Airbus A319-114

Service difficulty reports · 10,218

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A319114'
  ORDER BY difficulty_date DESC"

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SDR DALA2026021901181Floor Support · corrodedCORROSION FLOOR SUPPORT -Y765 LOCATED BTW FR 67 TO FR 68 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT -Y765 AND FASTENERS LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11 AND DWG D53472816. (LP 1457078)Feb 18, 2026 · N327NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026021901179Fan · faultyBAD VIBRATION AND NOISE UNDER FLOOR OF FWD GALLEY AT PUSH TIME. T/S PER AMM 21-26, FOUND BAD EXTRACT AND BLOWER FAN (ONLY ONE FAN TWO FUNCTIONS), R & R SAME IAW AMM 21-26, OPS CHKD GOOD. (LP: 7732812)Feb 18, 2026 · N360NB · Airbus A319114 · Air Distribution FanSDR DALA2026022301264Bracket · out of adjustRIGHT OVERWING EXIT LIGHT ON INTERMITTENTLY. ADJUSTED COVER FLAP BRACKETS PER AMM 25-23-47. OPS CK GOOD. (LP 8018899)Feb 17, 2026 · N358NB · Airbus A319114 · Emergency LightingSDR DALA2026021901183Stringer · damagedPER FAA AAI FINDING TWO RIVETS AT STRINGER 4R BETWEEN FRAME 36 AND 37 REQUIRE REPLACEMENT DUE TO SUBSTANDARD INSTALLATION. REPAIRED FUSELAGE STRINGER 4R SECTION BETWEEN FR35+47MM AND FR36+381MM DUE TO SUBSTANDARD SOLID RIVETS INSTALLATION I/A/W A319 SRM 53-0Feb 17, 2026 · N331NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2026082204777Skin · not reportedFUSELAGE SKIN, FR 34, BETWEEN S1R AND S1L, PCS TIMING DOUBLER AREA, INSTALLATION DEVIATION, INCORPORATION OF SECTION II SUPPLEMENTAL INSPECTIONS. REVISION B OF ER/A 554177-14 INCORPORATES SECTION II SUPPLEMENTAL INSPECTIONS. INSPECTIONS THRESHOLD IS 33,481Feb 16, 2026 · N301NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2026030401478Fan · faultedVENT AVIONICS SYS FAULT DISPLAYED. WARM ELECTRICAL ODOR IS PRESENT. R & R AEVC IAW AMM 21-26. STILL REQ OPS CHK. OPS TEST OF AEVC FAULTED 21-26-51 EXTRACT FAN 18HQ AND 21-26-55 ISOLATION VALVE 24HQ. R & R EXTRACT FAN 18HQ IAW AMM 21-26. AEVC TESTED GOOD,Feb 16, 2026 · N353NB · Airbus A319114 · Air Distribution FanSDR DALA2026021901215Oxygen Bottle · damagedOXYGEN CONTAINER AT ROW 28ABC FOUND DAMAGED. REMOVED AND REPLACED OXYGEN CONTAINER AT ROW 28ABC IAW AMM 35- 21-41-000-001-A AND 35-21-41-400-001-A. PERFORMED SATISFACTORY OP CHK OF MANUAL MASK RELEASE IAW AMM 35-23-00-710-001-A. JOB COMPLETE. (LP: 1453153)Feb 16, 2026 · N358NB · Airbus A319114 · Passenger Oxygen SystemSDR DALA2026021601063Seat Track · corrodedCORROSION SEAT TRACK +Y765 AT FWD GALLEY AREA. REPLACED SEAT TRACK Y765 ON FWD GALLEY AREA IAW SRM 51-42-11-801 AND SRM 51-72-11. (LP 1452655)Feb 15, 2026 · N327NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026022601353Plate · missingDURING WALK AROUND, FOUND LT SLAT 2 INBD SLAT TRACK CLOSING PLATE MISSING. FWD TO CDL 27-00-03. DISP APPROVED. NO "M" PROC. CDL AND PLACARD INSTALLED. (LP: 8558938)Feb 14, 2026 · N349NB · Airbus A319114 · Leading Edge DevicesSDR DALA2026021901217Oxygen Mask · unwanted deployAFT RIGHT LAV OXYGEN MASKS DEPLOYED. RESTOWED THE OXYGEN MASKS IN THE AFT RIGHT LAV IAW AMM 35-21. ACFT OK FOR SERVICE. (LP: 8130774)Feb 14, 2026 · N339NB · Airbus A319114 · Passenger Oxygen SystemSDR DALA2026022601355Tachometer · failedAUTO BRAKE FAIL ON FINAL WHEN GEAR HANDLE PUT