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 DALA2026012900702Receptacle · corrodedCORROSION BORE SPIGOT FITTING RECEPTACLE ON RT PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RT PYLON IAW SRM 54-51-12-300-001, & SRM 54-51-12-283-001. FOUND BEYOND LIMITS, MEASUREMENT OF CORRODED AREA: D: 0.0042 INCH & OF DIAMETER IS 4.348 INCH. (LP: 141796Jan 24, 2026 · N359NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA2026012900700Anchor Fitting · corrodedLEFT WING, REAR SPAR, MAIN LANDING GEAR ACTUATOR, ANCHOR FITTING CORRODED. REPLACED THE ANCHOR FITTING AT LT WING REAR SPAR IAW EO 631312-14, REV 00. AND RA 631312-14AD, REV ORIGINAL APPROVED AND DOCUMENTED ON AIRBUS FORM RDAF REF AND ISSUE 81713336/03/2025Jan 24, 2026 · N349NB · Airbus A319114 · Wing, Landing Gear Attach FittingsSDR DALA2026012600542Seat Track · damagedPASSENGER CABIN SEAT TRACK AND SPLICES WITH ELONGATED HOLES AT FR64, +Y=1292. PERFORMED PERMANENT REPAIR ON UPPER FUSELAGE PASSENGER CABIN SEAT TRACK SECTION AND SPLICES BETWEEN 160MM AFT FR62 AND FR64, AT Y=1292 IAW ER/A #631509-14 REV: ORIGINAL THIS IS A MAJan 24, 2026 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026012600541Fitting · damagedAVIONICS RACK 80VU L/H LOWER LATERAL FITTING WITH MATERIAL BURRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. C/A: PERFORMED MAJOR REPAIR ON FWD FUSELAGE EQUIPMENT / RACK 80VU LH LOWER LATERAL SUPPORT DUE TO MATERIAL BURRED (OVALJan 24, 2026 · N349NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026012600540Fitting · damagedAVIONICS RACK 80VU RT LOWER LATERAL FITTING WITH MATERIAL BURRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. PERFORMED MAJOR REPAIR ON FWD FUSELAGE EQUIPMENT 1 RACK 80VU RT LOWER LATERAL SUPPORT DUE TO MATERIAL BURRED (OVALIATIOJan 24, 2026 · N349NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026012600548Floor Panel · corrodedCORROSION INSERT FLOOR PANEL 221PF IN PASSENGER CABIN. C/A: COMPLIED WITH ER/A 631181-14 REV ORIGINAL APPROVED DATE: 06/JAN/ 26. MATCHES WITH ALL STEPS ON ER/A 631181-14 PRI REV.0 IT HAS BEEN VALIDATED. REPLACE FLOOR PANEL 221PF IN PASSENGER CABIN AS PER ER/A Jan 23, 2026 · N359NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2026012600547Post · corrodedCORROSION ON AFT LATERAL POST LAVATORY A AT FWD GALLEY AREA. COMPLIED WITH ER/A 631052-14 REV. A. APPROVED DATE: 16-JAN-26 MATCHES WITH ALL STEPS OF ER/A 631052-14 PRI REV. 0 AND REV 1 IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON AFT LATERAL POST LJan 23, 2026 · N359NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026012600545Frame · damagedDURING M2 PERMANENT REPAIR (REPLACEMENT OF FR16 LHS) IS DUE AS REQUIRED PER EXISTING LOG 0917237 OF ER/A 586145-14AD, REV C. C/A: *DTE* PER SECTION DTE-1 OF 586145-14AD, REV D, THE REPAIR OF SECTION IV IS LIMITED TO 6 MONTHS (180 DAYS) SERVICE FROM SECTION