Airbus A319-114

Service difficulty reports · 10,218

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Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA2026040602163Engine · faultedREJECT TAKEOFF DUE TO ASYMMETRICAL POWER AND GATE RETURN FOR SIGNIFICANT LAG BETWEEN ENG & 2 ENG 1 LAGS 4 SEC TO ENG 2. INSPECTED PS3 LINE IAW AMM 72-00. PERFORMED ACCEL CHKD IAW AMM 71-00710-010-A ACCEL TIME OF 6.0 SECOND WITH IN LIMIT OF 7.5 AMM LIMIT. RUN Apr 4, 2026 · N349NB · Airbus A319114 · Engine (Turbine/Turboprop)SDR DALA2026040602164Oil System · leakingUPON ARRIVING AT THE AIRCRAFT APU WAS RUNNING AND SMELLED LIKE DIRTY SOCKS. TURNED OFF APU BLEED, SMELL IMPROVED. TURNED APU BLEED BACK ON, SMELL INCREASED. INTIAL INVESTIGATION FOUND APU OVER SERVICED. REMOVED EXCESS OIL IAW AMM 49-80. UPON FURTHER INVESTIGAApr 2, 2026 · N347NB · Airbus A319114 · APU Oil SystemSDR DALA2026040602162Brake · no discrepancyABORTED TAKEOFF RIGHT SHORT OF 80 KNOTS. FLIGHT CAME TO FULL STOP ON THE RUNWAY. PERFORMED INSP AFTER BRAKE EMERGENCY APPLICATION PER AMM 05 -51. OP CHKD GOOD AT THIS TIME. HIGHEST BRAKE TEMP <205C. NO DEFECTS NOTED. (LP: 8583172) AIRCRAFT WAS GROUNDEDApr 1, 2026 · N339NB · Airbus A319114 · Landing Gear Brake SystemSDR DALA2026040302146Circuit Breaker · failedDIV - TO RDU DUE TO CAPTAIN'S PITOT HEAT INOP (ANTI ICE CAPT PITOT ECAM WARNING) AND FLYING INTO ICING CONDITIONS. REPLACED C/BS 3DA1 AND 2DA1. FOUND 3DA1 LOCK NUT LOOSE, AND WIRE STRAIN FROM BACK SHELL ON PITOT PROBE CONNECTOR (9DA1-A). LGCIU-1 REPLACED AS Apr 1, 2026 · N349NB · Airbus A319114 · Ice/Rain Protection System WiringSDR DALA2026040202138Packing · damagedDIVERTED TO MIA DUE TO LOSS OF BLUE HYDRAULIC SYSTEM WITH HYD B RSVR LO LVL ECAM WARNING. FOUND DAMAGED PACKING AT FITTING IN THE BLUE SYSTEM PRESSURE LINE GOING TO THE SLATS WTB. (LP: 8323720) AIRCRAFT WAS GROUNDEDApr 1, 2026 · N351NB · Airbus A319114 · Hydraulic System, MainSDR DALA2026040302147Ecs · contaminatedSTRONG DIRTY SOCK ODOR COMING FROM FLIGHT DECK. NOTICED THE ODOR IMMEDIATELY UPON BOARDING. APU & PACKS ON FOR MEL. SUSPECT POSSIBLE APU BLEED CONTAMINATION. PERFORMED LEVEL A DECONTAMINATION OF ECS PER WORKCARD 2100-2007. REF MD LOG 1521040 FOR COMPLETION OFMar 31, 2026 · N335NB · Airbus A319114 · Cabin Cooling SystemSDR DALA2026040202137Skin · damagedLOWER EXTERNAL FUSELAGE AT FR 25+160MM, STGR 40L SKIN WITH TOOL MARKS. FOUND DURING PROCESS WITH ORNRC 100-269. REPAIRED LOWER FUSELAGE SKIN PANEL FROM FR25 +66.5MM TO FR25 + 296.6MM BETWEEN STRG 39LH-41LH DUE TO TOOL MARK OUT LIMITS I/A/W A319 SRM 53-21-11-3Mar 30, 2026 · N325NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2026040402153Not Reported · not reportedPERFORM ER/A 632197-14 FOR GAIN ACCESS TO REPLACEMENT CONTINUITY FITTINGS LT & RT. COMPLIED WITH ER/A 632197-14 REV ORIGINAL MATCHES WITH ALL STEPS OF ER/A 632197-14 PRI REV 0 IT IS BEEN VALIDATED, PERFORMED REPAIR INSTRUCTIONS FOR GAIN ACCESS TO