# N914FR: 2002 Airbus A319-111, registration cancelled 2013-07-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 31, 2013
- 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: 1841
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 9, 2002
- Certificate issued: November 13, 2002
- Last registry action: October 24, 2012
- Mode S code: ACA614
- Owner when cancelled: [Afs Investments Xix LLC](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%20XIX%20LLC)
- Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford)
- Owner type: Corporation
- Owner's area on the map: 41.0593° N, 73.5444° W: Placed by OpenAirDocs at the center of ZIP code 06902, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N914FR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=914FR
- Page: https://openairdocs.org/deregistered/N914FR-2013-07-31

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 (47)

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

- [SDR F3LA2013031100836](https://openairdocs.org/sdr/F3LA2013031100836), Feb 12, 2013: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR SUPPORT CORROSION AT FR16, Y1292. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5 AND 7.
- [SDR F3LA2013031100835](https://openairdocs.org/sdr/F3LA2013031100835), Feb 12, 2013: SHEAR PLATE. CRACKED. CABIN UNDER FLOOR LT SIDE BETWEEN STATION 69-70 LT SHEAR PLATE CRACKED. R & R LT SHEAR PLATE IAW SRM 51-42-11, PAR 6.B. 1-8.
- [SDR F3LA2011040500631](https://openairdocs.org/sdr/F3LA2011040500631), Mar 31, 2011: FLOOR SUPPORT. CORRODED. C-CHECK: NON ROTINE 36933; CABIN FR66, Y-765 FWD OF SPLICE, FLOOR SUPPORT HAS CORROSION AT FLOOR PANEL. REPLACED CABIN FLOOR SUPPORT FR66, Y-765 IAW SRM 51-42-1
- [SDR F3LA2011040500630](https://openairdocs.org/sdr/F3LA2011040500630), Mar 31, 2011: FLOOR SUPPORT. CORRODED. C-CHECK: NON ROUTINE NR 36931; CABIN FR66 Y-1292 FWD OF SPLICE FLOOR SUPPORT HAS CORROSION. REPLACED FWD FLOOR SUPPORT IN MAIN CABIN AT FR66 Y-1292 IAW SRM 51-4
- [SDR F3LA2011040500629](https://openairdocs.org/sdr/F3LA2011040500629), Mar 31, 2011: FLOORBEAM. CORRODED. C-CHECK: NON ROUTINE NR 36930; CABIN FR66, Y-765 FWD OF SPLICE HAS CORROSION AT FLOOR PANEL ON FLOOR SUPPORT. REPLACED CABIN FLOOR SUPPORT FR66, Y-765 IAW A319 
- [SDR F3LA2011040500628](https://openairdocs.org/sdr/F3LA2011040500628), Mar 31, 2011: FLOOR SUPPORT. CORRODED. C-CHECK: NON ROUTINE 36929; CABIN FRAME 68 Y-765, FLOOR SUPPORT HAS SURFACE CORROSION. R & R FLOOR IAW SRM 51-42-11, PARA 5 AND 6.B, PARA 7.B, SRM 51-44-11, PAR
- [SDR F3LA2011040500627](https://openairdocs.org/sdr/F3LA2011040500627), Mar 31, 2011: FLOOR SUPPORT. CORRODED. C-CHECK: NON ROUTINE NR 36907; CABIN FR66, Y-1292 AFT OF SPLICE FLOOR SUPPORT HAS CORROSION. REPLACED AFT FLOOR SUPPORT IAW SRM 51-42-11, PARA 5, PARA 6.A.(3) A
- [SDR F3LA2011040500626](https://openairdocs.org/sdr/F3LA2011040500626), Mar 31, 2011: FLOOR SUPPORT. CORRODED. C-CHECK: NON ROUTINE 36906; CABIN FR68 - FR66 Y-1292 FLOOR SUPPORT HAS CORROSION IN NUMEROUS AREAS. REPLACED FLOOR SUPPORT, MAIN CABIN AT FR68 - FR66 Y-1292 IAW
- [SDR F3LA2011040500625](https://openairdocs.org/sdr/F3LA2011040500625), Mar 31, 2011: FLOOR SUPPORT. CORRODED. NON-ROUTINE 36905; CABIN FR68 Y-1292 AFT OF SPLICE FLOOR SUPPORT HAS CORROSION. REPLACED AFT FLOOR SUPPORT IN MAIN CABIN AT FR68 Y-1292 IAW SRM 51-42-11 PARA 5,
- [SDR F3LA2011040500624](https://openairdocs.org/sdr/F3LA2011040500624), Mar 31, 2011: SILL. CORRODED. NON ROUTINE NR 36903; CABIN FR68 AT RT AT DOOR SILL BEAM HAS CORROSION. REPAIRED SILL BEAM IAW SRM 53-41-14. REPAIR PRINCIPLE K.
