# N928FR: 2004 Airbus A319-111, registration cancelled 2017-05-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 22, 2017
- 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: 2236
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 7, 2004
- Certificate issued: November 16, 2010
- Last registry action: June 16, 2016
- Mode S code: ACDC6F
- 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/N928FR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=928FR
- Page: https://openairdocs.org/deregistered/N928FR-2017-05-22

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 (60, newest 50)

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

- [SDR F3LA2016040800032](https://openairdocs.org/sdr/F3LA2016040800032), Apr 8, 2016: FLOORBEAM. CORRODED. DURING C CHECK, NOTED CORROSION AT FRAME 66 & FLOORBEAM Y1292. R & R FLOORBEAM IAW SRM 51-42-11.
- [SDR F3LA2016040800031](https://openairdocs.org/sdr/F3LA2016040800031), Apr 8, 2016: PLATE. CORRODED. DURING C CHECK, NOTED CORROSION AT FRAME 66 & Y1732. PERFORMED REPAIR IAW SRM 53-41-14.
- [SDR F3LA2016040800030](https://openairdocs.org/sdr/F3LA2016040800030), Apr 8, 2016: DOOR SILL. CORRODED. DURING C CHECK, NOTED CORROSION ON NUTPLATE HOLE ON L2 AFT GIRT BAR FITTING. R & R L2 DOOR SILL IAW SRM 51-72-11.
- [SDR F3LA2016040800029](https://openairdocs.org/sdr/F3LA2016040800029), Apr 8, 2016: FITTING. CORRODED. DURING C CHECK, NOTED R1 DOOR AFT GIRT BAR FITTING HAS CORROSION. REPAIRED R1 DOOR GIRT BAR FITTING IAW SRM 51-73-00, SRM 51-74-00, NTM 51-10-08 & SRM 51-21-11.
- [SDR F3LA2016040800028](https://openairdocs.org/sdr/F3LA2016040800028), Apr 4, 2016: FLOORBEAM. CORRODED. DURING C CHECK, NOTED CORROSION, BETWEEN FRAME 64 & 67, Y254. R & R FLOORBEAM IAW SRM 51-42-11 & SRM 51-72-1.
- [SDR F3LA2016040800027](https://openairdocs.org/sdr/F3LA2016040800027), Apr 4, 2016: SHEAR PLATE. CORRODED. DURING C CHECK, NOTED RT SHEAR PLATE, BETWEEN STRINGER 23 & 24, AT FRAME 68 - 70 HAS CORROSION. R & R SHEAR WEB & WEB SUPPORT IAW SRM 51-42-11.
- [SDR F3LA2016040800026](https://openairdocs.org/sdr/F3LA2016040800026), Apr 4, 2016: FITTING. CORRODED. DURING C CHECK, NOTED R1 DOOR AFT GIRT BAR FITTING HAS CORROSION. REPAIRED R1 DOOR AFT GIRT BAR FITTING IAW SRM 51-73-00, 51-74-00, 53-11-11, NTM 51-10-08 & SRM
- [SDR F3LA2016040800025](https://openairdocs.org/sdr/F3LA2016040800025), Apr 4, 2016: SHEAR PLATE. CORRODED. DURING C CHECK, NOTED LT AFT SHEAR PLATE, BETWEEN STRINGER 23 & 24 AT FRAME 68 & 70 HAS CORROSION. R & R LT AFT SHEAR PLATE IAW SRM 51-42-11 & SRM 51-44-11.
- [SDR F3LA2016040800024](https://openairdocs.org/sdr/F3LA2016040800024), Mar 31, 2016: FLOORBEAM. CORRODED. DURING C CHECK, NOTED CORROSION AT FRAME 66 & Y1292. R & R THE FLOORBEAM AT FRAME 66 & Y1292 IAW SRM 51-42-11.
