# N915FR: 2002 Airbus A319-111, registration cancelled 2009-03-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 6, 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 CFM56-5B5/P series](https://openairdocs.org/engine/cfm-international-cfm56-5b5-p-series) (registry code 13016)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 1851
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 8, 2008
- Certificate issued: November 18, 2008
- Last registry action: November 18, 2008
- Mode S code: ACA9CB
- 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/N915FR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=915FR
- Page: https://openairdocs.org/deregistered/N915FR-2009-03-06

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 (50)

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

- [SDR F3LA200800545](https://openairdocs.org/sdr/F3LA200800545), Aug 7, 2008: FLOOR PANEL. DAMAGED. LINE MECHANIC NOTED THE AFT CARGO PIT TRANSITION PANEL 151AE WAS DAMAGED. MAINT REPAIRED DAMAGED PANEL 151AE IAW SRM 53-02-00, STEP 2, FIGURE 204. UPON COMPLETI
- [SDR F3LA200800343](https://openairdocs.org/sdr/F3LA200800343), Jun 13, 2008: PROXIMITY SWITCH. FAILED. REFERENCE NON ROUTINE C045163. DURING C4 S1 C-CHECK INSPECTION NOTED CHECK DOOR SWITCH POWER SUPPLIED BY EMERGENCY LIGHT SYSTEM FAILS AT PAGE 4 STEP 3, WORK CAR
- [SDR F3LA200800334](https://openairdocs.org/sdr/F3LA200800334), Jun 11, 2008: FRAME. CORRODED. DURING C-CHECK INSP NOTED AFT CARGO FLOOR FRAME 59 HAS CORROSION AT NUTPLATE HOLES. MAINT REPAIRED HOLES WITH REPAIR DOUBLERS IAW EA A9-53R-30346. UPON COMPLETI
- [SDR F3LA200800333](https://openairdocs.org/sdr/F3LA200800333), Jun 11, 2008: SILL. CORRODED. DURING C-CHECK INSP, NOTED UPON CLOSURE OF AFT PIT CORROSION WAS FOUND ON THE SILL WEDGE PANEL 152YG. MAINT INSTALLED A NEW PANEL IAW WORK CARD CP753-25. UPON C
- [SDR F3LA200800332](https://openairdocs.org/sdr/F3LA200800332), Jun 11, 2008: PLATE. CORRODED. DURING C-CHECK INSP, NOTED L1 DOOR GIRT BAR PLATE ON SILL IS CORRODED. MAINT REMOVED OLD GIRT BAR PLATE, FABRICATED NEW PLATE AND INSTALLED NEW GIRT BAR PLATE I
- [SDR F3LA200800326](https://openairdocs.org/sdr/F3LA200800326), Jun 10, 2008: FLOOR PANEL. DAMAGED. REFERENCE NON ROUTINE C44993. DURING C4 S1 C-CHECK INSPECTION NOTED AFT PIT FLOOR PANEL 151VG HAS A 2 INCH SECTION MISSING ON TOP PIECE SHOWING COMPOSITE ALONG 
- [SDR F3LA200800325](https://openairdocs.org/sdr/F3LA200800325), Jun 10, 2008: PROFILE. CORRODED. REFERENCE NON ROUTINE C044887. DURING C4 S1 C CHECK INSPECTION NOTED AFT CARGO COMPARTMENT FLOOR FRAME CAP AT FRAME 59 FROM STRINGER 38 LT TO STRINGER 38 RT IS 
- [SDR F3LA200800324](https://openairdocs.org/sdr/F3LA200800324), Jun 10, 2008: FLOORBEAM. CORRODED. REFERENCE NON ROUTINE C044879. DURING C4 S1 C-CHECK INSPECTION NOTED AFT CARGO COMPARTMENT STANCHION RECEPTABLE AND AREA CORRODED AT FLOOR FRAME 56 AND STRINGER
