# N423JS: 1995 Dornier Luftfahrt 328-100, registration cancelled 2009-02-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 17, 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: 3032
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 1995
- Certificate issued: February 21, 2008
- Last registry action: February 21, 2008
- Mode S code: A5079D
- 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/N423JS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=423JS
- Page: https://openairdocs.org/deregistered/N423JS-2009-02-17

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 (49)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR VNAA0403016](https://openairdocs.org/sdr/VNAA0403016), Mar 28, 2004: ROD. DAMAGED. THE CREW REPORTED THAT THE GALLEY DOOR WAS VIBRATING IN FLIGHT OVER 150 KNOTS. FLIGHT 2470 THEN DIVERTED TO BWI. THE AIRCRAFT WAS THEN FERRIED TO CAK. MAINTENAN
- [SDR VNAA0402003](https://openairdocs.org/sdr/VNAA0402003), Feb 8, 2004: SWITCH. DIRTY. DURING FLIGHT, THE CREW RECEIVED A GROUND AIR DOOR WARNING DURING CLIMBOUT AND RETURNED TO PIT. MAINTENANCE INSPECTED, CLEANED AND ACTUATED THE DOOR SWITCH IN A
- [SDR VNAA0311011](https://openairdocs.org/sdr/VNAA0311011), Nov 28, 2003: SMOKE DETECTOR. FAILED. THE CREW REPORTED A LAV SMOKE FAIL INDICATION. MAINTENANCE THEN DEFERRED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH 26-3 CODE C.
- [SDR VNAA0311008](https://openairdocs.org/sdr/VNAA0311008), Nov 21, 2003: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAIN
- [SDR VNAA0311002](https://openairdocs.org/sdr/VNAA0311002), Nov 10, 2003: HMU. FAILED. DURING TAKEOFF, THE AIRCRAFT FAILED TO PRODUCE TAKEOFF TORQUE AND THE CREW ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE HYDROMECHANICAL UNIT IN ACCOR
- [SDR VNAA0310006](https://openairdocs.org/sdr/VNAA0310006), Oct 7, 2003: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 9 AND 10 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WIT
- [SDR VNAA0309003](https://openairdocs.org/sdr/VNAA0309003), Sep 5, 2003: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 4 TO 7 WERE INTERMITTENT. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH 
- [SDR VNAA0308023](https://openairdocs.org/sdr/VNAA0308023), Aug 29, 2003: SMOKE DETECTOR. MALFUNCTIONED. THE CREW RECEIVED A LAV SMOKE CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPE
- [SDR VNAA0308019](https://openairdocs.org/sdr/VNAA0308019), Aug 26, 2003: SMOKE DETECTOR. MALFUNCTIONED. THE CREW RECEIVED A LAV SMOKE DETECTOR INOP INDICATION. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 
- [SDR VNAA0306015](https://openairdocs.org/sdr/VNAA0306015), Jun 27, 2003: LIGHT. FAILED. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING WAS NOT WORKING AT SEAT 9A. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY FLOOR PATH LIGHT STRIP IN ACCOR
- [SDR VNAA0303022](https://openairdocs.org/sdr/VNAA0303022), Mar 17, 2003: ALTERNATOR. FAILED. DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND ALTERNATOR FAIL CAS MESSAGE AND ABORTED TAKE OFF. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE REPLACE
- [SDR VNAA0303020](https://openairdocs.org/sdr/VNAA0303020), Mar 17, 2003: ALTERNATOR. FAILED. DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND ALTERNATOR FAIL CAS MESSAGE AND ABORTED TAKE OFF. AFTER THE POWER LEVERS WERE PULLED BACK THE ALTERNATOR RESET P
