# N304US: 1989 Airbus Industrie A320-211, registration cancelled 2009-04-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 8, 2009 - Status when cancelled: Valid registration - Airframe: [Airbus Industrie A320-211](https://openairdocs.org/model/airbus-industrie-a320-211) (registry code 3930320) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs) - Serial number: 040 - Year built: 1989 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 16, 1989 - Certificate issued: January 5, 2009 - Last registry action: January 5, 2009 - Mode S code: A33001 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N304US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=304US - Page: https://openairdocs.org/deregistered/N304US-2009-04-08 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 Airbus Industrie A320-211: https://openairdocs.org/model/airbus-industrie-a320-211.md ## Service difficulty reports (26) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 0602583204](https://openairdocs.org/sdr/0602583204), Dec 2, 2006: BATTERY PACK. INOPERATIVE. INOPERATIVE SEAT MOUNTED EMERGENCY ESCAPE LIGHTS, ROWS 8, 9, 10, 11. CORRECTED BY REPLACING 110WL2 BATTERY PACK. CHECKS OK. - [SDR 0602383204](https://openairdocs.org/sdr/0602383204), Nov 6, 2006: WIRE. BROKEN. DURING EMERGENCY LIGHT CHECK, EXTERNAL LOAD FORWARD FAULTED. REPAIRED BROKEN SLIDE LIGHT POWER WIRE AT DOOR 1 LEFT HINGE AREA, CHECKS OK. - [SDR 0602373204](https://openairdocs.org/sdr/0602373204), Nov 5, 2006: SOCKET. CORRODED. DURING EMERGENCY LIGHT CHECK, LT EXTERNAL LOAD FAULTED. FOUND LT AFT OVERWING LIGHT ASSEMBLY AT FAULT. REMOVED CORROSION AND REPLACED OVERWING LIGHT ASSEMBLY. C - [SDR 0601673204](https://openairdocs.org/sdr/0601673204), Jul 22, 2006: POWER SUPPLY. FAULTY. CIRCUIT BREAKER 5H (1WL, LIGHTING/EMERG LT/CABIN), POPPED DURING CLIMBOUT, FLIGHT COMPLETED UNEVENTFULLY. CIRCUIT BREAKER RESET, SYSTEM TEST DISPLAYED INT LOAD - [SDR 0500683204](https://openairdocs.org/sdr/0500683204), May 7, 2005: DRIVE SHAFT. BROKEN. DURING TAKEOFF ROLL, THE NR 2 ENGINE EGT EXCEEDED 890C. TAKEOFF ABORTED AT 110 KNOTS. MAINTENANCE FOUND NR 2 ENGINE VBV INTER CONNECTING FLEX DRIVE SHAFT AT 9:0 - [SDR 0201423204](https://openairdocs.org/sdr/0201423204), May 4, 2002: MODULE. FAULTY. DURING TAKEOFF ROLL, THE FIRST OFFICER'S AIRSPEED INDICATION NEVER EXCEEDED 45 KNOTS. ABORTED TAKEOFF AT 105 KNOTS. REPLACED THE LEFT NR 1 AIR DATA MODULE AND N - [SDR 9810843204](https://openairdocs.org/sdr/9810843204), Dec 8, 1998: ACTUATOR. LEAKING. DURING DESCENT, RECEIVED HYD R RSVR LOW LVL MESSAGE. CREW SHUT OFF GREEN HYDRAULIC PUMP, PTU, GRAVITY EXTENDED LANDING GEAR, AND LANDED WITHOUT INCIDENT. MAINTE - [SDR 9811333204](https://openairdocs.org/sdr/9811333204), Aug 7, 1998: BATTERY PACK. DISCHARGED. MID CABIN AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS. OPERATIONAL CHECK OK. - [SDR 9801073204](https://openairdocs.org/sdr/9801073204), Jan 16, 1998: RETRACT MECH. MALFUNCTIONED. DURING APPROACH WHEN FLAPS POSITION ONE SELECTED, RECEIVED F/CTL FLAPS LOCKED MESSAGE. DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED FLAP SYST - [SDR 9711803204](https://openairdocs.org/sdr/9711803204), Jun 16, 1997: B-NUT. LOOSE. DURING CRUISE, RECEIVED HYD 'Y' RSVR LO LVL MESSAGE. FOLLOWED ECAM PROCEDURES AND DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE YELLOW HYDR - [SDR 9711083204](https://openairdocs.org/sdr/9711083204), Jun 9, 1997: WARNING. MALFUNCTIONED. DURING TAKEOFF, RECEIVED FORWARD CARGO DOOR OPEN ECAM INDICATION. TAKEOFF WAS ABORTED WITH NO FURTHER INCIDENT. DOOR WAS CONFIRMED CLOSED AND DOOR INDICAITON WA - [SDR 9702643204](https://openairdocs.org/sdr/9702643204), Feb 7, 1997: BATTERY. DISCHARGED. DURING LINE MAINTENANCE, FOUND THE AFT EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK, OPERATIONAL CHECK OK. - [SDR 9627473204](https://openairdocs.org/sdr/9627473204), Dec 13, 1996: SILL. CORRODED. DURING C-CHECK, CORROSION