# N937FR: 2005 Airbus A319-111, registration cancelled 2012-12-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 3, 2012 - Exported to: Belgium - Status when cancelled: Valid registration - Airframe: [Airbus A319-111](https://openairdocs.org/model/airbus-a319-111) (registry code 3940000) - 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: 2400 - Year built: 2005 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 19, 2005 - Certificate issued: November 6, 2012 - Last registry action: November 6, 2012 - Mode S code: AD0037 - 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: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N937FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=937FR - Page: https://openairdocs.org/deregistered/N937FR-2012-12-03 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 A319-111: https://openairdocs.org/model/airbus-a319-111.md ## Service difficulty reports (17) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA2011032100617](https://openairdocs.org/sdr/F3LA2011032100617), Mar 17, 2011: WINDSHIELD. CRACKED. F/O WINDSHIELD CRACKED FOLLOWING ANTI-ICE RT WINDSHIELD ECAM. R & R THE F/O WINDSHIELD WITH SERVICEABLE WINSHIELD REF AMM 56-11-11-400-000-001. - [SDR F3LA2011031500614](https://openairdocs.org/sdr/F3LA2011031500614), Mar 11, 2011: HINGE FITTING. CORRODED. A/C C-CHECK: NON ROUTINE; FWD AIRFRAME HINGE FITTING FOR LT MAIN GEAR DOOR, FWD LUG FACE OF FITTING, HAS WEAR .013" TO .018" DEEP. CAUSED BY BOLT ROTATING. SPOT - [SDR F3LA2011031500613](https://openairdocs.org/sdr/F3LA2011031500613), Mar 11, 2011: FLOORBEAM. CORRODED. ACFT C-CHECK: NON ROUTINE NR 31644; MAIN CABIN FLOORBEAM HAS CORROSION 6" OF FR 66, Y 1732. CORROSION NOTED IS EXFOLIATION AND OUT OF LIMITS IAW SRM 53-41-14 P - [SDR F3LA2011031500612](https://openairdocs.org/sdr/F3LA2011031500612), Mar 11, 2011: SILL. CORRODED. ACFT C-CHECK: NON ROUTINE; MAIN CABIN FLOOR SILL BEAM (L2 DOOR) CORRODED BEYOND LIMITS AT FR 66, Y 1732 IAW SRM 53-41-14, P 4.B, FIG. 101. BLENDED CORROSION TRE - [SDR F3LA2010090100500](https://openairdocs.org/sdr/F3LA2010090100500), Sep 16, 2010: PITCH CONTROL. MALFUNCTIONED. PILOT REPORTED, ACFT PITCH WILL NOT STABLE WHILE HAND FLYING, UNCOMMANDED INCREASE IN PITCH UP. MX PERFORMED BITE TEST OF THE EFCS IAW AMM 27-96-00-740-001 WITH - [SDR F3LA2010030700357](https://openairdocs.org/sdr/F3LA2010030700357), Mar 4, 2010: SERVO. WORN. AIR TURN BACK DUE TO AIRFRAME VIBRATION ON CLIMB OUT. AIRSPEED 280 KIAS. ALTITUDE APPROX 17,000 FT. LOW FREQUENCY SIGNIFICANT AMPLITUDE INCREASING WITH FORE AND - [SDR F3LA2010021700344](https://openairdocs.org/sdr/F3LA2010021700344), Feb 15, 2010: CYLINDER. LOW. DURING CRUISE ALTITUDE THE FLIGHT CREW NOTED THE CREW OXYGEN LOW. MAINTENANCE SERVICED THE CREW OXYGEN AND RESET THE CREW OXYGEN MASKS IAW AMM 12-35-10 PB301, N - [SDR F3LA2009082500140](https://openairdocs.org/sdr/F3LA2009082500140), Aug 21, 2009: FLOOR SUPPORT. CORRODED. DURING C3 C-CHECK, INSP NOTED