# N307US: 1990 Airbus Industrie A320-211, registration cancelled 2006-08-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 3, 2006
- Status when cancelled: Triennial form not returned
- 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: 106
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 8, 1990
- Certificate issued: April 24, 1990
- Last registry action: January 20, 2004
- Mode S code: A33B26
- Owner when cancelled: [Northwest Airlines Inc](https://openairdocs.org/faa-owner/NORTHWEST%20AIRLINES%20INC)
- Location: [St Paul, MN](https://openairdocs.org/faa-place/MN/St%20Paul)
- Owner type: Corporation
- Owner's area on the map: 44.8873° N, 93.1924° W: Placed by OpenAirDocs at the center of ZIP code 55111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N307US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=307US
- Page: https://openairdocs.org/deregistered/N307US-2006-08-03

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 (9)

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

- [SDR 0301393207](https://openairdocs.org/sdr/0301393207), Jul 28, 2003: LINE. LEAKING. THIRTY MINUTES INTO FLIGHT, LOST ALL HYDRAULIC FLUID IN YELLOW SYSTEM. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED LEAKI
- [SDR 0100523207](https://openairdocs.org/sdr/0100523207), Feb 16, 2001: HYDRAULIC LINE. LEAKING. DURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED COM PROCEDURES, CONTINUED TO FINAL DESTINATION, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HY
- [SDR 0100393207](https://openairdocs.org/sdr/0100393207), Feb 1, 2001: B-NUT. LOOSE. DURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED ECAM AND COM PROCEDURES. CONTINUED TO FINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE SEC
- [SDR 9710403207](https://openairdocs.org/sdr/9710403207), May 28, 1997: BULB. FAILED. DURING LINE MAINTENANCE, FOUND ALL FOUR OVERWING EMERGENCY EXIT HANDLE LIGHTS INOPERATIVE. REPLACED LIGHT BULBS, OPERATIONAL CHECK OK.
- [SDR 9623303207](https://openairdocs.org/sdr/9623303207), Nov 4, 1996: POWER SUPPLY. INOPERATIVE. DURING LINE MAINTENANCE, FOUND AFT EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED EPSU, OPERATIONAL CHECK OK.
- [SDR 9604173207](https://openairdocs.org/sdr/9604173207), Feb 14, 1996: NUT. CRACKED. DURING '1C1' CHECK, LEFT ENGINE CHANGE FOUND THE FORWARD ENGINE MOUNT FORWARD ATTACH NUTS CRACKED. FURTHER INVESTIGATION REVEALED THAT IMPROPER CONFIGURATION NU
- [SDR 9504693207](https://openairdocs.org/sdr/9504693207), Mar 17, 1995: FLOOR SUPPORT. CORRODED. DURING THE INTERMEDIATE LAYOVER VISIT, THE AFT GALLEY FLOOR SUPPORT AT Y=1165 BETWEEN FRAME 68 AND 69 WAS FOUND CORRODED ON THE LOWER SURFACE OF THE UPPER FLANG
- [SDR 9503753207](https://openairdocs.org/sdr/9503753207), Mar 10, 1995: SEAT TRACK. CORRODED. DURING INTERMEDIATE LAYOVER CHECK, FOUND CORROSION ON THE UPPER FLANGE OF THE SEAT TRACK AT Y = +765, FRAME 18. CORROSION WAS AT A NUT CLIP LOCATION. REPAIRED P
- [SDR 9504683207](https://openairdocs.org/sdr/9504683207), Feb 17, 1995: SILL. CORRODED. DURING INTERMEDIATE LAYOVER VISIT, CORROSION WAS FOUND ON THE INBOARD FLANGE OF THE RIGHT AFT CABIN DOOR LOWER SILL. CORROSION WAS FOUND AROUND EXISTING NUT PLA

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