# N931FR: 2004 Airbus A319-111, registration cancelled 2016-01-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 14, 2016 - 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: 2253 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 22, 2004 - Certificate issued: June 22, 2004 - Last registry action: December 21, 2015 - Mode S code: ACE9ED - 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/N931FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=931FR - Page: https://openairdocs.org/deregistered/N931FR-2016-01-14 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 (40) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA2014081401051](https://openairdocs.org/sdr/F3LA2014081401051), Aug 13, 2014: BATTERY. FAILED. EMERGENCY LIGHT BATTERY AFT LT FIN 13WL FAILED TEST ON OVERNIGHT MX CHECK. R & R BATTERY 13WL IAW AMM 33-51-39-000-005A & 33-51-39-400-005A. - [SDR F3LA2013051600854](https://openairdocs.org/sdr/F3LA2013051600854), May 10, 2013: STRUCTURE. CONTAMINATED. RT ELEVATOR, THERMOGRAPHY INSPECTION SHOWS FOUR INDICATIONS OF WATER INGRESS, LOCATED ON UPPER SKIN PANEL. INDICATIONS ARE IRREGULAR IN SHAPE AND BLACK IN COLOR - [SDR F3LA2013051600855](https://openairdocs.org/sdr/F3LA2013051600855), May 9, 2013: STRUCTURE. CONTAMINATED. LT ELEVATOR, THERMOGRAPHY INSPECTION SHOWS ONE INDICATIONS OF WATER INGRESS, LOCATED ON UPPER SKIN PANEL, INDICATION IS IRREGULAR IN SHAPE AND BLACK IN COLOR. S - [SDR F3LA2010052500434](https://openairdocs.org/sdr/F3LA2010052500434), May 19, 2010: EPSU. INOPERATIVE. REFERENCE HEAVY MAINTENANCE NON ROUTINE N0772. EMERGENCY EXIT MARKER INOPERATIVE LOWER FWD AT L-1 DOOR. R & R EPSU 10WL IAW AMM 33-51-38-000-001 AND 33-51-38-40 - [SDR F3LA2010052200431](https://openairdocs.org/sdr/F3LA2010052200431), May 19, 2010: CONNECTOR. NOT SEATED. REF HEAVY MX NON ROUTINE N0771. EMERGENCY EXIT SIGN OVER LT AFT ENTRY DOOR DOES NOT ILLUMINATE. FOUND CONNECTOR IMPROPERLY SEATED. PROPERLY SEATED CONNECTOR IAW - [SDR F3LA2010052200422](https://openairdocs.org/sdr/F3LA2010052200422), May 19, 2010: SIGN. INOPERATIVE. REF HEAVY MX NON ROUTINE N0773. RT FWD LOWER EMERGENCY EXIT IDENTIFIER DOES NOT ILLUMINATE. R & R IDENTIFIER IAW AMM 33-51-13-000-001. - [SDR F3LA2010052200432](https://openairdocs.org/sdr/F3LA2010052200432), May 17, 2010: WIRE HARNESS. DAMAGED. REF HEAVY MX NON ROUTINE N0757. LT ROW 7 EMERGENCY ESCAPE PATH LIGHTING HARNESS HAS 1 EACH WIRE PULLED LOOSE. R & R WIRING HARNESS IAW ASM 33-51-00 SCH 04 P106. - [SDR F3LA2010052200426](https://openairdocs.org/sdr/F3LA2010052200426), May 13, 2010: FLOOR PANEL. DEBONDED. REF HEAVY MX NON ROUTINE N0733. FWD CARGO FLOOR PANEL 131AF DISBONDED AT CORNERS. REPAIRED IAW SRM 53-02-00, PAGE 208, FIG 203. - [SDR F3LA2010052200429](https://openairdocs.org/sdr/F3LA2010052200429), May 