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"

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 DALA2026052603148Glide Slope · faultedDIV - TO SAV DUE TO GLIDE SLOPE NOT CAPTURING DURING THE APPROACH TO ATL IN IFR CONDITIONS. COULD NOT DUPLICATE. SWAPPED MMR NR 1 AND NR 2. AIRCRAFT RETURNED TO SERVICE. (LP: 8881250) AIRCRAFT WAS GROUNDED.May 24, 2026 · N319NB · Airbus A319114 · Glide Slope SystemSDR DALA2026052403139Seat Track · corrodedLEVEL 2 CORRIOSION SEAT TRACK -Y765 LOC. FR 64 TO FR 66 AT AFT GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-42-11, SRM 51-72-11, AND DWG NAT10N01048 ISSUE E. MEASURE OF THE CORROSION ARE L: 0.923 IN W: 0.354 IN. (LP: 1609533) AIRCRAFT WAS GROUNDED.May 24, 2026 · N369NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026052403138Floor Support · corrodedLEVEL 2 CORROSION FR 68 FLOOR SUPPORT -Y765 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT -Y765 LOC. FR 66 TO FR 70 IAW SRM 51-42-11, SRM 51-72-11, DWG D53472780 ISSUE: K AND DWG D53478309 ISSUE E. MEASURE OF THE CORROSION ARE L: 1.298 IN W:1.061 IN D: 0.040May 24, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026052403137Seat Track · corrodedLEVEL 2 CORROSION ON SEAT TRACK -Y1292 LOC BTW FR 12 TO FR 24 AT FWD GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-42-11, SRM 51-72-11, DWG D531128126 ISSUE E00 AND DWG D53110920 ISSUE E00, MEASURES OF THE CORROSION ARE: L= 0.901INCH, W= 0.385 INCH, D= 0.0May 24, 2026 · N369NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026052703187Battery · overheatedAT CRUISE, FA HAD USE THE LITHUIUM CONTAINMENT BAG FOR AN OVERHEATING EXTERNAL BATTERY. FWD TO MCC PER NEF 25-32-13. ALL REMARK C/W SEE L//P 8936275. (LP: 8936274) AIRCRAFT WAS GROUNDEDMay 23, 2026 · N361NB · Airbus A319114 · Standard Practices/StructuresSDR DALA2026052403136Web · corrodedLEVEL 2 CORROSION, ON WEB LOCATED AT LEVEL S23R BTW FR 69 TO FR 70 AFT GALLEY AREA. REPLACED WEB AND FASTENERS LOCATED AT LEVEL S23R BTW FR 69 TO FR 70 AFT GALLEY AREA IAW SRM 51-42-11, DWG D53474180, ISSUE: E. (LP: 1609209) AIRCRAFT WAS GROUNDED.May 23, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026052403135Web · corrodedLEVEL 2 CORROSION, ON WEB LOCATED AT LEVEL S23R BTW FR 69 TO FR 70 AFT GALLEY AREA. INSTALLED WEB, BRACKET (1 EA) AND FASTENERS LOCATED AT LEVEL STR23RH BTW FR69 TO FR70 AFT GALLEY AREA AS PER A319 SRM 51-42- 11,DWG: D53474180 ISSUE: E. (LP: 1609200) AIRCRAFMay 23, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026052403134Floor Support · corrodedLEVEL 3 CORROSION, EVIDENCE OF REWORK FLOOR SUPPORT +Y254 LOC. FR 16 TO FR 20 AT FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT Y254 AND FASTENERS LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA IAW SRM 51-42-11 AND DWG D53112816, ISSUE : G00, DWG D53110984 ISSUE: CMay 23, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026052403133Cover