DOWN. AFTER LANDING BRAKE TEMPS: 215 - 245 40 - 530. POST FLIGHT REPORT SHOWS BRAKES AUTO BRK FAULT WITH FAILURE MESSAGE TACHOMETER 3(20GG), BSCU (10GG), BSCU 2, & BSCU 1. FWD TO MCO & PLACARD IAW MEL 32-42-05, Feb 13, 2026 · N370NB · Airbus A319114 · Landing Gear Brake SystemSDR DALA2026021901216Landing Gear · malfunctionedAFTER TAKEOFF, DELAYED LANDING GEAR RETRACTION FOR 1 MINUTE AND BELOW 220 KIAS IAW MEL 32-42-01B. UPON LANDING GEAR RETRACTION, ENCOUNTERED A VIBRATION AND RUMBLING. RECEIVED THE ECAM MESSAGE L/G DOORS NOT CLOSED. LANDING GEAR LEVER WAS UP PER ECAM PROCEDURFeb 13, 2026 · N370NB · Airbus A319114 · Landing Gear Retraction/Extension SystemSDR DALA2026022601354Proximity Sensor · out of toleranceAFTER TAKE OFF FROM KDTW, AFTER MLG LEVER SELECTED UP, DOORS SEQUENCED TO OPEN, BUT MLG DID NOT RETRACT. MLG NOT UPLOCKED ECAM APPEARED, FOLLOWED BY ANTI ICE STBY PITOT. SELECTED GEAR DOWN, ECAM CLEARED. ELECTED GEAR UP, GEAR CYCLED NORMALLY WITH WHEEL PAGE INFeb 11, 2026 · N368NB · Airbus A319114 · Landing Gear Position and WarningSDR DALA2026021201024Support · corrodedCORROSION ON THE LOWER SILL, FR 68 LT SIDE IN THE AFT GALLEY AREA. PERFORMED A PERMANENT REPAIR ON THE LOWER SILL IAW SRM 53-41-14-300-001, STEP 2.A, FIG.001, SHEET 4, PRINCIPLE 7. (LP 1447024)Feb 11, 2026 · N327NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026021201023Seat Track · corrodedCORRODED SEAT TRACK, -Y765 IN THE FWD GALLEY AREA. REPLACED SEAT TRACK -Y765, BTW FR 12 TO FR 24 IAW SRM 51-42-11, & SRM 51-72-11. (LP 1447020)Feb 11, 2026 · N327NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021201022Shear Web · corrodedAFT CABIN, BETWEEN FR 69-70, LT FLOOR SHEAR WEB WITH LEVEL 2 CORROSION. REPLACED THE SHEAR WEB IAW SRM 51-72- 11-911-001, & 53-41-17-01A, FIG 001, REV 155, & DWG D53474180. (LP 1446287)Feb 11, 2026 · N331NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026021101014Bracket · corrodedAFT CABIN. FLOOR TRIM BRACKETS BEHIND AFT GALLEY CORRODED, CRACKED AT MULTIPLE LOCATIONS (WET AREA). COMPLIED WITH ALL STEPS OF PRI 631659-14, REV 0. FOR AFT GALLEY AREA FLOOR PANEL SEALING ANGLE SECTION FABRICATION. (LP 1444687)Feb 10, 2026 · N358NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026021701070Inlet · contaminatedDURING DESCENT AROUND 10,000 FT AN ODOR WAS NOTICE THAT SEEMED TO SMELL LIKE A MUSTY BURNING. IT WAS SHORT LIVED, BUT RETURNED ON THE GROUND. WORK CARRIED 0550-2002 WAS ACCOMPLISHED TO IDENTIFY ISSUE. HEAVY OIL SATURATION WAS FOUND IN APU INLET UP INSIDE ENTIFeb 9, 2026 · N352NB · Airbus A319114 · APU Core EngineSDR DALA2026020900895Dampener · no testL1 DOOR FAILS DOOR DAMPING TEST (W/C 5210-7089-LF). REMOVED, REPLACED, AND SERVICED THE L1 DOOR DAMPER CYLINDER IAW AMM 52-11-14-000-001-B, 52-11-14-400-001-B, AND 52-10-00-614-001-A.Feb 7, 2026 · N358NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA2026020900896Unknown · odorSLIGHT SWEET ODOR APPEARED IMMEDIATELY AFTER TURNING ON THE APU BLEED WHEN PARKING. ACCOMPLISHED W/C 0550-2002 TYPE 1 APU TO STEP 5. ACCOMPLISHED LEVEL A DECONTAMINATION IAW W/C 2100-2007. NO ODOR FOUND MCC NOTIFIED. REFER TO LOG PAGE 1436089. ODI PREVENTIONFeb 5, 2026 · N334NB · Airbus A319114 · Air Distribution SystemSDR DALA2026020700883Light · detachedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED & INOPERATIVE. SEAT 16D, LIGHT