N352NB

Service difficulty reports · 138

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 = 'N352NB' 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 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 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 DALA2026021701070Inlet · contaminatedDURING DESCENT AROUND 10,000 FT AN ODOR WAS NOTICE THAT SEEMED TO SMELL LIKE A MUSTY BURNING. IT WAS SHORT LIVED, BUT RETURNED ON THE GROUND. WORK CARRIED 0550-2002 WAS ACCOMPLISHED TO IDENTIFY ISSUE. HEAVY OIL SATURATION WAS FOUND IN APU INLET UP INSIDE ENTIFeb 9, 2026 · N352NB · Airbus A319114 · APU Core EngineSDR DALA2025111808409Cids · faultedAFT TO EXIT SIGNS/NO SMOKING SIGNS OFF AND ON BLINKING WHOLE FLIGHT INTERPHONE L1 TO L2 CUT OUT SAME WHITE UP AS PREVIOUS. PERFORMED FULL CIDS RESET PER A319 TSM 24-00. NO FAULTS AT THIS TIME. OK FOR SVC. (8014238).Nov 17, 2025 · N352NB · Airbus A319114 · Emergency LightingSDR DALA2025100707282Outflow Valve · damagedSHIP 3152 - ATB - DUE TO CAB PR SYS 2 FAULT ECAM WARNING FOLLOWED BY CAB PR SYS 1 2 FAULT ECAM WARNING. CORRECTIVE ACTION: FOUND BROKEN DRILL BIT BETWEEN OUTFLOW VALVE AND THE CUTOUT FRAME NOT ALLOWING THE OUTFLOW VALVE TO CLOSE PROPERLY. REMOVED FOD AND OUTFLOct 4, 2025 · N352NB · Airbus A319114 · Pressure Regulator/Outflow ValveSDR DALA2025100307224Window Frame · crackedCRACK FOUND ON WINDSHIELD FRAMES ON LH AND RH SIDES. COMPLIED WITH ER/A 628472-14. (1230870).Oct 2, 2025 · N352NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025100307222Frame · crackedCRACK INDICATION FOUND ON FRAME 16LH HOLE C. ON DOUBLE JOGGLE AREA. COMPLIED WITH ER/A 628459-14AD. (1230633).Oct 2, 2025 · N352NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2025100307217Window Frame · crackedCRACK INDICATION FOUND ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA LOWER RADIO RT SIDE. COMPLIED WITH ER/A 628400-14AD. (1230996).Oct 2, 2025 · N352NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025100307216Skin · corrodedCORROSION INTERNAL SKIN LOCATED BTW FR 67 TO FR 68 AND BTW STR 30L TO STR 31L IN AFT CARGO COMPARTMENT. COMPLIED WITH ER/A 628904-14. (1230844).Oct 2, 2025 · N352NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2025100307211Window Frame · crackedCRACKS FOUND ON LT WINDSHIELD, CENTER POST, LOWER ATTACHMENT AREA, UPPER RADIUS, FRONT WINDSHIELD FRAMING , RT WINDSHIELD, CENTER POST, LOWER ATTACHMENT AREA, LOWER RADIUS, FRONT WINDSHIELD FRAMING. COMPLIED WITH ER/A 628585-14AD. (1230430).Oct 2, 2025 · N352NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025100207187Skin · corrodedCORROSION SPOTS FOUND ON FUSELAGE SKIN, INTERNAL SIDE BETWEEN STRGR 31L - STRGR 32L AND FR67 - FR69. COMPLIED WITH ER/A 628904-14. (1229384).Oct 1, 2025 · N352NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2025100207186Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231CF IN PASSENGER CABIN. COMPLIED WITH ER/A 628624-14. (1229123).Oct 1, 2025 · N352NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2025100207185Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231EF IN PASSENGER CABIN. COMPLIED WITH ER/A 628624-14. (1229113).Oct 1, 2025 · N352NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2025100207184Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231BF IN PASSENGER CABIN. COMPLIED WITH ER/A 628624-14. (1228110).Oct 1, 2025 · N352NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2025100207183Access Panel · deterioratedDETERIORATED ALUMINUM MESH ON ACCESS PANEL 191BB BELLY FAIRING. COMPLIED WITH ER/A 542077-14TR. (1229102).Oct 1, 2025 · N352NB · Airbus A319114 · Aerodynamic FairingsSDR DALA2025100107143Door Frame · crackedDURING M2 AND WHILE ACCOMPLISHING EM 5311-1246-01A, A CRACK WAS FOUND IN HOLE #C OF FR16 LHS DBL JGL AREA. COMPLIED WITH ER/A 628459-14AD. (1226712).Sep 30, 2025 · N352NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025100107140Frame · crackedCRACK INDICATION FOUND ON FRAME 16RH HOLE C. ON DOUBLE JOGGLE AREA, CRACK DIRECTION AT 3 O CLOCK LOOKING FROM OUTSIDE THE AIRCRAFT. COMPLIED WHIT ER/A 628458-14AD. (1226864).Sep 30, 2025 · N352NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2025100107139Frame · crackedCRACK INDICATION