- [SDR VNAA0212020](https://openairdocs.org/sdr/VNAA0212020), Dec 13, 2002: CONTROLLER. FAILED. THE CREW RECEIVED A FIRST OFFICER WINDSHIELD HEAT FAIL CAS MESSAGE. THE CREW THEN FOLLOWED THE QUICK REFERENCE HANDBOOK AND CALLED MAINTENANCE CONTROL. FLIGHT 4
- [SDR VNAA0211031](https://openairdocs.org/sdr/VNAA0211031), Nov 26, 2002: PUMP. FAILED. DURING TAKE OFF, THE CREW RECEIVED A TAKE OFF CONFIGURATION WARNING ON THE RED WARNING PANEL AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND THE HIGH PRESSURE P
- [SDR VNAA0209024](https://openairdocs.org/sdr/VNAA0209024), Sep 16, 2002: PROPELLER. FAILED. DURING CLIMB, THE CREW NOTICED A VIBRATION SUSPECTED FROM THE LEFT HAND PROPELLER AND RETURNED TO PIT. MAINTENANCE INSPECTED AND THEN BALANCED THE LEFT HAND PRO
- [SDR VNAA0207048](https://openairdocs.org/sdr/VNAA0207048), Jul 31, 2002: ECU. FAILED. THE CREW REPORTED THAT THE CABIN TEMPERATURE WOULD NOT GO BELOW 35 DEGREES CELSIUS AND RETURNED TO DCA. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPEC
- [SDR VNAA0207019](https://openairdocs.org/sdr/VNAA0207019), Jul 13, 2002: GENERATOR. FAILED. DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND DC GENERATOR FAILURE CAS MESSAGE. AFTER CLEARING THE RUNWAY, THE CREW RESET THE RIGHT HAND GENERATOR AND THE MES
- [SDR VNAA0207010](https://openairdocs.org/sdr/VNAA0207010), Jul 11, 2002: BRACKET. OUT OF ADJUST. EN ROUTE, THE CREW RECEIVED A DOORS RED WARNING PANEL LIGHT. ALL DOORS WERE SECURE AND THE AIRCRAFT DID NOT LOSE PRESSURIZATION. THE CREW FOLLOWED THE QUICK REF
- [SDR VNAA0205020](https://openairdocs.org/sdr/VNAA0205020), May 14, 2002: PROPELLER. FAILED. APPROXIMATELY SIX MILES FROM THE BAL VOR, THE CREW EXPERIENCED A FLASH AND LOUD BOOM. THE CREW ASSUMED THAT THE AIRCRAFT HAD BEEN STRUCK BY LIGHTNING. THE CREW 
- [SDR VNAA0110010](https://openairdocs.org/sdr/VNAA0110010), Oct 14, 2001: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING AT ROWS 6 THROUGH 9 ON ENGINE START UP. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY 
- [SDR VNAA0108015](https://openairdocs.org/sdr/VNAA0108015), Aug 24, 2001: FLIGHT DIR. MALFUNCTIONED. AFTER TAKE OFF, THE CREW WAS GIVEN A HEADING AND DISCOVERED THAT THE FLIGHT DIRECTOR WAS GIVING IMPROPER INDICATIONS. THE CREW DECIDED TO RETURN TO YOW AND CALL
- [SDR VNAA0108012](https://openairdocs.org/sdr/VNAA0108012), Aug 19, 2001: DOOR. DURING CLIMB, THE CABIN PRESSURE WAS CLIMBING WITH THE AIRCRAFT. AFTER CLIMBING TO 8000 FT MSL THE CABIN PRESSURE WAS INDICATING 7500 FT MSL. FLIGHT 4030 RETURN
- [SDR VNAA0107023](https://openairdocs.org/sdr/VNAA0107023), Jul 29, 2001: BATTERY. DISCHARGED. THE CREW REPORTED THAT SOME OF THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK POSITION IN ACCO
- [SDR VNAA0107022](https://openairdocs.org/sdr/VNAA0107022), Jul 21, 2001: BLEED VALVE. FAILED. AFTER STARTING THE TAKE OFF ROLL, THE CREW RECEIVED A RIGHT HAND ELECTRONIC CONTROL UNIT FAIL CAS MESSAGE AND ABORTED TAKE OFF. FLIGHT 4082 TAXIIED BACK TO THE 
- [SDR VNAA0105014](https://openairdocs.org/sdr/VNAA0105014), May 24, 2001: TIRE. BLOWN. WHILE TAXIING, THE CREW HEARD WHAT SOUNDED LIKE A TIRE BLOWING. THE CAPTAIN CONTACTED GROUND AND RECEIVED PERMISSION TO SHUT DOWN THE ENGINES AND DO A VISUAL CH
- [SDR VNAA0104001](https://openairdocs.org/sdr/VNAA0104001), Apr 3, 2001: LIGHT. INOPERATIVE. THE FLIGHT CREW REPORTED THAT THE EMERGENCY FLOOR PATHWAY LIGHTING STRIP WOULD NOT ILLUMINATE ADJACENT TO SEAT 1D/F. MAINTENANCE INSPECTED AND RESECURED THE LIG