REPLACEMENT Mar 29, 2026 · N365NB · Airbus A319114 · Standard Practices/StructuresSDR DALA2026040402154Tab · damagedDURING MTC FOUND ANTI ROTATION TAB ON SPOILER PANEL DAMAGED. INSPECTED & BLENDED DAMAGE IAW SRM 57-70. FOUND MAXIMUM ALLOWABLE DAMAGE OF 0.028 EXCEEDED. REMOVED NR 4 SPOILER IAW AMM 27-64. INSPECTED SPOILER PANEL MOUNTING BOLTS & VERIFIED 8130. INSTALLED NR 4Mar 29, 2026 · N357NB · Airbus A319114 · SpoilersSDR DALA2026033002092Fan · dirtyATB AND DE DUE TO A BURNING PLASTIC ODOR IN THE FLIGHT DECK AND FORWARD GALLEY. FOUND THE EXTRACT FAN WITH HOT TEMPERATURE, REMOVED AND FOUND DEBRIS IN FAN. REPLACED EXTRACT FAN (18HQ). (LP: 7796361)Mar 29, 2026 · N340NB · Airbus A319114 · Air Distribution FanSDR DALA2026033002091Pump · faultedATO AT 70 KNOTS DUE TO HYD G ENG 1 PUMP LOW PRESSURE ECAM WARNING. REPLACED THE NR 1 ENGINE EDP PUMP (1030GK) AND PRESSURE SWITCH (1074GK). OPS CHECKED GOOD. (LP: 8863450)Mar 29, 2026 · N371NB · Airbus A319114 · Hydraulic Pump (Electric/Engine), MainSDR DALA2026033002090Window Frame · crackedCRACK INDICATION ON WINDOW FRAME NR 2, LOWER NODE ATTACHMENT AREA CONTINUITY FITTING LT SIDE, CRACK LENGTH IS 0.200. CRACK DIRECTION IS VERTICAL. COMPLIED WITH ER/A 632268-14AD REV ORIGINAL MATCHES WITH ALL STEPS OF ER/A 632268-14AD PRI REV 0 AND REV 1, PEMar 29, 2026 · N365NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026033002089Seat Track · corrodedPASSENGER CABIN AT Y-765, BETWEEN FR20 AND FR21, SEAT TRACK CORRODED. REPLACED THE SEAT TRACK Y -765, BTW FR 12 TO FR 24 IAW SRM 51-72-11-911-001, PARAG 2.B, REV 155.00, DWGS D53112812, D53112813, D53112639, & D53110920. (LP: 1518556)Mar 29, 2026 · N325NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026033002088Seat Track · corrodedPASSENGER CABIN AT Y-1292, BETWEEN FR20 AND FR21 , SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK AT Y -1292, BTW FR 12 TO FR 24 IAW SRM 51-72-11-911-001, PARAG 2.B, REV 155.00, DWG D53112812, D53112813, D53110920, & D53112639. (LP: 1518547)Mar 29, 2026 · N325NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026033002087Window Frame · crackedCRACK INDICATION ON FRAME 2 OF WINDSHIELD CENTER POST LOWER NODE, ATTACHME NT POCKET LT SIDE, INBD FLANGE, FROM UPPER TENSION BOLT, CRACK LENG TH IS 0.120, CRACK DIRECTION IS 2 OCLOCK. AD 2020-17-03 / WORKC ARD 5311-01226-01. COMPLIED WITH ER/A 632195-14AD,Mar 29, 2026 · N365NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026040102119Skin · corrodedDURING M2 AND WHILE INSPECTING PER JIC 5320-6010-DE, CORROSION SPOTS FOUND ON FUSELAGE SKIN, INTERNAL SIDE BETWEEN STRGR 31L - STRGR 32L AND FR67 - FR69. AT REV A STAGE II DTE IS COMPLETE. STAGE III PENDING. C/A: *DTE* PER SECTION DTE I, THE REPAIR OF SECTION Mar 27, 2026 · N352NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2026033002086Floor Support · corrodedCORRODED FLOOR SUPPORT, +Y765, BTW FR 66 & FR 70 IN AFT GALLEY AREA. INSTALLED SPLICES ON FR 66 IAW SRM 51-42-11, AND DWG D53472816, ISSUE A. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-42-11, SRM 51-72-11, & DWG D53472816, ISSUE A. TOOK MEASUREMar 27, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026033002085Floor Support · corrodedCORRODED FLOOR SUPPORT +Y1162.5 LOCATED BTW FR 69 & FR 70 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-42-11, SRM 51-72-11, & DWG D53472780, TOOK MEASUREMENT OF CORROSION: L=1.014 IN, W= 0.840 IN, D= 0.044 IN, (LP: 1515362)Mar 27, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026032602016Apu · odorRAN APU WITHOUT BLEED FOR 8 MINUTES BEFORE TURNING ON BLEED WHEN BLEED TURNED ON DIRTY SOCKS SMELL STARTED, RAN WITH BLEED FOR ABOUT 1 MINUTE AND THE SMELL GOT STRONGER, TURNED BLEED OFF SMELL WENT AWAY. FLIGHT ATTENDANTS DID NOT SMELL IT BUT BOARDING DOOR WASMar 25, 2026 · N363NB · Airbus A319114 · APU Core EngineSDR DALA2026032602015Plate · corrodedCORROSION LOWER SURFACE EXTERNAL SKIN REINFORCING PLATE LOCATED AT LEVEL RIB 8 ON RH WING. C/A: COMPLIED WITH ER/A 632291-14AD REV ORIGINAL MATCHES WITH ALL STEPS OF PRI 632291-14AD REV 0 AND REV 1 IT IS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON BOTTOM Mar 24, 2026 · N365NB · Airbus A319114 · Wing, Plate/SkinSDR DALA2026032602014Power Supply · inoperativePAX CABIN EMERGENCY POWER SUPPLY UNIT INOP. REPLACED EMERGENCY POWER SUPPLY UNIT IAW A319 AMM TASK 33-51-38- 000-001-A AND AMM TASK 33-51-38-400-001-A. (LP: 1510385)Mar 24, 2026 · N325NB · Airbus A319114 · Emergency LightingSDR DALA2026032602012Skin · corrodedRIGHT WING, TOP SKIN, PANEL 2, LOWER SURFACE, T/E OVERHANG AREA WITH CORROSION AT RIB 11+520MM. C/A: PERFORMED REPAIR AT RH WING TOP SKIN PANEL 2/0 WER SURFACE T/E OVERHANG AREA AT RIB 11 + 520MM (AREA2) IAW ER/A NO. 632748-14AD REV ORIGINAL DATED 21 MAR 26. TMar 24, 2026 · N364NB · Airbus A319114 · Wing, Plate/SkinSDR DALA2026032602011Support Angle · corrodedFORWARD PASSENGER DOOR (LT) CUTOUT SILL AREA BETWEEN FR16 AND FR20, SCUFF PLATE SUPPORT ANGLE WITH CORROSION. REPLACED SUPPORT ANGLE (FITTING) P/N: D5311219820006 IAW A319 SRM TASK 51-72-11-911-001 REV 155.00 DATED 17/NOV/25 AND DRAWING REF D531 12109 ISSUE CMar 24, 2026 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026032602010Skin · corrodedRIGHT WING, TOP SKIN, PANEL 2, LOWER SURFACE, T/E OVERHANG WITH CORROSION AT RIB 10 AREA. C/A: PERFORMED REPAIR AT RH WING TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 10 (AREA1) I.A.W ER/A NO. 632748-14AD REV ORIGINAL DATED 21-MAR-26. THIS IS A MAMar 24, 2026 · N364NB · Airbus A319114 · Wing, Plate/SkinSDR DALA2026032602009Stop Fitting · not reportedPASSENGER CABIN AT FR68 AFT FACE AREA, BETWEEN STGR21R AND STGR23R, LEVEL DOOR STOP 1 FOUND REPAIR FITTING INSTALLED. WORK CARD 5311-01244-02B, SB A320-53-1491. CONTACT DELTA LIAISON ENGINEERING FOR ALTERNATE INSPECTION INSTRUCTION THAT MAY BE REQUIRED TO COMPMar 24, 2026 · N364NB · Airbus A319114 · Standard Practices/StructuresSDR