FELL OFF AND NEEDS TO BE REATTACHED. REFASTENED 16D EMERGENCY LIGHT FIXTURE AS REQUIRED. (LP: 1435872)Feb 4, 2026 · N315NB · Airbus A319114 · Emergency LightingSDR DALA2026020600879Unknown · odorUPON TOUCH DOWN STRONG ODOR OF BURNED CRAYON, WAXY ODOR LASTED ABOUT 60 SECONDS AND DISAPPEARED. FA'S SMELLED IT AT BACK OF CABIN ODOR LASTED A FEW MINUTES. ENGINE BLEEDS OPEN PACKS ON APU BLEED OFF. PERFORMED AMM 05-50-00-810-831-A. NO ODORS PRESENT. OK FOR Feb 4, 2026 · N351NB · Airbus A319114 · Air Distribution SystemSDR DALA2026020600878None · noneER/A 627460-14 HAS BEEN REVISED TO 'A'. FOLLOW ON ACTION IS REQU IRED. PERFORM SECTION IV THE SOONER OF EVERY 15000FC/30000FH AFTER SEC TION I. ASSOCIATED ER/A 14-627460 ADDED FOR AC 3146. (LP: 1435703)Feb 4, 2026 · N346NB · Airbus A319114 · Standard Practices/StructuresSDR DALA2026020600877None · noneER/A 627460-14 HAS BEEN REVISED TO 'A'. FOLLOW ON ACTION IS REQU IRED. PERFORM SECTION III WITHIN THE SOONER OF EVERY 10000FC/20000FH A FTER SECTION I. ASSOCIATED ER/A 14-627460 ADDED FOR AC 3146. (LP: 1435700)Feb 4, 2026 · N346NB · Airbus A319114 · Standard Practices/StructuresSDR DALA2026020700884Oxygen Mask · unwanted deploySEAT 16 DEF MASKS DROPPED. REPACKED MASKS IAW AMM 35-21. OK FOR SERVICE. (LP: 8224408)Feb 3, 2026 · N342NB · Airbus A319114 · Passenger Oxygen SystemSDR DALA2026020600876Intercostal · crackedUPPER FUSELAGE, FORWARD ENTRY AREA, DOOR STOP FITTING 7 ON FR 16 RT SIDE, HOLE 1 & 3, WITH CRACK INDICATION AT INTERCOSTAL LAYER. REPLACED THE INTERCOSTAL IAW SRM 51-72-11-911-001, REV 155, AND DRAWING D5312300, ISSUE E, SHEET 01. FITTING P/N: D53114236201Feb 3, 2026 · N331NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026020600875Door Frame · crackedWORK CARD 5311-01229-02, UPPER FUSELAGE, FORWARD ENTRY AREA, DOOR STOP FITTING NR 7 ON FR 16 LT SIDE, HOLES 1 & 3, CRACK INDICATION AT INTERCOSTAL LAYER. REPLACED THE INTERCOSTAL D5311423620091 IAW SRM 51-72-11-911-001, REV 155. AND DWG D5312300, ISSUE E, SHFeb 2, 2026 · N331NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026020600880Unknown · odorAFTER LANDING THERE WAS A HINT OF SMELLY SCENT IN FLIGHT DECK AND CABIN. LASTED FOR ABOUT 1 MINUTE BEFORE DISSIPATING. VERY FAINT SMELL. C/W NO MSI WORK CARD 0550-2002, ENGINES AND APU CLEAN, NO ODORS IN THE CABIN AFTER RUNNING RECIRC FANS FOR 20 MIN. OK FOR Feb 1, 2026 · N343NB · Airbus A319114 · Air Distribution SystemSDR DALA2026020200752Unknown · odorDURING APPOACH OUT OF 12000', FA 1 REPORTED FUMES IN THE FWD GALLEY. SMELLED LIKE BURNING RUBBER. DEADHEAD CREW IN FIRST CLASS DID NOT SMELL. ODOR DISSIPATED AFTER TURNING OFF EXTRACT BLOWER, AND GALLEY AND PUSH BUTTONS ON OVERHEAD. EVENT LASTED 3-5 MINS. Jan 31, 2026 · N328NB · Airbus A319114 · Air Distribution SystemSDR DALA2026021000962Fitting · corrodedNR 1 ENGINE ATTACHMENT SPIGOT FITTING OUT OF LIMITS, LEVEL 2 CORROSION. REPLACED NR 1 PYLON LOWER SPIGOT FITTING IAW A319 SRM TASK 54-51-12-300-001. (LP 1443400)Jan 29, 2026 · N331NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA2026020700885Unknown · odorWALKED BOARDED THE AIRCRAFT AND INTO THE FLIGHT DECK, INSTANTLY SMELLED A METALLIC ODOR, APU INOPERATIVE ONLY GROUND AIR CONNECTED HAD GROUND AIR DISCONNECTED AND THE ODOR GOT WORSE TO THE POINT OF BEING ABLE TO TASTE IT. INSPECTED APU FOR OIL LEAKS IAW WC 