- [SDR F3LA2016040800023](https://openairdocs.org/sdr/F3LA2016040800023), Mar 23, 2016: SPLICE. DAMAGED. DURING C CHECK, NOTED THE RT EMER EXIT LOWER FWD EXIT LIGHT INOPERATIVE. REPAIRED THE SPLICE IAW ESPM 20-43-13. OPERATIONAL CHECKED GOOD.
- [SDR F3LA2014091501072](https://openairdocs.org/sdr/F3LA2014091501072), Sep 14, 2014: POWER SUPPLY. FAILED. FORWARD LT EPSU FAILS EMER LIGHTS TEST. R & R FWD LT EPSU 10WL. OPERATIONAL CHECKED NORMAL IAW AMM 33-51-38 PAGE BLOCK 401.
- [SDR F3LA2014081201050](https://openairdocs.org/sdr/F3LA2014081201050), Aug 8, 2014: VALVE. CLOSED. IN CRUISE AT 31000 FT UNABLE TO MAINTAIN CABIN PRESS. CABIN ALTITUDE ROSE TO 10,200. R & R NR 2 ENG PRV IAW AMM 36-11-52-PB 401. OPERATIONS & LEAK CHECKED VLV &
- [SDR F3LA2014061601042](https://openairdocs.org/sdr/F3LA2014061601042), Jun 12, 2014: POWER SUPPLY. INOPERATIVE. L1 DOOR EMER POWER SUPPLY UNIT INOPERATIVE 10WL. R & R L1 DOOR EMER POWER SUPPLY UNIT. OPERATIONS CHECKED GOOD IAW AMM 33-51-38 PB 401.
- [SDR F3LA2013052200859](https://openairdocs.org/sdr/F3LA2013052200859), May 8, 2013: FLOORBEAM. CORRODED. DURING C6 CHECK. AFT GALLEY FLOORBEAM AT FRAME 69 HAS LIGHT CORROSION AROUND FASTENER HOLE. CLEANED UP HOLE TO .354' IAW SRM 53-41-14, FIGURE 101, SRM 51-21-11 
- [SDR F3LA2013052200858](https://openairdocs.org/sdr/F3LA2013052200858), May 8, 2013: FLOORBEAM. CORRODED. DURING C6 CHECK. AFT GALLEY FLOORBEAM AT FRAME 66 APPROX Y1292 HAS LIGHT CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5 AND 6.B. ACFT SCHEDULED TO GO BACK 
- [SDR F3LA2013052200857](https://openairdocs.org/sdr/F3LA2013052200857), May 8, 2013: FLOORBEAM. CORRODED. ACFT WAS OUT OF SERVICE DUE TO C6 MX CHECK. AFT GALLEY FLOORBEAM AT FRAME 66, Y765 HAS LIGHT CORROSION AROUND FASTENER HOLE. R & R FLOORBEAM IAW SRM 51-42-11. P
- [SDR F3LA2013050800850](https://openairdocs.org/sdr/F3LA2013050800850), May 6, 2013: BATTERY. DISCHARGED. EPSU, MIDDLE RIGHT, BATTERY FAILED TEST ON HEAVY SERVICE CHECK. R & R BATTERY ASSY MIDDLE RIGHT EPSU. OPS CHECK GOOD. REF AMM 33-51-38 PAGE BLOCK 401.
- [SDR F3LA2011091300670](https://openairdocs.org/sdr/F3LA2011091300670), Sep 11, 2011: LAMP. BURNED OUT. OVERWING EMERGENCY LIGHT 60WL HAD AFT BULB INOPERATIVE. RELAMPED EMERGENCY LIGHT 60WL IAW AMM 33-51-15 PB 401. OPS CHECKED GOOD.
- [SDR F3LA2011021000599](https://openairdocs.org/sdr/F3LA2011021000599), Jan 31, 2011: PUMP. FAILED. YELLOW HYD FLUID & SYSTEM LOST ON APPROACH. R & R RT ENGINE HYD PUMP IAW AMM 29-13-51- PB 407. LEAK & OPS CHECKS OK.
