# N436JS: 1995 Dornier Luftfahrt 328-100, registration cancelled 2006-05-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 5, 2006
- Exported to: Germany
- Status when cancelled: Sale reported
- 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: 3052
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: August 22, 1995
- Last registry action: May 5, 2006
- Mode S code: A53A41
- Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)
- Owner type: Individual
- Owner's area on the map: 35.0164° N, 97.4498° W: Placed by OpenAirDocs at the center of ZIP code 73080, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N436JS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=436JS
- Page: https://openairdocs.org/deregistered/N436JS-2006-05-05

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 (72, newest 50)

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

- [SDR VNAA0311010](https://openairdocs.org/sdr/VNAA0311010), Nov 26, 2003: ECU. FAILED. DURING TAKEOFF, WHEN THE CONTROL LEVERS WERE ADVANCED THE LT ENGINE ECU FAILED AND THE CREW ABORTED TAKEOFF. THE CREW RESET THE ECU AND WAS CLEARED FOR ANOTHER 
- [SDR VNAA0309011](https://openairdocs.org/sdr/VNAA0309011), Sep 18, 2003: LIGHT. INOPERATIVE. THE CREW REPORTED THAT THE ROW 10 EMERGENCY FLOOR LIGHTING STRIP WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP IN ACC
- [SDR VNAA0308024](https://openairdocs.org/sdr/VNAA0308024), Aug 29, 2003: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY LIGHTS AT 9A WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER
- [SDR VNAA0308001](https://openairdocs.org/sdr/VNAA0308001), Aug 1, 2003: SMOKE DETECTOR. FAULTY. THE CREW RECEIVED A LAV SMOKE CAS MESSAGE AND CALLED MAINTENANCE. MAINTENANCE DEFERRED THE LAV SMOKE DETECTOR WITH THE CREW. UPON ARRIVAL AT PIT, MAINTENANCE IN
- [SDR VNAA0301003](https://openairdocs.org/sdr/VNAA0301003), Jan 5, 2003: LIGHT. INOPERATIVE. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING IN THE GALLEY AREA WAS NOT ILLUMINATING. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND REP
- [SDR VNAA0212032](https://openairdocs.org/sdr/VNAA0212032), Dec 25, 2002: TARGET. OUT OF ADJUST. EN ROUTE, THE CREW RECEIVED A GALLEY DOOR OPEN MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND LANDED BACK AT PIT. MAINTENANCE INSPECTED AND FOUND
- [SDR VNAA0203022](https://openairdocs.org/sdr/VNAA0203022), Mar 13, 2002: FLIGHT DIR. MALFUNCTIONED. DURING THE TAKEOFF, THE CREW RECEIVED A VNAV SYSTEM FAIL INDICATION AGAIN AND ABORTED TAKEOFF. FLIGHT 4092 RETURNED TO THE GATE. MAINTENANCE CONTROL THEN MEL'D 
- [SDR VNAA0203021](https://openairdocs.org/sdr/VNAA0203021), Mar 13, 2002: FLIGHT DIR. MALFUNCTIONED. DURING THE TAKEOFF, THE CREW RECEIVED A VNAV SYSTEM FAIL INDICATION AND ABORTED TAKEOFF. BEFORE THE AIRCRAFT CLEARED THE RUNWAY THE SYSTEM RESET ITSELF. THE CRE
- [SDR VNAA0203019](https://openairdocs.org/sdr/VNAA0203019), Mar 13, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING STRIP WAS NOT WORKING. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POW
- [SDR VNAA0201020](https://openairdocs.org/sdr/VNAA0201020), Jan 27, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE FIRST STRIP OF EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WI
- [SDR VNAA0201013](https://openairdocs.org/sdr/VNAA0201013), Jan 13, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK POSITION IN ACCO
