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 DALA2026031401776Unknown · odorAFT FA REPORTED SUSPICIONS SMELL COMING FROM GASPER CENT JUST ABOVE COFFEE MAKERS. INSP AFT GALLEY AREA, NO ABNORMAL ODOR PRESENT RAN ENGINES ISOLATED BOTH PACKS, ENG AND APU BLEED SOURCES, NO ODORS NOTED. REF W/C 0550-2002 , TYPE 9. A/C OK TO CONTINUE. (LP: Mar 14, 2026 · N368NB · Airbus A319114 · Air Distribution SystemSDR DALA2026031301774Seat Track · corrodedCORROSION ON THE SEAT TRACK +Y1292 AT FWD GALLEY AREA (SSI:531189). REPLACED THE SEAT TRACK Y1292 LOC. BTW FR 12 TO FR 24 AT FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11. (LP 1491705)Mar 12, 2026 · N327NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026031301773Floor Support · corrodedCORROSION FLOOR SUPPORT -Y1292.0, BTW FR 66 TO FR 68 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR SUPPORT - Y1292.0, BTW FR 66 TO FR68 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72-11. (LP 1491698)Mar 12, 2026 · N327NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026031301775Wire Harness · faultedATB - DUE TO LANDING GEAR WILL NOT RETRACT, L/G SHOCK ABSORBER FAULT, L/G DOORS NOT CLOSED, AND L/G GEAR NOT UPLOCKED ECAM WARNINGS. REPLACED NLG UPPER HARNESS 2M, PROX SENSOR 25GA, LGCIU2, AND SERVICED NLG SHOCK ABSORBER PER AMM 12-12. (LP 8416394, 8416398)Mar 11, 2026 · N302NB · Airbus A319114 · Landing Gear System WiringSDR DALA2026031101673Actuator · leakingDURING TAXI OUT, STRONG FUME ODOR FILLED THE FLIGHT DECK. FO DID NOT NOTICE (BUT SAID HE HAS BAD SENSE OF SMELL) STRONGER ODOR AFTER PARKING AT GATE. SMELLED LIKE EXHAUST NOTICED ON ARRIVAL PREV FLIGHT A SMELL BUT IT WAS QUICK AND I WASN'T SURE OR WAS ABLE TO Mar 10, 2026 · N322NB · Airbus A319114 · APU Engine Fuel and ControlSDR DALA2026031101672Skin · misrepairedDURING THE INSPECTION OF EXISTING MAJOR REPAIR AT LOWER FUSELAGE FR1 BL0 (INTERNAL SIDE) BETWEEN FR1 AND FR2 / LBL12 TO RBL 12. SEVERAL FASTENERS (3EA) ARE LOCATED IN THE CHEM MILLED RADIUS AREA THAT ARE NOT SPOT FACED. REFERENCE DELTA AIR LINES ER/A 548858-14Mar 10, 2026 · N365NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2026031101671Skin · misrepairedDURING THE INSPECTION OF EXISTING MAJOR REPAIR AT LOWER FUSELAGE FR1 BL0 (INTERNAL SIDE). ONE FASTENER LOCATED 11 ROWS OUTBOARD (LEFT) OF THE FILLER CUTOUT AND 3 ROWS AFT OF FORWARD BULKHEAD IS SPOT FACED BUT DOES NOT MEET THE SRM REQUIREMENTS (EDGES ARE NOT BMar 10, 2026 · N365NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2026031101670Seat Track · corrodedUPPER FUSELAGE,FR 16,Y+1292,LH LONGITUDINAL BEAM WITH CORROSION. REPLACED SEAT TRACK BTW FR12 THRU FR24 AT Y+ 1292 IAW SRM 51-72-11-911-001 REV 155.00 AND DWG D53112812.Mar 10, 2026 · N364NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026031001636Control Box · faultySHIP 3149 DSC: AFTER T/O AUTO FLT RUD TRV LIM SYS ECAM MESSAGE. FOLLOWED THE ECAM RESET PROCEDURE BUT