Airbus A320-232

Service difficulty reports · 32,648

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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 aircraft_model_key = 'A320232'
  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 YENA2026033100362Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / LHS LOWER LATERAL PANEL / BTWN FR5-FR6 / EXISTING REWORKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0027-26 REV. 0 (COVER + PARTS 1-2) /2/ AIRBUS DOSSIER 81764255 /3/ AIRBUS RDAF 81764255/004/20Mar 27, 2026 · N662JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026033100361Structure · wornDURING HEAVY MAINTENANCE. WEAR ON VERTICAL MEMBER Y254 LOC ON FR24A ON FWD CARGO COMPARTMENT; REMOVED AND REPLACED VERTICAL MEMBER Y254 LOC FR24A ON FWD CARGO COMPARTMENT IAW AMM 25-54-81-400-801-A.Mar 27, 2026 · N662JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026033100360Structure · wornDURING HEAVY MAINTENANCE: WEAR ON VERTICAL MEMBER Y765 FR24A ON FWD CARGO COMPARTMENT; REMOVED AND REPLACED VERTICAL MEMBER Y765 FR24A ON FWD CARGO COMPARTMENT IAW AMM 25-54-81-400-801-A.Mar 27, 2026 · N662JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026033100359Skin · dentedDURING HEAVY MAINTENANCE: DAMAGE ON CAPT SIDE FUSELAGE BTWN FR 5 & 7 LOWER HALF DENTED. ACCOMPLISHED REPAIR OF EXISTING REWORKS NOSE FWD FUSELAGE LT LOWER LATERAL PANEL BTW FR 5 TO 6 IAW EA 53-0027-26, REV 0, & RDAF 81764255/004/2026, ISSUE A, & EC A26-248-Mar 27, 2026 · N662JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2026033014900Hydraulic Line · brokenIN FLIGHT ECAMG SYS LO PRESSUREG RSVR LO LVLG ENG1 PUMP LO PR LOCKING LOG CAPT STATED THEY FOLOWED PROCEDURES AFTER ECAM WARNING. PUMP RAN APROX 2MIN AFTER ECAM WARNING FOR G HYD LOW PRESS AS THEY FOLLOWED CHECKLIST. HYD FLUID COMING FROM ENG 1 PYLON. ZONE CMar 27, 2026 · N438UA · Airbus A320232 · Hydraulic System, MainSDR YENA2026032700344Air Filter · contaminatedFLT 808 SJU- BOS. AFTER ENG SHUTDOWN FA'S IN THE AFT CABIN COMPLAINED OF A DIRTY SOCKS ODOR AND THE ODOR WAS OBSERVED IN FORWARD CABIN. ODOR IN AFT DISSIPATED ONCE CATERING OPENED AFT DOOR. ; COMPLIED WITH INFO NOTICE 2017-T015 STEP 1, ISOLATED FAULT TO TYPE Mar 27, 2026 · N632JB · Airbus A320232 · Air Distribution SystemSDR YENA2026032700346Unknown · odorFLT # 961 LGA- PBI. STRONG DIRTY SOCK / OIL TCP FUMES IN CKPT AND CABIN PREVIOUS FA'S COMPLAINED OF FUMES ON LAST 2 DECENTS .; STRONG DIRTY SOCK / OIL TCP FUMES IN CKPT AND CABIN PREVIOUS FA'S COMPLAINED OF FUMES ON LAST 2 DECENTS.Mar 26, 2026 · N536JB · Airbus A320232 · Air Distribution SystemSDR GTIA2026032639337Flashlight · inoperativeR2 FA FLASHLIGHT INOP, R &R R2 FLASHLIGHT, OPS CHKD GOOD IAW CMM 25-60-13. THIS CLEARS DMI 6004608-1.Mar 26, 2026 · N630NK · Airbus A320232 · Emergency EquipmentSDR CALA2026032614840Door · out of rigF/A FOUND THAT DOOR 2L ARM/DISARM HANDLE MOVED OUT 1 INCH DURING FLIGHT.NO ECAM MESSAGE. ITEM LOCKED TO CONFIRM FINDINGS EMERGENCY ESCAPE SLIDE REF AMM 52-10-00-720-005-A. AT 2 LEFT AT APPROX 6 LBF RELEASE