# N106US: 1999 Airbus Industrie A320-214, registration cancelled 2009-05-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 28, 2009 - Status when cancelled: Triennial form not returned - Airframe: [Airbus Industrie A320-214](https://openairdocs.org/model/airbus-industrie-a320-214) (registry code 3930316) - 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: 1044 - Year built: 1999 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 30, 1999 - Certificate issued: August 5, 1999 - Last registry action: October 21, 2008 - Mode S code: A01CD1 - 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/N106US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=106US - Page: https://openairdocs.org/deregistered/N106US-2009-05-28 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 A320-214: https://openairdocs.org/model/airbus-industrie-a320-214.md ## Service difficulty reports (24) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA2009011690084](https://openairdocs.org/sdr/USAA2009011690084), Jan 15, 2009: ENGINE. BIRD INGESTION. FLT 1549 LGA-CLT - EMERGENCY DITCHING - DUAL ENGINE FAILURE - CREW REPORTED BIRD INGESTION SHORTLY AFTER TAKEOFF AND REQUESTED TO RETURN TO FIELD. ACFT MADE AN - [SDR SA07034](https://openairdocs.org/sdr/SA07034), Jun 6, 2007: BOTTLE. READS LOW. DCA - THE RIGHT HAND OVERWING EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE WAS FOUND LOW DURING INSPECTION. MAINTENANCE ACCOMPLISHED REPLACEMENT OF THE RIGHT HAND OVE - [SDR SA07017](https://openairdocs.org/sdr/SA07017), Feb 28, 2007: SLIDE. FAULTY. PHL - THE FRONT ENTRY DOOR WAS OPENED INADVERTENTLY AFTER IT WAS ARMED. THE SLIDE DID NOT DEPLOY. MAINTENANCE REPLACED THE FORWARD, LEFT ENTRY DOOR EMERGENCY ES - [SDR SA07023](https://openairdocs.org/sdr/SA07023), Mar 20, 2006: EPSU. FAULTED. RIC - THE MID CABIN, RIGHT HAND EMERGENCY POWER SUPPLY UNIT FAILED THE WEEKLY CHECK. MAINTENANCE REPLACED THE MID CABIN, RIGHT HAND EMERGENCY POWER SUPPLY UNIT. - [SDR SA05088](https://openairdocs.org/sdr/SA05088), Jul 21, 2005: LANYARD. MISSING. PIT - THE LEFT FORWARD DOOR ESCAPE SLIDE SURVIVAL KIT LANYARD WAS FOUND INCORRECTLY ROUTED. MAINTENANCE CORRECTLY ROUTED THE SURVIVAL KIT LANYARD. OK FOR SERVIC - [SDR SA05087](https://openairdocs.org/sdr/SA05087), Jul 21, 2005: LANYARD. MISSING. PIT - THE AFT RIGHT DOOR ESCAPE SLIDE SURVIVAL KIT LANYARD WAS FOUND INCORRECTLY ROUTED. MAINTENANCE CORRECTLY ROUTED THE AFT RIGHT DOOR ESCAPE SLIDE SURVIVAL K - [SDR SA05086](https://openairdocs.org/sdr/SA05086), Jul 21, 2005: LANYARD. MISSING. PIT - THE AFT LEFT EMERGENCY EXIT DOOR ESCAPE SLIDE SURVIVAL KIT LANYARD WAS FOUND NOT IN VIEW. MAINTENANCE INSTALLED SURVIVAL KIT LANYARD. OK FOR SERVICE. - [SDR USAA050477](https://openairdocs.org/sdr/USAA050477), Apr 10, 2005: FLOORBEAM. CORRODED. PIT - FOUND FLOORBEAM CORRODED 2.5 INCHES DIAMETER AREAS, FLOORBEAM GALLEY MOUNTING HOLES OUTBOARD FLOORBEAM, BETWEEN RT SIDE C68-69. DEFECTIVE PART REPLACED WI - [SDR USAA050496](https://openairdocs.org/sdr/USAA050496), Apr 10, 2005: FLOORBEAM. CORRODED. FOUND FLOORBEAM CORRODED 1 SQUARE INCH, AROUND NUT PLATE HOLES, FLOORBEAM C66-C69 LEFT OUTBOARD. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11. CORRO - [SDR USAA050479](https://openairdocs.org/sdr/USAA050479), Apr 10, 2005: FLOORBEAM. CORRODED. PIT - FOUND FLOORBEAM CORRODED 2 INCHES BY 2 INCHES BY .060 INCH DEEP AREA, FLOOR SUPPORT AT Y750 ABOVE C68. CORROSION LEVEL 1, TASK JA-260-53500. DEFECTIVE PAR - [SDR USAA050478](https://openairdocs.org/sdr/USAA050478), Apr 10, 2005: FLOORBEAM. CORRODED. FLOORBEAM CORRODED .5 INCH DIAMETER AREA, FLOORBEAM AT FRAME 20, 9 INCH RIGHT OF CENTER. REMOVED CORROSION, INSTALLED DOUBLER PER SRM 53-11-14. CORROSION LEVEL - [SDR USAA050522](https://openairdocs.org/sdr/USAA050522), Apr 5, 2005: FLOORBEAM. CORRODED. PIT - FOUND FLOORBEAM CORRODED 2 INCH BY 2 INCH AREA, LEFT INBOARD AFT FLOORBEAM Y765 FRAME C64-C70. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-41-14. C - [SDR USAA050465](https://openairdocs.org/sdr/USAA050465), Apr 5, 2005: FLOORBEAM. CORRODED. PIT - FOUND FLOORBEAM CORRODED 1 BY .5 BY .030 INCH, .75 INCH BY .5 INCH BY .030 INCH, .75 BY .3750 BY .05, FLOOR BEAM 10 INCHES LEFT OF CENTER LINE BETWEEN C16 - [SDR SA05016](https://openairdocs.org/sdr/SA05016), Feb 6, 2005: PROXIMITY SENSOR. FAULTY. EN ROUTE MSY TO CLT - AFTER TAKEOFF, THE LANDING GEAR INDICATES DOWN AFTER THE LANDING GEAR LEVER WAS MOVED UP. UPON ARRIVAL, THE LANDING GEAR HAD AMBER -X- IND - [SDR USAASA04034](https://openairdocs.org/sdr/USAASA04034), Apr 3, 2004: POWER SUPPLY. INOPERATIVE. THE LEFT AFT EMERGENCY POWER SUPPLY UNIT FAULTED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE LEFT AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY - [SDR USAASA03036](https://openairdocs.org/sdr/USAASA03036), May 1, 2003: PROXIMITY SWITCH. INOPERATIVE. AFTER TAKEOFF, CREW RECEIVED ECAM INDICATIONS OF 'GEAR NOT UPLOCKED', 'ENG 2 REVERSER FAULT', AND 'CAPT PITOT'. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT - [SDR USAASA03016](https://openairdocs.org/sdr/USAASA03016), Feb 16, 2003: POWER SUPPLY. MALFUNCTIONED. DCA - DURING THE EMERGENCY LIGHT SYSTEM TEST, RECEIVED 'EPSU INT LOAD FWD LT FAULT' MESSAGE. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT. OPERA - [SDR USAASA03010](https://openairdocs.org/sdr/USAASA03010), Jan 28, 2003: GIRT BAR. LACK OF LUBE. LGA - THE L1 DOOR WAS DIFFICULT TO KEEP IN THE ARMED POSITION. MAINTENANCE CLEANED AND LUBRICATED THE GIRT BAR ASSEMBLY AND LOCKING MECHANISM, AND REPLACED THE - [SDR USAADUPE](https://openairdocs.org/sdr/USAADUPE), Jan 28, 2003: GIRT BAR. DIRTY. LGA - THE L1 DOOR WAS DIFFICULT TO KEEP IN THE ARMED POSITION. MAINTENANCE CLEANED AND LUBRICATED THE GIRT BAR ASSEMBLY AND LOCKING MECHANISM, AND REPLACED THE - [SDR USAASA02105](https://openairdocs.org/sdr/USAASA02105), Dec 7, 2002: FLAP. OUT OF POSITION. THE SLIDE FOR DOOR L1 WOULD NOT REMAIN ARMED. MAINTENANCE REPOSITIONED THE GIRT FLAP ON THE GIRT BAR TO ELIMINATE FRICTION. THE SLIDE ARMING OF THE L1 DOOR NOW - [SDR USAASA02101](https://openairdocs.org/sdr/USAASA02101), Nov 20, 2002: BATTERY PACK. DISCHARGED. BOS - THE LEFT OVERWING BATTERY PACK EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECKED OK. (M) - [SDR USA2002F00057](https://openairdocs.org/sdr/USA2002F00057), Jun 21, 2002: SLIDE. INTERMITTENT. THE FORWARD CABIN, RIGHT SIDE, EMERGENCY ESCAPE SLIDE WAS DIFFICULT TO ARM AND INTERMITTENTLY INDICATED DISARMED. MAINTENANCE REPLACED THE EMERGENCY ESCAPE SLID - [SDR USAA020157](https://openairdocs.org/sdr/USAA020157), May 2, 2002: SKIN. CRACKED. TPA - FOUND SKIN CRACKED .150 INCH, FRAME 30 STRINGER 8L. INSTALLED DOUBLER AND FILLER PER SRM 53-21-11 AND 53-00-11. (M) - [SDR USAASA01037](https://openairdocs.org/sdr/USAASA01037), Jul 20, 2001: ENGINE. FAILED. JFK - FLT 6808 - EN ROUTE LGA-BOS, WHILE CLIMBING THROUGH FL080, FELT MULTIPLE COMPRESSION STALLS AND OBSERVED SHOTS OF FLAME FROM THE LEFT SIDE OF THE AIRCRAFT ## 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 DCA09MA026](https://openairdocs.org/ntsb/DCA09MA026), Jan 15, 2009: Airbus A320 (N106US), Weehawken, NJ, substantial damage. Probable cause: The ingestion of large birds into each engine, which resulted in an almost total loss of thrust in both engines and the subsequent ditching on the Hudson River. Contributing to the fuselage damage… ## 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. - [Accident 20090115024869A](https://openairdocs.org/incident/20090115024869A), Jan 15, 2009: Airbus A320214 (N106US), New York, NY, Destroyed. After departing lga, and while climbing through 3,200 feet, us flight 1549 suffered multiple birdstrikes resulting in a total loss of power from both engines.… --- 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.