- [SDR F3LA200800323](https://openairdocs.org/sdr/F3LA200800323), Jun 10, 2008: FLOORBEAM. CORRODED. REFERENCE NON ROUTIN C044731. DURING C4 S1 C-CHECK INSPECTION NOTED CORROSION ON OUTBOARD NUT CLIP HOLE 2 INCHES FORWARD OF FRAME 66 ON FLOORBEAM Y1732 LT. MAIN
- [SDR F3LA200800322](https://openairdocs.org/sdr/F3LA200800322), Jun 10, 2008: PROFILE. CORRODED. REFERENCE NON ROUTINE C044450. DURING C4 S1 C-CHECK INSPECTION NOTED FORWARD CARGO PIT PROFILE FOR LOWER AFT BULKHEAD HAS CORROSION IN NUT PLATE HOLES FROM STRI
- [SDR F3LA200800321](https://openairdocs.org/sdr/F3LA200800321), Jun 10, 2008: FLOOR PANEL. CORRODED. REFERENCE NON ROUTINE C044794. DURING C4 S1 C-CHECK INSPECTION NOTED PANEL 221FF HAS LITE CORROSION ON BOTTOM SIDE. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL
- [SDR F3LA200800320](https://openairdocs.org/sdr/F3LA200800320), Jun 10, 2008: FLOOR PANEL. CORRODED. REFERENCE NON ROUTINE C044797. DURING C4 S1 C-CHECK INSPECTION NOTED PANEL 222FF HAS SEVERE CORROSION ON BOTTOM SIDE. MAINTENANCE REMOVED AND REPLACED FLOOR PAN
- [SDR F3LA200800319](https://openairdocs.org/sdr/F3LA200800319), Jun 10, 2008: FLOOR PANEL. CORRODED. REFERENCE NON ROUTINE C044808. DURING C4 S1 C-CHECK INSPECTION NOTED PANEL 222EF SPLICE PLATE CORRODED. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL SPLICE PLAT
- [SDR F3LA200800318](https://openairdocs.org/sdr/F3LA200800318), Jun 10, 2008: FLOORBEAM. CORRODED. REFERENCE NON ROUTINE C044885. DURING C4 S1 C-CHECK INSPECTION NOTED AFT CARGO COMPARTMENT FLOOR FRAME 59 U-CHANNEL IS CORRODED FROM STRINGER 41 RT TO STRINGER 
- [SDR F3LA200800302](https://openairdocs.org/sdr/F3LA200800302), Jun 9, 2008: SEAT TRACK. CORRODED. REFERENCE NON ROUTINE C044835. DURING C4 S1 C-CHECK INSPECTION NOTED CORROSION ON SEAT TRACK AT Y1292 BETWEEN FRAME 19 AND FRAME 20. MAINTENANCE REMOVED AND REP
- [SDR F3LA200800301](https://openairdocs.org/sdr/F3LA200800301), Jun 9, 2008: PROFILE. CORRODED. DURING C4 S1 C-CHECK INSP, NOTED AFT CARGO COMPARTMENT LT FLOOR PROFILE IS CORRODED FROM FRAME 51 TO FRAME 56 AT STRINGER 38 LT. MAINT REMOVED AND REPLACED LT H
- [SDR F3LA200800300](https://openairdocs.org/sdr/F3LA200800300), Jun 9, 2008: FLOORBEAM. CORRODED. DURING C-CHECK INSP, NOTED CORROSION ON FLOOR TRACK AT Y189 FRAME 20. MAINT REMOVED DAMAGED FLOORBEAM Y189 AND INSTALLED NEW FLOORBEAM FROM FRAME 20 TO FRAME 24
- [SDR F3LA200800317](https://openairdocs.org/sdr/F3LA200800317), Jun 8, 2008: PANEL. PUNCTURED. REFERENCE NON ROUTINE C044396. DURING C4 S1 C CHECK INSPECTION NOTED AFT PIT TRANSITION PANEL 151AE HAS PUNCTURE DAMAGE. MAINTENANCE REMOVED DAMAGE, CLEANED PAN
- [SDR F3LA200800294](https://openairdocs.org/sdr/F3LA200800294), Jun 8, 2008: FLOORBEAM. CORRODED. DURING C-CHECK INSP NOTED THE CENTER LONGITUDINAL FLOORBEAM FROM FRAME 58 TO FRAME 59 HAS CORROSION AROUND THE FWD NUTPLATE HOLE. MAINT REPAIRED THE FLOORBEAM I
