Airbus A320-232
Service difficulty reports · 32,652
Newest first. General aviation reporting is voluntary.
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AALA202510068077Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON MEASURES ARE L:13.380 INCH, W: 1.328 INCH, D= 0.005INCH. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE LOC. ON RH PYLON IAW A320 SRM 54-51-12-300-002.SDR AALA202509268562Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE, CORROSION ON UPPER BOLT AT AFT ATTACH FITTING ON LT PYLON L=0.017 INCH, W=0.033, INCH AND D=0.011 INCH. MAINTENANCE REPLACED BOLT.SDR GTIA2025091139070Unknown · odorCABIN ODOR IN FLIGHT. AIR QUALITY FORM SUBMITTED. DESCRIPTION OF ODOR/FUMES: CONTINUOUS AND DISCOMFORTABLE, DIRTY SOCKS/MUSTY DRY/ BODY ODOR/ BIOHAZED/WASTE SMELL. APPRENT CABIN SOURCE: UNKNOWN. FWD CABIN/GALLEY(LAV), MID CABIN, AND AFT CABIN/GALLEY(LAV). NO VSDR CALA2025091108756None · noneRIGHT OVERWING SLIDE INFLATION BOTTLE PINNED FOM, REMOVED PIN, REACTIVATED RH BOTTLE REF AMM 25-62-00-081-001-A. VERIFIED REMOVAL OF THE PIN FROM THE R/H OFF WING SLIDE BOTTLE IN REF TO AMM 25-62-00-061-001-A.SDR CALA2025091108754Control Panel · malfunctionedLIGHT ON PANEL 2L INOPERATIVE, CONFIRMED LT CONTROL PANEL AT L2 DOOR WOULD NOT COMMAND THE AFT ENTRY LIGHTS ON. RESET CONTROL PANEL. AFT ENTRY LTS NOW COMMAND NORMAL. IAW AMM 33-21-00-710-801SDR CALA2025091008726Fan · faultedNOTICED BURNING SMELL COMING FROM UPPER VENT BY COCKPIT ENTRY DOOR AND AMBER 'FAN' WARNING ON AIRCONDITIONING ECAM PAGE COMPLETED CABIN TEMP CONTROL TEST REF AMM TASK 21-21-00-710-052-B AND TEST FAILED. RECIEVED 'RECIRC FAN 2 OR SUPPLY' MESSAGE CREATED SEPERATSDR CALA2025091008714Sensor · out of alignmentDOOR R FWD EMER EXIT ECAM. DOOR IND OPEN. PRESS NORMAL PERFORMED RENDER SAFE FOR RT FWD OVERWING EXIT HATCH. SLIDE INDICATION OF HATCH IS DEFECTIVE ON LOWER ECAM, HATCH IS IN THE ARM MODE, EMERGENCY EXIT INDICATION IS DEFECTIVE ON LOWER ECAM DU, HATCH IS COSDR YENA2025090900919Warning Light · false activationFLT#1251, HPN-RSW. "MULTIPLE DOOR/SLIDE INDICATORS DURING TAXI OUT INDIACTING SLIDES DISARMED WHEN THEY WERE ARMED; C/W WITH RESET OF PAX DOORS SLIDE INDIACTION SYSTEM IAW TSM 52-11-00 C/W WITH ARMING AND DIARAMING PROCEDURES.NO FAULTS NOTED.A/C OK FOR SVC."SDR YENA2025090900918Unknown · odorFLT#1904, RDU-SJU. FUMES EVENT ODOR REPORT SUBMITED DESCENDING THRU 10,700 FT, FLT CREW EXPERIENCED BURNING OF NOSE AND THROAT, CHEMICAL ODOR, PACK 1 ISOLATED, FUMES DISIPATED SLOWLY. REPEAT EVENT. OPENSDR CALA2025090908667Battery · no testCABIN EMER LIGHTING OPS CHK FAIL REPLACE LT EPSU BATTERY REPLACED LT EPSU IAW 33-51-38-400-002-A OPS CHK PASSED.SDR AALA202510230580Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM -Y765 BTW FR 64 TO FR 66 AT AFT GALLEY AREA CORROSION ARE: L:0.378 IN. W=0.500 IN. D=0.019. MAINTENANCE REPLACED FLOOR BEAM -Y765 BTW FR 64 TO FR 66 AT AFT GALLEY AREA I.A.W A320 SRM 51-42-11-801 AND DWG SDR AALA202510155351Shackle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SHACKLES AFT ON RH PYLON. MEASURE CORROSION ARE L=0.020 INCH W=0.020 INCH D=0.001 INCH. MAINTENANCE REPLACED