THAT WAS NOT SUCCESSFUL. T/S PER A319 TSM 22-61-00-810-803-A. FOUND FAULT FAC 1/RTL ACTR 4CC. UNABLE TO RESET/HARD FAULT. NEXT STEP IS TO R/R ELECTRONIC MODUMar 10, 2026 · N349NB · Airbus A319114 · Rudder Control SystemSDR DALA2026031001635Light · faultedEMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:604 / EMERGENCY FLOORING LIGHTS AND CEILING LIGHTS ILLUMINATION AS THE GEAR COMES UP ON TAKEOFF. A RED CEILING LIGHT STAYS ILLUMINATED UNTIL THE GEAR IS DOWN FOR LANDING. / INTERIOR. C/A: PERFORMED OPMar 7, 2026 · N323NB · Airbus A319114 · Emergency LightingSDR DALA2026031001634Fitting · damagedDURING CURRENT M2 FRONT WINDSHIELD FRAMES SCHEDULED TO BE REPLACED PER ER/A 569090-14AD REV A, HOWEVER MIRROR FTG REPAIR WAS FOUND FEASIBLE. MIRROR FTG REPAIR INSTALLED PER THIS ER/A 569090-14AD REV B. PER SECTION IV OF 56909014AD REV B ACCOMPLISH SECTION IV Mar 5, 2026 · N327NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026031001633Window Frame · damagedDURING CURRENT M2 FRONT WINDSHIELD FRAMES SCHEDULED TO BE REPLACED PER ER/A 569090-14AD REV A, HOWEVER MIRROR FTG REPAIR WAS FOUND FEASIBLE. MIRROR FTG REPAIR INSTALLED PER THIS ER/A 569090-14AD REV B. C/A: *DTE* PER SECTION DTE OF 569090-14AD REV B THE REPAIRMar 5, 2026 · N327NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026030801586Fitting · damaged1 RPTD BY BAMBERG 00197334 SAL 05MAR26 ENTR 00197334 S DURING CURRENT M2 FRONT WINDSHIELD FRAMES WERE SCHEDULED TO BE REPLACED PER ER/A 569090-14AD REV A, HOWEVER MIRROR FTG REPAIR WAS FOUND FEASIBLE. THIS ER/A IS ISSUED TO REPLACE CONTINUITY FTGS IN CONJUNCTIMar 5, 2026 · N327NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026030801585Floor Support · corrodedCORROSION FLOOR SUPPORT -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLE Y AREA (SSI 534147). REPLACED FLOOR SUPPORT - Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72-11 AND DWG D53472189, DWG D53472089, DWG D53474250. MEAMar 5, 2026 · N327NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026030801584Shear Tie · corrodedCORROSION INTERNAL STRUCTURE SHEAR TIE FR30 STE40R TO STR41R IN FWD CARGO COMPARTMENT. REPLACED SHEAR TIE LOCATED FR30 AND STR40R TO STR41R IN FWD CARGO COMPARTMENT IAW SRM 51-42-11, SRM 51-72-11 AND DWG D53233211 ISSUE: D00 RELEASE DATE: 28-MAY-98 TOOK MEASUMar 5, 2026 · N327NB · Airbus A319114 · Fuselage Internal Mounting StructureSDR DALA2026030801583Floor Support · corrodedCORROSION FLOOR SUPPORT -Y1292 BTW FR 66 TO FR 68 AT AFT GAL LEY AREA (SSI 534147). C/A: REPLACED FLOOR SUPPORT -Y1292 LOCATED BTW FR66 TO FR68 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 DWG D53472172 RELEASE DATE :24/NOV/22 ISSUE : K, DWG Mar 4, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026030801582Floor Support · corrodedCORROSION FLOORBEAM -Y765 LOCATED AT FR 68 AT AFT GALLEY AREA (SSI 5 34147). REPLACED FLOOR BEAM -Y765 AND FASTENERS LOCATED AT FR 67 TO FR 