DALA2026032602013Torque Link · corrodedLOWER FUSELAGE RH MLG TORQUE LINK UPPER PIN WITH CORROSION. REPLACED RH MLG TORQUE LINK UPPER PIN IAW A319 AMM TASK 32-11-27 -000-001-A AND AMM TASK 32-11-27-400-001-A REV 134.01 DATED 12/ FEB/26. (LP: 1508509)Mar 23, 2026 · N364NB · Airbus A319114 · Main Landing GearSDR DALA2026032602008Fitting · not reportedDTE ERA 632268-14AD REV. ORIGINAL. REPLACEMENT OF CONTINUITY FITTING IS TIME LIMITED, REQUIRING DTE FOLLOW UP PRIOR TO 61,196 TFC. REVISE AND UPDATE ERA 632268-14AD WITH DTE RESULTS PRIOR TO 61,196 TFC. REFERENCE AIRBUS DOSSIER 81739836. ASSOCIATED AA 5311-01Mar 23, 2026 · N365NB · Airbus A319114 · Standard Practices/StructuresSDR DALA2026032602007Fitting · not reportedTE ERA 632195-14AD REV ORIGINAL. REPAIR AT MIRROR FITTINGS, AREA 3 IS TIME LIMITED, REQUIRING DTE FOLLOW UP PRIOR TO 91,696 TFC. REVISE AND UPDATE ERA 632195-14AD WITH DTE RESULTS, PRIOR TO 91,696 TFC. ASSOCIATED AA 5311-01226 ADDED FOR AC 3165 ASSOCIATED ER/Mar 23, 2026 · N365NB · Airbus A319114 · Standard Practices/StructuresSDR DALA2026032602006Not Reported · not reportedINSPECTION ERA 632195-14AD REV. ORIGINAL. REPAIR OF WINDSHIELD FRAMING AREA 2 REQUIRES FOLLOW-ON INSPECTIONS PRIOR TO 58,696 TFC AND EVERY 4,700 FC, THEREAFTER. ACCOMPLISH FOLLOW-ON INSPECTIONS PER ERA 632195-14AD SECTION II PRIOR TO 58,696 TFC AND EVERY 4,70Mar 23, 2026 · N365NB · Airbus A319114 · Standard Practices/StructuresSDR DALA2026032401961Skin · corrodedSHIP 3164 DISC: RH WING TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 11+140MM SKIN WITH CORROSION. NOTE: WAS FOUND DURING THE PROCESS OF ORNRC 600-126. C/A: PERFORMED REPAIR AT RH WING TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 11+140Mar 23, 2026 · N364NB · Airbus A319114 · Wing, Plate/SkinSDR DALA2026032401960Skin · corrodedR/H WING, TOP SKIN, PANEL 2, LOWER SURFACE, T/E OVERHANG WITH CORROSION AT RIB 15 AREA. C/A: PERFORMED REPAIR AT RH WING TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 15 (AREA 4) I.A.W ER/A NO. 632748-14AD REV ORIGINAL DATED 21-MAR-26. THIS IS A MAJMar 23, 2026 · N364NB · Airbus A319114 · Wing, Plate/SkinSDR DALA2026032301930Generator · faultedDUE TO LOSS OF BOTH ENGINE GENERATORS (ELEC GEN 1 FAULT AND ELEC GEN 2 FAULT ECAM WARNINGS), RAT DEPLOYED, AND APU GENERATOR RUNNING, #2 GENERATOR RECOVERED. CORRECTIVE ACTION: FOUND IDG #1 OVERSERVICED IN THE RED BAND. MAINTENANCE STILL IN PROGRESS. (LP: 8427Mar 22, 2026 · N334NB · Airbus A319114 · AC Generator-AlternatorSDR DALA2026032602018Skin · corrodedER/A 632748-14AD ISSUED FOR REPAIR AND REWORK TO RH WING TRAILIN G EDGE SKIN CORROSION. FOLLOW ON ACTION REQUIRED. C/A: PERFORM SECTION IV EVERY SOONER OF 12200FC OR 24500FH AFTER SECT ION I. ASSOCIATED ER/A 14-632748 ADDED FOR AC 3164. (LP: 1505733)Mar 21, 2026 · N364NB · Airbus A319114 · Wing, Plate/SkinSDR DALA2026032602019Skin · corrodedER/A 632748-14AD ISSUED FOR REPAIR AND REWORK TO RH WING TRAILIN G EDGE SKIN CORROSION. FOLLOW ON ACTION REQUIRED. C/A: PERFORM SECTION III EVERY SOONER OF 15000FC OR 30000FH AFTER SEC TION I. ASSOCIATED ER/A 14-632748 ADDED FOR AC 3164. (LP: 1505729)Mar 21, 2026 · N364NB · Airbus A319114 · Wing, Plate/SkinSDR DALA2026032401959Skin · corrodedER/A 632748-14AD ISSUED FOR REPAIR OF CORROSION TO RH WING TRAIL ING EDGE SKIN. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION V EVERY SOONER OF 15000FC OR 30000FH AFTER SECTI ON I.Mar 21, 2026 · N364NB · Airbus A319114 · Wing, Plate/SkinSDR DALA2026032401958Skin · corrodedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR OF RH WI NG TRAILING EDGE SKIN CORROSION PER ER/A 632748-14AD. C/A: SECTION I IS LIMITED TO SOONER OF 60000FC / 120000FH. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE.Mar 21, 2026 · N364NB · Airbus A319114 · Wing, Plate/SkinSDR DALA2026032401957Skin · damagedER/A 632748-14AD ISSUED FOR RH WING TRAILING EDGE SKIN CORROSION REWORK. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II EVERY SOONER OF 10000FC OR 20000FH AFTER SECTION I.Mar 21, 2026 · N364NB · Airbus A319114 · Wing, Plate/SkinSDR DALA2026032201925Shear Plate · corrodedCORROSION SHEAR PLATE LOCATED BTW FR 69 TO FR 70 AT LEVEL STR 23L AT AFT GALLEY AREA. C/A: REPLACED SHEAR PLATE, AND FASTENERS LOC BTW FR69TO FR70 STR 23L AFT GALLEY AREA AS PER A319 SRM 51-72-11, SRM 51-42-11 AND DWG: D53474180 ISSUE: AA RELEASE DATE: 09/SEP/Mar 21, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026032201924Floor Support · corrodedCORROSION FLOOR STRUCTURE ON FRAME WEB LOC BTW FR69 TO FR70 STR23RH SIDE IN PASSENGER CABIN. C/A: REPLACED FRAME WEB, AND FASTENERS LOC BTW FR69 TO FR70 STR 23 RH SIDE IN PASSENGER CABIN AS PER A319 SRM 51-72-11, SRM 51-42-11 AND DWG: D53474180 ISSUE: AA RELEAMar 21, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026032201923Floor Support · corrodedCORROSION FLOOR STRUCTURE ON FRAME WEB LOC BTW FR 69 - FR 70, STR 23L SIDE IN PASSENGER CABIN. REPLACED FRAME WEB, AND FASTENERS LOC BTW FR 69 TO FR 70 STR 23L, PASSENGER CABIN IAW SRM 51-72-11, SRM 51-42-11 AND DWG D53474180, ISSUE AA. MEASURES OF CORROSIOMar 21, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026032201922Shear Plate · corrodedCORROSION SHEAR PLATE LOCATED BTW FR 69 TO FR 70 AT STR 23R, AFT GALLEY AREA. REPLACED SHEAR PLATE AND FASTENERS LOC BTW FR 69 TO FR 70, STR 23R AFT GALLEY AREA IAW SRM 51-72-11, SRM 51-42-11, AND DWG D53474180, ISSUE AA, MEASURES OF CORROSION ON SHEAR PLAMar 21, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026032201926Unknown · odorSULPHUR, FOUL ODOR ON TAXI OUT. STRONG, ENTIRE CABIN. FELT IN THROAT, NO PERCEPTIBLE VISUAL CUES. LASTED 5-10 MINS. RAN FUMES QRH. SEEMED TO IMPROVE WITH AIR/COND FUMES SUSPECTED PROCEDURE. NO APU AND ON ENGINES PACK/BLEEDS FOR AT LEAST 10 MINS. CHEMICAL SMELLMar 20, 2026 · N352NB · Airbus A319114 · Air Distribution SystemSDR DALA2026032201921Angle · corrodedNR 