FOUND ON FRAME 16RH HOLE C. ON DOUBLE JOGGLE AREA. COMPLIED WHIT ER/A 628458-14AD. (1226841).Sep 30, 2025 · N352NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2025093007086Window Frame · crackedCRACKS FOUND IN LT AND RT FRONT WINDSHIELD FRAMES AT LWR CENTER NODE. COMPLIED WITH ER/A 628400-14. (1225292).Sep 29, 2025 · N352NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025092907074Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231FF IN PASSENGER CABIN. COMPLIED WITH ER/A 628624-14. (1223263).Sep 28, 2025 · N352NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2025092907073Floor Panel · delaminatedDELAMINATED FLOOR PANEL 232FF IN PASSENGER CABIN. COMPLIED WITH ER/A 628624-14. (1223255).Sep 28, 2025 · N352NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2025092907072Floor Panel · delaminatedDELAMINATED FLOOR PANEL 221PF AT FWD GALLEY AREA. COMPLIED WITH ER/A 628624-14. (1223257).Sep 28, 2025 · N352NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2025092907071Floor Panel · delaminatedDELAMINATED FLOOR PANEL 222EF AT FWD GALLEY AREA. COMPLIED WITH ER/A 628624-14. (1223246).Sep 28, 2025 · N352NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2025092907070Floor Panel · delaminatedDELAMINATED FLOOR PANEL 222CF AT FWD GALLEY AREA. COMPLIED WITH ER/A 628624-14. (1223252).Sep 28, 2025 · N352NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2025092907069Floor Panel · delaminatedDELAMINATED FLOOR PANEL 221EF AT FWD GALLEY AREA. COMPLIED WITH ER/A 628624-14. (1223219).Sep 28, 2025 · N352NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2025092907079Window Frame · crackedCRACKS FOUND IN LT AND RT FRONT WINDSHIELD FRAMES AT LWR CENTER NOD. COMPLIED WITH ER/A 628585-14AD. (1219746).Sep 26, 2025 · N352NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025092607006Bonding Plate · corrodedCORRODED STATIC DISCHARGER PLATE-BONDING FLAP TRACK FAIRING 532CB ON LT WING. COMPLIED WITH ER/A 622998-14TR. (1217688).Sep 25, 2025 · N352NB · Airbus A319114 · Wing Main, Frame StructureSDR DALA2025092607005Bonding Plate · corrodedCORRODED BONDING PLATE FLAP TRACK FAIRING 631CB ON RT WING. COMPLIED WITH ER/A 622998-14TR. (1217597).Sep 25, 2025 · N352NB · Airbus A319114 · Wing Main, Frame StructureSDR DALA2025092607004Bonding Plate · corrodedCORRODED FLAP TRACK FAIRING 632CB BONDING PLATE ON RH WING. COMPLIED WITH ER/A 622998-14TR. (1217586).Sep 25, 2025 · N352NB · Airbus A319114 · Wing Main, Frame StructureSDR DALA2025092506987Door Frame · crackedCRACK FOUND ON FASTENER HOLE AT THE DOUBLE JOGGLE AREA OF THE FR16RH AROUND THE PASSENGER SERVICE DOOR. COMPLIED WITH ER/A 628458-14AD. (1215573).Sep 24, 2025 · N352NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025092506986Bonding Plate · corrodedCORROSION BONDING PLATE FLAP TRACK FAIRING (533CB) ON LH WING. COMPLIED WITH ER/A 622998-14TR. (1216019).Sep 24, 2025 · N352NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2025092506985Bonding Plate · corrodedCORROSION BONDING PLATE FLAP TRACK FAIRING 633CB ON RH WING. COMPLIED WITH ER/A 622998-14TR. (1216002).Sep 24, 2025 · N352NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2025092506983Crossbeam · crackedCRACK INDICATION ON CROSS BEAM IN PASSENGER CABIN, ON FR 16 L, HOLE H3. CORRECTIVE ACTION: COMPLIED WITH ER/A 628546-14AD. (1214415).Sep 23, 2025 · N352NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025092506982Stringer · corrodedCORROSION STRINGER 42R BTW FR 59 TO FR 60 AFT CARGO COMPARTMENT. REPLACED STRINGER 42R AND FASTENER LOC BTW FR59 TO FR64 AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1214470).Sep 23, 2025 · N352NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2025091906887Access Panel · crackedDELAMINATED ACCESS PANEL 191BB BELLY FAIRING AT LOWER FUSELAGE. COMPLIED WITH ER/A 542077-14TR. (1205793).Sep 18, 2025 · N352NB · Airbus A319114 · Aerodynamic FairingsSDR DALA2025091906886Access Panel · crackedCRACK ACCESS PANEL 322BL ON VERTICAL STABILIZER. COMPLIED WITH ER/A 628592-14. (1205816).Sep 18, 2025 · N352NB · Airbus A319114 · Vertical Stabilizer, Plate/SkinSDR DALA2025091906892Floor Panel · delaminatedDELAMINATED FLOOR PANEL 261DF AT AFT GALLEY AREA. COMPLIED WITH