# N331MX: 1996 Dornier Luftfahrt 328-100, registration cancelled 2018-03-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 2, 2018
- 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: 3074
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: November 15, 1996
- Certificate issued: March 12, 2013
- Last registry action: March 12, 2013
- Mode S code: A39AAF
- Owner when cancelled: [Dornier 3095 LLC](https://openairdocs.org/faa-owner/DORNIER%203095%20LLC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7965° N, 75.6128° W: Placed by OpenAirDocs at the center of ZIP code 19807, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N331MX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=331MX
- Page: https://openairdocs.org/deregistered/N331MX-2018-03-02

From the FAA registry file of October 29, 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 (14)

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

- [SDR XV6A2009031600005](https://openairdocs.org/sdr/XV6A2009031600005), Mar 16, 2009: BATTERY PACK. DISCHARGED. ON LINE SERVICE CHECK, FOUND 6LK EPSU BATTERY PACK INOP.
- [SDR XV6A2009030600001](https://openairdocs.org/sdr/XV6A2009030600001), Mar 6, 2009: STRUCTURE. CRACKED. REPETITIVE EDDY CURRENT INSPECTION IAW RAS-328-57-3051 AND AD 2008-10-15.
- [SDR XV62008F00000](https://openairdocs.org/sdr/XV62008F00000), Jun 3, 2008: CONTROL CABLE. OBSTRUCTED. R/S POWER LEVER WOULD NOT GO INTO GROUND IDLE AFTER LANDING. FOUND HINGE FROM COCKPIT DOOR INTERFERING WITH CABLES/ PULLEYS TRAVEL AT RT AVIONICS AFT SIDE. REMO
- [SDR A6WA200330005](https://openairdocs.org/sdr/A6WA200330005), Mar 4, 2003: CONNECTOR. INTERMITTENT. PROXY SYSTEM FAIL MESSAGE IN FLT. FOUND INTERMITTENT CONNECTION AT GROUND MATRIX 80VPNV. CLEANED AND RERACKED GROUND MATRIX. OPS CHECK GOOD AT THIS TIME. (IPC R
- [SDR A6WA200330002](https://openairdocs.org/sdr/A6WA200330002), Feb 10, 2003: PSEU. FAILED. PSEU SYSTEM FAILURE IN FLIGHT. MULTIPLE INDICATIONS FAIL HYDRAULIC, GEAR, GROUND SPOILER PROXIMITY WOW AND AOA. INSTALLED PSEU. (M)
- [SDR A6WA0000016](https://openairdocs.org/sdr/A6WA0000016), Feb 13, 2000: EJECTOR VALVE. FAILED. AIRFOIL DE-ICE FAILED IN FLIGHT IN ALL MODES. REMOVED AND REPLACED LEFT AND RIGHT EJECTOR FLOW CONTROL VALVES AND PATCHED SEVERAL HOLES IN LT WING OUTBOARD BOOT
- [SDR M8XA9800010](https://openairdocs.org/sdr/M8XA9800010), Jun 3, 1998: FLAP CONTROL. MALFUNCTIONED. SHORTLY AFTER TAKE-OFF, THE FLIGHT CREW REPORTED A FLAP CONTROL FAULT AND ASYMMETRY WARNING MESSAGE. AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT FURTHER I
- [SDR M8XA9800012](https://openairdocs.org/sdr/M8XA9800012), May 22, 1998: CONTROLLER. DEFECTIVE. SHORTLY AFTER T/O, THE FLIGHT CREW REPORTED A PROBLEM WITH THE AIRCRAFT PRESSURIZATION SYSTEM. AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR MANUAL MODE. AIRCRAFT RE
- [SDR M8XA9800007](https://openairdocs.org/sdr/M8XA9800007), May 12, 1998: PITOT HEAT. FAILED. EN ROUTE FROM DEN TO CYS, AIRCRAFT ENCOUNTERED ICING CONDITIONS. SINCE THE PITOT HEAT SYSTEM WAS MEL'D, AIRCRAFT WAS FORCED TO RETURN TO DEN. AIRCRAFT LANDED IN
- [SDR MBXA9800003](https://openairdocs.org/sdr/MBXA9800003), Apr 23, 1998: WINDSHIELD. CRACKED. DEN - FLT 7405 - EN ROUTE FROM DEN TO RAP, CREW REPORTED THE CAPTAIN'S WINDSCREEN HAD CRACKED AND THE AIRCRAFT WAS RETURNING TO DEN. AIRCRAFT LANDED IN DENVER W
- [SDR M8XA9700015](https://openairdocs.org/sdr/M8XA9700015), Sep 29, 1997: BEARING. DEFECTIVE. PROPELLER SERIAL NUMBER HL-146, WAS REMOVED FROM AIRCRAFT N331MX (S/N 3067) FOR SCHEDULED MAINTENANCE. WHEN THE PROPELLER WAS BEING DISASSEMBLED IN PREPARATION 
- [SDR M8XA9700014](https://openairdocs.org/sdr/M8XA9700014), Sep 16, 1997: CAS WARNING. ACTIVATED. DURING THE TAKEOFF ROLL PRIOR TO REACHING V1, THE CREW WAS ALERTED BY THE CAS SYSTEM THAT THEY HAD ENCOUNTERED AN INVERTER BUS FAIL. THIS WAS ACCOMPANIED BY AN 
- [SDR M8XA970008](https://openairdocs.org/sdr/M8XA970008), May 22, 1997: CONTROL CABLE. LACK OF LUBE. CREW REPORTED, A BINDING CONDITION WITH THE LEFT ENGINE POWER LEVER CREW ELECTED TO RETURN TO COS. AIRCRAFT LANDED COS WITH NO FURTHER INCIDENT. MAX MX INSPECTE
- [SDR M8XA961205](https://openairdocs.org/sdr/M8XA961205), Dec 24, 1996: HALL EFFECT SENS. DEFECTIVE. FLT 3535 - AIRCRAFT RETURNED FROM FLIGHT. CREW WAS ALERTED BY A RT GENERATOR FAILURE INDICATION. AIRCRAFT LANDED COS WITHOUT FURTHER INCIDENT. COS - MX REPLACED

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