# N901FR: 2001 Airbus A319-111, registration cancelled 2009-02-12 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 12, 2009 - Exported to: Bermuda - 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: 1488 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 4, 2004 - Certificate issued: September 5, 2008 - Last registry action: November 26, 2008 - Mode S code: AC7370 - 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/N901FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=901FR - Page: https://openairdocs.org/deregistered/N901FR-2009-02-12 From the FAA registry file of October 31, 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 (40) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA200800410](https://openairdocs.org/sdr/F3LA200800410), Jul 2, 2008: STUD. BROKEN. DURING A DAILY CHECK MAINT NOTED THE L1 DOOR EVACUATION SLIDE AT ATTACH BOLT BROKEN AFT SIDE OF L1 DOOR EVACUATION SLIDE. MAINT REMOVED AND REPLACED ATTACH STUD - [SDR F3LA200700367](https://openairdocs.org/sdr/F3LA200700367), Dec 10, 2007: HOOK. DAMAGED. DURING C-5 CHECK, INSPECTION REPORTED UPON INSTALLATION OF R2 DOOR SLIDE, OPEN/CLOSE HANDLE COULD BE OPERATED BEFORE DOOR WAS IN HOLE. REMOVED AND REPLACED HOOK - [SDR F3LA200700366](https://openairdocs.org/sdr/F3LA200700366), Dec 9, 2007: HINGE FITTING. CORRODED. DURING C-5 CHECK, INSPECTION REPORTED NR 2 PYLON T/R COWL FITTINGS AT RIB 1 AND RIB 2 CORRODED. REMOVED AND REPLACED NR 2 PYLON OTBD T/R COWL FITTINGS AT RIBS 1 - [SDR F3LA200700368](https://openairdocs.org/sdr/F3LA200700368), Dec 7, 2007: FLOOR PANEL. BROKEN. DURING C-5 CHECK, INSPECTION REPORTED FLOOR PANEL 151PE IN AFT CARGO COMPARTMENT BROKEN INTERNALLY. REMOVED PANEL 151PE IAW SRM 51-42-11. DETERMINED PANEL TO BE - [SDR F3LA200700365](https://openairdocs.org/sdr/F3LA200700365), Dec 7, 2007: SHEAR PLATE. CORRODED. DURING C-5 CHECK, INSPECTION REPORTED CORROSION ON FWD CARGO COMPARTMENT FLOORBEAM AT FR 28, AND ON THE AFT DOOR SILL. CORROSION WAS CLASSIFIED AS EXFOLIATION. - [SDR F3LA20700364](https://openairdocs.org/sdr/F3LA20700364), Dec 5, 2007: PIN. CORRODED. DURING C-5 CHECK, INSPECTION REPORTED PITTING ON SHOULDER OF NLG TORQUE LINK CENTER PIN. REMOVED AND REPLACED NLG TORQUE LINK CENTER PIN IAW 32-21-27-420-050. P - [SDR F3LA200700363](https://openairdocs.org/sdr/F3LA200700363), Dec 5, 2007: LOCK TAB. FAILED. DURING C-5 CHECK, INSPECTION REPORTED NR 2 ENG AFT MOUNT INBD LWR LOCKING TAB THAT SECURES BOLT FROM ROTATING BLOWN OUT OF ITS SECURING POSITION TO PREVENT BOLT - [SDR F3LA200700370](https://openairdocs.org/sdr/F3LA200700370), Dec 4, 2007: BATTERY PACK. NO TEST. DURING C-5 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY BATTERY EPSU FAILED CAPACITY TEST. REMOVED AND REPLACED EPSU BATTERY AND PERFORMED OPS CHECK IAW AMM - [SDR F3LA200700372](https://openairdocs.org/sdr/F3LA200700372), Dec 4, 2007: BATTERY PACK. NO