- [SDR F3LA2010063000445](https://openairdocs.org/sdr/F3LA2010063000445), Jun 27, 2010: ENTERTAIN SYS. SMOKE. REFERENCE LOG PAGE 529827 ITEM 1 AND LOG PAGE 529836 ITEM 1. SEAT 13A TV SMELLS HOT AND WAS SMOKING. INSPECTED ROW 13 ABC FOR SMOKE AND INSPECTED EPSU'S. NO DEF
- [SDR F3LA2010060400435](https://openairdocs.org/sdr/F3LA2010060400435), Jun 3, 2010: COMPUTER. MALFUNCTIONED. PILOT REPORT REF LOG PAGE 524666 ITEMS 1 AND 2. SMOKE WARNING ACTUATED UPON LANDING. NO SMOKE NOTICED IN COCKPIT. BOTH BLOWER AND EXTRACT FAULTED AT SAME TIME O
- [SDR F3LA2010032800376](https://openairdocs.org/sdr/F3LA2010032800376), Mar 22, 2010: EPSU. INOPERATIVE. DURING C4 S1 CHECK, INSP NOTED EMERGENCY LIGHTS ON SEATS 6C, 12C, AND 13C INOPERATIVE. MX TROUBLESHOT SYS IAW TSM 33-51-00-810-813, DISCONNECTED EACH EPSU, CLEA
- [SDR F3LA2010032700373](https://openairdocs.org/sdr/F3LA2010032700373), Mar 18, 2010: FLOOR PANEL. DELAMINATED. DURING C4 S1 CHECK INSP NOTED AFT CARGO PIT FLOOR PANEL 152UG DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW MCGILL 9701 REV. G
- [SDR F3LA2010032800375](https://openairdocs.org/sdr/F3LA2010032800375), Mar 16, 2010: COVER. CORRODED. DURING C4 S1 CHECK, INSP NOTED AFT CARGO COMPARTMENT DOOR CUTOUT THRESHOLD AREA COVER SHEET CORRODED. MX R & R AFT CARGO COMPARTMENT DOOR CUTOUT THRESHOLD AREA 
- [SDR F3LA2010032700374](https://openairdocs.org/sdr/F3LA2010032700374), Mar 15, 2010: SHEAR WEB. CRACKED. REFERENCE NON ROUTINE N0014 AFT CABIN SHEAR WEB AT FRAME 69 AT AFT END OF BEAM =Y1292 HAS A CRACK. R & R SHEAR WEB IAW EO A0-53EO-31434 AND SRM 51-72-11.
- [SDR F3LA2010032700372](https://openairdocs.org/sdr/F3LA2010032700372), Mar 15, 2010: SHEAR WEB. CRACKED. DURING C4 S1 CHECK INSP NOTED SHEAR WEB AT FRAME 69 AT AFT END OF BEAM -Y1292 HAS A FIFTEEN INCH CRACK. R & R SHEAR WEB IAW EO A0-53-31934 AND A319 SRM 51-72-11
- [SDR F3LA2010032700371](https://openairdocs.org/sdr/F3LA2010032700371), Mar 15, 2010: FLOORBEAM. CORRODED. DURING C4 S1 INSP NOTED FLOORBEAM -Y765 BETWEEN FRAME 67 AND FRAME 68 HAD CORROSION ON UPPER SURFACE. REPAIRED FLOORBEAM IAW SRM 53-00-14 PARAGRAPH 4 D FIGURE 2
- [SDR F3LA2010032700370](https://openairdocs.org/sdr/F3LA2010032700370), Mar 15, 2010: FLOORBOARD. DELAMINATED. DURING C4 S1 CHECK INSP, NOTED AFT CARGO FLOOR PANEL 151TG PUNCTURED AND DELAMAINATED BEYOND ECONOMICAL LIMITS. MX R & R IAW AMM 53-12-14-400-001.