Plate · damagedELONGATED HOLES ON COVER SHEET LOCATED FROM FR55A TO FR59 IN AFT CARGO COMPARTMENT. REPLACED COVER SHEET LOCATED FROM FR55A TO FR59 IN AFT CARGO COMPARTMENT IAW SRM 51-42-11, SRM 51-72-11 AND DWG E53476320, ISSUE: BD. MEASURE OF ELONGATED HOLE IS : D = 0.300May 23, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026052703180Fitting · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLE D PER ER/A 633743-14AD FOR MIRROR FITTING INSTALLATION AND CONTI NUITY FITTING REPLACEMENT. SECTION I IS LIMITED TO 60000FC FROM SECTION I. ER/A TO BE REVIS ED PRIOR TO THIS LIMIT ELSE REMOVE A/CMay 22, 2026 · N368NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026052703179Fitting · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR MIRROR FITTING REPAIR AND CONTINUITY FITTING REPLACEMENT PER ER/A 633743-14AD. C/A: SECTION I IS LIMITED TO 29500FC FROM SECTION I. ER/A TO BE REVIS ED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATEMay 22, 2026 · N368NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026052703178Fitting · not reportedER/A 633743-14AD ISSUED FOR CONTINUITY FITTING REPLACEMENT AND MIRROR FITTING REPAIR. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN 27000FC FROM SECTION I AND EVERY 4700F C THEREAFTER. ASSOCIATED ER/A 14-633743 ADDED FOR AC 3168. (LP: 1607258) AIRCRAMay 22, 2026 · N368NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026052403132Floor Support · corrodedLEVEL 2 CORROSION FLOOR SUPPORT -Y1292-1162.5 LOC. FR 66 TO FR 68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y1292, -Y1162.5 AND LOCATED BETWEEN FR66 TO FR68 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72-11 AND DWG D53472816, ISSUE F, AND DWG D53472780 IMay 21, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026052403131Rib · corrodedLEVEL 2 CORROSION, LT WING, TRAILING EDGE REAR SPAR RIBLET WITH CORROSION AT RIB 19. PERFORMED REPLACEMENT REPAIR AT RIBLET M LOCATED AT LT WING TRAILING EDGE REAR SPAR AREA AT RIB 19 IAW SRM 57-51-12-300 -007 PARG 2.B REV 157. THIS TASK IS CATEGORY A WITH NMay 21, 2026 · N368NB · Airbus A319114 · Wing, Rib/BulkheadSDR DALA2026052403130Seat Track · corrodedLEVEL 2 CORROSION SEAT TRACK -Y1292 LOCATED AT FR 20 AT FWD GALLEY AREA. : REPLACED SEAT TRACK -Y1292 AND FASTENERS LOC. BTW FR12 TO FR24 FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11 AND DWG D53112812 ISSUE E00. DWG D53110920 ISSUE E00.RELEASE, DWG D53110May 21, 2026 · N366NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026052403127Floor Support · corrodedLEVEL 2 CORROSION, FLOOR SUPPORT -Y1162.5 FROM FR68 TO FR69 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y1162.5 LOCATED BETWEEN FR68 TO FR69 AT AFT GALLEY AREA IAW SRM 51-42-11 AND A319 SRM 51-72-11 AND DWG D53472780.May 21, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026052403129Dampener · failedDONT