# N929FR: 2004 Airbus A319-111, registration cancelled 2015-11-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 16, 2015
- Exported to: Ireland
- 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: 2240
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 7, 2004
- Certificate issued: June 4, 2004
- Last registry action: December 31, 2014
- Mode S code: ACE026
- Owner when cancelled: [Afs Investments 54 LLC](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%2054%20LLC)
- Location: [Norwalk, CT](https://openairdocs.org/faa-place/CT/Norwalk)
- Owner type: Corporation
- Owner's area on the map: 41.1382° N, 73.4016° W: Placed by OpenAirDocs at the center of ZIP code 06851, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N929FR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=929FR
- Page: https://openairdocs.org/deregistered/N929FR-2015-11-16

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 (58, newest 50)

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

- [SDR F3LA2014111001084](https://openairdocs.org/sdr/F3LA2014111001084), Nov 7, 2014: SLIDE. DEFECTIVE. AIRCRAFT DUE C 7 CHECK. DURING SCHEDULED OPERATIONAL CHECK OF R 2 DOOR SLIDE, LIGHTS DID NOT ILLUMINATE WHEN SLIDE DEPLOYED. R & R R2 DOOR SLIDE WITH SERVICEABL
- [SDR F3LA2014090801063](https://openairdocs.org/sdr/F3LA2014090801063), Sep 7, 2014: BOTTLE. DISCHARGED. LOUD NOISE & RUSH OF AIR IN AFT GALLEY AREA RT SIDE OVERHEAD. BLOCK RETURN. FOUND PORTABLE OXYGEN BOTTLE IN AFT CABIN POSITION TO HAVE SUDDENLY DEPRESSURIZED TO
- [SDR F3LA2013050700849](https://openairdocs.org/sdr/F3LA2013050700849), Apr 23, 2013: LEVER. STUCK. RIGHT EMERGENCY EXIT SLIDE RELEASE LEVER ON DOOR WILL NOT RETURN TO NORMAL POSITION. INSTALLED RELEASE CABLE TEST TOOL AND PERFORMED TEST NUMEROUS TIMES. CABLE 
- [SDR F3LA2012121300818](https://openairdocs.org/sdr/F3LA2012121300818), Dec 13, 2012: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT EPSU BATTERY 10WL FAILED TEST, HEAVY SERVICE. R & R BATTERY FOR 10WL EPSU. OPS CHECK OK, REF AMM 33-51 -38-000-002A AND 33-51-38-400-002A.
- [SDR F3LA2010050600419](https://openairdocs.org/sdr/F3LA2010050600419), May 4, 2010: EPSU. FAILED. REFERENCE C-CHECK NON ROUTINE N0768. MULTIPLE EMERGENCY LIGHTS FOR SEAT ROWS INOPERATIVE. R & R EMERGENCY LIGHT HARNESS AT SEAT ROW 18 ABC IAW ESPM 20-33-11. R 
- [SDR F3LA2010043100406](https://openairdocs.org/sdr/F3LA2010043100406), Apr 24, 2010: FLOOR PANEL. DENTED. REF HEAVY MX NON ROUTINE N0689. AFT CARGO PIT PANEL 151UG HAS NUMEROUS DENTS. OFF ACFT PART. FABRICATED PANEL 151UG IAW IRM 9701 REV G.