SHACKLE FITTING ASSY IAW JC 26C42554028.SDR AALA202510147260Shackle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SHACKLES AFT ON RH PYLON MEASURE CORROSION ARE L=0.020 INCH W=0.025 INCH D=0.001. MAINTENANCE REPLACED SHACKLES FITTING ASSY WITH IDENTIACAL PART IAW JOB CARD 26C42554028.SDR AALA202510149455Shackle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SHACKLES FWD INB SIDE ON RH PYLON (CPCP 545116-01) MEASURE CORROSION ARE L=0.024 INCH W=0.020 INCH D=0.001 INCH. MAINTENANCE REPLACED SHACKLE FITTING ASSY WITH IDENTICAL PART.SDR CALA2025091008710Lamp · inoperativeDOOR 1R ENTRY LT INOP. REQUESTING MEL 3320A MEL 3320A APPROVED STICKER APPLIED. RELAMPED OPS CHECK GOOD.SDR CALA2025090908643Power Supply · inoperativeCAPTAIN`S FWD LEFT MESSAGE DISPLAYED AFTER CAPACITY TEST WAS PERFORMED. REMOVED AND REPLACED BATTERY FOR EMERGENCY POWER SUPPLY IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A.SDR CALA2025091008720Unknown · odorFLIGHT CREW CLAIMS TO HAVE SMELLED A LIGHT ODOR IN CABIN AREA WHEN TURNING ON APU BLEED FOR AIR COND, IN COCKPIT AREA AND GALLEY AREAS FLIGHT CREW EXPOUNDED THAT ODOR WAS NOT THAT OF BURNING OR OF SMOKE, BUT A DIFFERENT KIND OF ODOR. RAN APU WITH APU BLEED OPSDR CALA2025090908664Pin · installedINSTALLED L2 DOOR SLIDE ARM HANDLE PIN & DOOR DAMPNER PIN. REMOVED L2 DOOR SLIDE ARM HANDLE SAFETY PIN AND DOOR DAMPNER PIN, SAFETIED DOOR DAMPNER KNOB. REF. AMM 25-62-44-400-006-A. VERIFIED L2 DOOR SLIDE ARM HANDLE SAFETY PIN AND DOOR DAMPNER PIN REMOVAL, SASDR CALA2025090908639Seat Track · corrodedY1292 HAS CORROSION FR12-24. SEAT TRACK AT Y1292 FR12-24 FOUND TO BE OUT OF LIMITS WITH A DEP TH OF .041" AND A MAX ALLOWED DEPTH OF .031" IAW A320 SRM 53-11- 14-283-007 REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-11 -911-001 AND SRM 51-42-11.SDR CALA2025090908638Seat Track · corroded-Y1292 HAS CORROSION JUST FWD OF FR 20. EVALUATED FOUND OUT OF LIMITS IAW SRM 53-11-15-283-011 REMOVED A ND REPLACED -Y1292 FR12-FR24 IAW SRM 51-42-11/001.SDR CALA2025090908637Structure · corrodedY503.2 HAS CORROSION FR12-16. EVALUATED BEAM Y503.2 FOUND TO BE OUT OF LIMITS IAW SRM 53- 11-14-283-001, REMOVED AND REPLACED Y503.2 AS REQUIRED IAW A 320 SRM 51-42-11/001.SDR GTIA2025090839068Megaphone · inoperativeAFT MEGAPHONE INOP. R & R AFT MEGAPHONE IAW AMM 25-65-51 OPS TEST OKSDR CALA2025090808568None · noneODD SMELL NOTICED BY MULTIPLE CREW MOSTLY IN COCKPIT, GLUEY-ISH IN NATURE UPON INSPECTION FOUND SMELL COMING FROM JET BRIDGE /PC AIR. COULD NOT FIND ANY ISSUES WITH ACFT. INSPECTED E&E BAYS, NO DEFECTS NOTED AT THIS TIME.SDR AALA202510311622Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOOR BEAM COMMON TO VERTICAL STRINGER 2L AT FR 36, AND Y765, CENTER WING BOX FRONT SPAR, FORWARD CARGO COMPARTMENT. REPAIRED FLOOR BEAM PER EA 367962SDR AALA202510319224Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOOR BEAM COMMON TO VERTICAL STRINGER 3L AT FR 36, AND Y254, CENTER WING BOX FRONT SPAR, FORWARD CARGO COMPARTMENT. REPAIRED FLOOR BEAM PER EA 367962SDR AALA202510311486Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOOR BEAM COMMON TO VERTICAL STRINGER 4R