IV.Jan 23, 2026 · N359NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2026012600544Frame · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIRED & REPLACED FR16LH PER ER/A 631351-14AD. FOLLOW ON ACTION IS REQUIRED. SECTION I IS LIMITED TO 33500FC AFTER SECTION I. ER/A TO BE REVI SED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED EJan 23, 2026 · N349NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2026012600543Frame · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR AND FRAME REPLACEMENT OF FR16LH PER ER/A 631351-14AD. FOLLOW ON ACTION R EQUIRED. SECTION I IS LIMITED TO 69600FC AFTER SECTION I. ER/A TO BE REVI SED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSJan 23, 2026 · N349NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2026012600539Seat Track · corrodedUPPER FUSELAGE PAX CABIN, AFT ENTRY AREA FR 66 +Y1292 LT SEAT TRACK CORRODED. REPLACED THE SEAT TRACK IAW SRM SUPP 53-41-15, REV A. DRAWING # 14N000331, ER/A #631239-14 REV ORIGINAL AND AIPC 53-41-04-20E SHEET 1. REV 133.02.Jan 23, 2026 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026012600554Oxygen Mask · unwanted deployOXYGEN MASK DEPLOYED IN FRONT LAVATORY ONLY AFTER TAKE OFF. REPLACED AND STOWED O2 MASK IN FWD LAVATORY IAW AMM 35-12. ACFT OK FOR SERVICE. (LP: 7336862)Jan 22, 2026 · N318NB · Airbus A319114 · Passenger Oxygen SystemSDR DALA2026012600553Hmu · failedOBSERVED LARGE FLAMES EXITING NR 2 ROTOR ON START. TOWER CAM VERIFIED. NO COCKPIT/ECAM INDICATIONS. SHUTDOWN NR 2 AND TOWED BACK IN. R & R NR 2 ENGINE HMU IAW AMM 73-21. PERFORMED ENGINE IDLE LEAK CHECK. LEAK CHECKS GOOD. (LP: 8056744)Jan 22, 2026 · N361NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026012600546Repair · not reportedER/A 496231-14 REVISION B ISSUED FOR FUSELAGE SKIN REPAIR LOCATE D AT FR36 & S-4RH. FOLLOW ON ACTION IS REQUIRED. C/A: PERFORM SECTION II WITHIN SOONER OF 54200FC / 108400FH FROM SECT ION I AND EVERY SOONER OF 5000FC / 10000FH THEREAFTER. ASSOCIATED ER/A 14-49Jan 22, 2026 · N331NB · Airbus A319114 · Standard Practices/StructuresSDR DALA2026012300519Seat Track · corrodedAFT FUSELAGE FLOOR STRUCTURE AT FR66+90 MM Y-1292 MM LONGITUDINAL BEAM WITH CORROSION. REPLACED SEAT TRACK P/N: 14N00031-101 AT UPPER FUSELAGE PAX CABIN, AFT ENTRY AREA FR66+90MM, Y-1292MM RH SIDE IAW NAT STRUCTURAL REPAIR MANUAL SUPPLEMENT 53-41-15 REV A DATJan 22, 2026 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026012300518Support Arm · corrodedAFT FUSELAGE FLOOR STRUCTURE AT FR 68 Y1260 MM, SILL BEAM WITH CORROSION. PERFORMED REPAIR AT AFT FUSELAGE FLOOR STRUCTURE, FR68 Y12060MM, SILL BEAM IAW ER/A 631462-14 REV ORIGINAL DATED 16/JAN/26. THIS IS A MAJOR REPAIR CATEGORY A WITH NO ADDITIONAL REQUIREMJan 22, 2026 · N349NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026012200489Web · damagedELONGATED HOLE WEB FR 56 TO FR 57 AND