOOR WAS SECURE. FLIGH - [SDR VNAA0212030](https://openairdocs.org/sdr/VNAA0212030), Dec 25, 2002: WARNING SYSTEM. MALFUNCTIONED. AFTER THE POWER LEVERS WERE ADVANCED, THE CREW RECEIVED A ANGLE OF ATTACK FAIL MESSAGE AND ABORTED TAKEOFF. THE MESSAGE EXTINGUISHED BY ITSELF AND FLIGHT 4172 W - [SDR VNAA0211016](https://openairdocs.org/sdr/VNAA0211016), Nov 14, 2002: STALL WARNING. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED AN AOA SENSOR FAIL CAWS MESSAGE AND ABORTED TAKEOFF. AFTER CLEARING THE RUNWAY THE MESSAGE CLEARED AND FLIGHT 4165 WAS CLEARED - [SDR VNAA0210025](https://openairdocs.org/sdr/VNAA0210025), Oct 23, 2002: SENSOR. OUT OF ADJUST. EN ROUTE AT 27,000 FEET, THE CREW RECEIVED A DOORS LIGHT ON THE RED WARNING PANEL. THERE WAS NO CHANGE IN THE PRESSURIZATION. THE CREW DESCENDED TO 15,000 FEET - [SDR VNAA0208021](https://openairdocs.org/sdr/VNAA0208021), Aug 13, 2002: PANEL. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLACE - [SDR VNAA0207008](https://openairdocs.org/sdr/VNAA0207008), Jul 9, 2002: POWER SUPPLY. FAILED. THE CREW REPORTED THAT THE FORWARD EMERGENCY POWER SUPPLY WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNI - [SDR VNAA0207004](https://openairdocs.org/sdr/VNAA0207004), Jul 5, 2002: WARNING SYSTEM. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. AFTER EXITING THE RUNWAY, THE SYSTEM RESET ITSELF AND THE MESSAGE EXTINGUISHE - [SDR VNAA0203024](https://openairdocs.org/sdr/VNAA0203024), Mar 16, 2002: STALL WARNING. MALFUNCTIONED. THE FLIGHT WAS ON THE TAKEOFF ROLL WHEN THE FLIGHT CREW RECEIVED A STALL PUSHER FAIL WARNING MESSAGE ON THE EICAS DISPLAY. THE FLIGHT CREW ABORTED THE TAKEOFF A - [SDR VNAA0202015](https://openairdocs.org/sdr/VNAA0202015), Feb 13, 2002: ENGINE. FAILED. AFTER BEING CLEAR FOR A VISUAL APPROACH, THE CREW REPORTED ENTERING AN AREA OF MODERATE TURBULENCE. THERE WAS A SINGLE JOLT, NOBODY SUSTAIN ANY SERIOUS INJURIES - [SDR VNAA0201017](https://openairdocs.org/sdr/VNAA0201017), Jan 21, 2002: STICK SHAKER. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND SHAKER FAIL MESSAGE AND ABORTED TAKEOFF. THE MESSAGE CLEARED AND MAINTENANCE CONTROL CLEARED FLIGHT 4050 FOR ANOTH - [SDR VNAA0111002](https://openairdocs.org/sdr/VNAA0111002), Nov 2, 2001: WARNING SYSTEM. MALFUNCTIONED. AT THE BEGINNING OF THE TAKEOFF ROLL, THE CREW RECEIVED A PUSHER CAS MESSAGE AND ABORTED TAKEOFF. AFTER CLEARING THE RUNWAY THE MESSAGES CLEARED. THE CREW AND M - [SDR VNAA0110020](https://openairdocs.org/sdr/VNAA0110020), Oct 26, 2001: WARNING SYSTEM. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A PUSHER FAIL AND AOA CAS MESSAGES AND ABORTED TAKEOFF. THE MESSAGES WENT OUT ALMOST IMMEDIATELY AND THE CREW ATTEMPTED ANOTHE - [SDR VNAA0110011](https://openairdocs.org/sdr/VNAA0110011), Oct 16, 2001: STALL WARNING. MALFUNCTIONED. DURING THE TAKEOFF ROLL, THE CREW RECEIVED AN ANGLE OF ATTACK CHIME AND FAILURE. ABORTED THE TAKEOFF. AS FLIGHT 4138 CLEARED THE RUNWAY THE MESSAGE CLEARED. THE - [SDR VNAA0109012](https://openairdocs.org/sdr/VNAA0109012), Sep 20, 2001: STARTER GEN. FAILED. AT APPROXIMATELY 60 KNOTS THE CREW RECEIVED A LEFT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE STARTER GENERATOR IN - [SDR VNAA0108008](https://openairdocs.org/sdr/VNAA0108008), Aug 15, 2001: VALVE. FAILED. ON APPROACH