- [SDR F3LA2010043100405](https://openairdocs.org/sdr/F3LA2010043100405), Apr 24, 2010: TRANSITION PANEL. DENTED. HEAVY MX NON-ROUTINE N0688. AFT CARGO PIT TRANSITION PANEL 152UG HAS NUMEROUS DENTS THROUGHOUT ENTIRE PANEL . OFF ACFT PART. FABRICATED PANEL IAW IRM 9701 REV G
- [SDR F3LA2010043100404](https://openairdocs.org/sdr/F3LA2010043100404), Apr 24, 2010: TRANSITION PANEL. PUNCTURED. REF C-CHECK NON ROUTINE N0686. AFT CARGO COMPARTMENT TRANSITION PANEL 161BF HAS (2) PUNCTURES. OFF ACFT PART. FABRICATED REPLACEMENT TRANSITION PANEL 161BF IAW 
- [SDR F3LA2010043100403](https://openairdocs.org/sdr/F3LA2010043100403), Apr 24, 2010: FLOOR PANEL. DELAMINATED. REF HEAVY MX NON-ROUTINE N0687. AFT CARGO PIT PANEL 152TG HAS SEVERAL AREAS OF EDGE DELAMINATION AND SEVERAL SMALL DENTS. OFF ACFT PART. FABRICATED PANEL 152TG 
- [SDR F3LA2010043100402](https://openairdocs.org/sdr/F3LA2010043100402), Apr 24, 2010: TRANSITION PANEL. DENTED. REF C-CHECK NON ROUTINE N0682. AFT CARGO COMPARTMENT TRANSITION PANEL 151BE HAS (2) PUNCTURES AND NUMEROUS DENTS THROUGHOUT ENTIRE PANEL. OFF ACFT PART. FABRICA
- [SDR F3LA2010043100401](https://openairdocs.org/sdr/F3LA2010043100401), Apr 24, 2010: TRANSITION PANEL. DELAMINATED. REF HEAVY MX NON-ROUTINE N0678. AFT CARGO TRANSITION PANEL 151FE HAS DELAMINATION AROUND EDGE. OFF ACFT PART. FABRICATED PANEL IAW IRM 9701 REV G.
- [SDR F3LA2010043100400](https://openairdocs.org/sdr/F3LA2010043100400), Apr 24, 2010: TRANSITION PANEL. DENTED. REFERENCE C-CHECK NON ROUTINE N0685 AFT CARGO COMPARTMENT TRANSITION PANEL 161CF HAS NUMEROUS DENTS AND BULGES THROUGHOUT PANEL. R & R PANEL 161CF IAW MCG IRM 9
- [SDR F3LA2010043100399](https://openairdocs.org/sdr/F3LA2010043100399), Apr 24, 2010: FLOOR PANEL. DELAMINATED. REFERENCE HEAVY MX NON-ROUTINE N00680. AFT CARGO PIT PANEL 162BF HAS AREAS OF DELAMINATION AROUND EDGE OF PANEL. FABRICATED PANEL IAW IRM 9701 REV G.
- [SDR F3LA2010043100398](https://openairdocs.org/sdr/F3LA2010043100398), Apr 24, 2010: FLOOR PANEL. DENTED. REF HEAVY MX NON-ROUTINE N0679. AFT CARGO PANEL 151DE HAS NUMEROUS DENTS THROUGHOUT PANEL. R & R PANEL.
- [SDR F3LA2010050200409](https://openairdocs.org/sdr/F3LA2010050200409), Apr 20, 2010: FLOOR PANEL. DELAMINATED. REF C-CHECK NON ROUTINE N0587. CABIN FLOOR PANEL 222CF IS DELAMINATED. OFF ACFT PART. FABRICATED REPLACEMENT CABIN FLOOR PANEL 222CF IAW IRM 9701 REV G.
- [SDR F3LA2010050600418](https://openairdocs.org/sdr/F3LA2010050600418), Apr 19, 2010: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM JUST INBD OF Y765 AT FRAME 68. R & R FLOORBEAM IAW A319 SRM 51-42-11, PAGE 1, STEP A, 51-44-11, PAGE 1 AND 51-21-11 PAGE 1 TABLE 1.
- [SDR F3LA2010050500417](https://openairdocs.org/sdr/F3LA2010050500417), Apr 19, 2010: FLOORBEAM. CORRODED. REFERENCE C-CHECK NON ROUTINE N0479. CORROSION ON NUT PLATE HOLES AT SPLICE ON FLOORBEAM AT Y-1292 FRAME 69. UPPER AND LOWER SIDES OF BEAM. R & R FLOORBEAM IAW 
- [SDR F3LA2010050500416](https://openairdocs.org/sdr/F3LA2010050500416), Apr 19, 2010: FLOORBEAM. CORRODED. REFERENCE C-CHECK NON ROUTINE N0481. CORROSION ON PREVIOUS REPAIR AT FLOORBEAM, Y1292, FRAME 66. R & R FLOORBEAM IAW SRM 51-72-11, SHEETS 1 THROUGH 6.
