N357NB

Service difficulty reports · 181

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N357NB' AND registry_match = 'registration'
  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 DALA2026080704566Cover · detachedEES, OVERHEAD EMERGENCY LIGHT COVER AROUND AISLE 20 FELL OFF. INSTALLED LIGHT COVER AS NECESSARY. (LP: 8319084, AIRCRAFT WAS GROUNDED)Aug 2, 2026 · N357NB · Airbus A319114 · Emergency LightingSDR DALA2026070103871Computer · faultyREJECTED TAKE OFF AT LOW SPEED BELOW 50 KNOTS DUE TO FLIGHT CONTROL CAUTION MSG. BITE TEST SFCC 1 FAULTS SLTS SFCC 1. R & R IAW TSM 27-51 AND AMM 27-51 BITE TEST NO FAULTS NOTED RESET SYS IAW AMM 27-51 NO FAULTS NOTED OK FOR SVC. (LP: 8651838, AIRCRAFT WAS Jun 30, 2026 · N357NB · Airbus A319114 · Flight Management Computing Hardware SystemSDR DALA2026060503397Unknown · odorPASSANGERS IN 15 D AND 15E REPORTED OCCASIONAL WHIFS OF BURNING OIL SMELL THAT THEY REPORTED AT TOP OF DESCENT TO THE FLIGHT ATTENDANT. I SPOKE TO THE PASSANGERS AND THEY SAID THEY HAD NO ILLNESS SYMPTOMS AND CONFIRMED INTERMITTANT WHIFFS. INSPECTED PSU PANELJun 1, 2026 · N357NB · Airbus A319114 · Air Distribution 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 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 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 DALA2025121609158Oxygen Mask · unwanted deployOXYGEN PANEL MASK DEPLOYED. RESECURED COMPARTMENT AT LAV 202 IAW AMM 35-21. (1353632).Dec 16, 2025 · N357NB · Airbus A319114 · Passenger Oxygen SystemSDR DALA2025121209082Radome · delaminatedDURING WALK AROUND, FOUND DELAMINATION TO RADOME. R & R RADOME IAW A319 AMM 53-15. (7892405).Dec 12, 2025 · N357NB · Airbus A319114 · Aerodynamic FairingsSDR DALA2025091806854A/C Pack · failedDECLARED EMERGENCY DURING APPROACH INTO ATL DUE TO A DUAL PACK FAILURE AT FL200. LT ENGINE EIU FAULT LED TO THE LT PACK FAULT. THE RT PACK WAS ALREADY ON MEL FOR A PRIOR OVERHEAT MESSAGE. CORRECTIVE ACTION: DURING TS, LT ENGINE PYLON CONNECTOR 406VC1 WAS FOUNDSep 18, 2025 · N357NB · Airbus A319114 · Cabin Cooling SystemSDR DALA2025091506783Circuit Breaker · trippedDURING FLIGHT OPERATIONAL TEST GOT CIRCUIT BREAKER H07 TRIPPED. REPLACED CIRCUIT BREAKER H07 ON OVERHEAD PANEL 49VU IAW AIRBUS ESPM 20-52 -22. (1198052).Sep 14, 2025 · N357NB · Airbus A319114 · Electrical Power System WiringSDR DALA2025091506788Support Fitting · corrodedCORROSION ON FITTING SUPPORT THE SPHERICAL BEARING TRACK 2 INBD FLAP LT WING. COMPLIED WITH ER/A 628405-14. (1197264).Sep 13, 2025 · N357NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2025091506782Elec Connector · brokenBROKEN BACKSHELL ON ELECTRICAL CONNECTOR 205WLA AT PASSENGER CABIN. REPLACED BACKSHELL ON ELECTRICAL CONNECTOR 205WL-A AT PASSENGER CABIN IAW FAM AWM 33-51-02 AND IAW AIRBUS ESPM20-44-11. (1197407).Sep 13, 2025 · N357NB · Airbus A319114 · Light System WiringSDR DALA2025091506781Window Post · crackedCRACK INDICATION ON RH WINDSHIELD CENTER POST UPPER ATTACHMENT AREA UPPER CORNER RADIUS. COMPLIED WITH ER/A 628084-14AD. (1197373).Sep 13, 2025 · N357NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025091506780Window Post · crackedCRACK INDICATION ON RH CONTINUITY FITTING AT