TO AZO, THE GEAR WAS SELECTED DOWN AND THE CREW RECEIVED NO GEAR INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND MANUALLY LOWERED THE - [SDR VNAA0108003](https://openairdocs.org/sdr/VNAA0108003), Aug 6, 2001: WARNING SYSTEM. MALFUNCTIONED. DURING THE TAKEOFF ROLL, THE CREW RECEIVED A TAKEOFF CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. THE CREW RESET THE SYSTEM AND ATTEMPTED ANOTHER TAKEOFF. FLI - [SDR VNAA0107013](https://openairdocs.org/sdr/VNAA0107013), Jul 9, 2001: WARNING SYSTEM. MALFUNCTIONED. DURING THE TAKEOFF ROLL, THE CREW RECEIVED A ENGINE MISCOMPARE CAS MESSAGE. THE CREW ABORTED TAKEOFF AND EXITED THE RUNWAY. THE CREW FOLLOWED THE QUICK REFERENC - [SDR VNAA0105004](https://openairdocs.org/sdr/VNAA0105004), May 8, 2001: METERING VALVE. FAILED. FLIGHT 4097 WAS TAXIING AND THE FIRST OFFICER'S LEFT HAND BRAKE WAS INEFFECTIVE AND THE CREW RETURNED TO THE GATE. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTEN - [SDR VNAA0103019](https://openairdocs.org/sdr/VNAA0103019), Mar 31, 2001: WINDOW. CRACKED. DURING CLIMBOUT THE FLIGHT CREW REPORTED THAT THE FIRST OFFICERS SIDE WINDOW HAD CRACKED. THE FLIGHT CREW RETURNED TO THE FIELD AND MADE AN UNEVENTFUL LANDING. - [SDR VNAA0012030](https://openairdocs.org/sdr/VNAA0012030), Dec 30, 2000: WARNING SYSTEM. FAILED. AFTER 10 MINUTES INTO THE FLIGHT, THE CREW RECEIVED AN AIRFOIL DEICE FAIL CAS MESSAGE. DISPATCH ADVISED THE CREW TO RETURN TO DAY WHERE MAINTENANCE INSPECTED AN - [SDR VNAA0012025](https://openairdocs.org/sdr/VNAA0012025), Dec 26, 2000: APU. FAILED. FLIGHT 4145 WAS EVACUATED AT THE GATE DUE TO SMOKE IN CABIN. OUTSTATION MAINTENANCE INSPECTED AND FOUND THE AUXILIARY POWER UNIT WAS BURNING OIL. THE AUXILIARY - [SDR VNAA0012009](https://openairdocs.org/sdr/VNAA0012009), Dec 9, 2000: CHIP DETECTOR. FAILED. AFTER DEPARTURE, THE CREW RECEIVED A LEFT HAND ENGINE CHIP DETECTOR LIGHT. MAINTENANCE CONTROL AND DISPATCH HAD FLIGHT 4012 RETURN TO DAY FOR MAINTENANCE. MAINT - [SDR VNAA0010003](https://openairdocs.org/sdr/VNAA0010003), Oct 3, 2000: BRAKE ASSY. MALFUNCTIONED. THE CREW REPORTED THAT THE FIRST OFFICER''S RIGHT HAND BRAKE PEDAL WENT TO THE FLOOR WITHOUT A RESPONSE FROM THE BRAKE SYSTEM. MAINTENANCE INSPECTED AND BLED TH - [SDR VNAA0007015](https://openairdocs.org/sdr/VNAA0007015), Jul 26, 2000: COMPUTER. FAILED. THE CREW REPORTED A SERIES OF PROXI FAIL MESSAGES. AFTER FOLLOWING THE QRH AND CHECKING THE CIRCUIT BREAKERS, THE CREW SELECTED THE GEAR HANDLE DOWN AND RECEIVE - [SDR VNAA0007010](https://openairdocs.org/sdr/VNAA0007010), Jul 13, 2000: BRAKE. FAILED. AFTER BEING PUSHED BACK FROM THE GATE, THE CAPTAIN NOTICE THE BRAKES WERE INOPERATIVE. THE CREW RETURNED TO THE GATE. MAINTENANCE INSPECTED AND BLED THE BRAKES - [SDR VNAA0005003](https://openairdocs.org/sdr/VNAA0005003), May 3, 2000: CONTROL BOX. FAILED. THE CREW REPORTED THAT THE BRAKES WERE COMPLETELY INEFFECTIVE WHILE TAXIING. FLIGHT 4102 RETURNED TO THE GATE WHERE MAINTENANCE BLED THE BRAKES AND REPLACED THE - [SDR VNAA0004014](https://openairdocs.org/sdr/VNAA0004014), Apr 8, 2000: BRAKE. FAILED. AFTER DEPARTING THE GATE, THE CREW DISCOVERED THAT THE FIRST OFFICERS BRAKES WERE INEFFECTIVE. THE CREW RETURNED TO THE GATE WHERE MAINTENANCE, AFTER ARRIVING F - [SDR VNAA0004012](https://openairdocs.org/sdr/VNAA0004012), Apr 