STR 38L IN AFT CARGO BAY. REPLACED WEB AND FASTENERS LOC FR 56 TO FR 57 AND STR 38L IN AFT CARGO BAY IAW SRM 51-42- 11, SRM 51-72-11, AND DWG D53476318, ISSUE: N. (LP: 1413058)Jan 21, 2026 · N359NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026012200488Web · corrodedAFT FUSELAGE INTERNAL FLOOR STRUCTURE BTWN FR 69 & FR 70, S23L, WEB WITH CORRDED. REPLACED SHEAR PLATE IAW SRM 53-41-17-01A, FIGURE 001, ITEM 310A AND INSTALLED IAW DWG D534 74180, ISSUE U, SHEET 6.Jan 21, 2026 · N349NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026012300516None · noneER/A 627650-14 HAS BEEN REVISED TO REV A TO INCORPORATE STAGE III DTE. ER/A 627650-14 WAS ISSUED FOR EXISTING REWORK FOUND IN THE EXTERNAL LOWER SKIN LOCATED AT FR66. FOLLOW ON ACTION IS REQUIRED.Jan 20, 2026 · N330NB · Airbus A319114 · Standard Practices/StructuresSDR DALA2026012200487Structure · corrodedAFT FUSELAGE FLOOR STRUCTURE, BETWEEN FR67+300 MM & FR 67+ 480 MM , Y1160 MM LONGITUDINAL BEAMS CORRODED. REPLACED LONGITUDINAL BEAMS IAW SRM 51-41-03A, FIG 303, ITEMS 195A AND 190A INSTALLED IAW DWG D534 72780, ISSUE D, ITEMS 42, & 44. DWG D53472088, ISSUE FJan 20, 2026 · N349NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026012200486Seat Track · corrodedAFT CABIN SEAT TRACK AT FR 66, Y765 CORRODED. REMOVED AND EVALUATED CORROSION ON THE SEAT TRACK. FOUND TO BE OUT OF LIMITS, R & R THE SEAT TRACK FROM FR 64 - 66 IAW SRM 51-72-11-911-001. (LP: 1411425)Jan 20, 2026 · N358NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026012200485Seat Track · corrodedAFT CABIN SEAT TRACK, FR 66, Y1292 CORRODED. REMOVED AND EVALUATED THE SEAT TRACK, FOUND NO DAMAGE TO BE OUT OF LIMITS. R & R THE SEAT TRACK, FR 64 - 68, Y1292 IAW SRM 51-72-11-911-001. (LP: 1411421)Jan 20, 2026 · N358NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026012200484Seat Track · corrodedAFT CABIN SEAT TRACK AT Y-765 HAS CORROSION FROM FR 66 - FR 68. REMOVED AND EVALUATED CORROSION ON AFT CABIN FLOORBEAM AND SEAT TRACK FROM FR 64-68 AT Y-765 FOUND DAMAGE ON FLOORBEAM TO BE WITHIN LIMITS AND DAMAGE ON SEAT TRACK TO BE OUT OF LIMITS. R & R THJan 20, 2026 · N358NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026012200483Seat Track · corrodedAFT CABIN SEAT TRACK FR 66, Y-1292 CORRODED. REMOVED AND EVALUATED CORROSION ON AFT CABIN SEAT TRACK. FOUND DAMAGE TO BE OUT OF LIMITS. R & R THE SEAT TRACK FROM FR 64 - 66 IAW SRM 51-72-11-911-001.Jan 20, 2026 · N358NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026012200480Beam · corrodedAFT FUSELAGE FLOOR STRUCTURE AT FR 66+160 MM AT Y765 MM, LONGITUDINAL BEAM CORRODED. REPLACED LONGITUDINAL BEAM IAW SRM 51-72-11-911-001, REV 155, DWG D53472780, ISSUE H, & DWG D53472815, ISSUE E. (LP: 1409456)Jan 19, 2026 · N349NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026012200482Slide · low pressureRIGHT FWD DERVICE DOOR SLIDE