4Jan 29, 2026 · N318NB · Airbus A319114 · Air Distribution SystemSDR DALA2026020100739Filter · odorAFTER ENG START, NR 2 WITH AIRCART. AFT FA REPORTS CHEMICAL BURNING ODOR AFTER BLEED AIR & PACKS. PACKS/BLEEDS TURNED OFF AND FA REPORTS ODOR WAS DISSIPATING. PER MCC REQUEST BEGAN A LEVEL C DECONTAMINATION IAW AMM 21- 00-00-615-804-A THROUGH STEP 3. CONDENSJan 29, 2026 · N329NB · Airbus A319114 · Air Distribution SystemSDR DALA2026020100738Threshold Web · corrodedAFT CARGO DOORWAY THRESHOLD WEB HAS CORROSION AT C56 - C58. EVALUATED AFT CARGO DOORWAY THERSHOLD WEB FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED AFT CARGO DOORWAY THERSHOLD IAW SRM 53-41-49-283-004, 51-42-11, 51-44-11. (LP: 1426275)Jan 29, 2026 · N358NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026020100737Door Frame · crackedAD RELATED, A.A. 5311-01216-04, AFT PASSENGER/CREW DOOR, FR68 LT, DOOR STOP FITTING NR 1, HOLE NR 4 (DIA. 0.250") HAD A CRACK INDICATION AT FRAME LAYER. EVALUATE & REPAIR IAW SRM 53-41-12. PERFORMED FREEZE PLUG REPAIR AT FR 68 DOOR FRAME STOP FITTING NR 1 HOJan 29, 2026 · N331NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026020100736Shear Tie · corrodedFWD CARGO COMPARTMENT FR 34 BETWEEN STR 41R - 42R FRAME SHEAR TIE CORRODED. REPLACED SHEAR VCLIP P/N: D5323094520000 AT FWD CARGO COMPARTMENT FR 34 BETWEEN STR 41R - STR 42R IAW A319 SRM 51-72- 11-911-001 REV 155.00 DATED 17/NOV/25 AND AIRBUS REFERENCE DRAWINJan 29, 2026 · N331NB · Airbus A319114 · Fuselage Internal Mounting StructureSDR DALA2026020100740Unknown · odorDURING PREFLIGHT, RAMP CREW STARTED DE-ICING AIRCRAFT WITHOUT OUR KNOWLEDGE NOR WITH AIRCRAFT CONFIGURED FOR DE-ICING. RECEIVED LAV SMOKE WARNING FOLLOWED QUICKLY BY FUMES & SMOKE LIKE SUBSTANCE THROUGHOUT ENTIRE CABIN. APU BLEED WAS ON, PACKS ON DESPITE IMMEDJan 27, 2026 · N318NB · Airbus A319114 · Air Distribution SystemSDR DALA2026020100735Flap Track · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) STAGE III APPROVAL REQUIRED FOR REPAIR ON THE LT OUTBOARD FLAP, TRACK 3, RIB 5 BORE PER ER/A 627489-14 REV A. SECTION I IS LIMITED TO 72000FC FROM SECTION I. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE ACFT FROM SERJan 27, 2026 · N346NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2026020100734Skin · noneSTAGE III DAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR FUSELAGE SKIN REPAIR INSTALLED AT FR25 S-13R/14R PER ER/A 627770-14 R EV A. SECTION I IS LIMITED TO 64000FC FROM SECTION I. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. (LP: 1Jan 27, 2026 · N346NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2026012900705Oil System · leakingFUMES AFTER LANDING. MODERATE INTENSITY PRESENT IN FLT DECK & FWD CABIN APU ON BLEED OFF. C/W W/C 0550-2002. AFTER NR 1 ENGINE & APU INSPECTION FOUND OIL POOLING AT BOTTOM OF APU GENERATOR AND SIGNS OF DE-ICING FLUID IN APU BAY. IAW MCC REQUEST PERFORMED A LJan 27, 2026 · N345NB · Airbus A319114 · APU Oil SystemSDR DALA2026012900704Apu · odorDIRTY SOCK SMELL WHEN APU BLEED SELECTED ON. SEE MD-ODI LOG 1420595 FOR WORK PERFORMED AND CORRECTIVE ACTION. (LP: 8035639)Jan 27, 2026 · N329NB · Airbus A319114 · APU Bleed Air SystemSDR DALA2026012900703Unknown · odorDIRTY SOCK ODOR VERY BAD IN CABIN. REF MD-ODI LOG 1420595 AND A/C LOG 8035642. VERIFIED P-TRACK READINGS 6000 DURING ENG RUN