- [SDR VNAA0101015](https://openairdocs.org/sdr/VNAA0101015), Jan 17, 2001: WIRE. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHT AND BOARDING LIGHT BY ROW 9A WAS NOT WORKING. MAINTENANCE INSPECT AND REPAIRED A BROKEN WIRE IN ACCORDANCE WITH STAND
- [SDR VNAA0101013](https://openairdocs.org/sdr/VNAA0101013), Jan 16, 2001: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROW 9A WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAI
- [SDR VNAA0011003](https://openairdocs.org/sdr/VNAA0011003), Nov 3, 2000: WARNING SYSTEM. FAILED. DURING TAKEOFF, THE CREW RECEIVED A GEAR WARNING HORN CAS MESSAGE. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. THE AIRCRAFT WAS THEN FERRIED TO CAK. MAIN
- [SDR VNAA0009008](https://openairdocs.org/sdr/VNAA0009008), Sep 12, 2000: POWER LEVER. STUCK. THE CREW ADVANCED POWER FOR TAKEOFF, THE LEFT HAND LEVER WAS STICKING. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECT AND LUBRICATED THE
- [SDR VNAA0004019](https://openairdocs.org/sdr/VNAA0004019), Apr 17, 2000: ENGINE. FAILED. FLIGHT 4060 WAS EN ROUTE AT FL240 AND THE RIGHT HAND ENGINE OIL PRESSURE BEGAN TO FLUCTUATE. THE RIGHT HAND ENGINE COMPLETELY LOST POWER. THE CREW REFERENCED TH
- [SDR VNAA9910013](https://openairdocs.org/sdr/VNAA9910013), Oct 21, 1999: CONTROL UNIT. FAILED. ON THE TAKEOFF ROLL, THE CREW RECEIVED A NOSE WHEEL STEERING POWER UP FAIL MESSAGE. ONCE THE TAKEOFF WAS ABORTED, THE CREW RECEIVED THREE GEAR UNSAFE INDICATION
- [SDR VNAA9910004](https://openairdocs.org/sdr/VNAA9910004), Oct 7, 1999: SWITCH. STICKING. FLIGHT 4087- WAS ON APPROACH TO PIT WHEN A NOSE WHEEL STEERING POWER-UP CAS MESSAGE WAS DISPLAYED. THE FLIGHT CREW REVIEWED THE QRH AND PERFORMED A SECOND APPRO
- [SDR VNAA9910002](https://openairdocs.org/sdr/VNAA9910002), Oct 6, 1999: SEAL. FAILED. WHILE IN CRUISE FLIGHT, THE LEFT ENGINE OIL PRESSURE INDICATION BEGAN TO FLUCTUATE AND THEN TURNED AMBER. THE FLIGHT CREW FOLLOWED THE QRH AND FEATHERED THE LEF
- [SDR VNAA9808003](https://openairdocs.org/sdr/VNAA9808003), Aug 1, 1998: BRAKES. REQD SERVICE. THE LEFT HAND BRAKES WERE REPORTED FROM THE CREW AS SPONGEY WHEN SELECTED, DURING THE TAXI FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED
- [SDR VNAA9709004](https://openairdocs.org/sdr/VNAA9709004), Sep 17, 1997: CHECK VALVE. DEFECTIVE. AT 12,000 FT, RECEIVED EMERGENCY PARKING BRAKE ACCUMULATOR LOW WARNING LIGHT. COMPLIED WITH QUICK REFERENCE HANDBOOK AND LIGHT EXTINGUISHED, 3 MINUTES LATER LIG
- [SDR VNAA9701005](https://openairdocs.org/sdr/VNAA9701005), Jan 9, 1997: INLET DE-ICE. FAILED. AFTER TAKEOFF, THE LEFT ENGINE INLET DE-ICE FAILED. RESET SWITCH AND THE SYSTEM FAILED AGAIN. RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REMOVED AND RE
- [SDR VNAA9606003](https://openairdocs.org/sdr/VNAA9606003), Jun 3, 1996: RUDDER. LIGHTNING STRIKE. CREW REPORTED HEARING A LOUD BANG, NO APPARENT CHANGE IN ANY OF THE AIRCRAFT SYSTEMS. AIRCRAFT CONTINUED ON WITH THE FLIGHT AND LANDED IN PIT WITHOUT FURTHER IN
- [SDR VNAA9600020](https://openairdocs.org/sdr/VNAA9600020), Apr 20, 1996: WINDSHIELD. FAILED. CLT - FLT 4081 - EN ROUTE FROM CLT TO CAK, CREW REPORTED THAT OUTER PANE OF CAPTAIN'S WINDSHIELD FAILED. CREW THEN FOLLOWED ESTABLISHED ABNORMAL PROCEDURES BY D
- [SDR 96ZZZX1322](https://openairdocs.org/sdr/96ZZZX1322), Mar 3, 1996: UPOCK ROLLERS. LACK OF LUBE. FLT 4079 - AFTER TAKEOFF, CREW REPORTED A 'RED' INTRANSIT LIGHT LT MAIN GEAR, AFTER GEAR WAS SELECTED 'UP'. AIRCRAFT RETURNED TO THE FIELD, LANDED WITHOUT FURTH