HAS LOW PRESSURE. REMOVED AND REPLACED RIGHT FORWARD DOOR SLIDE IAW AMDS TC 2561-4004-RF. (LP: 9141074)Jan 17, 2026 · N325NB · Airbus A319114 · Escape SlideSDR DALA2026012200490Selector Valve · faultedBRAKES, AUTO BRAKE FAULT A SECOND TIME. LOST NORMAL BRAKING. HAD TO USE ACT BRAKING. DURING BRAKING THE ACFT JOLTED FWD. LOST BRAKES FOR 1-2 SECS, GRABBING AGAIN. DID NOT PULL TO EITHER SIDE. TROUBLESHOT IAW TSM 32-42-00-810-849-A. WHEN ACFT ARRIVED AT GATEJan 16, 2026 · N301NB · Airbus A319114 · Landing Gear Brake SystemSDR DALA2026012200481Window Frame · crackedDURING M2 & WHILE ACCOMPLISHING EM 5311-01226-01, CRACKS WERE FOUND IN LT & RT FRONT WINDSHIELD FRAMES, LWR CTR NODE AREA. PER SECTION DTE OF 630808-14 THE REPAIR OF SECTION I IS LIMITED TO 30,600 FC FROM SECTION I.Jan 16, 2026 · N359NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026011800404Wire Harness · shortedDURING PUSHBACK SAW ARCING COMING FROM WIRE GOING TO LEFT WINDOW. FOUND WIRE CHAFFED, DEACTIVATED WHC NR 1 PER AMM 30-42-00- 0404-001-A. AND APPLIED MEL 30-42-01 MCO & PLAC INSTALLED M PROC C/W DISP APPROVED. NR 1 WHC INOPERATIVE. FOUND VENDOR FURNISHED HARNJan 16, 2026 · N338NB · Airbus A319114 · Ice/Rain Protection System WiringSDR DALA2026011700394Apu · contaminatedODOR IN FLIGHT DECK WITH APU BLEED ON DURING PREFLIGHT. FOUND POSSIBLE DE ICE FLUID INJECTED INTO APU. (JH 924595) C/W LEVEL A AND B DECONTAMINATION IAW AMM 21-00-00. REPLACED RECIRC FILTERS. REF LOG 1403258. (LP: 8394134)Jan 16, 2026 · N326NB · Airbus A319114 · APU Core EngineSDR DALA2026011700393Unknown · fumesF/A REPORTED FUMES EVENT AFTER LANDING IN CABIN, SMELLED ELECTRICAL ODOR AND CABIN WAS HAZY, NO REPORTS IN COCKPIT. PERFORMED NO GO ODI, MSI PREVENTION PROGRAM ATA 21-72 SMOKE/ FUMES AND COMPLETED W/C 0550-2002 STEPS 1-4, INCLUDING TYPE 9 ELEC. SMOKE/ODOR IN Jan 15, 2026 · N341NB · Airbus A319114 · Air Distribution SystemSDR DALA2026011700389Not Reported · not reportedER/A 631013-14AD ISSUED FOR REPAIR 80VU RACK LOWER LATERAL FITTI NGS. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN 19500 FROM SECTION I AND EVERY 1000FC THEREAFTER. ASSOCIATED AA 2515-01014 ADDED FOR AC 3149. (LP: 1403132)Jan 15, 2026 · N349NB · Airbus A319114 · Standard Practices/StructuresSDR DALA2026011700388Seat Track · corrodedFWD CABIN SEAT TRACK AT FR20 AND Y-765 CORRODED. REMOVED AND REPLACED FWD CABIN FR 12-24 SEAT TRACK BEAM IAW SRM 51-72-11, 51-44-11 AND 51-42-11. JOB COMPLETE. (LP: 1403643)Jan 15, 2026 · N358NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026011700387Seat Track · corrodedFWD CABIN SEAT TRACK AT FR20 AND Y-1292 CORRODED. REMOVED AND REPLACED FWD CABIN SEAT TRACK-Y-1292, FR- 13F-FR24 R/H SIDE IAW A319 SRM 51-72-11-911-001 JOB COMPLETE. (LP: 1403195)Jan 15, 2026 · N358NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026011700386Floor Support · corrodedAFT