WINDSHIELD CENTER POST LO WER ATTACHMENT AREA. COMPLIED WITH ER/A 628127-14AD. (1197365).Sep 13, 2025 · N357NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025091506779Window Post · crackedCRACK INDICATION ON RT WINDSHIELD CENTER POST UPPER ATTACHMENT AREA UPPER CORNER RADIUS. COMPLIED WITH ER/A 628084-14AD. (1197362).Sep 13, 2025 · N357NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025091506778Window Post · crackedCRACK INDICATION ON RT WINDSHIELD CENTER POST LOWER ATTACHMENT AREA L OWER CORNER RADIUS. COMPLIED WITH ER/A 628084-14AD. (1197182).Sep 13, 2025 · N357NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025091506777Window Post · crackedCRACK INDICATION ON LT WINDSHIELD CENTER POST LOWER ATTACHMENT AREA LOWER CORNER RADIUS. COMPLIED WITH ER/A 628084-14AD. (1197175).Sep 13, 2025 · N357NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025091506776Window Post · crackedCRACK INDICATION ON LH WINDSHIELD CENTER POST UPPER ATTACHMENT AREA UPPER CORNER RADIUS. COMPLIED WITH ER/A 628084-14AD. (1197169).Sep 13, 2025 · N357NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025091506786Retainer · corrodedCORROSION ON TROLLEY RETAINER BLOCK COMPARTMENTS 110 AND 111 OF GALLEY 1 AT FWD GALLEY AREA. COMPLIED WITH ER/A 628362-14. (1195648).Sep 12, 2025 · N357NB · Airbus A319114 · Buffet/GalleysSDR DALA2025091206729Skin · wornWEAR EXTERNAL SKIN UPPER CUT OUT ON PASSENGER CREW DOOR L/H LOC. FR 66 TO FR 68 IN PASSENGER CABIN. COMPLIED WITH ER/A 628846-14. (1194627).Sep 12, 2025 · N357NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2025091206728Floor Panel · delaminatedDELAMINATED FLOOR PANEL 222EF TA FWD GALLEY AREA. COMPLIED WITH ER/A 628477-14. (1194617).Sep 12, 2025 · N357NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2025091206727Skin · wornWEAR ON EXTERNAL SKIN UPPER CUT OUT ON PASSENGER CREW DOOR R/H LOC. FR 66 TO FR 68 IN PASSENGER CABIN. COMPLIED WITH ER/A 628845-14. (1194664).Sep 12, 2025 · N357NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2025091206726Support · corrodedCORROSION ON FITTING SUPPORT THE SPHERICAL BEARING TRACK 3 0/B FLAP RT WING. COMPLIED WITH ER/A 628388-14. (1194658).Sep 12, 2025 · N357NB · Airbus A319114 · Wing Miscellaneous StructureSDR DALA2025091206725Support Fitting · corrodedCORROSION ON FITTING SUPPORT THE SPHERICAL BEARING TRACK 3 O/B FLAP LH WING. COMPLIED WITH ER/A 628387-14. (1194652).Sep 12, 2025 · N357NB · Airbus A319114 · Wing Miscellaneous StructureSDR DALA2025091206733Window Frame · crackedCRACK INDICATIONS FOUND IN LT AND RT FRONT WINDSHIELDS AND CONTINUITY FITTINGS AS WELL AS HOLES D1 LT AND RT SIDES. COMPLIED WITH ER/A 628127-14. (1193607).Sep 11, 2025 · N357NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025091206732Skin · wornWEARS FOUND ON EXTERNAL FUSELAGE SKIN AT THE CIRCULAR ZONE OF THE UPPER FWD AND AFT CORNERS OF AFT PASSENGER DOOR CUTOUT, 1 WEAR AT FR66 RHS AND 1 WEAR AT FR68 LHS. COMPLIED WITH ER/A 628845-14. (1193783).Sep 11, 2025 · N357NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2025091206731Bearing · corrodedCORROSION WAS FOUND AFFECTING INB'D AND OUTB'D ALUMINUM PLATES IN INNER AND OUTER RIB 5 ECCENTRIC BEARING LH WING OUTG'D FLAP