Airbus A320-232
Service difficulty reports · 32,653
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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.
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 YENA2018061420242Frame · crackedDURING HEAVY MAINTENANCE, FRAME 36 HAD CRACK INDICATIONS. REPAIRED THE FRAME IAW SRM 51-44-11, 57-72-11, AND 57-16-00, FIG 002.SDR YENA2018061420241Frame · crackedDURING HEAVY MAINTENANCE, FRAME 36 LEFT ATTACHMENT HOLES 6, 7, 8, 9, AND 18 HAD CRACK INDICATIONS. REPAIRED THE FRAME IAW SRM 51-44-11, 57-72-11, AND 57-16-00, FIG 002.SDR YENA201806120239Battery Pack · no testEMERGENCY LIGHT FAILED TO TEST. R & R THE EMERGENCY LIGHT BATTERY AT EPSU 10WL IAW AMM 33-51-38.SDR YENA201806110922Pressure Panel · crackedDURING HEAVY MAINTENANCE, CRACKS WERE FOUND ON MULTIPLE HOLES. REFER TO EC A18-465-01. FUSELAGE / CENTER FUSELAGE / FR36 LT PRESSURE PANEL (ACCOMPLISHMENT OF SB 53-1263) CRACKED FASTENER HOLES - TEMPORARY REPAIR; THIS TEMPORARY REPAIR IS APPROVED PER REF /2/ RSDR YENA2018100510504Beam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BEAM FR67-FR68; REF LHT NR 5000765532-0010. CORR BEAM FR67-FR68 -Y1162 RPL BEAM PER SRM 51-72-11-911-001.SDR YENA2018100510505Beam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BEAM FR68-FR69 Y1162; REF LHT NR 5000765501-0010: FLOOR BEAM CORR BEYOND BLEND LIM RPL PER SRM 51-72-11-911-001SDR YENA2018100510503Beam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BEAM FR68-FR69 Y1162; REF LHT NR 5000765501-0010: BEAM BEYOND BLEND LIM RPL PER SRM 51-72-11-911-001SDR CALA2018062101457Plate · corrodedCORROSION FOUND ON A PLATE BETWEEN STRINGER 42 AND 43R IN THE FWD CARGO BILGE AREA, FRAME 26. REMOVED THE CORRODED FISH PLATE. INSTALLED A NEW FISH PLATE. ROTO PROBE PERFORMED ON OPEN HOLES SHOWED NO DEFECTS. RESTORED SURFACE PROTECTION. IAW SRM 51-72-11-911SDR CALA2018062101463Circuit Breaker · brokenEMERGENCY LIGHT CIRCUIT BREAKER H5, WAS BROKEN. REPLACED THE CIRCUIT BREAKER IAW ESPM 20-46-10 IDT.SDR CALA2018062101456Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 42 AND 43R IN THE FWD BILGE AREA AT FRAME 33. REMOVED AND REPLACED THE FISHPLATE, HOLES WERE ROTO PROBED, NO DEFECTS FOUND. RESTORED SURFACE PROTECTION IAW SRM 51-72-11-9 11-001, ER5100R01017, REV E, AND NTSDR AALA2018061829011Engine · failedAT 4000 FEET, AN ECAM MESSAGE FOR ENG 1 FAIL ILLUMINATED, EGT IN RED, FOLLOWED ECAM PROCEDURES RESULTING IN MANUAL SHUTDOWN OF THE RIGHT ENGINE. DIVERTED, AIRCRAFT FLEW ON A SINGLE ENGINE FOR 25 MINUTES. EMERGENCY WAS DECLARED AND LANDED WITHOUT INCIDENT. SDR GTIA2018061412694Unknown · odorAFT FLIGHT ATENDANT REPORTED FUMES DURING THE NR 1 ENGINE START. INSPECTED THE SEAL ON THE ENGINES, NO DEFECTS IAW AMM 72-60-29. INSPECTED APU, NO EVIDENCE OF LEAKS. PERFORMED A NR 1 & 2 ENGINE RUN UP. NO ODOR IAW AMM 71-00-00. CAN NOT DUPLICATE THE ODOR,SDR GTIA201806110694Megaphone · inoperativeL1 DOOR MEGAPHONE INOPERATIVE. R & R THE MEGAPHONE.SDR CALA2018062101449Stringer · corrodedCORROSION ALONG STRINGER 40R BETWEEN FRAMES 32 AND 33 IN THE FWD CARGO BILGE AREA. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-13-283-001. INSTALLED A REPAIR IAW SRM 53-21-13-300-004.SDR CALA2018062101448Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 42 AND 43R, FRAME 29, IN THE FWD CARGO BILGE. REMOVED & REPLACED THE FISH PLATE IAW SRM 51-72-11-911-001, PERFORMED ROTO PROBE IAW NTM 51-10-0 1, NO DEFECTS FOUND. RESTORED PROTECTIVE FINISH IAW SRM 51-75 SDR CALA2018062101447Wire Harness · damagedEEPL HARNESS BETWEEN SEAT ROW 29 TO 31 HAS DAMAGED INSULATION. REMOVED AND REPLACED EEPL HARNESS BETWEEN SEAT ROW 29 TO 31 IAW AMM 33-51-22-400-802C1. OPS TESTS TO BE PERFORMED.SDR GTIA2018061002693Bottle · low pressureDURING A WEEKLY CHECK, FOUND THE L1 DOOR ASSIST BOTTLE BELOW LIMITS. SERVICED THE L1 DOOR ASSIST BOTTLE IAW 52-10-00.SDR GTIA2018061102692A/C Pack · odorDURING CRUISE, A FOUL ODOR WAS REPORTED IN THE AFT GALLEY. PERFORMED 3.226.1, TURNED OFF THE NR 2 PACK. ODOR DISSIPATED, PERFORMED TSM 05-50-00.SDR CALA2018062101445Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGER 43 AND 44L, IN THE FWD CARGO BILGE AREA, FRAME 27. REMOVED THE FISH PLATE, HOLES WERE ROTO PROBED. NO DEFECTS NOTED. INSTALLED A NEW FISH PLATE, RESTORED SURFACE PROTECTION IAW SRM 51-72-11-911-001, NTM 51SDR AALA201806119053Fastener · unsecureAIRCRAFT WAS NOT GROUNDED: RIGHT OVERWING SLIDE CONTAINER HAD ONE FASTENER AT LOWER AFT NOT SECURED. MAINTENANCE INSTALLED CORRECT LENGTH STUD AS REQUIRED AND PERFORMED SATISFACTORY OPERATIONAL CHECK.SDR GTIA2018061192690Unknown · odorFLIGHT ATTENDANTS AND PASSENGERS COMPLAINED OF A FOUL ODOR THROUGHOUT ENTIRE CABIN. ODOR SIMILAR TO DIRTY CAT LITTER. RAN BOTH ENGINES AND APU TO ISOLATE BLEED SORCES, FOUND NO DIRTY CAT LITTER ODOR COMING FROM EITHER THE ENGINES OR APU IAW AMM 71-00-00 AND SDR GTIA201806110689Unknown · odorMULTIPLE FLIGHT ATTENDANTS AND PASSENGERS REPORTED A STRONG DIRTY SOCK ODOR MOSTLY ROWS 8 - 10. PERFORMED TSM 05-50-00-810-831-A. PERFORMED ENGINE RUNS & PACK BURN OUT IAW TSM 71-00-00-810-801, AND 21-00-00-810-802. NO EVIDENCE OF ODOR NOTED. AIRCRAFT OK FORSDR GTIA2018061102688Unknown · odorFA'S REPORT A DIRTY SOCK ODOR IN THE FWD CABIN. TROUBLESHOT IAW TSM 5-50-00. ACFT ON GROUND SOURCE, REMOVED AND PUT AIRCRAFT ON PACKS SYS. NO ODOR NOTED, OK TO CONTINUE.SDR CALA2018062101444Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 43 AND 44R IN THE CARGO BILGE AREA, FRAME 26. REMOVED THE FISH PLATE, HOLES WERE ROTO PROBED, NO DEFECTS NOTED. LOCATED, DRILLED AND INSTALLED