- [SDR F3LA200800299](https://openairdocs.org/sdr/F3LA200800299), Jun 7, 2008: FLOOR PANEL. CORRODED. DURING C-CHECK INSP, NOTED AFT PIT FLOOR PANEL 151PE HAS SURFACE CORROSION AROUND ATTACHMENT HOLES AND EDGES. MAINT CLEANED CORROSION, FILLED COUNTER SINK AREA,
- [SDR F3LA200800297](https://openairdocs.org/sdr/F3LA200800297), Jun 6, 2008: FLOOR PANEL. PUNCTURED. DURING C-CHECK INSP NOTED FLOOR PANEL 231XG HAS TWO SMALL PUNCTURE HOLES ON SURFACE. MAINT REPAIRED PUNCTURE DAMAGE TO FLOOR PANEL 231XG IAW SRM 53-02-00 STEP 8
- [SDR F3LA200800296](https://openairdocs.org/sdr/F3LA200800296), Jun 6, 2008: FLOOR PANEL. DELAMINATED. REFERENCE NON ROUTINE C045066. DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 221BF HAS DELAMINATION AROUND SCREW HOLES. MAINTENANCE REMOVED DELAMINATED AREA
- [SDR F3LA200800298](https://openairdocs.org/sdr/F3LA200800298), Jun 5, 2008: FITTING. CORRODED. DURING C-CHECK INSP, NOTED L2 DOOR AFT TOP SLIDE ATTACH POINT BRACKET CORRODED. MAINT REMOVED CORRODED FITTING AND INSTALLED SERVICEABLE FITTING IAW SRM 51-42-1
- [SDR F3LA200800295](https://openairdocs.org/sdr/F3LA200800295), Jun 5, 2008: FLOOR PANEL. DAMAGED. DURING C-CHECK INSP NOTED FLOOR PANEL 251JG HAS DAMAGE IN TWO PLACES ON UPPER SURFACE. MAINT REMOVED DAMAGE AND APPLIED MOISTURE BARRIER IAW SRM 53-02-00 AND SR
- [SDR F3LA200800293](https://openairdocs.org/sdr/F3LA200800293), Jun 4, 2008: FLOORBEAM. CORRODED. DURING C-CHECK INSP NOTED CORROSION ON BEAM Y1292 LT UPPER OB SIDE NUTCLIP HOLE AT FRAME 68. MAINT REMOVED CORRODED FLOORBEAM Y1292 AND INSTALLED NEW FLOORBEAM 
- [SDR F3LA200800285](https://openairdocs.org/sdr/F3LA200800285), Jun 3, 2008: PANEL. DENTED. DURING C-CHECK INSP, NOTED AFT PIT TRANSITION PANEL 161BF HAS A DENTS. MAINT REMOVED DAMAGE AND CLEANED PANEL, FILLED DENTS ON PANEL 161BF IAW SRM 51-73-00 STEP
- [SDR F3LA200800292](https://openairdocs.org/sdr/F3LA200800292), Jun 2, 2008: PANEL. DAMAGED. DURING C4 S1 C-CHECK INSPECTION NOTED AFT PIT TRANSITION PANEL 162BF HAS DENTS. MAINT REMOVED DAMAGE AND CLEANED PANEL FILLED DENTS ON PANEL 162BF IAW SRM 53-02
- [SDR F3LA200800291](https://openairdocs.org/sdr/F3LA200800291), Jun 2, 2008: PANEL. DAMAGED. DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 162CF HAS DENTS AND GOUGES. REMOVED DAMAGE AND CLEANED PANEL FILLED DENTS AND REPAIRED PUNCTURE DAMAGE IAW SR
- [SDR F3LA2008290](https://openairdocs.org/sdr/F3LA2008290), Jun 2, 2008: PANEL. DAMAGED. DURING C-CHECK INSP, NOTED FWD PIT TRANSITION PANEL 131BF HAS GOUGE IN CORE. MAINT REMOVED DAMAGE AND CLEANED PANEL REPAIRED PUNCTURED DAMAGE PANEL 131BF IAW SR
- [SDR F3LA200800289](https://openairdocs.org/sdr/F3LA200800289), Jun 2, 2008: PANEL. DENTED. DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151HE HAS DENTS. MAINT REMOVED DAMAGE AND CLEANED PANEL FILLED DENTS ON PANEL 151HE IAW SRM 53-73-00 STEP 3C.