MECHANISM HANDLE BEGINS TO MOVE. UNLOCKED FOR UPDATINGMar 25, 2026 · N476UA · Airbus A320232 · Service DoorsSDR CALA2026032714859Skin · contaminatedLH TOP SKIN PANEL, FOUND LIQUID ENGRESS INDICATION AT 12 INCHES FROM I/B EDGE AND 14 INCHES FROM T/E DEFECT IS 1 INCH DIA. IN SI ZE. REPAIRED L/H ELEVATOR TOP SKIN 12IN FROM I/B 14IN FROM T/E 1.38I N DIG ZONE A IAW SRM 55-21-11-300-004 CATEGORY A REPAIR.Mar 24, 2026 · N488UA · Airbus A320232 · Elevator StructureSDR GTIA2026032639333Floor Support · corrodedCORROSION FLOOR SUPPORT TY254 LOC BTW FR12/ FR24 AT FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW DWG D53135202 ISSUE:A, D53911757 ISSUE:H AND D53212367 ISSUE: DOO.Mar 24, 2026 · N629NK · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2026032639332Support · corrodedCORRODED LOWER SUPPORT, STR 23L BTW FR 66 - 68 IN THE AFT GALLEY AREA. PERFORMED REPAIR INSTRUCTIONS ON THE LOWER SUPPORT IAW SRM 53-41-14-300-001. THIS REPAIR IS CATEGORY A.Mar 24, 2026 · N629NK · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2026032639331Seat Track · corrodedCORRODED SEAT TRACK, -Y765 IN THE AFT GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-42-11, DWG D53472816, ISSUE F, DWG D57472000, ISSUE A,, DWG D53472093, ISSUE F. REPAIR IS CATEGORY A.Mar 24, 2026 · N629NK · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA2026032639330Dummy Rail · corrodedCORRODED DUMMY RAIL, Y503.2, BTWN FR 12 - 16, IN THE FWD GALLEY AREA. REPLACED THE DUMMY RAIL IAW SRM 51-42-11, DWG D53112758, DWG D53110984, & DWG D53114410.Mar 24, 2026 · N629NK · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA2026032639329Seat Track · corrodedCORRODED SEAT TRACK, -Y254, BTWN FR 12 - 24, IN THE FWD GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-42-11, DWG D53135166, DWG D53911108, DWG D53212367, AND DWG D53135202.Mar 24, 2026 · N629NK · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA2026032639328Seat Track · corrodedCORRODED SEAT TRACK, +Y1162, BTWN FR 68 - 69 IN THE AFT GALLEY AREA. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53470150, ISSUE S, D53472088, ISSUE G, & D38370318.Mar 24, 2026 · N629NK · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA2026032639327Fitting · corrodedCORROSION ON LOWER CORNER CUTOUT, FRAME 28 IN FWD CARGO BAY. REPLACED THE FITTING ON THE LOWER CORNER CUTOUT IAW SRM 51-42-11, & DWG E53230005.Mar 24, 2026 · N629NK · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2026032639326Fitting · corrodedCORRODED CENTER FITTING, BTW FR 66 - 68, STR 23L AFT GALLEY AREA. REPLACED THE CENTER FITTING IAW SRM 51-42-11, AND DWG D53480009.Mar 24, 2026 · N629NK · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2026032639325Hinge Fitting · corrodedCORROSION FOUND ON LT ELEVATOR HINGE FITTINGS NR 1, 2, 3, AND 5. REPAIRED IAW SRM 55-26-41-300-010.Mar 24, 2026 · N629NK · Airbus A320232 · Elevator StructureSDR GTIA2026032639324Hinge Fitting · corrodedCORROSION FOUND ON HINGE FITTINGS, RT ELEVATOR, NR 1, 2, 3, AND 5, REPAIRED IAW SRM 55-26-41-300-010,Mar 24, 2026 · N629NK · Airbus A320232 · Elevator StructureSDR GTIA2026032639323Seat Track · corrodedCORROSION SEAT TRACK -Y1292, BTW FR 12 - 24 IN THE FWD GALLEY AREA, REPLACED THE SEAT TRACK IAW SRM 51-42-11, DWGS D53212367, D53112627, & D53135202.Mar 24, 2026 · N629NK · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA2026032639322Support · corrodedCORROSION LOWER SUPPORT, STR 23R, FR 66 - 68, IN THE AFT GALLEY AREA. PERFORMED A PERMANENT REPAIR ON THE SUPPORT IAW SRM 53-41-14-300-001,. THIS REPAIR IS CATEGORY A.Mar 24, 2026 · N629NK · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026032500340Unknown · odorFLT # 727 FLL-FLL. BURNING SMELL IN FLT DECK AND FWD GALLEY. FYI JUST PRIOR TO SMELL, THE PUSHBACK TUG HAD A BRAKE FAILURE WITH SMOKE.; COMPLIED WITH INFORMATION NOTICE 2017-T015 STEP 1. ISOLATED FAULT TO BE TYPE 10 PUSHBACK TUG BRAKE FAILURE WITH SMOKE. ACCOMMar 23, 2026 · N712JB · Airbus A320232 · Air Distribution SystemSDR YENA2026032500339Unknown · odorFLT # 525 PVD-SJU." INFLIGHT REPORTED FUMES EVENT ON DESCENT THROUGH 10,000'.; ACCOMPLISHED INFO NOTICE 2017-T015M, STEPS 1 AND 2 IDENTIFIED AS TYPE 9 ELECTRICAL. C/W TYPE 9 INSPECTION IAW AMM SUBTASK 05-50-00-810-085 NO TRIPPED C/B AND ELECTRICAL SMELL NOTED.Mar 23, 2026 · N608JB · Airbus A320232 · Air Distribution SystemSDR CALA2026032414817B-Nut · leakingCREW REPORTED HYD G RSVR LO LEVEL CREW REPORTED THAT THEY TURNED OFF THE PTU AND THE ENG DRIVEN PUMPP WITHIN A MIN OF THE ECAM SERVICED GREEN SYSTEM HYDRAULIC RESERVOIRS TO SERVICEABLE LIMITS REF AMM 12-12-29/301. FOUND GREEN HYD PRESSURE LINE B NUT LOOSE AND Mar 22, 2026 · N470UA · Airbus A320232 · Hydraulic Power Accumulator, MainSDR GTIA2026032339319Bottle · low pressureR1 DOOR ASSIST ACTUATOR PRESSURE LOW. SERVICED R1 DOOR ASSIST ACTUATOR PRESSURE IAW AMM 52-10-00.Mar 22, 2026 · N649NK · Airbus A320232 · Passenger/Crew DoorsSDR YENA2026032300329Unknown · odorFLT # 1371 LGA-FLL." SOCKS SMELL DURING FINAL APPROACH INTO FLL .; PER INFO NOTICE 2017-T015M, CHECKED TRAX FOR 30 DAY HISTORY, NONE FOUND, INSP. APU FOR LEAKS AND OIL LEVEL, ALL IN LIMITS AND GOOD, AND VERIFIED ENG OIL LEVELS AT CORRECT LEVELS. FAULT HAS BEENMar 22, 2026 · N793JB · Airbus A320232 · Air Distribution SystemSDR CALA2026032314762Skin · damagedLEFT TOP SKIN PANEL, FOUND LIQUID ENGRESS INDICATION AT 154.5 INCH ES FROM INBD EDGE AND 9 INCHES FROM T/E. DEFECT IS 1 INCH DIA. IN SIZE. REPAIRED LT ELEVATOR TOP SKIN 154.5 IN FROM INBD 9IN FROM T/E 1. 25IN DIA ZONE A IAW SRM 55-21-11-300-004, CATEGORY A REMar 22, 2026 · N488UA · Airbus A320232 · Horizontal Stabilizer, Plate/SkinSDR CALA2026032314760Lamp · inoperativeROW 38 EMERGENCY PATHWAY LIGHTING INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-38 PG. 601 AND TESTED IAW TASK 33-51-38-400-001-A. ALL EMERGENCY LIGHTS OPS CHECKED GOOD.Mar 22, 2026 · N444UA · Airbus A320232 · Emergency LightingSDR YENA2026032300330Apu · contaminatedFLT 610. SDQ-JFK, ( APU BLEED AIR SUPPLY SYSTEM ) FA'S REPORTED FUMES SIMILAR TO HYD FLUID ON T/O FROM SDQ THAT STARTED IN THE AFT SEC OF D/C. SAME THING OCCURED