AND PACKS OPS FOLLOWING EXTENDED RUNS FOR BOTH. NO FURTHER ODOR NOTED. OK FOR SVC. (LP: 8035645)Jan 27, 2026 · N329NB · Airbus A319114 · Air Distribution SystemSDR DALA2026012900699Window Frame · damagedAD 2020-17-03 / A.A. WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. FLIGHT DECK, RT WINDSHIELD FRAMING LOWER CENTER POST, & RT CONTINUITY FITTING CRACKED. PERFORMED WING FRAMING MIRROR REPAIR & CONTJan 26, 2026 · N349NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026020100733Window Frame · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR FR 4 WINDOW FRAME. REPAIR PERFORMED PER ER/A 631144-14AD. SECTION I IS LIMITED TO 60000FC FROM EMBODIMENT. ER/A TO BE REVI SED PRIOR TO THIS LIMIT ELSE REMOVE ACFT FROM SERVICE. ASSOCIATED ER/A 14-631144 ADDEDJan 25, 2026 · N349NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026012900708Anchor Fitting · corrodedRIGHT WING REAR SPAR MAIN LANDING GEAR ACTUATOR ANCHORAGE FITTING WITH CORROSION. REPLACED ANCHORAGE FITTING AT RT WING REAR SPAR IAW REPAIR AUTHORIZATION 631319-14AD, REV. ORIGINAL, APPROVED AND DOCUMENTED ON AIRBUS RDAF REF AND ISSUE: 81710803/003/2025 A. CJan 25, 2026 · N349NB · Airbus A319114 · Wing, Landing Gear Attach FittingsSDR DALA2026012900707Window Frame · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR LH & RH CONTINU ITY FITTING REPLACEMENT PERFORMED PER ER/A 631144-14AD. SECTION I LIMITED TO 29500FC FROM SECTION I. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 14-63114Jan 25, 2026 · N349NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026012900706Window Frame · damagedER/A 631144-14AD ISSUED FOR LT & RT MIRROR FITTING REPAIR. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN 27000FC FROM SECTION I AND EVERY 4700F C THEREAFTER. ASSOCIATED ER/A 14-631144 ADDED. (LP: 1419073)Jan 25, 2026 · N349NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026012600552Frame · crackedFWD FUSELAGE CROSSBEAM SPLICING FR16 L/H, HOLES "H2" AND "H3" WITH CRACK INDICATION AT FRAME LAYER. CONTACT LIAISON ENGINNERING FOR REPAIR DISPOSITION. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. REFER TO EM 5311-01221, Jan 25, 2026 · N349NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2026012600551Fitting · damagedPERFORM ER/A 630835-14 AD FOR REPLACEMENT OF CONTINUITY FITTINGS. C/A: COMPLIED WITH ER/A 630835-14AD REV ORIGINAL MATCHES WITH ALL STEPS OF ERA 630835-14AD PRI REV 0 TO REV 2 IT IS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON CONTINUITY FITTINGS LH AND RJan 25, 2026 · N359NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026012600550Not Reported · not reportedPERFORM ER/A 586145-14AD REV D FOR REPLACEMENT OF FR16 LT IN PASSENGER CABIN. ER/A 586145-14AD REV D, APPROVED DATE: 23/JAN/26 WAS VERIFIED AGAINST ER/A 586145-14AD REV D PRI REV 0 AND WERE FOUND INCOMPLIANCE WITH THE SCOPE OF THE WORK ACCOMPLISHED, STEP RELAJan 25, 2026 · N359NB · Airbus A319114 · Fuselage Structure (General)SDR DALA2026012600549Window Frame · crackedCRACK INDICATION FOUND ON RH WINDSHIELD CENTER POST, LOWER ATTACHMENT ARIA, LOWER CORNER RADIUS, CRACK IS HORIZONTAL DIRECTION, CRACK LENGTH IS 0.190 INCH. AD 2020-17-03/ WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR Jan 25, 2026 · N359NB · Airbus A319114 · Fuselage Main, Structure
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