- [SDR F3LA200800288](https://openairdocs.org/sdr/F3LA200800288), Jun 2, 2008: FLOORBEAM. CORRODED. DURING C-CHECK INSP, NOTED FLOORBEAM 1292 RT AT FRAME 68 CORROSION IN OB NUTCLIP HOLE. MAINT INSTALLED NEW FLOORBEAM Y1292 FROM FRAME 68 TO FRAME 69 IAW THE REQ
- [SDR F3LA200800287](https://openairdocs.org/sdr/F3LA200800287), Jun 2, 2008: PANEL. DENTED. DURING C-CHECK INSP, NOTED AFT PIT TRANSITION PANEL 151FE HAS DENTS. MAINT REMOVED DAMAGE AND CLEANED PANEL, FILLED DENTS, PANEL 151FE IAW SRM 51-73-00 STEP 3C.
- [SDR F3LA200800286](https://openairdocs.org/sdr/F3LA200800286), Jun 2, 2008: BEAM. CORRODED. REFERENCE NON ROUTINE C044730. DURING C4 S1 C-CHECK INSPECTION NOTED CORROSION ON UPPER SURFACE OF Y1292 RT BEAM 7 INCHES FORWARD OF FRAME 68. MAINTENANCE REMOV
- [SDR F3LA200800284](https://openairdocs.org/sdr/F3LA200800284), Jun 2, 2008: PANEL. DELAMINATED. DURING C4 S1 C-CHECK INSP NOTED FWD PIT TRANSITION PANEL 32DG HAD A CORNER DELAMINATED. MAINT CLEANED DAMAGED AREA AND REPAIRED DAMAGE IAW SRM 53-02-00 PAGE 209
- [SDR F3LA200800283](https://openairdocs.org/sdr/F3LA200800283), Jun 2, 2008: FLOORBEAM. CORRODED. DURING C-CHECK INSP, NOTED FLOORBEAM Y765 RT HAS PITTING CORROSION AT FRAME 68 ON TOP SURFACE. MAINT REMOVED BEAM AND INSTALLED NEW BEAM IAW DRAWING D53472815 A
- [SDR F3LA200800282](https://openairdocs.org/sdr/F3LA200800282), Jun 1, 2008: SUPPORT. CORRODED. DURING C-CHECK INSP, NOTED THE SUPPORT FRAME FOR SHEAR PLATE CORRODED ON BOTTOM SURFACE AT NUTCLIP HOLES LOCATED AT THE LT OB SIDE AT FRAME 70. MAINT REMOVED CO
- [SDR F3LA200800281](https://openairdocs.org/sdr/F3LA200800281), May 31, 2008: FRAME. CORRODED. DURING C4 S1 C-CHECK INSPECTION NOTED SUPPORT FRAME FOR SHEAR PLATE CORRODED ON BOTTOM SURFACE AT NUT CLIP HOLE. MAINTENANCE REMOVED OLD SUPPORT FRAME AND INSTA
- [SDR F3LA200700219](https://openairdocs.org/sdr/F3LA200700219), Sep 7, 2007: WARNING LIGHT. FALSE ACTIVATION. AIR TURN BACK AT 1244, FLIGHT CREW REPORTED VENT EXTRACT FAULT. AIRCRAFT RETURNED TO KMDW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND PERFOR
- [SDR F3LA200700011](https://openairdocs.org/sdr/F3LA200700011), Jan 31, 2007: CYLINDER DAMPER. FAILED. WHILE PERFORMING OPS TEST OF SLIDE DEPLOYMENT PER TC 25830-1, L1 DOOR ASSIST BOTTLE DID NOT FULLY OPEN DOOR TO DEPLOY SLIDE. REPLACED L1 DOOR CYLINDER DAMPER AS
- [SDR F3LA200600156](https://openairdocs.org/sdr/F3LA200600156), Nov 5, 2006: LONGERON. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION AT LONGERON Y1292, 14 FT AFT OF FR67. REMOVED CORROSION FROM AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14
- [SDR F3LA200600155](https://openairdocs.org/sdr/F3LA200600155), Nov 5, 2006: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED 2ND FLOORBEAM IB OF R2 DOOR HAD MULTIPLE AREAS OF CORROSION AROUND NUTPLATE HOLES. REMOVED CORROSION AND FOUND 3 AREAS TO 
- [SDR F3LA200600154](https://openairdocs.org/sdr/F3LA200600154), Nov 5, 2006: THRESHOLD. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON BOTTOM OF L2 DOOR THRESHOLD PLATE. REPLACED L2 DOOR THRESHOLD PLATE IAW TASK CARD C252001-22.