70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72- 11, DWG D53472816, DWG D53478309 AND DWG D53472093. TOOMar 4, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026030801581Seat Track · corrodedSHIP 3165 DISC: CORROSION SEAT TRACK -Y765 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 5 31189 ). C/A: REPLACED SEAT TRACK -Y765 LOCATED BTW FR12 TO FR24 FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG D53112812, ISSUE: E00, RELEASE DATE: 08/JAN/Mar 4, 2026 · N365NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026030801587Tailpipe · fireTAILPIPE FIRE ON ENG 2. INFORMATION WAS FORWARDED FROM ANOTHER CREW ALL START INDICATIONS ON ECAM NORMAL. PERFORMED FADEC 2A/B OP TEST PER A319 AMM-NO FAULTS NO LAST LEG FAULTS.RAN ENGINE 2 PER A319 AMM 71-00-00 NO DEFECTS. (LP: 8280298)Mar 3, 2026 · N361NB · Airbus A319114 · Engine Collector/Tailpipe/NozzleSDR DALA2026030801580Floorbeam · damagedMISSING MATERIAL FLOOR BEAM LOCATED BTW FR 20 TO FR 21 AND - Y 250 AT FWD GALLEY AREA. REPLACED FLOOR BEAM -Y189 AND FASTENERS LOCATED BTW FR20 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DWG D53111406 RELEASE DATE: 20/DEC/96 ISSMar 3, 2026 · N365NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2026030801579Fitting · damagedENGINE NR 2 PYLON FOUND SPIGOT LOWER FITTING AND SPIGOT BALL JOINT DAMAGE. REPLACED ENGINE # 2 PYLON SPIGOT LOWER FITTING AND SPIGOT BALL JOINT IAW SRM 54-51-12. REPLACED #2 PYLON LOWER SPIGOT FITTIN G IAW A319 SRM TASK 54-51-12-300-001 REV 155 DATED 17 NOV 2Mar 3, 2026 · N364NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA2026030801578Fitting · damagedENGINE NR 1 PYLON FOUND SPIGOT LOWER FITTING AND SPIGOT BALL JOINT DAMAGE. REPLACE ENGINE NR 1 PYLON SPIGOT LOWER FITTING AND SPIGOT BALL JOINT IAW SRM 54-51-12. (LP: 1477390)Mar 3, 2026 · N364NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA2026030801577Seat Track · corrodedUPPER FUSELAGE, FR 16, Y+765, LH LONGITUDINAL BEAM WITH CORROSION. REPLACED SEAT TRACK AT UPPER FUSELAGE, BETWEEN FR12 AND FR24, Y+765 IAW A319 SRM 53-11-15-01A FIGURE 001, ITEM 015-A REV 155.00 DATED 17/NOV/25 AND REFRENCE AIRBUS DWG #D53112813, ISSUE B, ITEMMar 3, 2026 · N364NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026031901901Strut · corrodedCORROSION ON INTERCONNECTING STRUTS LH. REMOVED INTERCONNECTING STRUTS L/H P/N:D5757032201100, S/N: 02370 ON UNSERVICEABLE CONDITION AS PER FAM AMM 27-51-44- 000-001-A EXCEPT STEP 3.D.(2). JOB IN PROGRESS. REPLACED INTERCONNECTING STRUT ON LH WING AS PER A320Mar 2, 2026 · N365NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2026031901896Strut · corrodedCORROSION ON INTERCONNECTING STRUTS RT. REMOVED INTERCONNECTING STRUTS IAW AMM 27-51-44- 000-001-A EXCEPT STEP 3.D.