A NEW FISHPLATE. RESTORED SURFACE PROTECTION IAW SRM 51-72-SDR AALA201806199002Hinge Fitting · wornTHE NR SPOILER HINGE, CENTER FITTING WAS FOUND TO BE WORN, WS 924 TO 970, RIB 17. REPAIRED THE HINGE FITTING IAW SRM 57-70-00-300-003, FIG 20101, SHEET 2.SDR AALA201806089013Slide · deterioratedTHE AIRCRAFT IS IN BASE MAINTENANCE. DETERIORATED ENCLOSURE OFFWING ESCAPE SLIDE COMPOUND ON LEFT HAND WING. REPLACED ENCLOSURE OFFWING SCAPE SLIDE ON LEFT HAND WING PER AMM 25-62-42-400-001-A.SDR CALA2018062101442Torsion Box · corrodedAFT CARGO BAY ENTRY TORSION BOX HAD CORROSION. PERFORMED A REPAIR IAW AVO DLH 240518-4655-2501782-07, AND ECRA 5341-01120.SDR CALA2018062101441Stringer Splice · corrodedCORROSION ON STRINGER SPLICE 43R, BETWEEN FRAMES 27 AND 28 REMOVED AND REPLACED STRINGER SPLICE AT STR 43R BETWEEN FR 27-FR 28. OPEN HOLES ROTOPROBED, NO DEFECTS NOTED. RESTORED SURFACE PR OTECTION. IAW A320 SRM 51-42-11-001, SRM 51-72-11-911-001, NTM 5 1-10-SDR AALA2018061289019Apu · odorODOR IN CABIN, REPORTED BY FLIGHT ATTENDANT, AFT AND REPORTED A DIRTY SOCK ODOR DURING DESCENT. ACCOMPLISHED J/C 26L00021001 AND J/C 26L00021002, FOUND APU TO BE SOURCE OF CABIN ODOR. THE AIRCRAFT WAS GROUNDED.SDR AALA201806119002Sign · missingSMALL EXIT SIGN ON LOWER PART OF THE L2 DOOR WAS MISSING. REPLACED EXIT SIGN, OK FOR SERVICE.SDR AALA201806089020Girt Bar · obstructedAIRCRAFT WAS NOT GROUNDED. 2L DOOR DIFFICULT TO ARM. REMOVED DEBRIS FROM GIRT BAR, OPERATIONS CHECK GOOD.SDR YENA201806070236Battery Pack · inoperativeDURING A CABIN EMERGENCY LIGHT TEST, FAILED FOR EMERGENCY LIGHT 12WL. REMOVED AND REPLACED THE EPSU 12WL BATTERY PACK IAW AMM 33-51-38-000-002-A, AND 33-51-38-400-002-A. OPS TESTED GOOD IAW AMM 33-54-38-805-058-A. OPENSDR CALA2018062101440Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE 41L FRAMES 30 AND 31. REMOVED AND REPLACED THE STRINGER SPLICE, NO DEFECTS NOTED. RESTORED SURFACE PROTECTION IAW SRM 51-42-11-001, SRM 51-44-11-001, NTM51-10-01, SRM 51-72-11-911-001, ER 5100R01017, REV E, AND NON-ROUTISDR AALA2018060869031Wedge · delaminatedRIGHT WING OUTBOARD TRAILING EDGE FLAP WEDGE DELAMINATED. REPLACED THE FLAP WEDGE. AIRCRAFT WAS GROUNDED.SDR GTIA201806072684Smoke Warning · false activationFWD CARGO SMOKE DURING CLIMB OUT, RETURNED TO DEPARTURE. R & R THE FWD CARGO SMOKE DETECTORS 1WH AND 2WH AS A PRECAUTION IAW AMM 26-16-15. PERFORMED AN OPS TEST OF THE SMOKE DETECTION SYSTEM IAW AMM 26-16-00. OPS TESTED GOOD. NO FAULTS NOTED.SDR AALA201806079006Seal · tornTORN PRESSURE SEAL WINDSHIELD, LEFT COCKPIT. REPLACED THE WINSHIELD IAW 26C00053065.SDR AALA201806079005Seal · tornTORN PRESSURE SEAL ON THE RIGHT WINDSHIELD. REPLACED THE WINSHIELD IAW 26C00035015.SDR YENA201806050923Structure · corrodedFLT 391, BOS-TPA. DURING WALK AROUND