TEST. DURING C-5 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY BATTERY EPSU FAILED CAPACITY TEST. REMOVED AND REPLACED EPSU BATTERY AND PERFORMED OPERATIONAL CHECK - [SDR F3LA200700371](https://openairdocs.org/sdr/F3LA200700371), Dec 4, 2007: BATTERY PACK. NO TEST. DURING C-5 CHECK, INSPECTION REPORTED AFT EMERGENCY BATTERY EPSU FAILED CAPACITY TEST. REMOVED AND REPLACED EPSU BATTERY AND PERFORMED OPS CHECK IAW AMM 33-51-3 - [SDR F3LA200700369](https://openairdocs.org/sdr/F3LA200700369), Dec 4, 2007: BATTERY PACK. NO TEST. DURING C-5 CHECK, INSPECTION REPORTED FWD EMERGENCY BATTERY EPSU FAILED CAPACITY TEST. REMOVED AND REPLACED FWD EPSU BATTERY AND PERFORMED OPS CHECK IAW 33-51-3 - [SDR F3LA200700362](https://openairdocs.org/sdr/F3LA200700362), Dec 4, 2007: SILL. CORRODED. DURING C-5 CHECK, INSPECTION REPORTED LIGHT SURFACE CORROSION ON FWD CARGO DOOR SILL WEB. REMOVED NUTPLATE AND REWORKED FOUR SMALL AREAS OF CORROSION IAW SRM 51 - [SDR F3LA200600055](https://openairdocs.org/sdr/F3LA200600055), Jun 10, 2006: BATTERY. FAILED. DURING C-4 CHECK, INSPECTION REPORTED RT OVERWING EXIT EPSU BATTERY FAILED CAPACITY CHECK. REPLACED EPSU BATTERY AT RT OVERWING EXIT. OPS CHECKED GOOD PER AMM 3 - [SDR F3LA200600052](https://openairdocs.org/sdr/F3LA200600052), Jun 9, 2006: BATTERY. FAULTED. DURING C-4 CHECK, INSPECTION REPORTED FWD EPSU BATTERY FAULT. REPLACED EPSU BATTERY AT 10WL ABOVE L1 DOOR. OPS CHECKED GOOD PER AMM 33-51-38-000-002 AND 33-51-3 - [SDR F3LA200600054](https://openairdocs.org/sdr/F3LA200600054), Jun 9, 2006: BATTERY. FAULTED. DURING C-4 CHECK, INSPECTION REPORTED EPSU BATTERY EMER LEFT FAULT. REPLACED EPSU BATTERY AT LT OVERWING EMERGENCY EXIT. OPS CHECKED GOOD PER AMM 33-51-38-000-0 - [SDR F3LA200600053](https://openairdocs.org/sdr/F3LA200600053), Jun 9, 2006: BATTERY. FAULTED. DURING C-4 CHECK, INSPECTION REPORTED AFT EPSU BATTERY FAULT. REPLACED EPSU BATTERY AT 13WL. OPS CHECKED GOOD PER AMM 33-51-38-000-002 AND 33-51-38-400-002. - [SDR F3LA200600044](https://openairdocs.org/sdr/F3LA200600044), May 31, 2006: BEARING. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED LT MLG LWR BEARING ASSY CORRODED, PITTED AND DEFORMED. REMOVED CORROSION ON LT MLG SHOCK ABSORBER GLAND SEAL PER EA A9-32R - [SDR F3LA200600041](https://openairdocs.org/sdr/F3LA200600041), May 30, 2006: FLOOR PANEL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CABIN FLOOR PANEL 222FF AT R1 ENTRYWAY CORRODED IN 3 AREAS. REPLACED FLOOR PANEL PER WORK CARD NR CP753-12. - [SDR F3LA200600039](https://openairdocs.org/sdr/F3LA200600039), May 17, 2006: JOINT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED JOINT SHEET BETWEEN FR68 AND FR69, LT. SIDE JUST AFT OF L2 SILL, CORRODED. FABRICATED AND INSTALLED NEW JOINT SHEET PER SR - [SDR F3LA200600038](https://openairdocs.org/sdr/F3LA200600038), May 17, 2006: ATTACH BRACKET. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED MILD SURFACE CORROSION ON CABIN FLOORBOARD PANEL NR 262EF ATTACHMENT BRACKET. FABRICATED AND INSTALLED NEW CONNECTING BRAC - [SDR F3LA200600035](https://openairdocs.org/sdr/F3LA200600035), May 17, 2006: FAIRING. CRACKED. DURING C-4 CHECK, INSPECTION REPORTED NR 1 ENGINE PYLON AFT LOWER FAIRING CRACKED. REPAIRED LOWER ENGINE PYLON FAIRING BY WELD PER EA A0-54T-11332. PERFORMED FL - [SDR F3LA200600028](https://openairdocs.org/sdr/F3LA200600028), May 17, 2006: SUPPORT ANGLE. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED SUPPORT ANGLE AT FR 69-70, RT SIDE OF AIRCRAFT UNDER WEB SUPPORT PLATE, CORRODED. REPLACED ANGLE SUPPORT AND WEB ASSY PER - [SDR F3LA200600051](https://openairdocs.org/sdr/F3LA200600051), May 15, 2006: BUSHING. CRACKED. DURING C-4 CHECK, INSPECTION REPORTED I/B RT SEAT TRACK EXPANSION JOINT THROUGH BOLT BUSHING CRACKED AT FR35 TO FR36. REPLACED BOLT AND BUSHINGS PER SRM 51-42-1 - [SDR F3LA200600050](https://openairdocs.org/sdr/F3LA200600050), May 15, 2006: BUSHING. BROKEN. DURING C-4 CHECK, INSPECTION REPORTED I/B LT SEAT TRACK EXPANSION JOINT THROUGH BOLT HAD BROKEN BUSHING AT FR35 TO FR36. REPLACED BOLT AND BUSHINGS PER SRM 51-4 - [SDR F3LA200600046](https://openairdocs.org/sdr/F3LA200600046), May 15, 2006: FLOOR PANEL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOOR PANEL 221FF CORRODED ALONG INBD EDGE OF L1 DOOR THRESHOLD. REPLACED PANEL 221FF PER WORK CARD CP753-12 AND AMM 53-12 - [SDR F3LA200600037](https://openairdocs.org/sdr/F3LA200600037), May 13, 2006: WEB. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON WEB BETWEEN FR69 AND FR70, R/H NEXT TO FUSELAGE. INSTALLED NEW ANGLE AND WEB ASSY. PER SRM 51-42-11 AND DRAWI - [SDR F3LA200600036](https://openairdocs.org/sdr/F3LA200600036), May 13, 2006: FLOOR PANEL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED L2 DOOR THRESHOLD PANEL 261EF CORRODED. INSTALLED NEW FLOOR PANEL PER DRAWING D5367-1805. - [SDR F3LA200600034](https://openairdocs.org/sdr/F3LA200600034), May 13, 2006: FLOORBOARD. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CORRODED AT FRAME 15, 6TH FLOORBEAM FROM RT CENTER OF FUSELAGE ON THE AFT END OF BEAM. BLENDED CORROSION AND PER - [SDR F3LA200600033](https://openairdocs.org/sdr/F3LA200600033), May 13, 2006: SUPPORT ANGLE. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON SUPPORT ANGLE AT FR69 TO FR70, LT. SIDE UNDER SUPPORT WEB PLATE. REPLACED WEB AND SUPPORT ANGLE PER SRM 51-44 - [SDR F3LA200600032](https://openairdocs.org/sdr/F3LA200600032), May 13, 2006: WEB. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR WEB NEXT TO FUSELAGE BETWEEN FRAMES 69 AND 70. REPLACED SUPPORT ANGLE AND WEB PER SRM 51-42-11, ARM 51- - [SDR F3LA200600031](https://openairdocs.org/sdr/F3LA200600031), May 13, 2006: DUMMY RAIL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CORRODED AT FR15, 5TH FLOORBEAM FROM LT. CENTER OF FUSELAGE ON AFT END. DUMMY RAIL AT STATION Y503.2 FOUND TO BE - [SDR F3LA200600030](https://openairdocs.org/sdr/F3LA200600030), May 13, 2006: SUPPORT ANGLE. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON LT SIDE OF SUPPORT ANGLE THAT ATTACHES WEB SUPPORT PLATE BETWEEN FR69 AND FR70 AT FLOOR LEVEL. INSTALLED NEW - [SDR F3LA200600029](https://openairdocs.org/sdr/F3LA200600029), May 13, 2006: FLOOR SUPPORT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT NUT PLATE HOLES BETWEEN FRAMES 66 AND 68, AND 44 IN RIGHT OF CENTERLINE. REPLACED FLOORBEAM FR6 - [SDR F3LA200600042](https://openairdocs.org/sdr/F3LA200600042), May 12, 2006: FLOOR PANEL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON THRESHOLD PANEL AT R2 DOOR. REMOVED CORROSION ON TOP AND BOTTOM SKIN PER SRM 51-22-00. ALLOWABLE SKIN REMOVED - [SDR F3LA200600045](https://openairdocs.org/sdr/F3LA200600045), May 11, 2006: PANEL. CRACKED. DURING C-4 CHECK, INSPECTION REPORTED LT PYLON PANEL 473AL CRACKED ON RADIUS OF INNER DOUBLER. STOP DRILLED CRACK AND WELDED PER EA A9-54R-11430. PERFORMED HFEC - [SDR F3LA200600049](https://openairdocs.org/sdr/F3LA200600049), May 9, 2006: BRACKET. WORN. DURING C-4 CHECK, INSPECTION REPORTED NR 1 ENGINE IB FWD COWL BRACE BRACKET WORN INTO THE ENGINE CASE. INSTALLED NEW BRACKETS AND HARDWARE ON NR 1 ENGINE CASE F - [SDR F3LA200600043](https://openairdocs.org/sdr/F3LA200600043), May 8, 2006: HOOK. WORN. DURING C-4 CHECK, INSPECTION REPORTED L2 DOOR GEARBOX ASSY HOOK WORN. REPLACED GEARBOX HOOK PER AMM 52-13-21-400-001, STEP 3C(17)(C) THRU (E). - [SDR F3LA200500043](https://openairdocs.org/sdr/F3LA200500043), Oct 3, 2005: TIRE. FAILED. ON LANDING, BOTH NOSE TIRES BLEW. STOPPED ACFT ON RUNWAY. PERFORMED INSPECTION AFTER TIRE BURST. NO DAMAGE NOTED. REPLACED LT NOSE WHEEL & TIRE ASSEMBLY, P/N 3- - [SDR F3LA200500024](https://openairdocs.org/sdr/F3LA200500024), Jun 1, 2005: BLOWER. SMOKE. AIR TURNBACK, FLIGHT CREW REPORTED AVIONICS SMOKE INDICATION ON DEPARTURE. AIRCRAFT RETURNED TO CUN AND LANDED WITHOUT INCIDENT. PERFORMED OPERATIONAL CHECK OF - [SDR F3LA200100065](https://openairdocs.org/sdr/F3LA200100065), May 16, 2001: B-NUT. LOOSE. DURING TRAINING FLIGHT, FLIGHT CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED IN PHX WITHOUT INCIDENT. AIRCRAFT WAS ## 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 20030331004449I](https://openairdocs.org/incident/20030331004449I), Mar 31, 2003: Airbus A319111 (N901FR), Grand Junction, CO. (-23) The following information was obtained from the inflight incident report submitted by frontier airline flight attendant jennifer davidson: a male… ## Other aircraft with N901FR - [Cancelled 1990-10-16](https://openairdocs.org/deregistered/N901FR-1990-10-16): Dassault/Sud FAN JET FALCON, S/N 270. Exported to United Kingdom --- 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.