AT FR 36, AND -Y254, CENTER FORWARD CARGO COMPARTMENT. REPAIRED FLOOR BEAM PER EA 367962SDR AALA202510239031Stringer Splice · damagedAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE ON LOWER SPLICE OUTBOARD SIDE ON LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA. MEASURE IS 0.043 IN. MAINTENANCE REPLACED LOWER SPLICE OUTBOARD SIDE ON LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA, IASDR AALA202510236165Stringer Splice · damagedAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE ON UPPER SPLICE INBOARD SIDE ON LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA. MEASURE IS 0.049 IN. MAINTENANCE REPLACED UPPER SPLICE INBOARD SIDE LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA, IAW A320 SRM 51-72SDR AALA202510233940Stringer Splice · elongatedAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE ON UPPER SPLICE OUTBOARD SIDE ON LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA. MEASURE IS 0.05 IN. MAINTENANCE REPLACED UPPER SPLICE OUTBOARD SIDE LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA, IAW A3SDR AALA202510235799Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL STR 23R AT LEVEL FR68 AFT GALLEY AREA (CPCP 534195-1).CORROSION MEASURE L=3.870 IN, W=2.035 IN, D=0.030 IN. MAINTENANCE REPLACED LOWER SILL LOC. STR23R AT LEVEL FR68 AFT GALLEY AREA IAW A320 SRM 51-72-11-911-SDR AALA202510239373Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SEAT TRACK -Y1162.5 AT LEVEL FR 68 AFT GALLEY AREA (CPCPC 5341 95-01) MEASURES OF CORROSION ARE L: 0.898 INCH, W: 0.540 INCH, D: 0.034 INCH. MAINTENANCE REPLACED SEAT TRACK -Y1162.5 AT LEVEL FR68 TO FR69 AFT GALLEY AREASDR AALA202510238657Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 L BTW FR 69 AND FR 70 AT AFT GALLEY AREA. L= 0.780 INCHES. MAINTENANCE REPLACED SHEAR PLATE STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA IAW A32O SRM 51-42-11-801, SRM 51-72-11-911-001 AND DWG D58474180.SDR AALA202510148261Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING STR 23L BTW FR66 AND FR68 AFT GALLEY AREA. MEASURES OF CORROSION: L= 5.279 IN W=1.586IN D= 0.080 IN. MAINTENANCE REPLACED CENTER FITTING LOCATED STR 23L BTW FR 66 AND FR 68 AFT GALLEY AREA IAW A320 SRM 51SDR AALA202510088256Dummy Rail · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR DUMMY RAIL AT FR 16 AT +Y503.2. REPLACED DUMMY RAIL PER SRM 51-72-11.SDR AALA202510087062Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PER RM 51-72-11.SDR CALA2025091708994Plate · corrodedAFT PIT CORROSION AT 38R PROFILE FR 52. REMOVED AND REPLACED CORRODED PROFILE PANEL AT FR43-FR52A IAW SRM 51-72-11.SDR CALA2025090908669Drain Valve · leakingFLIGHT CREW REPORT WATER LEAKING IN FWD LAV AND SEEPING INTO FIRST CLASS. WATER LEAKING FROM FWD LAV CHECK FWD LAV FOR LEAKS CHECK WATER HEATER AND PLUMING SUSPECT THE DIAPHRAGM IS CAUSING THE LEAK DRAIN VALVE SUSPECTED TO BE FAILING. REMOVED AND REPLACED FWDSDR CALA2025090908663Slide · no discrepancyDOOR 2L SLIDE PACK ASSEMBLY REMOVED TO FOM IAW AMM 25-62-44-000-002-A. REINSTALLED L2 DOOR SLIDE PACK ASSEMBLY AFTER DOOR MAINTENANCE REF. AMM 25-62-44-400-006-A. C/W GMM 09-25-05 RII