11, 2010: FLOOR PANEL. DEBONDED. REF HEAVY MX NON ROUTINE N0601. AFT CARGO FLOOR PANEL 152UG DISBONDED. FABRICATED NEW PANEL IAW MCG IRM 9701 REV G. - [SDR F3LA2010052200428](https://openairdocs.org/sdr/F3LA2010052200428), May 11, 2010: FLOOR PANEL. DEBONDED. REFERENCE HEAVY MX NON ROUTINE N0639. AFT CARGO PANEL 151UG DISBONDED. FABRICATED NEW PANEL IAW NCG IRM 9701 REV G. - [SDR F3LA2010052200427](https://openairdocs.org/sdr/F3LA2010052200427), May 11, 2010: FLOOR PANEL. DEBONDED. REF HEAVY MX NON ROUTINE N0654 AFT CARGO FLOOR PANEL 151FE DISBONDED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REV G. - [SDR F3LA2010052200430](https://openairdocs.org/sdr/F3LA2010052200430), May 10, 2010: STRUT. CORRODED. REF HEAVY MX NON ROUTINE N0538. RT MLG INNER BARREL (CYL) HAS CORROSION. REMOVED CORROSION AND REPAIRED IAW EA 3 AC-32R-31779. - [SDR F3LA2010052500433](https://openairdocs.org/sdr/F3LA2010052500433), May 9, 2010: SILL. CORRODED. REFERENCE HEAVY MX NON ROUTINE N0432. AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL HAS 6 AREAS OF CORROSION TOTALING 10 SQ INCHES. REPAIRED DOOR SEAL IAW EA A9- - [SDR F3LA2010052200424](https://openairdocs.org/sdr/F3LA2010052200424), May 9, 2010: FLOOR PANEL. DELAMINATED. REFERENCE HEAVY MAINTENANCE NON ROUTINE N0366. COCKPIT FLOOR PANEL 211GF IS DELAMINATED. REPAIRED PANEL IAW SRM 5302-00. - [SDR F3LA2010052200425](https://openairdocs.org/sdr/F3LA2010052200425), May 8, 2010: FLOORBEAM. CORRODED. REF HEAVY MX NON ROUTINE N0281. FLOORBEAM AT FRAME 68 BEAM +4765 CORRODED. CUT OUT DAMAGED AREA.FABRICATED REPAIR SECTION AND INSTALLED IAW SRM 53-00-14 FIG 204 - [SDR F3LA2010052200423](https://openairdocs.org/sdr/F3LA2010052200423), May 8, 2010: SHEAR PLATE. CORRODED. REF HEAVY MX NON-ROUTINE N0280. AFTER FINDING MINOR CORROSION ON SHEAR PLATE FOUND PART TO BE WRONG CONFIGURATION. R & R SHEAR PLATE IAW EO- A0-53EO-31434. - [SDR F3LA2010052200421](https://openairdocs.org/sdr/F3LA2010052200421), May 8, 2010: FLOORBEAM. CORRODED. HEAVY MX NON-ROUTINE N0283. REAR FUSELAGE FLOORBEAM AT FRAME 66 HAS CORROSION AROUND FASTENER HOLE. REPAIRED AREA IAW SRM 53-41-14, PAGE 201, FIGURE 201 PRINCIP - [SDR F3LA2010052200420](https://openairdocs.org/sdr/F3LA2010052200420), May 8, 2010: SILL. CORRODED. REF HEAVY MX NON ROUTINE N0295. LT AFT DOOR SILL AREA FWD OF FRAME 66 ATTACH SUPPORT HAS (6) SQUARE INCHES OF CORROSION ON UPPER SURFACE. R & R DOOR SILL IAW SR - [SDR F3LA2010011800304](https://openairdocs.org/sdr/F3LA2010011800304), Jan 15, 2010: STRUT. DISCHARGED. DURING CLIMB OUT THE FLIGHT CREW RECEIVED A WARNING THAT THE NLG WOULD NOT FULLY RETRACT. MX COMPLIED WITH BORESCOPE INSP OF THE ANTI ROTATION LUG IAW AMM 32-21 - [SDR F3LA2009120900255](https://openairdocs.org/sdr/F3LA2009120900255), Dec 