- [SDR F3LA2011040500623](https://openairdocs.org/sdr/F3LA2011040500623), Mar 31, 2011: PLATE. CORRODED. C-CHECK: NON ROUTINE NR 36902; FRAME 70 RT INTERNAL SHEAR PLATE HAS CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11, FIG 8, 51-44-11 PARA 6A (1), 7A(1) AND PARA 7
- [SDR F3LA2011040500622](https://openairdocs.org/sdr/F3LA2011040500622), Mar 31, 2011: FLOOR SUPPORT. CORRODED. C-CHECK: NON ROUTINE NR 36890; CABIN FR68 AT L2 DOOR OTBD FLOOR SUPPORT HAS CORROSION. REPAIRED SILL BEAM IAW SRM 53-41-14, FIG 201, REPAIR PRINCIPLE K.
- [SDR F3LA2011040500621](https://openairdocs.org/sdr/F3LA2011040500621), Mar 31, 2011: FLOOR SUPPORT. CORRODED. C-CHECK: NON ROUTINE NR 36889; CABIN FR68-FR66, Y1292 FWD OF SPLICE FLOOR SUPPORT HAS CORROSION. REPLACED FWD FLOOR SUPPORT IN MAIN CABIN AT FR68-FR666, Y1292 I
- [SDR F3LA2011040500620](https://openairdocs.org/sdr/F3LA2011040500620), Mar 31, 2011: SKIN. DENTED. C-CHECK: NON ROUTINE NR 36804; FUSELAGE UNDER FWD CARGO DOOR FRAME 26, BETWEEN STR 43 RT AND 43 LT HAS A DENT. REPAIR SKIN DENT REF SRM 53-21-11, PARA 5.K, FIG 
- [SDR F3LA2009091700182](https://openairdocs.org/sdr/F3LA2009091700182), Sep 16, 2009: PROFILE. CORRODED. DURING C5 C-CHECK, INSPECTION NOTED THE PROFILE LOCATED BETWEEN THE FORWARD AND AFT FLOOR PANELS AT FRAME 28 HAD CORRODED ATTACH HOLES. MAINTENANCE REMOVED AND 
- [SDR F3LA2009091700180](https://openairdocs.org/sdr/F3LA2009091700180), Sep 16, 2009: PROFILE. CORRODED. DURING C5 C-CHECK, INSPECTION NOTED THAT THE PROFILE LOCATED BETWEEN FRAME 24.5 AND FRAME 28, HAD CORROSION AROUND THE FLOOR PANEL ATTACH HOLES. MAINTENANCE REM
- [SDR F3LA2009091700179](https://openairdocs.org/sdr/F3LA2009091700179), Sep 16, 2009: PROFILE. CORRODED. DURING C5 C-CHECK, INSPECTION NOTED THAT THE PROFILE AT FRAME 28 IN THE FORWARD CARGO PIT HAD CORRODED FLOOR PANEL ATTACH HOLES. MAINTENANCE REMOVED AND REPLACE
- [SDR F3LA2009091700178](https://openairdocs.org/sdr/F3LA2009091700178), Sep 16, 2009: PROFILE. CORRODED. DURING C5 C-CHECK, INSPECTION NOTED THE PROFILE AT FRAME 34 IN THE FORWARD CARGO PIT HAD CORRODED FLOOR PANEL ATTACH HOLES. MAINTENANCE REMOVED AND REPLACED THE
- [SDR F3LA2009091700181](https://openairdocs.org/sdr/F3LA2009091700181), Sep 15, 2009: CONTROL CABLE. LACK OF LUBE. DURING C5 C-CHECK, INSPECTION NOTED THAT THE RT OVERWING EXIT FLEX CONTROL CABLE FOR THE INFLATION RESERVOIR FAILED THE FUNCTIONAL TEST. MAINTENANCE LUBRICATED 