- [SDR VNAA0112001](https://openairdocs.org/sdr/VNAA0112001), Dec 1, 2001: CONTROL UNIT. MALFUNCTIONED. PULLING OFF THE GATE, THE NOSE WHEEL STEERING FAILED. AS SOON AS THE WHEEL WAS STRAIGHTENED THE FAIL LIGHT WENT OUT. AS FLIGHT 4106 TOOK THE RUNWAY THE NOSE WHE
- [SDR VNAA0111004](https://openairdocs.org/sdr/VNAA0111004), Nov 5, 2001: PANEL. FAILED. DURING CLIMBOUT, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE W
- [SDR VNAA0110004](https://openairdocs.org/sdr/VNAA0110004), Oct 7, 2001: ODOR. DETECTED. THE APU WAS RUNNING AND THE FLIGHT ATTENDANT REPORTED SMELLING SMOKE. MAINTENANCE INSPECTED THE AIRCRAFT AND COULD NOT DUPLICATE OR FIND ANY DISCREPANCIES. THE 
- [SDR VNAA0107016](https://openairdocs.org/sdr/VNAA0107016), Jul 16, 2001: WHEEL. VIBRATION. AFTER ROTATION, THE CREW FELT A VIBRATION COMING FROM THE NOSE GEAR. THE CREW LOWERED THE GEAR ASSUMING THAT THERE WAS A BLOWN TIRE. MAINTENANCE CONTROL REQUEST
- [SDR VNAA0107014](https://openairdocs.org/sdr/VNAA0107014), Jul 11, 2001: CONNECTOR. DIRTY. DURING THE TAKEOFF ROLL, THE CREW RECEIVED A ELECTRONIC CONTROL UNIT FAIL LIGHT AND A GENERATOR OFF LINE LIGHT. OUT STATION MAINTENANCE INSPECTED AND CLEANED TH
- [SDR VNAA0107008](https://openairdocs.org/sdr/VNAA0107008), Jul 6, 2001: BATTERY. DEFECTIVE. THE CREW RECEIVED A BATTERY OVERHEAT INDICATION ON THE RED WARNING PANEL APPROXIMATELY TEN MINUTES OUT OF DAY. THE CREW CONTACTED MAINTENANCE CONTROL AND WAS AD
- [SDR VNAA0107006](https://openairdocs.org/sdr/VNAA0107006), Jul 4, 2001: HARNESS. FAILED. AFTER APPLYING POWER FOR TAKE OFF, THE AIRCRAFT LOST 50 PERCENT TORQUE AS THE AIRCRAFT ROTATED. THE POWER CAME BACK AND THE CREW DECIDED TO RETURN TO THE FIELD.
- [SDR VNAA0105010](https://openairdocs.org/sdr/VNAA0105010), May 17, 2001: FIRE DETECTOR. MALFUNCTIONED. FLIGHT 4044 WAS CLIMBING AND THE CREW RECEIVED A CARGO FIRE LIGHT INDICATION ACCOMPANIED BY THE TRIPLE CHIME. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK, ME
- [SDR VNAA0103012](https://openairdocs.org/sdr/VNAA0103012), Mar 14, 2001: WARNING SYSTEM. ACTIVATED. AS THE AIRCRAFT WAS TAXIING ONTO THE RUNWAY, THE FLIGHT RECEIVED A PROXI DOOR FAIL WARNING MESSAGE FOR THE MAIN CABIN DOOR. THE FLIGHT CREW EXITED THE RUNWAY AN
- [SDR VNAA0103004](https://openairdocs.org/sdr/VNAA0103004), Mar 4, 2001: ANTI-ICE SYSTEM. FAILED. DURING CLIMBOUT THE FLIGHT CREW RECEIVED A RIGHT WING MIDDLE AIRFOIL DEICE FAIL MESSAGE. THE FLIGHT CREW RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAIN
- [SDR VNAA0102011](https://openairdocs.org/sdr/VNAA0102011), Feb 18, 2001: BLEED VALVE. FAILED. AFTER CLIMB OUT, THE CREW RECEIVED A RIGHT HAND PACK OVERHEAT MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK THEN CONTACTED MAINTENANCE CONTROL WHO D
- [SDR VNAA0102003](https://openairdocs.org/sdr/VNAA0102003), Feb 7, 2001: ELEVATOR. MALFUNCTIONED. DURING CLIMB, THE CREW NOTICED THAT THE ELEVATOR TRIM WOULD NOT WORK WHEN SELECTED UP. FLIGHT 4061 RETURNED TO GSP. MAINTENANCE INSPECTED AND RECYCLED AIRCRAFT 
- [SDR VNAA0101022](https://openairdocs.org/sdr/VNAA0101022), Jan 24, 2001: OXYGEN MASK. DEPLOYED. WHILE CLIMBING THROUGH 10,000 FEET THE OXYGEN MASKS DEPLOYED INADVERTENTLY. THE FLIGHT LANDED IN PIT WITH NO FURTHER INCIDENTS. MAINTENANCE TROUBLESHOT THE WIRI