PASS OPERATIONAL TEST DAMPER PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. REMOVED DOOR DAMPER OF PASSENGER CREW DOOR 832 ON UNSERVICEABLE CONDITION IAW FAM AMM 52-13-14-000 -001-B EXCEPT STEP 3A ITEM (4) AND 3E. JOB IN PROGRESS. (LP: 1604234) AIRCRAFT WASMay 20, 2026 · N369NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA2026052703188Rib · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR PERFORME D ON LT INBD FLAP RIB 9 LUG PER ER/A 633957-14. SECTION I IS LIMITED TO 6 MONTHS ( 182 DAYS ) FROM 15MAY26. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 1May 19, 2026 · N368NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2026052403128Dampener · failedDONT PASS OPERATIONAL TEST DOOR DAMPER ON PASSENGER DOOR 841 AT FWD GA LLEY AREA AT AFT GALLEY AREA. REMOVED DOOR DAMPER OF PASSENGER CREW DOOR 841 ON UNSERVICEABLE CONDITION IAW FAM AMM 52-11-14- 000-001-B. EXCEPT 3.A.(4) AND 3.E. AIRCRAFT WAS GROUNDEDMay 19, 2026 · N369NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA2026051903073Seat Track · corrodedCORROSION SEAT TRACK -Y765 LOCATED AT FR 20 FWD GALLEY AREA (SSI 5311 89). REPLACED SEAT TRACK -Y765 AND FASTENERS LOC. BTW FR12 TO FR24 FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 ANDDWG D53112812 ISSUE E00. RELEASE DATE 08-JAN-97, DWG D53110May 18, 2026 · N366NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026051903072Floor Support · corrodedCORROSION FLOOR SUPPORT +Y1162.5 LOC. FR 68 TO FR 69 AT AFT GALLEY AREA (SSI:534147). REPLACED FLOOR SUPPORT Y1162.5 LOC.FR68 TO FR69 AT AFT GALLEY AREA AS PER SRM 51-72-11, A319 SRM 51-42-11 AND DWG D53472780ISSUE: K RELEASE DATE:26-APR-18, DWG: D53474180 ISMay 18, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026051903076Light · failedWE HAD A LOT OF WATER COME OUT OF GASPERS AT 16DF. PAX REPORTED SPARK FROM OVERHEAD LIGHT. NOW THAT LIGHT IS OUT. INSPECTED THE OVERHEAD PANEL AT 16DEF NOT FAULTS DETECTED PER AMM 33-20, ACFT OK FOR SERVICE. (LP: 8880930). AIRCRAFT WAS GROUNDEDMay 17, 2026 · N335NB · Airbus A319114 · Passenger Compartment LightingSDR DALA2026051803035Unknown · fumesFA'S REPORTED FUMES IN BACK OF AIRPLANE ON DECENT, POTENTIAL. INSPECTED ENGINE AND APU AREA FOR LEAKS NTF. SEE ADDITIONAL MTC PERFORMED ON LP 1597370. OK FOR SVC. (LP: 8892554). AIRCRAFT WAS GROUNDEDMay 17, 2026 · N315NB · Airbus A319114 · Air Distribution SystemSDR DALA2026053103307Window · blisteredFO MIDDLE WINDSCREEN DELAMINTING ATTHE BOTTOM. ABOUT HALF DOLLR SIZE AND GROWING. CANNOT TOUCH WINDSCREEN IN THAT AREA DO TO HEAT. PULLED\ C/B W13 PER MAINT CONTROL DIRECTION. PERFORMED SLIDING WINDOW INSPECTION PER A319 AMM 56-12. FOUND TO BE WITHIN DELAM LIMay 16, 2026 · N361NB · Airbus A319114 · Flight Compartment WindowsSDR DALA2026051903074Light · damagedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED, INOP. THE LIGHT IS HANGING BY CORD TO