- [SDR F3LA2009091700177](https://openairdocs.org/sdr/F3LA2009091700177), Sep 15, 2009: ROLL PIN. SHEARED. DURING DEN C5 C-CHECK, INSPECTION NOTED THAT THE LT EMERGENCY EXIT DOOR LOCKING PIN WILL NOT LOCK IN THE ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE RO
- [SDR F3LA2009091700176](https://openairdocs.org/sdr/F3LA2009091700176), Sep 14, 2009: PROFILE. CORRODED. DURING DEN C5 C-CHECK, INSPECTION NOTED CORROSION BETWEEN FRAME 28 AND FRAME 30 ON THE AFT RIGHT HAND FLOOR PROFILE ATTACH HOLES. MAINTENANCE REMOVED AND REPLAC
- [SDR F3LA200800192](https://openairdocs.org/sdr/F3LA200800192), Apr 20, 2008: PLATE. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED MAIN DECK WEB AT FRAME 70 RBL 52 WAS CORRODED. MAINTENANCE REMOVED AND REPLACED MAIN DECK WEB AT FRAME 70 RBL 52 IN ACCORD
- [SDR F3LA200800193](https://openairdocs.org/sdr/F3LA200800193), Apr 17, 2008: FITTING. FAILED. DURING C4 S1 C CHECK INSPECTION NOTED THE FORWARD ENTRY DOOR FAILED RIG CHECK AT THE TORSION BAR BELL CRANK AND REDUCER SHAFT. MAINTENANCE REMOVED AND REPLACED 
- [SDR F3LA200800180](https://openairdocs.org/sdr/F3LA200800180), Apr 17, 2008: FITTING. FAILED. DURING C4 S1 C CHECK INSPECTION REPORTED THE FORWARD ENTRY DOOR FAILED RIG CHECK AT TORSION BAR BELL CRANK AND REDUCER SHAFT BELLCRANK. MAINTENANCE REMOVED AND 
- [SDR F3LA200800181](https://openairdocs.org/sdr/F3LA200800181), Apr 15, 2008: FLOOR PANEL. CORRODED. DURING C4 S1 C CHECK INSPECTION REPORTED CORROSION ON MAIN CABIN R1 DOOR ENTRY FLOOR PANEL LOWER SURFACE AND AT VARIOUS FASTENER HOLES. MAINTENANCE REMOVED AND 
- [SDR F3LA200800176](https://openairdocs.org/sdr/F3LA200800176), Apr 15, 2008: FLOOR PANEL. PUNCTURED. DURING C4 S1 C CHECK INSPECTION NOTED PANEL 251RF HAS TWO PUNCTURES. MAINTENANCE CLEANED AREA OF DAMAGE, PREPPED AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUI
- [SDR F3LA200800175](https://openairdocs.org/sdr/F3LA200800175), Apr 15, 2008: STRAP. CORRODED. DURING C4 S1 C CHECK INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO BAY FLOOR STRAP FROM FLOOR STRAP 2350-2030 STRINGER 38 LEFT. MAINTENANCE FABRICATED NEW 
- [SDR F3LA200800169](https://openairdocs.org/sdr/F3LA200800169), Apr 8, 2008: WIRE HARNESS. MISSING. DURING C4 S1 C CHECK INSPECTION REPORTED EMERGENCY LIGHT CONNECTOR MISSING MATE LOCK CAP SEAT ROW 1 HARNESS 350WLI. MAINTENANCE REPLACED CONNECTOR HARNESS, HARN
- [SDR F3LA200800149](https://openairdocs.org/sdr/F3LA200800149), Apr 6, 2008: FLOOR PANEL. DAMAGED. DURING C4 S1 C CHECK, INSPECTION REPORTED DELAMINATION, AT THE EDGES, AND A LARGE GOUGE, IN FLOOR PANEL 221DF. MAINTENANCE REPAIRED THE FLOOR PANEL IN ACCORDANC