1 ENGINE INBD AND OTBD THRUST REVERSERS T/E HEAT SHIELD SUPPORT ANGLES WITH CORROSION. FOUND DURING PROCESS OF ORNRC N 131. REPLACED ANGLES RADIAL REAR P/N: 321-162-001-6 (2EA) AT ENGINE 1 INBD AND OTBD TRUST REVERSE IAW SPM (GFM) 70-43-31-390-005, PARAGMar 20, 2026 · N364NB · Airbus A319114 · Engine Thrust ReverserSDR DALA2026032201927Oven · odorOVEN TURNED OFF, SERVICE MESSAGE SAID MOTOR ISSUE. STRONG BURNT SMELL PRESENT. NO VISIBLE REASON. DUE TO BURNT SMELL FROM OVEN. R/R FWD GALLEY OVEN PER A319 AMM 25-35. RAN OVEN FULL CYCLE. OPS CHECK GOOD. NO SMELL OR FAULT NOTED. PINS/CONNECTOR BEHIND OVEN CHMar 19, 2026 · N329NB · Airbus A319114 · Buffet/GalleysSDR DALA2026031901895Angle · corrodedNR 1 ENGINE AFT PYLON ACCESS PANEL # 476BR AFT I/B CUT-OUT ANGLE WITH CORROSION. REPLACED ANGLE P/N: ATTACHED WITH SOLID RIVETS IAW A319 BSRM 51-72-11-911-001 PARAG B AND 51-42-11-801 2E (2) ( REV 155 DATED 17/NOV/25) AND REF DWG D545 10054 ITEM 32 ISSUE U. (Mar 18, 2026 · N364NB · Airbus A319114 · Nacelle/Pylon Miscellaneous StructureSDR DALA2026031901897Uplock Sensor · faultyON TAKEOFF, NLG DID NOT RETRACT. RESET IAW ECAM. CONTACTED MX DISPATCH & ELECTED TO CONTINUE MLG NOT UPLOCKED ECAM. SECONDARY INDICATION WERE SIGNIFICANT BUFFETING THAT WENT AWAY WHEN ECAM CLEARED. AMPLE NLG SENSOR HISTORY LGCIU 1&2 BITE TEST GOOD. T/S IAW TSMar 17, 2026 · N347NB · Airbus A319114 · Landing Gear Position and WarningSDR DALA2026031701840Unknown · hazeFA'S ADVISED SLIGHT HAZE IN CABIN ON TAXI IN. THRUST REVERSERS WERE HELD OUT TO MAX REVERSE UNTIL ROUGHLY 45-50KN DUE TO RUNWAY CONDITIONS. NO ODOR NOTICED BY FA'S. SMOKE & FUMES REPORT COMPLETED. C/A: CONFERRED WITH MCC, DUE TO THIS SPECIFIC EVENT BEING REPORMar 15, 2026 · N359NB · Airbus A319114 · Air Distribution SystemSDR DALA2026031701839Fitting · not reportedPERFORM ER/A 569090-14AD. C/A: COMPLIED WITH ER/A 631878-14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON PRI 631878-14AD REV.0 IT HAS BEEN VALIDATED. PERFORMEDREPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUITY FITTINGS LH AND RH AS PER ERA 6Mar 15, 2026 · N327NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026031701838Fitting · not reportedPERFORM ER/A 631878-14AD CONTINUITY FITTINGS REPLACEMENT. C/A: COMPLIED WITH ER/A 631878-14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON PRI 631878-14AD REV.0 IT HAS BEEN VALIDATED. PERFORMEDREPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUITYMar 14, 2026 · N327NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026031701837Fitting · not reportedPERFORM ER/A 631878-14AD CONTINUITY FITTINGS REPLACEMENT. COMPLIED WITH ER/A 631878-14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON PRI 631878-14AD REV.0 IT HAS BEEN VALIDATED. PERFORMEDREPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUITY FITTMar 14, 2026 · N327NB · Airbus A319114 · Fuselage Main, Structure
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