- [SDR F3LA2009010500001](https://openairdocs.org/sdr/F3LA2009010500001), Jan 1, 2009: COVER. DEFECTIVE. PILOT MADE AN AIR TURNBACK DUE TO AN AFT CARGO DOOR MESSAGE ON THE ELECTRONIC CENTRALIZED ACFT MONITORING SYS. MX REMOVED AND REPLACED THE COVER ASSY AND PERFOR
- [SDR F3LA200800588](https://openairdocs.org/sdr/F3LA200800588), Aug 26, 2008: FLOOR PANEL. CORRODED. REFERENCE NON ROUTINE CO50125. DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 261PF HAS A CORRODED INSERT ON THE LT HAND SIDE AND DELAMINATION IN THE SAME AREA
- [SDR F3LA200800584](https://openairdocs.org/sdr/F3LA200800584), Aug 23, 2008: FLOORBEAM. CORRODED. REFERENCE NON ROUTINE CO50117. DURING C3 C-CHECK, INSP NOTED LT FLOORBEAM Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES FROM FRAME 66 TO FRAME 68 (L2 DOOR AREA)
- [SDR F3LA200800585](https://openairdocs.org/sdr/F3LA200800585), Aug 23, 2008: FLOOR SUPPORT. CORRODED. REFERENCE NON ROUTINE CO50117. DURING C3 C-CHECK, INSP NOTED LT FLOOR SUPPORT Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES FROM FRAME 66 TO FRAME 68 (L2 DOOR A
- [SDR F3LA200800580](https://openairdocs.org/sdr/F3LA200800580), Aug 22, 2008: FLOOR PANEL. DAMAGED. REFERENCE NON ROUTINE C049995. DURING C3 C-CHECK INSPECTION NOTED THE FORWARD OUTBOARD CORNER WAS DAMAGED ON FLOOR PANEL 242LF. MX REPAIRED DAMAGE TO PANEL 242L
- [SDR F3LA200800583](https://openairdocs.org/sdr/F3LA200800583), Aug 22, 2008: FLOORBEAM. CORRODED. REFERENCE NON ROUTINE CO50040. DURING C3 C-CHECK, INSP NOTED FLOOR BEAM Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES FROM RT HAND FRAME 67 TO FRAME 68. MAINTEN
- [SDR F3LA200800582](https://openairdocs.org/sdr/F3LA200800582), Aug 22, 2008: FLOORBEAM. CORRODED. REFERENCE NON ROUTINE CO50039. DURING C3 C-CHECK, INSP NOTED FLOOR BEAM Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES FROM RT HAND FRAME 66 TO FRAME 67. SUPPLEM
- [SDR F3L2008F00004](https://openairdocs.org/sdr/F3L2008F00004), Aug 22, 2008: FLOORBEAM. CORRODED. REFERENCE NON ROUTINE C050039. DURING C3 C-CHECK, INSP NOTED FLOOR BEAM Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES FROM RT HAND FRAME 66 TO FRAME 67. SUPPLEM
- [SDR F3L2008F00003](https://openairdocs.org/sdr/F3L2008F00003), Aug 22, 2008: SHEAR PLATE. CORRODED. REFERENCE NON ROUTINE C050055. DURING C3 C-CHECK, INSP NOTED INDICATIONS OF CORROSION ON TOP OF RIGHT AFT SHEAR PLATE BETWEEN FRAME 68 AND FRAME 70. MAINTENANCE
- [SDR F3LA200800586](https://openairdocs.org/sdr/F3LA200800586), Aug 21, 2008: SILL. CORRODED. REFERENCE NON ROUTINE CO50131. DURING C3 C-CHECK, INSPECTION NOTED NUT PLATE HOLE ON R-2 DOOR SILL, AFT AND OUTBOARD OF R-2 AFT GIRT BAR ATTACH FITTING WAS CORR
- [SDR F3L2008F00002](https://openairdocs.org/sdr/F3L2008F00002), Aug 21, 2008: SEAL. CORRODED. REFERENCE NON ROUTINE C050131. DURING C3 C-CHECK, INSPECTION NOTED NUT PLATE HOLE ON R-2 DOOR SEAL, AFT AND OUTBOARD OF R-2 AFT GIRT BAR ATTACH FITTING WAS CORR
- [SDR F3LA200800579](https://openairdocs.org/sdr/F3LA200800579), Aug 21, 2008: SHEAR PLATE. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED THE LT LATERAL SHEAR PLATE HAS LIGHT CORROSION AT CLIP NUT HOLES BETWEEN FR 68 AND FR 70. MAINTENANCE REMOVED AND REPLACED S