(2). REPLACED INTERCONNECTING STRUT IAW AMM 27 -51-44-000-001-A AND AMM 27-51-44-400-001-A,Mar 2, 2026 · N365NB · Airbus A319114 · Wing Main, Frame StructureSDR DALA2026030301461Seat Track · corrodedCORROSION SEAT TRACK -Y1292 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 531189). REPLACED SEAT TRACK -Y1292 LOCATED BTW FR12 TO FR24 FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11, DWG D53110984, DWG D53110920, DWG D53112812, AND DWG D53918124. TOOK MEASUREMar 1, 2026 · N365NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026030301460Stringer · corrodedCORRODED STRINGER 42R BTW FR29 TO FR30 IN FWD CARGO COMPARTMENT. REPLACED DOUBLER STRINGER 42R AND FASTENERS.LOC BTW FR28 TO FR34 IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11, DWG: D53233523, RELEASE DATE:21/OCT/98, ISSUE: D00 AND DWG: D53230319 , RELEASFeb 28, 2026 · N327NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2026030401477Door · malfunctionedLANDING GEAR DOORS NOT CLOSED, RT DOOR CLOSED, PROXIMITY SENSOR (26GA)TGT POS, LGCIU 1, RT DOOR CLOSED, PROXIMITY SENSOR (28GA) TGT POS, LGCIU 2. FOLLOW TSM TASK 32-31-00-810-861-A. (LP: 1470853)Feb 27, 2026 · N369NB · Airbus A319114 · Landing Gear Door Retract SectionSDR DALA2026030301462Harness · brokenOXYGEN PANEL AT ROW 27 ABC DID NOT DROP WHILE WORKING CARD 2527- 01041-02. FOUND JUMPER BETWEEN SPEAKER AND PSU, BROKEN. REMOVED SND REPLACED JUMPER HARNESS IAW AMM 25-25-23. OPS CHECK GOOD. (LP: 8464026)Feb 27, 2026 · N314NB · Airbus A319114 · Oxygen System WiringSDR DALA2026030301459Shear Tie · corrodedCORROSION INTERNAL STRUCTURE ON SHEAR TIE FR30 LOC STR41R TO STR42R IN FWD CARGO COMPARTMENT. REPLACED SHEAR TIE AND FASTENERS ON FR30 LOC STR41R TO STR42R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11-801, SRM 51-72-11 AND DWG: D53230337, ISSUE:DO0 RELEAFeb 27, 2026 · N327NB · Airbus A319114 · Fuselage Internal Mounting StructureSDR DALA2026030301458Shear Tie · corrodedCORROSION INTERNAL STRUCTURE SHEAR TIE FR28 STR41R TO STR42R IN FWD CARGO COMPARTMENT. FINAL REPAIR RESOLUTION: ADDED INFORMATION REQUIRED.REPLACED SHEAR TIE AND FASTENERS ON FR28 STR41R TO STR42R IN FWD CARGO BAY IAW SRM 51-42-11-801, SRM 51-72-11 AND DWG: DFeb 27, 2026 · N327NB · Airbus A319114 · Fuselage Internal Mounting StructureSDR DALA2026030301457Beam · corrodedUPPER FUSELAGE, FR 67+530MM, Y-1162, RH LONGITUDINAL BEAM WITH CORROSION. REPLACED LONGITUDINAL BEAM BETWEEN FR67+530MM AND FR68, Y-162 IAW A319 SRM 53-41-14-03A FIGURE 303, ITEM 145A AND SRM 51-72-11-911-001 PARAG C, REV 155.00 AND AIRBUS DWG D53472780 ITEM Feb 27, 2026 · N364NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026030301456Web · crackedUPPER FUSELAGE, FR 68+180MM, LH LATERAL WEB WITH CRACK. REPLACED LATERAL WEB IAW SRM 51-72-11- 911-001 AND SRM 53-41-14-804A PAGE 24, ITEM 20 REV 155.00 AND DWG D534480505 SHEET 38, ITEM 339 AND 266 ( ISSUE EG) AND ITEM 142. (LP: 1470915)Feb 27, 2026 · N364NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026030301455Beam · corrodedUPPER FUSELAGE, FR 69+490MM, Y-160, LONGITUDINAL BEAM WITH CORROSION. REPLACED LONGITUDINAL