8, 2009: SELECTOR VALVE. UNSERVICEABLE. THE FLIGHT CREW MADE AN AIR RETURN TO DEPARTURE DUE TO AN ELECTRONIC CENTRALIZED ACFT MONITORING MESSAGE FOR NLG DOORS NOT CLOSED AND LANDING GEAR SYS DISAGREE. - [SDR F3LA2008100600667](https://openairdocs.org/sdr/F3LA2008100600667), Oct 4, 2008: CONTROL PANEL. FAILED. DURING C3 C-CHECK, INSPECTION NOTED THE FIRE PANEL DISCHARGE LIGHT FOR THE NR 1 FIRE BOTTLE OF THE NR 2 ENGINE FAILS TO ILLUMINATE DURING THE OPERATIONAL CHECK - [SDR F3LA2008100600666](https://openairdocs.org/sdr/F3LA2008100600666), Oct 4, 2008: FLOOR PANEL. PUNCTURED. DURING C3 C-CHECK, INSPECTION NOTED SEVERAL PUNCTURES AND EDGE DELAMINATION TO AFT CARGO TRANSITION PANEL 151AE. MAINTENANCE REMOVED AND REPLACED CARGO PANEL IN - [SDR F3LA2008100600665](https://openairdocs.org/sdr/F3LA2008100600665), Oct 4, 2008: FLOOR PANEL. DELAMINATED. DURING C3 C-CHECK, INSPECTION NOTED PASSENGER FLOOR PANEL 261DF HAS AREAS OF DELAMINATION. MAINTENANCE REPAIRED FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS - [SDR F3LA2008100600664](https://openairdocs.org/sdr/F3LA2008100600664), Oct 4, 2008: FLOOR PANEL. DELAMINATED. DURING C3 C-CHECK, INSPECTION NOTED PASSENGER FLOOR PANEL 262EF HAS AREAS OF DELAMINATION. MAINTENANCE REPAIRED FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS - [SDR F3LA2008100600659](https://openairdocs.org/sdr/F3LA2008100600659), Oct 4, 2008: FLOOR PANEL. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF IS CORRODED ON UPPER AND LOWER SURFACE. MAINTENANCE REMOVED FLOOR PANEL AND INSTALLED SERVICEABLE PANEL IN - [SDR F3LA2008100600663](https://openairdocs.org/sdr/F3LA2008100600663), Oct 3, 2008: FLOOR PANEL. DAMAGED. REFERENCE NON-ROUTINE C052153. DURING C3 C-CHECK, INSPECTION NOTED PASSENGER FLOOR PANEL 261EF HAS A CUT ON THE SURFACE. MAINTENANCE REPAIRED FLOOR PANEL IN ACC - [SDR F3LA2008100600662](https://openairdocs.org/sdr/F3LA2008100600662), Oct 3, 2008: FLOORBEAM. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 AT FRAME 68, FORWARD AND AFT HOLES HAVE CORROSION. MAINTENANCE BLENDED CORROSION AND OVERSIZED HOLES IN ACCO - [SDR F3LA2008100600661](https://openairdocs.org/sdr/F3LA2008100600661), Oct 3, 2008: FLOORBEAM. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 BETWEEN FRAME 66 AND FRAME 68, HAS CORROSION IN SEVERAL HOLES. MAINTENANCE BLENDED CORROSION AND OVERSIZED H - [SDR F3LA2008100600660](https://openairdocs.org/sdr/F3LA2008100600660), Oct 3, 2008: FLOORBEAM. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 BETWEEN FRAME 66 AND FRAME 68, HAS CORROSION IN SEVERAL HOLES. MAINTENANCE BLENDED CORROSION AND OVERSIZED H - [SDR F3LA2008100600658](https://openairdocs.org/sdr/F3LA2008100600658), Oct 3, 2008: FLOORBEAM. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 AT FRAME 66, FORWARD HOLE HAS CORROSION. MAINTENANCE BLENDED CORROSION, OVERSIZED HOLE, ROTO-PROBED, TREATED - [SDR F3LA200800656](https://openairdocs.org/sdr/F3LA200800656), Oct 2, 2008: FLOORBEAM. CORRODED. REFERENCE NON ROUTINE C051966. DURING C3 C CHECK, INSPECTION NOTED FLOOR BEAM Y-1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION IN SEVERAL HOLES. MX R&R FLOOR - [SDR F3LA200800655](https://openairdocs.org/sdr/F3LA200800655), Oct 2, 2008: LIGHT. INOPERATIVE. REFERENCE NON ROUTINE C051883. DURING C3 C CHECK INSPECTION NOTED THE RED EMERGENCY FLOOR PATH INDICATOR ON ROW 11ABC IS NOT ILLUMINATING. MX R&R LIGHT ASSEMBLY - [SDR F3LA200800654](https://openairdocs.org/sdr/F3LA200800654), Oct 2, 2008: BATTERY. FAILED. REFERENCE NON ROUTINE CO51711. DURING C3 C-CHECK, INSPECTION NOTED AFT EMERGENCY POWER SUPPLY UNIT BATTERY FAILED CAPACITY CHECK. MX R&R BATTERY IN ACCORDANCE W - [SDR F3LA2008100600670](https://openairdocs.org/sdr/F3LA2008100600670), Oct 2, 2008: PLATE. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED L-2 GIRT BAR FITTINGS ATTACH PLATE HOLES HAVE CORROSION. MAINTENANCE FABRICATED REPAIR DOUBLER AND FILLER, TREATED, PRIMED, - [SDR F3LA2008100600669](https://openairdocs.org/sdr/F3LA2008100600669), Oct 2, 2008: PLATE. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED THE L-2 FORWARD GIRT BAR FITTING BLANKING PLATE HAS CORROSION ON CORNER. MAINTENANCE REMOVED AND REPLACED L-2 DOOR FORWARD G - [SDR F3LA2008100700672](https://openairdocs.org/sdr/F3LA2008100700672), Sep 29, 2008: BLANKING PLATE. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED THE R2 DOOR AFT GIRT BAR FITTING BLANKING PLATE IS CORRODED ON LOWER SURFACE. MAINTENANCE REMOVED GIRT BAR BLANKING PLATE AN - [SDR F3LA2008100700671](https://openairdocs.org/sdr/F3LA2008100700671), Sep 29, 2008: BLANKING PLATE. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED THE R2 FORWARD DOOR GIRT BAR FITTING BLANKING PLATE IS CORRODED ON UPPER AND LOWER SURFACE. MAINTENANCE REMOVED CORRODED GIR - [SDR F3LA200800134](https://openairdocs.org/sdr/F3LA200800134), Apr 1, 2008: BATTERY. INOPERATIVE. DURING HEAVY SERVICE CHECK INSPECTION REPORTED RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IN ACCO - [SDR F3LA200700040](https://openairdocs.org/sdr/F3LA200700040), Mar 1, 2007: LATCH. STUCK. DURING C-2 CHECK INSPECTION, REPORTED GIRT BAR LATCH STUCK IN THE DOWN POSITION - L1 DOOR AFT LATCH. CLEANED GIRT BAR FITTING IAW AMM 12-21-12-100-006. - [SDR F3LA200700030](https://openairdocs.org/sdr/F3LA200700030), Mar 1, 2007: STOWAGE BOX. NO TEST. DURING C-2 CHECK, INSPECTION REPORTED 3RD CREW O2 STOWAGE BOX DID NOT FUNCTION DURING PUSH-TO-TEST. REPLACED 3RD CREW O2 STOWAGE BOX IAW 35-12-41, PB 401. 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