- [SDR F3LA200800578](https://openairdocs.org/sdr/F3LA200800578), Aug 20, 2008: FLOOR PANEL. PUNCTURED. DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD PIT PANEL 132EG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURED DAMAGE TO FLOOR PANEL IN ACCORDANCE WITH A319 SRM 53
- [SDR F3LA200800577](https://openairdocs.org/sdr/F3LA200800577), Aug 20, 2008: BLANKING PLATE. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED R1 FORWARD GIRT BAR BLANKING PLATE HAS CORROSION AT HOLES. MAINTENANCE FABRICATED NEW NUT PLATE ASSEMBLY FOR GIRT BAR BLANKI
- [SDR F3LA200800576](https://openairdocs.org/sdr/F3LA200800576), Aug 19, 2008: FLOOR PANEL. PUNCTURED. DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 161BF WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 161BF IAW THE REQUIREMENTS OF A319 SRM 53-02-
- [SDR F3LA200800575](https://openairdocs.org/sdr/F3LA200800575), Aug 19, 2008: FLOOR PANEL. PUNCTURED. DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 162CF WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 162CF IAW THE REQUIREMENTS OF A319 SRM 53-02-
- [SDR F3LA200800574](https://openairdocs.org/sdr/F3LA200800574), Aug 19, 2008: FLOOR PANEL. PUNCTURED. DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 151BE WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 151BE IAW THE REQUIREMENTS OF A319 SRM 53-02-
- [SDR F3LA200800573](https://openairdocs.org/sdr/F3LA200800573), Aug 19, 2008: FLOOR PANEL. PUNCTURED. DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 151UG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO TRANSITION PANEL 151UG IAW THE REQUIREMENTS OF A319
- [SDR F3LA200800572](https://openairdocs.org/sdr/F3LA200800572), Aug 19, 2008: FLOOR PANEL. PUNCTURED. DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 152WG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO TRANSITION PANEL 152WG IAW THE REQUIREMENTS OF A319
- [SDR F3LA200800571](https://openairdocs.org/sdr/F3LA200800571), Aug 19, 2008: FLOOR PANEL. PUNCTURED. DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 152XG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO TRANSITION PANEL 152XG IAW THE REQUIREMENTS OF A319
- [SDR F3LA200800570](https://openairdocs.org/sdr/F3LA200800570), Aug 19, 2008: FLOOR PANEL. PUNCTURED. DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 152TG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO TRANSITION PANEL 152TG IAW THE REQUIREMENTS OF A319
- [SDR F3LA200800569](https://openairdocs.org/sdr/F3LA200800569), Aug 19, 2008: FLOOR PANEL. PUNCTURED. DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 152UG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 152UG IAW THE REQUIREMENTS OF A319 SRM 53-02-

All 60: https://openairdocs.org/deregistered/N928FR-2017-05-22/reports.md

## 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 20150322003279I](https://openairdocs.org/incident/20150322003279I), Mar 22, 2015: Airbus A319-111 (N928FR), New Castle, DE, Minor damage. On Sunday March 22, 2015 at approximately 21:20 local time, aircraft registered as N928RF operated by frontier airlines, inc. as a 14 CFR part 121 scheduled…

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