ON FINAL APP. THE APU WAS OFF IN BOTH OCCURANCES NO PHYSICAL SYMPTONS REPORTED BY CREW. THE ODOMar 21, 2026 · N652JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR YENA2026032300327Unknown · odorFLT # 291 BOS- TPA. " FLIGHT ATTENDANTS SMELLED DIRTY SOCK SMELL ON CLIMB OUT & DESCENT.; COMPLIED W/ INFO NOTICE 2017-T015 STEP 1 AND 2 IDENTIFIED ODOR AS TYPE 1 APU PLACED ON MEL ON ITEM 2. DECONTAMINATION LEVEL WAS ACCOMPLISHED PER AMM 21-00-00-615-802. A/CMar 21, 2026 · N828JB · Airbus A320232 · Air Distribution SystemSDR YENA2026032300328Unknown · odorFLT # 1068 PBI-HPN. "FLIGHT ATTENDANTS REPORTING ELECTRICAL BURNING ODOR DURING DESCENT. ODOR WAS INTERMITTENT. NO ODOR IN COCKPIT. ; AFTER FURTHER INSPECTION FWD FA REPORTED ODOR UPON DESCENT FOR APPROX 10-15 MIN. NO SIGNS OF SMOKE, NO BREAKERS POPPED. UPON IMar 20, 2026 · N746JB · Airbus A320232 · Air Distribution SystemSDR CALA2026032014710Light · inoperativePROCEDURE - EMERGENCY EXIT ROW LIGHTING AT SEAT 7C INOP REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7C, REF. AMM 33-51-19-000-002-A. OPERATIONAL TESTS OF CABIN EMERGENCY LIGHTING, REF. AMM 33-51-00-710-009-A. CHECKS NORMAL.Mar 19, 2026 · N473UA · Airbus A320232 · Emergency LightingSDR AALA202603196118Power Supply · no testAIRCRAFT WAS NOT GROUNDED: FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT 13WL DISPLAYED DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO FAMar 19, 2026 · N657AW · Airbus A320232 · Emergency LightingSDR YENA2026031600315A/C Pack · odorFLT # 149 JFK-GND." OIL SMELL COMING FROM FLIGHT DECK VENT AIR SMELL STOPPED WITH PACK 1 OFF PACK 1 VERY LOUD ON PRE FLIGHT .; COMPLIED WITH INFORMATION NOTICE 2017-T015 STEP 1 ISOLATED FAULT TO TYPE 10 (F) DIRTY CABIN SURFACE FURNISHINGS PER TSM 05-50-00-810-Mar 18, 2026 · N522JB · Airbus A320232 · Cabin Cooling SystemSDR GTIA2026031939315Hinge Fitting · corrodedCORROSION FOUN ON BOTH HOLES OF IB ACTUATOR AND OUTBOARD ACTUATOR ATTACH FITTINGS OF RH ELEVATOR, REPAIRED BY SRM 55-26-47-300-002. RAF01 6023862-2 CREATED.-REPAIRED INBOARD AND OUTBOARD ACTUATOR FITTINGS OF RH ELEVATOR IAW A320 SRM 55-26-47-300-002Mar 18, 2026 · N627NK · Airbus A320232 · Elevator StructureSDR GTIA2026031939314Hinge Fitting · corrodedCORROSION FOUN ON BOTH HOLES OF IB ACTUATOR AND OUTBOARD ACTUATOR ATTACH FITTINGS OF LH ELEVATOR, REPAIRED BY SRM 55-26-47-300-002, RAF01 6023862-2 CREATED.-REPAIRED INBOARD AND OUTBOARD ACTUATOR FITTING OF LH ELEVATOR IAW A320 SRM 55-26-47-300-002Mar 18, 2026 · N627NK · Airbus A320232 · Elevator StructureSDR GTIA2026031939313Hinge Fitting · corrodedCORROSION FOUN ON BOTH HOLES OF HINGE FITTING 4 OF LT ELEVATOR, RAF01 6023860-2 CREATED. REPAIRED AND REPLACED BUSHINGS (2 EA) ON HINGE FITTING #4 AT LH ELEVATOR IAW A320 SRM 55-26-41-300-005Mar 18, 2026 · N627NK · Airbus A320232 · Elevator StructureSDR GTIA2026031939312Stringer · corrodedCORRODED STRINGER 37L BTWN FR 63 & 64. PERFORMED PERMANENT REPAIR ON THE STRINGER IAW SRM 53-41-13-300-010. DWGS D534770320, E53470342, R53470320, E53474160, & EA 53-0019.Mar 