- [SDR F3LA200600153](https://openairdocs.org/sdr/F3LA200600153), Nov 5, 2006: FLOOR PANEL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF CORRODED. REPLACED FLOOR PANEL 262FF PER AMM 53-42-12-400-002.
- [SDR F3LA200600152](https://openairdocs.org/sdr/F3LA200600152), Nov 5, 2006: FLOOR PANEL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 261FF CORRODED. REPLACED FLOOR PANEL 261FF PER AMM 53-42-12-400-002.
- [SDR F3LA200600151](https://openairdocs.org/sdr/F3LA200600151), Nov 5, 2006: BOTTLE. BROKEN. DURING C-3 CHECK, INSPECTION REPORTED RT. OVERWING RESERVOIR INFLATION CABLE IN AFT PIT HAD TIP BROKEN OFF THAT HOOKS TO THE FLEX RELEASE CABLE. REPLACED OVERWI
- [SDR F3LA200600150](https://openairdocs.org/sdr/F3LA200600150), Nov 5, 2006: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM IB OF L2 DOOR HAD MULTIPLE AREAS OF CORROSION LOCATED AROUND NUTPLATE HOLES. REMOVED CORROSION AND DETERMINED TO
- [SDR F3LA200500036](https://openairdocs.org/sdr/F3LA200500036), Jul 25, 2005: WARNING LIGHT. ILLUMINATED. UPON APPROACH, FLIGHT CREW REPORTED F/CTL FLAPS FAULT WHEN SELECTING FLAPS TWO. FLAPS STAYED AT ZERO. DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. P
- [SDR F3LA200500030](https://openairdocs.org/sdr/F3LA200500030), Jul 5, 2005: FLAP SYSTEM. MALFUNCTIONED. DURING ARRIVAL IN ANC, FLIGHT CREW REPORTED FLT CONTROL FLAPS FAULT ON ECAM. SLATS TRAVELED TO THE 2 POSITION, FLAPS DID NOT MOVE FROM THE ZERO POSITION. AIRCRA
- [SDR F3LA200500020](https://openairdocs.org/sdr/F3LA200500020), May 18, 2005: COMPUTER. INOPERATIVE. FLIGHT CREW REPORTED ELAC 2 FAULT. ON SHORT FINAL LOST BOTH AILERONS WENT TO DIRECT LAW. REPLACED NR 2 ELAC. OPERATIONAL CHECK GOOD PER MM 27-93-34, PAGE 401. P
- [SDR F3LA200300120](https://openairdocs.org/sdr/F3LA200300120), Jun 15, 2003: SWITCH. FAULTY. ABORTED TAKEOFF DUE TO REFUELING PANEL INDICATION. PERFORMED BRAKE INSPECTION IAW AMM 05-51-16-06. NO DEFECTS NOTED. REPLACED REFUELING PANEL DOOR SWITCH 20QJ I

## 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 OPS07IA001](https://openairdocs.org/ntsb/OPS07IA001), Jan 5, 2007: Airbus Industrie A-319 (N915FR), Denver, CO, incident, no damage. Probable cause: The probable cause of the incident was the Key Lime Air flight 4216 pilot's inadvertant entry onto the active runway. A contributing factor to the incident was the failure of the Denver tower ground…

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