TRACK 3. COMPLIED WITH ER/A 628388-14. (1193993).Sep 11, 2025 · N357NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2025091206730Bearing · corrodedCORROSION WAS FOUND AFFECTING INB'D AND OUTB'D ALUMINUM PLATES IN INNER AND OUTER RIB 5 ECCENTRIC BEARING LH WING OUTG'D FLAP. COMPLIED WITH ER/A 628387-14. (1193865).Sep 11, 2025 · N357NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2025091106713Support Fitting · corrodedCORROSION ON FITTING SUPPORT THE SPHERICAL BEARING TRACK 4 O/B FLAP RH WING. REPAIRED PER ER/A 628418-14. (1192970)Sep 11, 2025 · N357NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2025091106712Fitting · crackedSHIP 3157 CRACK INDICATIONS FOUND IN LH AND RH FRONT WINDSHIELDS AND CONTINUITY FTGS AS WELL AS HOLES D1 LH AND RH SIDES. CORRECTIVE ACTION: COMPLIED WITH ER/A 628084-14. (1192691).Sep 10, 2025 · N357NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025091106711Fitting · crackedCRACK INDICATIONS FOUND IN LH AND RH FRONT WINDSHIELDS AND CONTINUITY FTGS AS WELL AS HOLES D1 LH AND RH SIDES. COMPLIED WITH ER/A 628084-14. (1192669)Sep 10, 2025 · N357NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025091106710Frame · crackedCRACK INDICATION ON FRAME 16 RH SIDE OPEN FASTENER HOLE H3 IN CROSSBEAM SPLICING AREA. COMPLIED WITH ER/A 628163-14AD. (1192537).Sep 10, 2025 · N357NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2025091106709Frame · crackedCRACK INDICATION ON FRAME 16 RH SIDE OPEN FASTENER HOLE H2 IN CROSSBEAM SPLICING AREA. COMPLIED WITH ER/A 628163-14AD. (1192533).Sep 10, 2025 · N357NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2025091106707Bearing · corrodedCORROSION FOUND AFFECTING INB'D AND OUTB'D AL PLATES AT TRACK #2 IN THE INNER AND OUT RIB 9 ECCENTRIC BEARING, LH WING,INB'D FLAP. COMPLIED WITH ER/A 628405-14. (1190565).Sep 9, 2025 · N357NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2025090906647Access Panel · puncturedPUNCTURE ON ACCESS PANEL 192KB AT LOWER FUSELAGE. COMPLIED WITH ER/A 524189-14. (1188635).Sep 8, 2025 · N357NB · Airbus A319114 · Fuselage Structure (General)SDR DALA2025090806614Skin · wornWEAR ON EXTERNAL SKIN LOC FR34 AT LEVEL STR44 AT LOWER FUSELAGE. COMPLIED WITH ER/A 628714-14. (1187074).Sep 7, 2025 · N357NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2025090806612Skin · wornWEAR FOUND ON EXTERNAL FUSELAGE SKIN AT LWER SKIN PANEL BETWEEN FR34 TO FR35 AND STGR 43LH TO 43RH. COMPLIED WITH ER/A 628714-14 . (1183404).Sep 5, 2025 · N357NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2025090806616Floor Panel · delaminatedDELAMINATED FLOOR PANEL (261DF) AT AFT GALLEY AREA. COMPLIED WITH ER/A 624842-14. (1183420).Sep 5, 2025 · N357NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2025090406540Shear Tie · corrodedSHIP 3157 CORROSION SHEAR TIE AT LEVEL OF FR 65 AND BTW STR 44 TO STR 43L IN AF T CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AT LEVEL OF FR 65 AND BTW STR 44 TO STR 43L IN AFT CARGO COMPARTMENT, AS PER A319 SRM 51-42-11 AND A319 SRM 51- 72-11. (1Sep 3, 2025 · N357NB · Airbus A319114 · Fuselage Internal Mounting StructureSDR DALA2025090306530Bracket · crackedCRACK BRACKET TELESCOPIC DUCT OB FIXED LEADING EDGE IB SIDE