6, 2000: PCU. FAILED. WHILE CLIMBING THROUGH FLT 020, THE CREW RECEIVED AN INTERMITTENT RIGHT HAND PROPELLER LOW OIL PRESSURE CAS MESSAGE. REACHING FLT 100 THE MESSAGE REMAINED CONST - [SDR 20000413SH058](https://openairdocs.org/sdr/20000413SH058), Apr 4, 2000: PLATE. CRACKED. DURING SEARCH INSPECTION, 4 EACH C-6066-1 PRELOAD PLATES WERE FOUND CRACKED. ONE EACH PRELOAD PLATE WAS CRACKED IN SUCH A MANNER THAT IT BROKE DURING INSPECTION - [SDR VNAA0003023](https://openairdocs.org/sdr/VNAA0003023), Mar 24, 2000: BRAKE. FAILED. THE FLIGHT CREW REPORTED THAT THE FIRST OFFICER''S BRAKES WERE NOT RESPONDING WHEN APPLIED. MAINTENANCE INSPECTED THE AIRCRAFT AND FERRIED THE AIRCRAFT TO PIT. - [SDR VNAA0003005](https://openairdocs.org/sdr/VNAA0003005), Mar 6, 2000: BLEED VALVE. FAILED. DURING THE TAKEOFF ROLL, FLIGHT 4087, RECEIVED A RIGHT PACK OVER PRESSURE WARNING. THE FLIGHT CREW ABORTED THE TAKEOFF AND EXITED THE RUNWAY. THE WARNING MESSAG - [SDR VNAA9911009](https://openairdocs.org/sdr/VNAA9911009), Nov 12, 1999: NL PROBE. FAILED. DURING CLIMBOUT, THE FLIGHT CREW RECEIVED A CAS MESSAGE INDICATING AN ENGINE MISCOMPARE. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANC - [SDR VNAA9910022](https://openairdocs.org/sdr/VNAA9910022), Oct 31, 1999: BRAKE SYS. REQD SERVICE. DURING TAXI, THE FLIGHT CREW REPORTED THE FIRST OFFICERS' LEFT HAND BRAKE PEDAL HAD NO RESPONSE WHEN ACTIVATED. AIRCRAFT WAS FERRIED TO PIT. MAINTENANCE INSPECT - [SDR VNAA9903016](https://openairdocs.org/sdr/VNAA9903016), Mar 17, 1999: FAN. FAILED. DURING CLIMB AFTER TAKEOFF, THE CREW SMELLED AND NOTED SMOKE IN THE COCKPIT. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE INSP - [SDR VNAA9812004](https://openairdocs.org/sdr/VNAA9812004), Dec 6, 1998: CONNECTOR. DAMAGED. A NR 1 PITOT HEAT FAIL WARNING MESSAGE ILLUMINATED, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND APP All 81: https://openairdocs.org/deregistered/N426JS-2009-05-21/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 20011026029069I](https://openairdocs.org/incident/20011026029069I), Oct 26, 2001: Dorner DO328100 (N426JS), Pittsburgh, PA. (-23) On 26 oct 01, aircraft N426JS aborted takeoff from runway 28R at pit. While executing take off roll, the crew of flight 4052 received left hand shaker,… - [Incident 20000726035129I](https://openairdocs.org/incident/20000726035129I), Jul 26, 2000: Dorner DO328100 (N426JS), Pittsburgh, PA. (-23)On July 26,2000, psa flight #4059 (vnaa)landed on runway 10R at pit at 1935 local with a landing gear problem. Maintenance reported they found a failed… - [Incident 20000306004169I](https://openairdocs.org/incident/20000306004169I), Mar 6, 2000: Dorner DO328100 (N426JS), Pittsburgh, PA. (.23) On March 6, 2000, at 1810E, a DO-328-100, registered as N426JS, operated as psa (vnaa) flight 4087, twice aborted takeoff at "pit" on runway 28L and then… ## Other aircraft with N426JS - [Cancelled 2022-09-19](https://openairdocs.org/deregistered/N426JS-2022-09-19): Beechcraft B200GT, S/N BY-211. Exported to Botswana. Owner: [Liechty Automotive Management LLC](https://openairdocs.org/faa-owner/LIECHTY%20AUTOMOTIVE%20MANAGEMENT%20LLC), [Gulf Breeze, FL](https://openairdocs.org/faa-place/FL/Gulf%20Breeze) --- 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.