ER/A 628697-14. (1205802).Sep 18, 2025 · N352NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2025091506789Skin · not reportedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BT W FR 5 TO FR 6 AT THE LAP SEAM AND 5 INCHES BELOW LH SIDE STRINGER L OWER FUSELAGE. COMPLIED WITH ER/A 574394-14. (1197223).Sep 13, 2025 · N352NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2025091106708Floor Support · corrodedCORROSION FLOOR SUPPORT +Y1162.5 LOCATED AT LEVEL FR68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT Y1162.5 AND FASTENERS LOCATED IN FR68 TO FR69 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72 -11. (1191865).Sep 10, 2025 · N352NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2025090806613Bearing · corrodedCORROSION SPHERICAL BEARING OUTBOARD FLAP TRACK 3 LH WING. REPLACED SPHERICAL BEARINGS OUTBOARD FLAP TRACK 3 LH WING AS PER A320- FAM AMM 57-53-21-000-001-A AS PER A320-FAM AMM 57-53-21-400-001. (1185070).Sep 6, 2025 · N352NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2025090806609Seat Track · corrodedCORRODED SEAT TRACK -Y765 LOCATED AT FR 20 AT FWD GALLEY AREA. REPLACED SEAT TRACK -Y765 LOCATED FR 12 TO FR 24 FWD GALLEY AREA AS PER A319 SRM 53-11-15-283-011, A319 SRM 51-42-11 AND A319 SRM 51-44 -11. (1185106).Sep 6, 2025 · N352NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025090806608Seat Track · corrodedCORRODED SEAT TRACK +Y1292 LOCATED AT FR 66 AT AFT GALLEY AREA. REPLACED NEW SEAT TRACK AND FASTENERS LOC ON Y1292 (FR64 TO FR66) AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1183374).Sep 5, 2025 · N352NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025090806607Door Sill · corrodedCORROSION LOWER SILL LOCATED ON HOLE AT FR 68 LH SIDE AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON LOWER SILL LOCATED AT FR 68 LH SIDE AT AFT GALLEY AREA AS PER A319 SRM 53-41-14-300-001. (1183368).Sep 5, 2025 · N352NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025090506581Fastener · out of positionFASTENER ON H18 HAS BEEN FOUND IN WRONG POSITION RH SIDE. REMOVED AND REINSTALLED FASTENER CORRECTLY HOLE #18 LOCATED CROSSBEAM FR20 RH SIDE AS PER AD 5311-01221-12. (1182249).Sep 4, 2025 · N352NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2025090506580Seat Track · corrodedCORROSION SEAT TRACK -Y765 LOCATED AT FR 66 AT AFT GALLEY AREA. REPLACED SEAT TRACK -Y765 AND FASTENERS LOC BTW FR64 TO FR66 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72-11. (1182280).Sep 4, 2025 · N352NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025090506579Bushing · excess playEXCESSIVE PLAY, PASSENGER CREW DOOR 841 UPPER AND LOWER BUSHING BETWEEN DOOR AND SUPPORT ARM AT FWD GALLEY AREA. REMOVED AND REPLACED BUSHINGS BETWEEN UPPER AND LOWER CONNECTION LINK AND SUPPORT ARM PASSENGER CREW DOOR 841 IAW FAM AMM 52-11-21-000-001-A,AS PSep 4, 2025 · N352NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA2025090506578Floor Support · corrodedCORROSION FLOOR SUPPORT Y160.5 AT LEVEL FR68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT Y160.5, HARD POINT (2EA) AND FASTENERS LOCATED BETWEEN FR 68 TO FR 70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AS PER A319 SRM 51-72-11. (1182265).Sep 4, 2025 · N352NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2025090506577Seat Track · corrodedCORROSION SEAT TRACK -Y1292 LOCATED AT FR 66 AT AFT GALLEY AREA. REPLACED SEAT TRACK -Y1292 AND FASTENERS LOC BTW FR64 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1182258).Sep 4, 2025 · N352NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025090506576Floor Support · corrodedCORROSION FLOORBEAM +Y765 LOCATED AT LEVEL FR68 AT AFT GALLEY AREA. REPLACED FLOORBEAM Y765 AND FASTENERS LOC BETWEEN FR67 TO FR70 AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1182208).Sep 4, 2025 · N352NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2025090506575Floorbeam · corrodedCORROSION FLOOR BEAM -Y254 LOCATED BTW FR 18 TO FR 20 AT FWD GALLEY A REA . REPLACED FLOOR BEAM -Y254 AND FASTENERS LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1182178).Sep 4, 2025 · N352NB · Airbus A319114 · Fuselage Main, Floor Beam
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