WAS FOUND ON THE INBOARD FLANGE OF THE RIGHT AFT DOOR SILL. REPAIRED PER EA 32-120550. - [SDR 9625283204](https://openairdocs.org/sdr/9625283204), Nov 24, 1996: WINDOW. SHATTERED. DURING CLIMBOUT AT 16,000 FEET THE FIRST OFFICER'S NR 3 WINDOW OUTER PANE SHATTERED. AIRCRAFT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED - [SDR 9610843204](https://openairdocs.org/sdr/9610843204), May 16, 1996: FLEX SHAFT. WORN. DURING CLIMB, THE NR 1 ENGINE EGT REACHED 892 DEGREES CELSIUS. RETARDED THRUST, EGT DECREASED, BUT WAS STILL 50 DEGREES CELSIUS GREATER THAN NR 2 ENGINE. RETURN - [SDR 9610073204](https://openairdocs.org/sdr/9610073204), May 4, 1996: ENGINE. VIBRATION. DURING CLIMB AFTER FLAP RETRACTION, AN AIRCRAFT VIBRATION WHICH SEEMED TO FOLLOW NR 1 ENGINE RPM WAS FELT. AIRCRAFT RETURNED TO MSP. GROUND MAINTENANCE INSPECTI - [SDR 9607933204](https://openairdocs.org/sdr/9607933204), Apr 9, 1996: VBV. FAILED. DURING TAKEOFF ROLL, ENG NR 2 COMPRESSOR VANE FAULT ANNUNCIATED. ABORTED TAKEOFF AT 80 KNOTS, AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE VBV POSITI - [SDR 9603503204](https://openairdocs.org/sdr/9603503204), Feb 12, 1996: MOTOR. LEAKING. DURING CLIMBOUT, NOTICED AN ACCUMULATION OF NOXIOUS FUMES IN THE COCKPIT AND CABIN. CREW DONNED THE OXYGEN MASKS AND THE AIRCRAFT RETURNED TO MIA WITH EMERGENCY - [SDR 9521153204](https://openairdocs.org/sdr/9521153204), Dec 20, 1995: SMOKE DET. MALFUNCTIONED. DURING ENGINE START, RECEIVED 'SMOKE AFT CARGO SMOKE' WARNING. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DISCHARGED FIRE BOTTLE, RETURNED TO GATE AND DEPLAN - [SDR 9519963204](https://openairdocs.org/sdr/9519963204), Dec 8, 1995: SMOKE LIGHT. ILLUMINATED. DURING CRUISE, THE SMOKE LIGHT ON THE GEN 1 LINE PUSH BUTTON SWITCH ON THE FLIGHT DECK OVERHEAD PANEL ILLUMINATED ACCOMPANIED BY AN INTERMITTENT VENT EXTRACT FA - [SDR 9519953204](https://openairdocs.org/sdr/9519953204), Dec 8, 1995: EEL POWER SUPPLY. INOPERATIVE. CABIN EMERGENCY LIGHT CIRCUIT BREAKER POPPED ON THE OVERHEAD PANEL. MAINTENANCE REPLACED THE FORWARD EPSU AND BATTERIES. OPERATIONAL CHECK OK. - [SDR 9515133204](https://openairdocs.org/sdr/9515133204), Oct 6, 1995: LINE. LEAKING. DURING TAKEOFF ROLL, RECEIVED HYD 'Y' RSVR LO LVL MESSAGE. TAKEOFF WAS ABORTED AT 60 KNOTS AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPAIRED A LEAKING HYD - [SDR 9513553204](https://openairdocs.org/sdr/9513553204), Aug 31, 1995: HYD PUMP. FAILED. DURING CRUISE RECEIVED HYD-B ELEC PUMP LOW PRESSURE MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLUE HYDRAULIC SYS - [SDR 9512163204](https://openairdocs.org/sdr/9512163204), Aug 8, 1995: VBV. MALFUNCTIONED. DURING CLIMB, NR 2 ENGINE EGT REACHED 890 DEGREES AND NEVER COOLED BELOW 850 DEGREES. THE AIRCRAFT RETURNED TO MSP WHERE AN UNEVENTFUL LANDING TOOK PLACE. THE V - [SDR 9507493204](https://openairdocs.org/sdr/9507493204), May 7, 1995: THROTTLE CONTL. MALFUNCTIONED. DURING CLIMBOUT FROM MSP, RECEIVED ENG 2 THR LEVER FAULT MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RETURNED TO MSP WHERE AN UNEVENTFUL LANDING W - [SDR 9501833204](https://openairdocs.org/sdr/9501833204), Feb 3, 1995: ECU. MALFUNCTIONED. DURING CLIMB, THE NR 1 ENGINE EXPERIENCED TWO OR THREE POWER SURGES. NUMEROUS 'A' AND 'B' FADEC MESSAGES WERE OBSERVED. ENGINE THRUST WAS REDUCED TO IDLE AND EN ## FAA accident and incident reports (1) 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 20000805029229I](https://openairdocs.org/incident/20000805029229I), Aug 5, 2000: Airbus A320211 (N304US), Chicago, IL, Minor damage. (-23)Nwaa aircraft N304US was holding short of runway 14R-32L at taxiway tnago 10 when a dobbs food service van struck the aircraft on the outboard lower… ## Other aircraft with N304US - [Registered now](https://openairdocs.org/aircraft/N304US): Costruzioni Aeronautiche Tecna P2006T, S/N 403/US, built 2024 --- 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.