FOR REINSTALLATION OF L2 DOOR MOUNTED ESCAPE SLIDE PACK ASSY REF AMM 25-6SDR CALA2025090908661Handle · unknownDUE TO REPORTS OF DOOR 2L SLIDE ARM HANDLE NOT REMAINING ARMED IN FLIGHT. ADJUSTMENT/TEST OF THE RELEASE MECHANISM OF THE EMERGENCY ESCAPE SLIDE FOUND SOLID CONTACT BETWEEN THE STOP AND THE EMERGENCY CONTROL HANDLE IN THE ARMED POSITION, NO ASJUSTMENT REQUIRESDR CALA2025090808597Proximity Switch · out of adjustDOOR 2L WILL NOT ARM SHOWS CABIN PRESS LIGHT ARMED ON GROUND, FAILED IN FLIGHT FOUND PRESSURE LIGHT INTERMITTENT WHILE ARMED. WIGGLING HANDLE CAUSES LIGHT TO FLICKER.ADJUSTED EMERGENCY SLIDE ARM PROXIMITY SWITCH 7WN1 TARGET REF MM 52-71-00-820-002-A. TESTED SWSDR CALA2025090808586Floor Support · corrodedFLOOR SUPPORT AT Y765 HAS CORROSION FR12-24. REMOVED AND REPLACED FLOOR SUPPORT Y765 AT FR 12-24 IAW A320 SRM 51 -72-11.SDR AALA202511192809Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE (AFT-LOWER POSITION) LOCATED O N FR35 AT LEVEL OF STR30 RH SIDE, LOWER FUSELAGE. CRACK DEPTH = 0.108 INCHES APPROX, CRACK POSITION: 25 AND 8 OCLOCK LOOKING FROM OUTSIDE. MAINTENANCE ACCOMSDR AALA202511188310Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE (AFT-LOWER POSITION) LOCATED ON FR35 AT LEVEL OF STR30 LH SIDE, LOWER FUSELAGE. CRACK DEPTH = 0.100 INCHES APPROX, CRACK POSITION: 11 OCLOCK LOOKING FROM OUTSIDE. MAINTENANCE PERFORMED TIMESDR AALA202510280456Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 43L BTW FR 56 AND FR 57 IN AFT CARGO COMPARTMENT MEASURE OF CORROSION AREA L= 8.191 IN, W= 0.848 IN, D= 0.003 IN. MAINTENANCE PERFORMED PERMANENT REPAIR (SPLICE REPAIR) ON STRINGER 43L BTW FR55 TO FR58 IN AFT CSDR GTIA2025090839066Megaphone · faultedFORWARD FA MEGAPHONE TEST LIGHT NOT FLASHING-REMOVED AND REPLACED MEGAPHONE IAW AMM 25-65-51. OPS CHECK GOOD. AC OK FOR SERVICE, MOC #118486SDR YENA2025090800916Transmitter · failedFLT#1890, SHU-EWR. (AN EMERGENCY WAS DECLARED) "FL340 IN CRUISE ECAM ENG 1 OIL LO PR AMBER INDICATION. FROM 0 TO 224 FLUCTUATED WITH ALL OTHER INDICATIONS NORMAL; REMOVED AND REPLACED ENG #1 TRANSMITTER, OIL PRESS DIFF IAW AMM 79-34-00. ALL OPS CHK GOOD. FAULTSDR CALA2025090808580Seat Track · corrodedSEAT TRACK AT FR47-FR52 Y1292 MULTIPLE SPOTS OF CORROSION. REMOVED CORRODED SEAT TRACK Y1292 AT FR 47-FR52, INSTALLED SPLICE REPAIR AS REQUIRED IAW A320 SRM 53-41-15-300-003.SDR CALA2025090508520Battery · no testOPERATIONAL CHECK OF THE EMERGENCY POWER SUPPLY UNITS BY BITE-CHECK, EA2500-03960 AND EA2500-08031, REFERENCE EC2500-04561 FOR A/C 871-884, 888-899, 901-950 ) EMERGENCY LIGHTS TEST FAILED. MESSAGE EPSU BATTERY EMER L. POWER UNIT SHOWS BATTERY FAULT, REPLACESDR CALA2025090508514Lens · missingFOUND MISSING ESCAPE PATH LIGHT LENS ON SEAT 25ABC. INSTALLED LENS COVER AS REQUIRED IAW AIPC 33-51-19.SDR CALA2025090508495Cids · faultedEMER EXIT SIGN ON OVER WING AND OVER MCD STAYS ILLUMINATED ALL OTHER LTS REMAIN EXTIGUISHED TURNED OFF EMEGENCY LIGHT SWITCH AND PERFORMED FULL CIDS SYSTEM RESET. EMERGENCY LIGHTS EXTINGUISHED. CYCLED SWITCH IN ALL POSITIONS 3 TIMES. ALL EMERGENCY LIGHTS NOW O
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