- [SDR 96ZZZX3022](https://openairdocs.org/sdr/96ZZZX3022), Feb 15, 1996: DEICE BOOT. DEFECTIVE. FLT 4149 - THE LEFT PROPELLER DEICE FAILED EN ROUTE FROM KAY TO PHL. AIRCRAFT DIVERTED TO PIT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. LATER THE AIRCRAFT WAS 
- [SDR 96ZZZM643](https://openairdocs.org/sdr/96ZZZM643), Feb 12, 1996: UPLOCK ROLLER. DIRTY. FLT NR 4194 - LEFT MAIN LANDING GEAR WOULD NOT LOCK IN THE UP POSITION AFTER TAKEOFF, RED INTRANSIT LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO THE FIELD, 
- [SDR 96ZZZM646](https://openairdocs.org/sdr/96ZZZM646), Feb 9, 1996: BRAKES. HOT. FLT NR 4028 - DURING THE TAKEOFF ROLL, THE FLIGHT CREW WAS ALERTED BY A RED TAKEOFF CONFIGURATION WARNING. TAKEOFF WAS ABORTED, AIRCRAFT WAS RETURNING TO THE GA
- [SDR 96ZZZX892](https://openairdocs.org/sdr/96ZZZX892), Jan 26, 1996: UPLOCK ROLLER. DIRTY. FLT 4014 - LEFT MLG WOULD NOT LOCK IN THE 'UP' POSITION WHEN GEAR WAS RETRACTED AFTER TAKEOFF. AIRCRAFT RETURNED TO THE FIELD, LANDED WITHOUT FURTHER INCIDENT. 
- [SDR 96ZZZM104](https://openairdocs.org/sdr/96ZZZM104), Dec 21, 1995: UPLOCK ACT. DEFECTIVE. FLT NR 4118 - SHORTLY AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED 'UP', GEAR INTRANSIT LIGHT REMAINED ILLUMINATED. CREW CYCLED GEAR TWICE, INTRANSIT LIGHT STIL
- [SDR 95ZZZM238](https://openairdocs.org/sdr/95ZZZM238), Jul 12, 1995: BLEED AIR WARN. ACTIVATED. FLT NR 4023 - CREW REJECTED TAKEOFF AFTER RECEIVING BLEED AIR SHUTOFF VALVE CAS MESSAGE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE CONDUCT
- [SDR 95ZZZX1656](https://openairdocs.org/sdr/95ZZZX1656), Mar 14, 1995: DATA ACQUISITION. MALFUNCTION. FLT 4219 - DURING TAKEOFF, CREW ALERTED TO NR 1 PITOT HEAT FAIL - CAS MESSAGE, ABORTED TAKEOFF, RETURNED TO GATE. MAINTENANCE REPLACED NR 2 DATA ACQUISITION UNI
- [SDR 95ZZZX1658](https://openairdocs.org/sdr/95ZZZX1658), Mar 13, 1995: TRIM. OUT OF RIG. FLT 4234 - CREW ABORTED TAKEOFF AFTER RECEIVING AN AUDIBLE TAKEOFF TRIM CONFIGURATION WARNING. AIRCRAFT RETURNED TO THE GATE, FLIGHT CREW ADJUSTED ELEVATOR TRIM
- [SDR 95ZZZX1657](https://openairdocs.org/sdr/95ZZZX1657), Mar 9, 1995: ROLLER. CONTAMINATED. FLT 4003 - UNABLE TO EXTINGUISH 'RED' INTRANSIT LIGHT AFTER TAKEOFF WHEN GEAR WAS RETRACTED. RETURNED TO FIELD WITHOUT INCIDENT. PIT MAINTENANCE INSPECTED AIRCR

## 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 NYC01LA096](https://openairdocs.org/ntsb/NYC01LA096), Apr 10, 2001: Dornier 328-100 (N423JS), Springfield, VA, no damage. Probable cause: An inadvertent encounter with turbulence during descent.

## 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 20010721016569I](https://openairdocs.org/incident/20010721016569I), Jul 21, 2001: Dorner DO328100 (N423JS), Pittsburgh, PA. (-23) On 21 July 2001, a psa airlines aircraft, flight #4082, aborted takeoff on runway 28 due to a r/h ecu failure. No assistance was required, and the…
- [Accident 20010409006949A](https://openairdocs.org/incident/20010409006949A), Apr 9, 2001: Dorner DO328100 (N423JS), Springfield, VA. (-19) On April 9, 2001 about 2200 EDT, a dornier 328-100, N423JS, operated by psa airlines, inc., as flight 4110, was not damaged during an encounter with…

## Other aircraft with N423JS

- [Registered now](https://openairdocs.org/aircraft/N423JS): John Poe/Jim Reddy/John Helm RV-10, S/N 42318, built 2023

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