18, 2026 · N627NK · Airbus A320232 · Fuselage Main, Longeron/StringerSDR GTIA2026031939311Dummy Rail · corrodedCORRODED DUMMY RAIL, Y503.2 AT FWD GALLEY AREA. REPLACED DUMMY RAIL Y503.2 LOC. FWD GALLEY AREA BTW FR12 TO FR16 IAW SRM 51-42-11, DWG D53114410, DWG D53114411, AND DWG D53110984.Mar 18, 2026 · N627NK · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA2026031939310Seat Track · corrodedCORROSION SEAT TRACK, +Y765, FR 12 TO FR 24. REPLACED SEAT TRACK IAW SRM 51-42-11, DWGS D53215367, D53114404, & D53135202.Mar 18, 2026 · N627NK · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA2026031939309Hinge Fitting · corrodedCORROSION FOUND ON HINGE FITTINGS 1, 3, & 5 REPAIRED IAW SRM 55-26-41-300-004.Mar 18, 2026 · N627NK · Airbus A320232 · Elevator StructureSDR GTIA2026031939308Hinge Fitting · corrodedCORROSION FOUN ON BOTH HOLES OF HINGE FITTING NR 6 OF LT ELEVATOR, FINAL HOLE DIAMETER IS 14.500MM. REPAIRED AND REPLACED BUSHINGS (2 EA) ON HINGE FITTING #6 AT LT ELEVATOR IAW SRM 55-26-41-300-006.Mar 18, 2026 · N627NK · Airbus A320232 · Elevator StructureSDR GTIA2026031939307Seat Track · corrodedCORROSION SEAT TRACK -Y1292 LOCATED FR 12 TO FR 24 AT FWD GALLEY AREA. REPLACED THE SEAT TRACK -Y1292, FR12 TO FR24 FWD GALLET AREA IAW SRM 51-42-11, DWG D53114407, D53135202, D53212367, AND D53925046.Mar 18, 2026 · N627NK · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA2026031939306Bushing · corrodedCORROSION FOUND ON BOTH HOLES OF HINGE FITTING 6 OF RT ELEVATOR, REPAIRED INBD LUG BORE AND REPLACED BUSHINGS (2 EA) ON HINGE FITTING NR 6 AT RT ELEVATOR IAW SRM 53-26-41-300-006.Mar 18, 2026 · N627NK · Airbus A320232 · Elevator StructureSDR GTIA2026031939305Bushing · corrodedCORROSION FOUND ON BOTH HOLES OF HINGE FITTINGS 4 OF RT ELEVATOR, REPAIRED AND REPLACED BUSHINGS (2 EA) ON HINGE FITTING NR 4 AT RT ELEVATOR IAW SRM 53-26-41-300-005.Mar 18, 2026 · N627NK · Airbus A320232 · Elevator StructureSDR GTIA2026031939304Hinge Fitting · corrodedCORROSION ON HINGE FITTING 1, 2, 3, & 5 LT ELEVATOR. REPAIRED THE HINGE FITTING NR 1, 2, 3, & 5 LT ELEVATOR IAW SRM 55-26-41-300-004.Mar 18, 2026 · N627NK · Airbus A320232 · Elevator StructureSDR GTIA2026031939303Seat Track · corrodedCORRODED SEAT TRACK, +Y1292, FR 12 TO FR 24 AT FWD GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-72-11, SRM 51-42-11, & DWG D53212367, D53111472, D53135202, & D53112627.Mar 18, 2026 · N627NK · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA2026031939302Seat Track · corrodedCORROSION SEAT TRACK +Y254, FR 12 - FR 24 AT FWD GALLEY AREA. REPLACED SEAT TRACK IAW SRM 51-42-11 AND DWG D53112816.Mar 18, 2026 · N627NK · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA2026031939301Seat Track · corrodedCORRODED SEAT TRACK -Y254, FR 12 - FR 24 FWD GALLEY AREA. REPLACED SEAT TRACK -Y254, FR 12 - FR 24 AT FWD GALLEY AREA IAW SRM 51-72-11, SRM 51-42-11, AND DWGS D53111462, D53135202, & D53212367.Mar 18, 2026 · N627NK · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
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