- [SDR F3LA200800170](https://openairdocs.org/sdr/F3LA200800170), Apr 5, 2008: PANEL. DAMAGED. DURING C4 S1 C CHECK INSPECTION REPORTED PANEL 151TG AFT CARGO SLANT PANEL HAS HOLE. MAINTENANCE FABRICATED DOUBLER AND APPLIED REPAIR IN ACCORDANCE WITH SRM 53
- [SDR F3LA200800146](https://openairdocs.org/sdr/F3LA200800146), Apr 4, 2008: FLOOR PANEL. DAMAGED. DURING C4 S1 C CHECK, INSPECTION REPORTED FLOOR PANEL 221EF HAD PUNCTURE DAMAGE. MAINTENANCE REPAIRED THE PUNCTURE IN THE PANEL IN ACCORDANCE WITH THE REQUIREME
- [SDR F3LA200800168](https://openairdocs.org/sdr/F3LA200800168), Apr 3, 2008: STRAP. CORRODED. DURING C4 S1 C CHECK INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO BAY FLOOR STRAP FROM FLOOR STRAP 2216 TO 2030 STRINGER 38 RIGHT. MAINTENANCE REMOVED AND
- [SDR F3LA200800167](https://openairdocs.org/sdr/F3LA200800167), Apr 3, 2008: SEAT TRACK. CORRODED. DURING C4 S1 C CHECK INSPECTION REPORTED DEEP CORROSION CABIN FLOOR STRUCTURE SEAT TRACK AT FRAME 21, Y1292 FLOOR STRAP 810. MAINTENANCE REMOVED AND REPLACED NE
- [SDR F3LA200800166](https://openairdocs.org/sdr/F3LA200800166), Apr 3, 2008: STRAP. CORRODED. DURING C4 S1 C CHECK INSPECTION REPORTED CORROSION ON AFT CARGO BAY FLOOR FRAME STRAP UPPER SURFACE FLOOR STRAP 2350 FRAME 58. MAINTENANCE REMOVED AND REPLACED 
- [SDR F3LA200800165](https://openairdocs.org/sdr/F3LA200800165), Apr 3, 2008: STRAP. CORRODED. DURING C4 S1 C CHECK INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO BAY FLOOR FRAME STRAP UPPER SURFACE AT FLOOR STRAP 2243 FRAME 56. MAINTENANCE REMOVED AN
- [SDR F3LA200800164](https://openairdocs.org/sdr/F3LA200800164), Apr 3, 2008: STRAP. CORRODED. DURING C4 S1 CHECK INSPECTION REPORTED SURFACE CORROSION ON CARGO BAY FLOOR STRAP 2403 TO 2456 STRINGER 38R. MAINTENANCE REMOVED AND REPLACED FLOOR STRAP IN ACC
- [SDR F3LA200800145](https://openairdocs.org/sdr/F3LA200800145), Apr 3, 2008: WEB. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND UNDER THE WEB AT FRAME 70 AND RIGHT BUTT LINE 52. MAINTENANCE REMOVED AND REPLACED THE WEB AT FRAM
- [SDR F3LA200800144](https://openairdocs.org/sdr/F3LA200800144), Apr 3, 2008: SEAT TRACK. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON SEAT TRACK Y-1292, AT FUSELAGE STATION 810, ON THE RIGHT SIDE, EXTENDING FORWARD TOWARD FRAME 2
- [SDR F3LA2008OO144](https://openairdocs.org/sdr/F3LA2008OO144), Apr 3, 2008: SEAT TRACK. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON SEAT TRACK Y-1292, AT FUSELAGE STATION 810, ON THE RIGHT SIDE, EXTENDING FORWARD TOWARD FRAME 2