FOUND INTER-GRANULAR CORROSION AT RT REAR FUSELAGE AT LAV EXHAUST; REF NR 440510-38011-REPAIRED IAW SRM 53-41-11-300-004 AND EC A18-475-01. THIS REPAIR HAS BEEN APPROVED PER THE REF/4/ RDAS. PER THE MAJOR/ MINOR CLASSIFICATSDR CALA2018060601437Plate · corrodedCORROSION WAS FOUND ON THE FISH PLATE BETWEEN STRINGERS 41R AND 42R, FRAME 34 IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED FISH PLATE IAW SRM 51-72-11-9 11-001, NTM 51-10-01, AND ER 5100R01017, REV E.SDR CALA2018060601436Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 42R AND 43R, FRAME 27, IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51-72-11-911-001, NTM 51-10-01, AND ER 5100R01017, REV, E.SDR CALA2018060601435Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 42R AND 43R, FRAME 31 IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51- 72-11-911-001, NTM 51-10-01, AND ER 5100R01017, REV E.SDR CALA2018060601434Shear Tie · corrodedCORROSION FOUND ON THE SHEAR TIE AT FRAME 31, BETWEEN STRINGERS 38R AND 39R, IN THE CARGO BILGE AREA. REMOVED, FABRICATED, AND INSTALLED A SHEAR TIE IAW SRM 51-75-12- 911-002, 51-72-11-911-001, 56-26-00, 51-21-11, 51-23-00, ER5100R0 1017, REV E, AND NTM 51SDR CALA2018060601433Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 42 AND 43R, FRAME 32 IN THE CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51-72-11-001, SRM 51-72-11-911-001, NTM 51-10-01, AND ER 5100R01017, REV E.SDR YENA2018061100238Slide · damagedFOUND THE A SECTION OF THE ESCAPE SLIDE RAFT UNFOLDED. REMOVED AND REPLACED THE SLIDE IAW AMM 25-62-44-000-012-A, AND 25-62-44-400-007-A. OPENSDR AALA2018060869034Switch · inoperativeINOPERATIVE CENTER TANK PUMP NR 2 WARNING OCCURRED 20 MINUTES AFTER TAKEOFF. CENTER TANK EMPTY. REPLACED CENTER TANK NR 2 SWITCH 34QA IAW AMM 28-21-00. OPS CHECKED GOOD.SDR AALA2018060769011Lens · missingONE EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS.SDR AALA2018060769032Lens · missingEMERGENCY LIGHT LENS MISSING, SEAT 3 LEFT. REPLACED THE LENS IAW AMM 33-51-11. OPS CHECKED GOOD.SDR AALA2018061189023Pump · leakingDIRTY MUSTY ODOR THROUGHOUT AIRCRAFT. MAINTENANCE ACCOMPLISHED JC 26L00021004, 26T31049004, 26L00021002, AND 26L00021001. MAINTENANCE ALSO REPLACED THE APU LUBRICATION PUMP FITTING IAW MM 49-91-45, APU TURBINE CAVITY VENT O-RINGS IAW MM 49-91-34, AND PERFORMSDR GTIA2018060742682Unknown · odorDURING APPROACH, AT 4000 FT, THE FLIGHT ATTENDENT DETECTED A BURNING RUBBER ODOR IN THE REAR OF THE AIRCRAFT. PERFORMED TSM 05-50-00-810-831-A, NO ODOR SOURCE IDENTIFIED. ACFT OKAY FOR SERVICE.SDR YENA2018060430234Battery Pack · failedEMERGENCY LIGHT FAILED TO TEST. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY AT EPSU 12WL IAW AMM 33-51-38 OPS CHECKED GOOD.
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