CABIN FLOOR SUPPORT AT Y-1292 HAS CORROSION AND MISSING RIVET BETWEEN FR 68 AND FR69. REMOVED AND REPLACED AFT CABIN FLOOR SUPPORT AT Y-1292FR68-69 IAW SRM 51-72-11. JOB COMPLETE. (LP: 1403044)Jan 15, 2026 · N358NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026011700390Window Frame · crackedDURING M2 AND WHILE ACCOMPLISHING EM 5311-01226-01 CRACKS FOUND IN LT & RT FRONT WINDSHIELD FRAMES LWR CTR NODE AREA. *DTE* PER SECTION DTE OF 630808-14 THE REPAIR OF SECTION I IS LIMITED TO 30,600 FC FROM SECTION I (6JAN26). ADDITIONAL ENG'G AUTHORIZATION REJan 14, 2026 · N359NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026011500365Stop Fitting · damagedREPAIR PERFORMED ON FR 68 LT AT DOOR STOP FITTING NR 1 IAW ERA 631655-14, AND SRM 53-41-12-300-011. IAW SRM 53-41-12-205-010, REPEAT INSPECTIONS ARE REQUIRED. ACCOMPLISH ER/A 631655-14 SECTION II WITHIN 19,700FC FROM 21JUN25 (30,878FC). ASSOCIATED ER/A 00-6316Jan 14, 2026 · N335NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA2026011500364Seat Track · corrodedUPPER FUSELAGE PAX CABIN FLOOR STRUCTURE SEAT TRACK LOCATED AT FR 20 -Y1292 WITH CORROSION. REPLACED SEAT TRACK AT UPPER FUSELAGE FR20 - Y1292 IAW SRM 51-72-11-911-001 REV 155, & DRAWING D53112812 ISSUE E, D53110920 ISSUE E00, D53110984 ISSUE B AND D53918122 Jan 14, 2026 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026011500363Seat Track · corrodedUPPER FUSELAGE, PAX CABIN FWD ENTRY AREA, SEAT TRACK +Y765 LOCATED AT FRAME 20 WITH CORROSION. REPLACED SEAT TRACK AT FR20 +Y765 IAW A319 SRM 51-72-11-911-001 REV 155, AND DRAWING D53112812 ISSUE E, D53110920 ISSUE E00 AND ISSUE D AND D53110984 ISSUE B. (LP: Jan 14, 2026 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026011500362Seat Track · corrodedUPPER FUSELAGE, PAX CABIN FWD ENTRY AREA, SEAT TRACK -Y765 LOCATED AT FRAME 20 WITH CORROSION. REPLACED SEAT TRACK AT FR20 -Y765 IAW SRM 51-72-11-911-001, REV: 155. AND AIRBUS DRAWING D531 12812 ISSUE E, D531 10984 ISSUE B, D5311 10920 ISSUE E00 AND D539 18Jan 14, 2026 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026011500361Access Panel · corrodedTAIL CONE ACCESS PANEL NUMBER 317AL INTERNAL ANGLES WITH CORROSION. REPLACED TAIL CONE ACCESS PANEL 317AL INTERNAL ANGLES (2EA) IAW SRM 51-72-11-911-001 PARAG 2C REV 155, AND AIPC 53-58-04-05B SHEET 1 & 2 DETAIL H & J, REV 133.01, AND AIRBUS REFERENCE DWG D92Jan 14, 2026 · N349NB · Airbus A319114 · Aerodynamic FairingsSDR DALA2026011700392Light · damagedEMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:28D. SEAT BUSSEL THAT HOLDS LIGHT NEEDS TO BE REPAIRED & REPLACED. FWD (28D) EMERGENCY FLR LIGHT TO MEL 33-50-03A. MCC CONTACTED. CREW PLACARD INSTALLED. R & R DAMAGED HOUSING REF A319 AMM 25-21 OK FJan 13, 2026 · N369NB · Airbus A319114 · Emergency LightingSDR DALA2026011700391Latch · brokenO2 MASK LATCH 27DEF BROKEN AND 26DEF