- [SDR F3LA2010050500415](https://openairdocs.org/sdr/F3LA2010050500415), Apr 19, 2010: SILL. CORRODED. REFERENCE C-CHECK NON ROUTINE N0480. CORROSION ON L-2 DOOR SILL PLATE AT SPLICE FRAME 66. REPAIRED L-2 DOOR SILL PLATE IAW SRM 53-41-11 FIGURE 201 REPAIR PRINCI
- [SDR F3LA2010050400412](https://openairdocs.org/sdr/F3LA2010050400412), Apr 19, 2010: SILL. CORRODED. C-CHECK NON ROUTINE N0482. CORROSION ON R-2 DOORSILL PLATE AT FRAME 66 SPLICE. R & R DOOR SILL AND 3 EACH SCUFF PLATES IAW SRM 51-72-11 AND AMM 53-45-15-400-001
- [SDR F3LA2010050200411](https://openairdocs.org/sdr/F3LA2010050200411), Apr 19, 2010: SUPPORT FRAME. CORRODED. REFERENCE C-CHECK NON ROUTINE N0551. RIGHT HAND CABIN FLOOR SHEAR PLATE EXTRUSION IS CORRODED. REPLACED EXTRUSION REF A319 SRM 41-42-11, SRM 51-21-11 AND 51-72-
- [SDR F3LA2010050200410](https://openairdocs.org/sdr/F3LA2010050200410), Apr 19, 2010: FLOORBEAM. CORRODED. REFERENCE HEAVY MX NON-ROUTINE N0534. CORROSION DISCOVERED ON NUTPLATE HOLES ON FLOORBEAM Y1292. R & R FLOORBEAM.
- [SDR F3LA2010043100397](https://openairdocs.org/sdr/F3LA2010043100397), Apr 19, 2010: FLOORBEAM. CORRODED. REF C-CHECK NON ROUTINE N0478. CORROSION IN (2) AREAS OF FLOORBEAM -Y765 AT FRAME 68. R & R FLOORBEAM IAW A319 SRM 51-42-11 PAGE 11.
- [SDR F3LA2010050500414](https://openairdocs.org/sdr/F3LA2010050500414), Apr 18, 2010: SHEAR PLATE. CORRODED. REFERENCE C-CHECK NON ROUTINE N0318. SHEAR PLATE AT FRAME 69 TO FRAME 70 BETWEEN STRINGER 23 RT AND 24 RT HAS CORROSION IN 15 AREAS. R & R SHEAR PLATE IAW SRM 5
- [SDR F3LA2010050400413](https://openairdocs.org/sdr/F3LA2010050400413), Apr 18, 2010: SHEAR PLATE. CORRODED. REF C-CHECK NON ROUTINE N0317. SHEAR PLATE AT FRAME 69 TO 70 BETWEEN STRINGER 23 LT AND STRINGER 24 LT HAS 6 SQUARE INCHES OF CORROSION. R & R SHEAR PLATE IAW S
- [SDR F3LA2010050200408](https://openairdocs.org/sdr/F3LA2010050200408), Apr 18, 2010: TRANSITION PANEL. DELAMINATED. REF AERO FRAME HEAVY MX NON-ROUTINE N0336. TRANSITION PANEL 131BF HAS AREAS OF PUNCTURES DENTS AND EDGE DELAMINATION. OFF ACFT PART. FABRICATED PANEL IAW IRM 97
- [SDR F3LA2010050200407](https://openairdocs.org/sdr/F3LA2010050200407), Apr 18, 2010: TRANSITION PANEL. DENTED. REF C-CHECK NON ROUTINE N0299. FWD CARGO COMPARTMENT TRANSITION PANEL 131DG HAS NUMEROUS DENTS ACCROSS ENTIRE LENGTH OF PANEL. OFF ACFT PART. FABRICATED TRANSIT
- [SDR F3LA2010043100395](https://openairdocs.org/sdr/F3LA2010043100395), Apr 18, 2010: TRANSITION PANEL. DENTED. REFERENCE HEAVY MX NON ROUTINE N0319. FWD CARGO PIT TRANSITION PANEL HAS NUMEROUS DENTS THROUGHOUT ENTIRE LENGTH OF PANEL. FABRICATED REPLACEMENT PANEL IAW IRM9
- [SDR F3LA2010043000394](https://openairdocs.org/sdr/F3LA2010043000394), Apr 18, 2010: BRACKET. CRACKED. REF C4/SI CHECK NON-ROUTINE N0215. LT WING L/E TAI DUCT CUT OUT UPPER SURFACE OTBD PANEL ATTACH ANGLE HAS A 1.5 INCH CRACK. R & R BRACKET.