BEAM P/N D5347219720000 BETWEEEN FR68 ANF FR7, Y-160 IAW IAW A319 SRM 53-41-14-03A FIGURE 303, ITEM 165 AND SRM 51-72-11-911-001 PARG C. (REV 155.00 DATED 17 NOV 25) AFeb 27, 2026 · N364NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026022701382Floor Support · corrodedCORROSION FLOOR SUPPORT -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR SUPPORT -Y1162.5 AND FASTENERS LOC FR68 TO FR 69 AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG: DWG D53472780 RELEASE DATE: 26/APR/Feb 26, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026022701380Seat Track · corrodedCORROSION SEAT TRACK +Y1292 LOCATED AT FR 66 AT AFT GALLEY AREA (SSI 534147). REPLACED SEAT TRACK Y1292 LOCATED AT FR64 TO FR 66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG :10N01048 , ISSUE: F. RELEASE DATE: 19-MAY-15, MEASURE OF CORRFeb 26, 2026 · N327NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026022701383Tailpipe · fireAT THE GATE, START WITH GND CART SUPPLYING AIR, RAMP PERSONNEL REPORTED POSSIBLE TAILPIPE FIRE NR 1 ENG. ALL SIGNS OF FLAME WENT OUT UPON ENGINE GETTING TO IDLE. NO CREW INTERACTION OR COCKPIT INDICATIONS WERE REPORTED. T/S PER AMM 71-00-00-869-001A, ANY FLAFeb 25, 2026 · N337NB · Airbus A319114 · Engine Collector/Tailpipe/NozzleSDR DALA2026022701381Wire · brokenFOUND PROXY LIGHT OUT AT SEATS 26 & 27 DEF. FOUND NO POWER AT 26&27 D.E.F. FOUND POWER AT 9158VC, FOUND BROKEN WIRE AT 9158VCA IN B POSITION. RE-TERMINATED AT SAME LOCATION. LIGHT OP CHK NORMAL PER A319 AWM 33-51 & ESPM 28-48& AMM 33-51. (LP: 8243511)Feb 25, 2026 · N320NB · Airbus A319114 · Light System WiringSDR DALA2026022701379Fitting · corrodedCORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-300-001 AND AS PER A319 SRM 54-51-12-283-001 PARAGRAPH 2. FIGURE 001 SHEET 1 AND 2. FOUND BEYOND OUT MEASURED OF LIMITS TOOL USED CALIPER Feb 25, 2026 · N365NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA2026022701378Floor Support · corrodedCORROSION FLOOR BEAM LOCATED BTW FR 16 TO FR 18 AND Y254 AT FWD GALLEY AREA (SSI 531189). FINAL REPAIR RESOLUTION: REPLACED FLOOR BEAM Y254 LOCATED BETWEEN FR12 TO FR24 FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG.D53110920 ISSUE: E00 RELEFeb 25, 2026 · N327NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026022501345Proximity Sensor · faultedUPON GEAR RETRACTION NOSE GEAR REMAINED UNLOCKED AND DOORS OPEN, STAYED BELOW 220 AND RECYCLED PER OCAM DIRECTION. ACHIEVED NORMAL GEAR INDICATION AFTER RECYCLE. REPLACED PROXIMITY SENSOR 13GA IAW AMM 32-31. OPS CHKD GOOD. (LP 8130180)Feb 25, 2026 · N347NB · Airbus A319114 · Landing Gear Position and WarningSDR DALA2026022701377Dampener · no testAIRCRAFT 3165, DONT PASS OPERATIONAL TEST PASSENGER CREW DOOR 841 DOOR DAMPER (REFER TO AMDS CARD 5210-7089-RF (RII)) AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR 841 EMERGENCY DAMPER PN: FE240-004, SN: 3977 AS PER A320 FAM AMM 52-11-14-Feb 