BROKEN. FWD TO MEL 35- 21-01A (M) PROC C/W. PLACARD INSTALLED. WAS ABLE TO RESET O2 MASK PSU PANEL PER A319 AMM 35-21. OK FOR SVC. PLACARDS REMOVED. OK FOR SVC. (LP: 8008578)Jan 13, 2026 · N368NB · Airbus A319114 · Passenger Oxygen SystemSDR DALA2026011500360Repair · damagedON R1 DOOR AFT LWR SHEET REPAIR FOUND ONE RIVET BUCKTAIL ISN'T CENTER AND OFF TO ONE SIDE. ALSO FOUND SEALANT MISSING FOR SEAL RETAINER. APPLIED SEALANT ON FWD CHANNEL CORNER ON FWD PAX DOOR PER A319 SRM 52-10. REMOVED TWO RIVETS WITH POOR QUALITY BUCKTAILS RJan 12, 2026 · N361NB · Airbus A319114 · Service DoorsSDR DALA2026011500359Floor Support · corrodedAFT CABIN LONGITUDINAL BEAM AT Y1292 HAS CORROSION BETWEEN FR67 AND FR68. FLOOR SUPPORT IN AFT CABIN AT Y1292 AND BETWEEN FR67-68 HAD CORROSION REMOVED AND EVALUATED DAMAGE, FOUND DAMAGE TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED FLOOR SUPPORT IAW SRM Jan 12, 2026 · N358NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026011500358Seat Track · corrodedCORROSION SEAT TRACK +Y1292, FR 16 LT SIDE FWD GALLEY AREA. REPLACED SEAT TRACK Y1292 FR 12 TO FR 24 IAW SRM 51-42-11 AND SRM 51-72-11, AND DWG D53110920, ISSUE E00, DWG D53110984 ISSUE C00 TOOK MEASURES OF CORROSION ARE: L= 0.916 INCHW= 0.390 INCH D= 0.039Jan 12, 2026 · N359NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026011500357Floor Support · corrodedCORRODED FLOOR SUPPORT +Y1292, FR 66 LT SIDE AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT Y1292, AND FASTENERS FR 64 TO FR 66 IAW SRM 51-42-11, SRM 51-72- 11,AND DWG 10N01048, REV A, APPROVED DATE 21/AUG/14 TOOK MEASURE OF CORROSION ARE: L: 2.589 INCHES W:0Jan 12, 2026 · N359NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026011500356Receptacle · corrodedENGINE NR 1 PYLON SPIGOT RECPTACLE AND SPIGOT BALL JOINT WITH CORROSION. REPLACED LOWER SPIGOT FITTING OF PYLON NR 1 IAW SRM TASK 54- 51-12-300-001, REV 155, AND REPLACED PYLON SPIGOT BALL JOINT IAW AMM TASK 54-51-41-000-001-A, PARAG 4C, AND TASK 54-51-41-400Jan 12, 2026 · N349NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA2026011500355Floor Support · corrodedUPPER FUSELAGE PAX CABIN, AFT ENTRY AREA FR68 -Y1200 FLOOR SUPPORT ANGLE WITH CORROSION. REPLACED FLOOR SUPPORT ANGLE (BEAM - LONGITUDINAL) AND COUPLING (SECTION - CONNECTING) AT FR68 -Y1200 IAW SRM 51-72-11-911-001 REV: 155, AND DRAWINGS D534 72780 ISSUE D AJan 12, 2026 · N349NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026011500354Web · corrodedAFT FUSELAGE INTERNAL FLOOR STRUCTURE BETWEEN FR 68 AND FR 69 AT STGR 23R, WEB WITH CORROSION. REPLACED WEB (SHEET SHEAR) LOCATED BETWEEN FR68 AND FR69 STGR 23 IAW SRM 51-72-11-911-001 REV 155, AND DRAWINGS D53474250, ISSUE L, AND D53480505 ISSUE EU. (LP: 13Jan 12, 2026 · N349NB · Airbus A319114 · Fuselage Miscellaneous Structure
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