FLOOR. RESECURED EMER LIGHT BRACKET AS REQUIRED. (LP: 1597051 \). AIRCRAFT WAS GROIOUNDEDMay 16, 2026 · N320NB · Airbus A319114 · Emergency LightingSDR DALA2026051603025Sensor · faultedDECLARED EMERGENCY DUE TO A NOSE WHEEL STEERING FAULT DURING APPROACH. AIRCRAFT TOWED TO THE GATE. REPLACED NWS FEEDBACK SENSOR 3GC AND ADJUSTED OUT OF RANGE NWS SENSOR 4GC. (LP: 8934419). AIRCRAFT WAS GROUNDEDMay 15, 2026 · N301NB · Airbus A319114 · Landing Gear Steering SystemSDR DALA2026051903075Oven · odorFA SMELLED ELEC ODOR FROM FWD GALLEY OVEN. TURNED OFF OVEN AND ODOR CLEARED. C/A: VERIFIED THAT ODOR COMES FROM CLEANNG SOLUTION AFTER TURNING ON THE OVEN. CLEANED AND DRIED OUT THE SMELLING CLEANING SOLUTIONS THRO-OUT THE OVEN. RUN OVEN AT HIGH TEMP FOR 30 MIMay 14, 2026 · N357NB · Airbus A319114 · Buffet/GalleysSDR DALA2026052203122Oven · odorSHIP 3161 DISC: OVEN -INCLUDES OVEN TIMERS DAMAGED. WHEN ON AND IN USE, THE OVEN HAS A STRONG BURNT PLASTIC SMELL. THE SMELL FILLS UP THE GALLEY. I DO NOW THINK THIS OVEN SHOULD BE USED AGAIN BEFORE IT'S FIXED. C/A: DISCUSSION SMELL WITH F/A AND CAPT. RAN OVENMay 12, 2026 · N361NB · Airbus A319114 · Buffet/GalleysSDR DALA2026051302981Floor Support · corrodedLEVEL 2 CORROSION, A319 TASK 5320-6010, CPCP 2021-2001. PAX CABIN, AFT SECTION, FLOOR STRUCTURE AT FR68 Y-765MM, LONGITUDINAL BEAM WITH CORROSION. C/A: REPLACED LONGITUDINAL BEAM P/N: D5347219320000 IAW A319 SRM 51- 72-11-911-001 REV 157.00 DATED 15/PR/26. (LPMay 12, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026051302979Skin · debondedEMPENNAGE, RUDDER RH SIDE PANEL WITH DISBONDING DUE TO FLUID INGRESS WITH AN AREA OF 2073MM2 AT HOISTING POINT #3 RHS. C/A: REPAIRED RUDDER S/N TS-3438 HOIST POINTS #3 R/H SIDE AND #1 L/H SIDE I.A.W A319 SRM TASK 55-41-13-300-032 REV 157.00 DATED 15/ APR/26 (May 11, 2026 · N368NB · Airbus A319114 · Rudder, Plate/SkinSDR DALA2026051102940Unknown · fumesDECLARED EMERGENCY DUE TO FUMES IN THE FLIGHT DECK FROM LEFT VENT. NO TROUBLE FOUND. PERFORMED LEVEL B DECONTAMINATION. (LP: 8675796). AIRCRAFT WAS GROUNDEDMay 10, 2026 · N344NB · Airbus A319114 · Air Distribution SystemSDR DALA2026051102935Receptacle · corrodedLEVEL 2 CORRSION, CORROSION SPIGOT RECEPTACLE FITTING ON RH PYLON. REPLACED SPIGOT RECEPTACLE FITTING ON RH PYLON AS PER A319 SRM 54-51-41-000-001- A, A319 SRM 54-51-41-400-001-A AND A319 SRM54- 51-12-300-001 MEASURED OF CORROSION AREA: D:0.0041 INCH AND OF DMay 10, 2026 · N366NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA2026051102936Light Sys · malfunctionedFLIGHT ATTENDANTS REPORT ALL EXIT SIGNS STAY ON THEY NEVER CUT OFF. RAN CABIN EMERGENCY LIGHTING TEST AND OPS CHECK NORMAL PER A319 AMM 33-51. (LP: 8181372). AIRCRAFT WAS GROUNDEDMay 9, 2026 · N324NB · Airbus A319114 · Emergency LightingSDR DALA2026051102934Shear Tie · corrodedLEVEL 2 CORROSION, CORROSION SHEAR TIE FR 28 AND BTW STR 41R