23, 2026 · N365NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA2026022401326Skin · bulgedLOWER FUSELAGE FR66, STR39L POTABLE WATER SERVICE PANEL FWD LOWER CORNER WITH BULGED SKIN AND SOLID RIVETS WITH CORROSION. CORRECTIVE ACTION: REPLACED POTABLE WATER SERVICE PANEL INTERNAL REINFORCEMENT DOUBLER P/N D5348011420800 PER SRM 51-72-11-911-001 AND 51Feb 23, 2026 · N331NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2026022401325Skin · bulgedLOWER FUSELAGE FR66 BETWEEN STR 38R-39R (WASTE) TOILET SERVICE PANEL AFT LOWER CORNER WITH BULGED SKIN. CORRECTIVE ACTION: REPLACED (WASTE) TOILET SERVICE PANEL INTERNAL REINFORCEMENT DOUBLER P/N D5348011521201 PER SRM 51-72-11-911-001 AND 51-42-11- 801-PARG 2Feb 23, 2026 · N331NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2026022401324Floorbeam · corrodedCORRODED FLOORBEAM LOCATED BTW FR 18 - FR 20, -Y 254 AT FWD GALLEY AREA. REPLACED FLOORBEAM, FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11, & DWG D53111462. (LP 1464261)Feb 23, 2026 · N327NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2026022301262Shear Web · corrodedAIRCRAFT 3131, AFT CABIN, BETWEEN FR 69-70, RH FLOOR SHEAR WEB WITH CORROSION. CORRECTIVE ACTION: REPLACED SHEARPLATE P/N: D5347112420300 I/A/W A319 SRM 51-72-11-911-001 REV 155.00, DATED 17 NOV 25 AND AIRBUS REF.DWG#D53474180. (LP 1463318)Feb 22, 2026 · N331NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026022301263Warning Message · illuminatedDECLARED EMERGENCY DUE TO A CABIN DIFFERENTIAL PRESSURE LOW MESSAGE FOLLOWED BY A CABIN PRESSURE SAFETY VALVE OPEN MESSAGE. NO TROUBLE FOUND. ECS-19 REPORT GENERATED SHOWS THAT AIRCRAFT AND CABIN ALTITUDE WERE EQUAL AT MESSAGE OCCURRENCE. PASSENGER MASKS WERFeb 20, 2026 · N357NB · Airbus A319114 · Cabin Pressure Control SystemSDR DALA2026022101252Seat Track · corrodedAIRCRAFT 3127, CORROSION SEAT TRACK -Y1292 AT FWD GALLEY AREA (SSI:531189). CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1292 AND FASTENERS BTW FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DWG D53110920. (LP 1460565)Feb 20, 2026 · N327NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026022001233Seat Track · corrodedAIRCRAFT 3131, UPPER FUSELAGE, PAX CABIN, FR 64 TO FR 66 Y=1292 WET AREA SEAT TRACK CORRODED. CORRECTIVE ACTION: REPLACED SEAT TRACK P/N: 14N00031-101 AT FR64 TO FR66 Y=1292 WET AREA DUE TO CORRODED OUT- LIMITS IAW A319 SRM 51-72-11-911-001 REV 155.00 DATED 17Feb 19, 2026 · N331NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026022001232Fitting · crackedAIRCRAFT 3131, FLIGHT DECK, WINDSHIELD FRAMING, LT / RT CONTINUITY FITTING CRACKED. CORRECTIVE ACTION: REPLACED CONTINUITY FITTINGS (LH P/N D53111077202009) (RH P/N D5311107720300) IAW DELTA ERA 631770-14AD REV ORIGINAL DATED 10-FEB-26 AND REPAIR DWG R531-1291Feb 19, 2026 · N331NB · Airbus A319114 · Fuselage Main, Structure
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