- [SDR F3LA2010043100396](https://openairdocs.org/sdr/F3LA2010043100396), Apr 17, 2010: FLOOR PANEL. DENTED. REFERENCE HEAVY MX NON-ROUTINE N0684. AFT CARGO PIT FLOOR PANEL 162CF HAS NUMEROUS DENTS. R & R PANEL.
- [SDR F3LA2009062200089](https://openairdocs.org/sdr/F3LA2009062200089), Jun 19, 2009: SERVO CONTROL. INOPERATIVE. FLIGHT CREW MADE AN UNSCHEDULED LANDING IN RSW DUE TO "SPOILER FAULT 4". THE AIRCRAFT RETURNED TO DEN ON A SPECIAL FLIGHT PERMIT. MAINTENANCE REMOVED AND REPLAC
- [SDR F3LA2009031100041](https://openairdocs.org/sdr/F3LA2009031100041), Mar 9, 2009: COMPUTER. SMOKE. DURING THE BOARDING PROCESS, BOTH PILOTS DETECTED ELECTRONIC OVERHEAT ODOR. MAINTENANCE PERFORMED TROUBLESHOOTING USING REFERENCE TSM 24-00-00-810-823, ELECTRIC
- [SDR F3LA200800604](https://openairdocs.org/sdr/F3LA200800604), Sep 8, 2008: FLOOR PANEL. CORRODED. REF: NON ROUTINE C050752. DURING C3 C-CHECK, INSPECTION FOUND (1) MOUNT BUSHING CORRODED ON FLOOR PANEL 261DE. MAINTENANCE REMOVED AND REPLACED MOUNT BUSHING ON
- [SDR F3LA200800601](https://openairdocs.org/sdr/F3LA200800601), Sep 6, 2008: FLOORBEAM. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED SEVERAL NUT PLATE HOLES ON FRAME Y-1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED FLOORB
- [SDR F3LA200800600](https://openairdocs.org/sdr/F3LA200800600), Sep 6, 2008: FLOORBEAM. CORRODED. REF NON ROUTINE C050600. DURING C3 C-CHECK, INSPECTION NOTED FWD NUT PLATE HOLE ON FRAME Y-1292 AT FRAME 66, HAD CORROSION. MAINT REMOVED CORROSION FROM HOLE, F
- [SDR F3L2008F00005](https://openairdocs.org/sdr/F3L2008F00005), Sep 6, 2008: FLOOR SUPPORT. CORRODED. REF: NON ROUTINE C050602. DURING C3 C-CHECK, INSPECTION NOTED SEVERAL NUT PLATE HOLES ON FRAME Y-1292 BETWEEN FRAME 66 AND FRAME 68, HAD CORROSION. MAINTENANCE 
- [SDR F3LA200800599](https://openairdocs.org/sdr/F3LA200800599), Sep 4, 2008: FLOORBEAM. CORRODED. REF NON ROUTINE C050605. DURING C3 C-CHECK, INSPECTION NOTED SEVERAL NUT PLATE HOLES ON FRAME Y-1292 BETWEEN FRAME 66 AND FRAME 68, HAD CORROSION. MAINT REMOVED
- [SDR FELA200800597](https://openairdocs.org/sdr/FELA200800597), Sep 4, 2008: FLOOR PANEL. CORRODED. REFERENCE NON ROUTINE C050515. DURING C3 C-CHECK INSPECTION NOTED FLOOR PANEL 261FF HAS CORROSION ON LOWER SURFACE. MX R&R FLOOR PANEL IN ACCORDANCE WITH THE RE
- [SDR F3LA200800596](https://openairdocs.org/sdr/F3LA200800596), Sep 4, 2008: FLOOR PANEL. PUNCTURED. REFERENCE NON ROUTINE C050458. DURING C3 C-CHECK INSPECTION NOTED TRANSITION PANEL 131CF WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORD
- [SDR F3LA200800595](https://openairdocs.org/sdr/F3LA200800595), Sep 4, 2008: FLOOR PANEL. PUNCTURED. REFERENCE NON ROUTINE C050457. DURING C3 C-CHECK INSPECTION NOTED TRANSITION PANEL 131EG WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORD
- [SDR F3LA200800594](https://openairdocs.org/sdr/F3LA200800594), Sep 4, 2008: FLOOR PANEL. PUNCTURED. REFERENCE NON ROUTINE C050375. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL 161CF WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCOR
- [SDR F3LA200800593](https://openairdocs.org/sdr/F3LA200800593), Sep 4, 2008: FLOOR PANEL. PUNCTURED. REFERENCE NON ROUTINE C050374. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL 161BF WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCOR
- [SDR F3LA200800592](https://openairdocs.org/sdr/F3LA200800592), Sep 4, 2008: FLOOR PANEL. PUNCTURED. REFERENCE NON ROUTINE C050372. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I51FF WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCOR
- [SDR F3LA200800591](https://openairdocs.org/sdr/F3LA200800591), Sep 4, 2008: FLOOR PANEL. PUNCTURED. REFERENCE NON ROUTINE C050370. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I51UG WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCOR
- [SDR F3LA200800590](https://openairdocs.org/sdr/F3LA200800590), Sep 4, 2008: FLOOR PANEL. PUNCTURED. REFERENCE NON ROUTINE C050368. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I51TG WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCOR
- [SDR F3LA200800589](https://openairdocs.org/sdr/F3LA200800589), Sep 4, 2008: FLOOR PANEL. PUNCTURED. REFERENCE NON ROUTINE C050366. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I52UG WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCOR
- [SDR F3LA200800598](https://openairdocs.org/sdr/F3LA200800598), Sep 4, 2008: FLOOR PANEL. CORRODED. REFERENCE NON ROUTINE C050516. DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF HAS CORROSION ON LOWER SURFACE. MX R&R FLOOR PANEL IN ACCORDANCE WITH THE R
- [SDR F3LA200800602](https://openairdocs.org/sdr/F3LA200800602), Sep 3, 2008: HINGE. DAMAGED. REF NON ROUTINE C050746. DURING C3 C-CHECK, INSP FOUND DAMAGE ON THE RT NR (4) SPOILER ANTI-ROTATION WEB. MAINT MACHINED AREA, FABRICATED REINFORCING PLATE AND 
- [SDR F3LA200800603](https://openairdocs.org/sdr/F3LA200800603), Sep 3, 2008: HINGE. DAMAGED. REF: NOT ROUTINE C050745. DURING C3 C-CHECK, INSPECTION FOUND DAMAGE ON THE RT NR (2) SPOILER ANTI-ROTATION WEB. MAINT MACHINED AREA, FABRICATED REINFORCING PLA
- [SDR F3LA200800409](https://openairdocs.org/sdr/F3LA200800409), Jul 1, 2008: UNKNOWN. ODOR. DURING FLIGHT, FLIGHT CREW NOTED AN ODOR OF GAS IN AFT GALLEY. MAINT INSPECTED AC FOR UNSATISFACTORY CABIN AIR QUALITY IAW TSM 21-00-00-810-802. NO ODOR OR SOUR

All 58: https://openairdocs.org/deregistered/N929FR-2015-11-16/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 20060611013829I](https://openairdocs.org/incident/20060611013829I), Jun 11, 2006: Airbus A319111 (N929FR), Salt Lake City, UT, Minor damage. (-23) On 06/11/06 at 0730 MST, a frontier airlines (F3LA), flt #580, an Airbus A319-111, N929FR, received minor damage to the radome of the aircraft. The…

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