TO STR 42R IN FWD CARGO CO MPARTMENT (SSI 532180). REPLACED SHEAR TIE AND FASTENERS LOC. FR28 BTW STR 41R TO STR 42R IN FWD CARGO AS PER A319 SRM 51-42-11 AND DWG D53233523, ISSUE D00, RELEASE DATE May 9, 2026 · N366NB · Airbus A319114 · Fuselage Internal Mounting StructureSDR DALA2026051102933Hinge Fitting · wornWEAR ON HINGE FITTING 1, 2, 3, 4, 5 AND 6 ON RH ELEVATOR. REPLACED HINGE FITTING #1, #2, #3, #4, #5 AND #6 ON RH ELEVATOR AS PER A320 FAM AMM 55-16-42-000-001-A AND AS PER A320 FAM AMM 55-16-42-400-001-A SEE INDIVIDUAL SIGN OFF ON ORNRC 40/300 RII INSPECTION May 9, 2026 · N366NB · Airbus A319114 · Elevator StructureSDR DALA2026051102932Receptacle · corrodedLEVEL 2 CORRSION, CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON AS PER AS PER A319 SRM 54-51-12 AND AS PER A319 SRM 51-74-00 AND SRM 51-44-11 AND AS PER A320 FAM AMM 54-51-41-000-001-A AND AMM 54-51-41-400 -00May 9, 2026 · N366NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA2026051102931Floor Support · corrodedLEVEL 2 CORRSION, A319 TASK 5320-6010, CPCP 2021-2001. PAX CABIN AFT SECTION, FLOOR STRUCTURE BETWEEN FR66+120MM AND FR68 AT Y1292 AND Y1162.5 LONGITUDINAL BEAM (2EA SECTIONS) WITH CORROSION IN SEVERAL PLACES. REPLACED LONGITUDINAL BEAMS (2EA) P/N: D534 72172May 9, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026050802913Oxygen Mask · leakingYELLOW BLINKER ON CAPTAINS OXYGEN MASK DOES NOT GO BACK WHEN TEST/RESET BUTTON IS PUSHED. FOUND CAPTAINS O2 MASK LEAKING FROM HOSE FITTING ON MASK. REMOVED AND REPLACED CAPTS O2 MASK IAW A319 AMM 35-12-41. LEAK CHECK OK. RFID INDUCTION C/W. (LP: 8027166). AIRMay 7, 2026 · N328NB · Airbus A319114 · Crew Oxygen SystemSDR DALA2026050602891Bottle · low pressureDURING SERVICE CHK FOUND THE R2 DOOR ASSIST BOTTLE PRESSURE BELOW LIMITS. SERVICED R2 DOOR ASSIST BOTTLE WITH NOITROGEN IAW AMM 52-10 -00-610-801C1 (ALT PROCEDURE) NO LEAKS NOTED. OK FOR SERVICE. (LP: 8676291). AIRCRAFT WAS GROUNDEDMay 5, 2026 · N341NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA2026050602890Fitting · corrodedLEVEL 2 CORROSION. ENGINE NR 1 PYLON AREA SPIGOT RECEPTACLE FITTING BORE WITH CORROSION AND BALL JOINT WITH INUSUAL WEAR. REPLACED NR 1 PYLON SPIGOT BALL JOINT AND FITTING IAW SRM 54-51-12-300-001, REV 157, AND AMM 54-51 -41-400-001-A, AND 54-51-41-400-001-A May 5, 2026 · N368NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA2026050802912Skin · dentedAFTER COMPLETING HFEC INSPECTION REF LOG 8624949. IT WAS DETERMINED THAT THE DENT ON NR 2 RT SLAT WAS NOT EVALUATED. EVALUATED DENT ON NR 2 RT SLAT REF A319 SRM 57-41-11-283-005, FIGURE 001 SHEET 3 FOUND TO BE OUT OF LIMITS WITH DEPT GREATER THAT 0.2 INCHES. May 4, 2026 · N324NB · Airbus A319114 · Leading Edge DevicesSDR DALA2026050602892Oxygen Box · openCREW REPORTS O2 MASK DOOR OPENED ON LANDING SEAT 12DEF. PACKED AND SECURED O2 MASK DOOR AT SEAT 12 DEF IAW