- [SDR VNAA0011014](https://openairdocs.org/sdr/VNAA0011014), Nov 16, 2000: DOOR. NOT CLOSED. DURING THE TAKEOFF RUN, THE FUEL DOOR CAS MESSAGE ILLUMINATED. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. THE FUELER RETURNED AND SECURED THE FUEL DOOR.
- [SDR VNAA0011006](https://openairdocs.org/sdr/VNAA0011006), Nov 10, 2000: BLEED VALVE. FAILED. DAY - FLT 4026 - AFTER TAKING THE RUNWAY AND AS POWER WAS ADVANCED THE PUT BLEED SHUTOFF VALVE FAILED. MAINTENANCE REPLACED THE RIGHT LP BLEED VALVE. THE AIRCRA
- [SDR VNAA0010008](https://openairdocs.org/sdr/VNAA0010008), Oct 10, 2000: LEVER. FAILED. DURING THE TAKEOFF ROLL, THE UNSAFE GEAR LIGHT ILLUMINATED. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE DECIDED TO FERRY THE PLANE TO DAYTON.
- [SDR VNAA0010010](https://openairdocs.org/sdr/VNAA0010010), Oct 10, 2000: PIN. INSTALLED. DURING CLIMBOUT, THE CREW ATTEMPTED TO RETRACT THE GEAR AND RECEIVED ALL GEAR INDICATIONS. THE CREW CONTACTED MAINTENANCE CONTROL AND RETURNED TO THE FIELD. MAI
- [SDR VNAA0009021](https://openairdocs.org/sdr/VNAA0009021), Sep 23, 2000: STRUCTURE. BIRD STRIKE. DURING TAKEOFF, FLIGHT 4172 SUSTAINED MULTIPLE BIRD STRIKES. FLIGHT 4172 ABORTED TAKEOFF. MAINTENANCE INSPECTED THE AIRCRAFT IN ACCORDANCE WITH DORNIER MAINTENA
- [SDR VNAA0008015](https://openairdocs.org/sdr/VNAA0008015), Aug 28, 2000: ECU. FAILED. FLIGHT 4087 ABORTED TAKEOFF AFTER RECEIVING A LEFT HAND ELECTRONIC CONTROL UNIT FAIL MESSAGE. THE CREW WAS INSTRUCTED BY MAINTENANCE TO RESET THE ELECTRONIC CON
- [SDR VNAA0008014](https://openairdocs.org/sdr/VNAA0008014), Aug 21, 2000: PRESSURE SWITCH. FAILED. THE CREW RECEIVED A RIGHT HAND PROPELLER OIL PRESSURE CAS MESSAGE. THE CREW CALLED MAINTENANCE CONTROL AND ELECTED TO RETURN TO THE FIELD. MAINTENANCE INSPECTED
- [SDR VNAA0008012](https://openairdocs.org/sdr/VNAA0008012), Aug 17, 2000: CONNECTOR. DIRTY. FLIGHT 4066 PERFORMED AN AIR RETURN DUE TO RECEIVING A RIGHT HAND OIL PRESSURE CAS MESSAGE. MAINTENANCE INSPECTED BUT COULD NOT DUPLICATE THE PROBLEM. MAINTENAN
- [SDR VNAA0003004](https://openairdocs.org/sdr/VNAA0003004), Mar 6, 2000: WARNING SYSTEM. ACTIVATED. THE FIGHT CREW RECEIVED A TAKEOFF CONFIGURATION WARNING AS THE TAKEOFF ROLL WAS INITIATED. THE FLIGHT CREW ABORTED THE TAKEOFF AND EXITED THE RUNWAY. A PITCH TR
- [SDR VNAA0002017](https://openairdocs.org/sdr/VNAA0002017), Feb 22, 2000: CIRCUIT BREAKER. FAILED. AFTER TAKEOFF CLIMBING THROUGH 500 FEET, THE CAPTAIN NOTICED THAT THE OIL PRESSURE IN THE LEFT HAND ENGINE READ ZERO POUNDS PER SQAURE INCH. THE AIRCRAFT RETURN
- [SDR VNAA0002006](https://openairdocs.org/sdr/VNAA0002006), Feb 3, 2000: BATTERY. DISCHARGED. THE CREW NOTICED THAT THE EMERGENCY LIGHTS AT ROWS 3, 4, AND 5 WERE NOT WORKING. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED T
- [SDR VNAA0001016](https://openairdocs.org/sdr/VNAA0001016), Jan 21, 2000: BATTERY. DISCHARGED. THE CREW FOUND THAT THE EMERGENCY LIGHT ABOVE THE FLIGHT ATTENDENTS JUMPSEAT WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY AT THE 5LK POSITI
- [SDR VNAA9912012](https://openairdocs.org/sdr/VNAA9912012), Dec 17, 1999: SWITCH. FAILED. DURING CLIMBOUT FROM PIT, THE FLIGHT CREW RECEIVED A RIGHT HAND PROPELLER OIL PRESSURE CAS MESSAGE. MAINTENANCE CONTROL INSTRUCTED THE CREW TO RETURN TO THE FIE