- [SDR F3LA200800148](https://openairdocs.org/sdr/F3LA200800148), Apr 2, 2008: FLOOR PANEL. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION AND DAMAGE WAS FOUND ON FLOOR PANEL 261PF, UNDER THE RIGHT CORNER OF THE AFT GALLEY. MAINTENANCE REPAIRED TH
- [SDR F3LA200800147](https://openairdocs.org/sdr/F3LA200800147), Apr 2, 2008: FLOOR PANEL. DAMAGED. DURING C4 S1 C CHECK, INSPECTION REPORTED FLOOR PANEL 222EF HAD PUNCTURE DAMAGE. MAINTENANCE REPAIRED THE PUNCTURE IN THE FLOOR PANEL IN ACCORDANCE WITH THE REQ
- [SDR F3LA200800142](https://openairdocs.org/sdr/F3LA200800142), Apr 1, 2008: COVER. BROKEN. DURING C4 S1 C CHECK, INSPECTION REPORTED A CRACK WAS FOUND IN THE EMERGENCY EXIT LIGHT LENS COVER LOCATED ON THE AFT SIDE OF THE FORWARD RIGHT DOOR FRAME. MAIN
- [SDR F3LA200800143](https://openairdocs.org/sdr/F3LA200800143), Mar 30, 2008: LAMP. DEFECTIVE. DURING C4 S1 C CHECK, INSPECTION REPORTED THE EMERGENCY EXIT LIGHT, ABOVE THE L1 DOOR ENTRANCE, FLICKERED. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMER
- [SDR F3LA200600007](https://openairdocs.org/sdr/F3LA200600007), Feb 9, 2006: ATTACH FITTING. CORRODED. DURING REMOVAL OF FLOOR PANEL 262EF FOR DISCREPANCY REGARDING AFT LAVATORIES, MAINTENANCE REPORTED L-2 DOORWAY FLOOR PANEL AFT ATTACH PLATE CORRODED. FABRICATED
- [SDR F3LA200600006](https://openairdocs.org/sdr/F3LA200600006), Feb 9, 2006: FLOOR PANEL. CORRODED. DURING REMOVAL OF FLOOR PANEL 262EF FOR DISCREPANCY REGARDING AFT LAVATORIES, MAINTENANCE REPORTED CORROSION ON AFT GALLEY CONNECTING PLATE MOUNT HOLES FOR FLOO
- [SDR F3LA200600005](https://openairdocs.org/sdr/F3LA200600005), Feb 9, 2006: SUPPORT BEAM. CORRODED. DURING REMOVAL OF FLOOR PANEL 262EF FOR DISCREPANCY REGARDING AFT LAVATORIES, MAINTENANCE REPORTED CORROSION ON AFT GALLEY FLOOR SUPPORT BEAM BETWEEN FRAME 67-6
- [SDR F3LA200600004](https://openairdocs.org/sdr/F3LA200600004), Feb 9, 2006: FLOORBEAM. CORRODED. DURING REMOVAL OF FLOOR PANEL 262EF FOR DISCREPANCY REGARDING AFT LAVATORIES, MAINTENANCE REPORTED AFT GALLEY FLOOR SUPPORT BEAM AT R-2 DOOR CORRODED ON TOP OF 

## 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 20060727018679I](https://openairdocs.org/incident/20060727018679I), Jul 27, 2006: Airbus A319111 (N914FR), San Jose, CA. (-23) The captain stated: "pushed tail north from gate C-12, called for taxi, given the following route. "Taxi zulu" to "echo" down 30R for a 30L departure. No…

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