AMM 35- 21. (LP: 8885420). AIRCRAFT WAS GROUNDEDMay 4, 2026 · N325NB · Airbus A319114 · Passenger Oxygen SystemSDR DALA2026050502831Shaft · not reportedRIGHT WING REMOVE AND INSTALL TORQUE SHAFT 6282CM TO PERFORM REPAIR T/E OVERHANG AREA. : REMOVED AND REINSTALLED RT WING FLAP TORQUE SHAFT 6282CM IAW AMM TASK 27-54-45-000-013-A AND 27-54-45-400-013-A REV 135.00. (LP: 1577369)May 4, 2026 · N368NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2026050502830Floor Support · corrodedLEVEL 2 CORROSION, TASK 5320-6010, PAX CABIN, AFT SECTION, FLOOR STRUCTURE AT FR70 Y-464.8MM, LONGITUDINAL BEAM WITH CORROSION. REPLACED NEW BEAM P/N: D5347219520200 IAW A319 SRM 53-41-14-03A, FIG 303 SHEET 2, ITEM 155. REV 157.00 , AND INATALLED IAW DWG # DMay 4, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026050502829Floor Support · corrodedLEVEL 2 CORROSION, TASK 5320-6010. PAX CABIN, AFT SECTION, FLOOR STRUCTURE, BETWEEN FR67 AND FR68, Y-1292 AND Y-1162.5 LONGITUDINAL BEAM (2EA SECTIONS) WITH CORROSION. REPLACED LONGITUDINAL BEAM (2EA) LOCATED AT PAX CABIN, AFT SECTION BETWEEN FR66 AND FR69, YMay 4, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026050102766Computer · faultedATO - AT APPROXIMATELY 10KTS DUE TO F/CTL ELAC 1 PITCH FAULT. ELAC 1 PLACED ON MEL AND CONTINUED. LATER REPLACED ELAC 1. (LP 8038066 - AIRCRAFT WAS GROUNDED)Apr 30, 2026 · N353NB · Airbus A319114 · Flight Control SystemSDR DALA2026050102765Shear Plate · corrodedCORROSION LEVEL 2 SHEAR PLATE STR 23R BTW FR69 AND FR70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE AND FASTENERS LOC. STR 23R BTW FR69 AND FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (LP 1571111- AIRCRAFT WAS GROUNDED)Apr 30, 2026 · N366NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026050102764Web · corrodedCORROSION LEVEL 2 WEB BTW FR69 TO FR70 AND STR23R AT AFT GALLEY AREA (SSI 534 147). REPLACED WEB, AND FASTENERS BTW FR69 TO FR70 AND STR23R AT AFT GALLEY AREA AS PER A319 SRM 51-72-11, A319 SRM 51-42-11. (LP 1571108 - AIRCRAFT WAS GROUNDED)Apr 30, 2026 · N366NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026050102763Web · corrodedCORROSION LEVEL 2 WEB FRAME 20 RH SIDE AT LEVEL STR 23 AT FWD GALLEY AREA. REPLACED WEB AND FASTENERS LOC ON FR20 TO FR24 RH SIDE AT LEVEL STR 23 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND SRM 51-42-11. (LP 1570957 - AIRCRAFT WAS GROUNDED)Apr 30, 2026 · N366NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026050102762Seat Track · corrodedCORROSION LEVEL 2 SEAT TRACK +Y1292 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 531189). REPLACED SEAT TRACK Y1292 AND FASTENERS LOC.BTW FR 12 TO FR 24 FWD GALLEY AREA AS PER A319 SRM 51-42-11 A319 SRM 51-72-11. (LP 1570948 - AIRCRAFT WAS GROUNDED)Apr 30, 2026 · N366NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
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