- [SDR VNAA9912011](https://openairdocs.org/sdr/VNAA9912011), Dec 15, 1999: VALVE. FAILED. WHILE EN ROUTE TO CLARKSBURG, THE LEFT PACK OVERHEATED. THE FLIGHT CREW WAS INSTRUCTED TO RETURN TO THE FIELD. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAI
- [SDR VNAA9910008](https://openairdocs.org/sdr/VNAA9910008), Oct 15, 1999: VALVE. FAILED. AIRCRAFT WAS EN ROUTE TO PIT WHEN THE EMERGENCY PARKING BRAKE ACCUMULATOR CAS MESSAGE ILLUMINATED. THE FLIGHT CREW REFERENCED THE QRH AND ATTEMPTED TO CLEAR THE
- [SDR VNAA9909003](https://openairdocs.org/sdr/VNAA9909003), Sep 15, 1999: BATTERY. DISCHARGED. THE EMERGENCY FLOOR LIGHTING ADJACENT TO CABIN SEAT ROWS 5 THROUGH 7 WAS FOUND TO BE INOPERATIVE BY MAINTENANCE PERSONNEL. MAINTENANCE INSPECTED AND REPLACED TH
- [SDR VNAA9908005](https://openairdocs.org/sdr/VNAA9908005), Aug 13, 1999: STRUCTURE. DAMAGED. THE AIRCRAFT WAS STRUCK BY A PICKUP TRUCK WHILE SITTING STATIC AT THE GATE. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT
- [SDR VNAA9907002](https://openairdocs.org/sdr/VNAA9907002), Jul 7, 1999: GEARBOX. LIGHTNING STRIKE. WHILE EN ROUTE TO DCA, THE AIRCRAFT WAS STRUCK BY LIGHTNING. THE FLIGHT CONTINUED ON TO DCA AND LANDED WITHOUT ANY FURTHER PROBLEMS. OUTSTATION MAINTENANCE INSP
- [SDR VNAA9902018](https://openairdocs.org/sdr/VNAA9902018), Feb 27, 1999: HUB. CRACKED. A CRACK WAS FOUND ON THE RIGHT HAND PROPELLER HUB DURING COMPLIANCE OF HARTZELL ALERT SERVICE BULLETIN HD-ASB-61-021. MAINTENANCE REMOVED AND REPLACED THE RIGHT
- [SDR VNAA9902005](https://openairdocs.org/sdr/VNAA9902005), Feb 10, 1999: PCU. FAILED. AFTER PUSHBACK, THE LEFT HAND PROPELLER FAILED TO UNFEATHER WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND P
- [SDR VNAA9811024](https://openairdocs.org/sdr/VNAA9811024), Nov 26, 1998: VALVE. FAILED. DURING THE TAXI PRIOR TO TAKEOFF, A CROSS-BLEED FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE CROS
- [SDR VNAA9811019](https://openairdocs.org/sdr/VNAA9811019), Nov 18, 1998: WINDSHIELD. BIRD STRIKE. SHORTLY AFTER TAKEOFF, THE AIRCRAFT TOOK A BIRD STRIKE ON THE LEFT HAND FORWARD WINDSHIELD. THE AIRCRAFT CONTINUED ON TO PIT AND PERFORMED A NORMAL LANDING. WHE
- [SDR VNAA9810004](https://openairdocs.org/sdr/VNAA9810004), Oct 6, 1998: AHRU. FAILED. A NUMBER TWO ATTITUDE/HEADING FAIL WARNING MESSAGE ILLUMINATED, DURING THE CLIMB-OUT PHASE OF THE FLIGHT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED, WITHOUT
- [SDR VNAA9809023](https://openairdocs.org/sdr/VNAA9809023), Sep 26, 1998: PSEU. TRIPPED. A CARGO DOOR WARNING INDICATION ILLUMINATED, DURING THE TAXI FOR DEPARTURE. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND RERACKED THE PROXY SWIT
- [SDR VNAA9809022](https://openairdocs.org/sdr/VNAA9809022), Sep 25, 1998: SEAT. LOOSE. THE FLIGHT ATTENDANT REPORTED THAT THE ATTENDANT SEAT CAME OFF TRACK, DURING THE TAXI OUT FOR DEPARTURE. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTE
- [SDR VNAA9808005](https://openairdocs.org/sdr/VNAA9808005), Aug 4, 1998: CONTROL UNIT. FAILED. AN ANTI-SKID FAIL WARNING MESSAGE OCCURRED, DURING TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE ANTI-SKID CON

All 72: https://openairdocs.org/deregistered/N436JS-2006-05-05/reports.md

## Other aircraft with N436JS

- [Registered now](https://openairdocs.org/aircraft/N436JS): Sowalsky John W STALLION, S/N 024, built 2015

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