LH WING. REPLACED BRACKET AND FASTENERS ON TELESCOPIC DUCT OB FIXED LEADING EDGE IB SIDE LH WING AS PER A319 SRM 51-72-11 AND A319 SRM51-42-11. (1178540).Sep 2, 2025 · N357NB · Airbus A319114 · Wing, Attach FittingsSDR DALA2025090106452Elec Connector · wornWORN ELECTRICAL CONNECTOR 7540VC ON I/B FLAP RT. REPLACED ELECTRICAL CONNECTOR 7540VC ON I/B FLAP RT IAW AIRBUS ESPM 20-44-11. (1172999).Aug 30, 2025 · N357NB · Airbus A319114 · Flight Control System WiringSDR DALA2025090106448Frame · crackedCRACK INDICATION ON FRAME 16 LH SIDE OPEN FASTENER HOLE H2 IN CROSSBEAM SPLICING AREA. COMPLIED WITH ER/A 628162-14AD. (1171545).Aug 29, 2025 · N357NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2025082906398Floorbeam · corrodedCORROSION FLOOR BEAM -Y1292-1162.5 LOCATED BETWEEN FR66 TO FR68 AT AFT GALLEY AREA. REPLACED FLOOR BEAM -Y1292 -Y1162.5 AND FASTENER LOCATED. BTW FR66 TO FR68 AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1169846).Aug 28, 2025 · N357NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2025082906405Elec Connector · corrodedCORROSION ELECTRICAL CONNECTORS SPOILER 2,3,4 AND 5 ACTUATOR OF ON LH WING. REPLACED ELECTRICAL CONNECTORS SPOILER #2, 3, 4 AND 5 ACTUATOR OF LH WING AS PER AIRBUS ESPM 20-44-11. (1169860).Aug 28, 2025 · N357NB · Airbus A319114 · Flight Control System WiringSDR DALA2025082506321Floor Support · corrodedCORROSION FLOOR SUPPORT -Y1162.5 AT FR68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y1162.5 AND FASTENER LOCATED. BTW FR68 TO FR69 AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1162040).Aug 25, 2025 · N357NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2025082506320Seat Track · scratchedSCRATCH (3 E/A) LOC. ON SEAT TRACK -Y1292 ZONE 240 BTW FR35 TO FR 47. REPLACED SEAT TRACK -Y1292 AND FASTENERS LOCATED BTW FR36 TO FR41 AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (1161994).Aug 24, 2025 · N357NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025082506319Door Frame · crackedCRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE 4 AT DOOR STOP FITTING 1 POSITION. PERFORMED PERMANENT REPAIR LOC. ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE 4 AT DOOR STOP FITTING 1 POSITION AS PER A319 SRM 53-41-12-300-11. (1161986).Aug 24, 2025 · N357NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025082506318Floor Support · corrodedCORROSION FLOOR SUPPORT +Y1292-1162.5 LOCATED BETWEEN FR66 TO FR68 AT AF T GALLEY AREA. REPLACED FLOOR SUPPORT Y1292-1162 LOCATED BETWEEN FR66 TO FR68 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (1161967).Aug 24, 2025 · N357NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2025082506317Floor Support · corrodedCORROSION FLOOR SUPPORT -Y765 LOCATED BETWEEN FR67 TO FR68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y765 LOCATED BETWEEN FR66 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1161961).Aug 24, 2025 · N357NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2025091806846Counter · dentedDENTS WORK DECK GALLEY 1 AT FWD GALLEY AREA. R & R FWD GALLEY WORK DECK REF A319 CMM 25-31-561. (1156491).Aug 21, 2025 · N357NB · Airbus A319114 · Buffet/Galleys
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