THE LONGITUDINAL FLOORBEAM Y1292 AND FRAME 68 HAS CORROSION AROUND FLOOR PANEL NUTPLATES. MX REMOVED AND REPLACED FLOORBEAM IAW SR - [SDR F3LA2009082500139](https://openairdocs.org/sdr/F3LA2009082500139), Aug 21, 2009: SHEAR PLATE. CORRODED. DURING C3 C-CHECK, INSP NOTED THE LT SHEAR PLATE BETWEEN FRAME 69 AND FRAME 70 HAS CORROSION AROUND NUTPLATES. MX REMOVED AND REPLACED THE LT SHEAR PLATE IAW SR - [SDR F3LA2009082500145](https://openairdocs.org/sdr/F3LA2009082500145), Aug 18, 2009: SHEAR PLATE. CORRODED. DURING C3 C-CHECK, INSP NOTED THE RT SIDE LATERAL SHEAR PLATE WAS CORRODED AT FRAME 69 AND FRAME 70. MX REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-42-11 AN - [SDR F3LA2009082500144](https://openairdocs.org/sdr/F3LA2009082500144), Aug 18, 2009: FLOOR SUPPORT. CORRODED. DURING C3 C-CHECK, INSP NOTED THE R2 DOOR LONGITUDINAL FLOORBEAM -Y1292 AFT OF FRAME 66 HAS CORROSION AROUND NUTPLATES. MAINT REMOVED CORROSION AND PERFORMED RE - [SDR F3LA2009082500143](https://openairdocs.org/sdr/F3LA2009082500143), Aug 18, 2009: FLOOR SUPPORT. CORRODED. DURING C3 C-CHECK, INSP NOTED THE L2 DOOR LONGITUDINAL FLOORBEAM Y1292 AT FRAME 66 HAS CORROSION AROUND FLOOR PANEL NUTPLATES. MX REMOVED CORROSION AND PERFORME - [SDR F3LA2009082500142](https://openairdocs.org/sdr/F3LA2009082500142), Aug 18, 2009: SILL. CORRODED. DURING C3 C-CHECK, INSP NOTED THE L2 DOOR SILL PLATE HAS CORROSION AT FRAME 68. MX REMOVED CORROSION DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED IAW EA A9-5 - [SDR F3LA2009082500141](https://openairdocs.org/sdr/F3LA2009082500141), Aug 18, 2009: FLOOR SUPPORT. CORRODED. DURING C3 C-CHECK, INSP NOTED THE LONGITUDINAL FLOOR SUPPORT Y1292 AFT OF FRAME 66 AND FWD OF FRAME 68 HAS CORROSION AROUND FLOOR PANEL NUTPLATES. MX REMOVED AN - [SDR F3LA200800131](https://openairdocs.org/sdr/F3LA200800131), Mar 19, 2008: FLOOR PANEL. DAMAGED. DURING C2 C CHECK, INSPECTION REPORTED A HOLE WAS PUNCTURED INTO THE UPPER SKIN OF AFT CARGO PIT FLOOR PANEL 151VG, NEAR THE FORWARD EDGE, IN THE CENTER. MAINTE - [SDR F3LA200700385](https://openairdocs.org/sdr/F3LA200700385), Dec 24, 2007: ENGINE. FAILED. FLIGHT CREW REPORTED INFLIGHT SHUTDOWN OF NR 1 ENGINE DUE TO LOSS OF OIL QUANTITY/OIL PRESSURE. NR 1 ENGINE IS IN THE PROCESS OF BEING REPLACED. 1/7/008 FLT CRE - [SDR F3LA200500049](https://openairdocs.org/sdr/F3LA200500049), Dec 21, 2005: ACTUATOR. TRIPPED. UPON APPROACH, FLIGHT CREW REPORTED ECAM F/CTL SLATS FAULT. PERFORMED TSM TASK 27-81-00-810-810. FOUND TORQUE LIMITERS POPPED ON SLAT ROTARY ACTUATORS 6079 CM A ## 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 20080213011499I](https://openairdocs.org/incident/20080213011499I), Feb 13, 2008: Airbus A319111 (N937FR), Salt Lake City, UT, No damage. (-23) Following please find additional information concerning the injuries that occurred due to severe turbulence encountered by aircraft N937FR, flight 571,… --- 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.