Airbus A320-232

Service difficulty reports · 32,653

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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 CALA2018060601422Door Sill · corrodedAFTER REMOVAL OF LOWER GIRT BAR FITTINGS AT THE L2 DOOR SILL, FRAMES 66 AND 68, CORROSION WAS FOUND. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 51-72-11-911-001.Jun 2, 2018 · N455UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018060601421Door Frame · corrodedCORROSION ON L2 DOOR AFT FRAME 68, BLENDED THE CORROSION IAW SRM 51-74-00-001. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-12-283-001, FIGURE 10102, (SHEET 1). ACCOMPLISHED HFEC AND ROTOPROBE OF BLENDED AREA IAW NTM 51 -10-02,51-10-01. NE DEFECTS NOTED.Jun 2, 2018 · N423UA · Airbus A320232 · Fuselage Main, StructureSDR AALA201806139013Hinge · wornAIRCRAFT WAS IN BASE MAINTENANCE. THE LEFT HAND MAIN LANDING GEAR DOOR HAS BORE AREA OF 1.2365 LOCATED AT FR 43 AND BL +Y254. REPLACED HINGE ASSEMBLY PER CMM 52-81-18 AND SRM 51-44-11.Jun 2, 2018 · N679AW · Airbus A320232 · Landing Gear DoorsSDR AALA201806059030Lamp · inoperativeLAVATORY D, RED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LAMPS, AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00-710-007A.Jun 2, 2018 · N601AW · Airbus A320232 · Emergency LightingSDR YENA201806042232Epsu · failedDURING HEAVY MAINTENANCE, EMERGENCY LIGHT TEST EPSU (10WL) WAS FOUND INOP; REMOVED & REPLACED EPSU 10WL AS REQUESTED BITE TEST ALL OPS CHECKS OK PER AMM 33-51-38-740-050-B REV 73.Jun 2, 2018 · N615JB · Airbus A320232 · Emergency LightingSDR GTIA2018060422680Bottle · low pressureR1 DOOR ASSIST ACCUMULATOR WAS LOW. SERVICED THE R1 DOOR ASSIST BOTTLE IAW AMM 52-10-00.Jun 2, 2018 · N651NK · Airbus A320232 · Emergency EquipmentSDR CALA2018060601416Stringer · corrodedCORRODED STRINGER 41R, FRAME 58. FOUND TO BE OUT OF LIMITS, NO DEFECTS NOTED. CUTOUT THE DAMAGE SECTION OF THE STRINGER BETWEEN FRAMES 58 TO 59, AND INSTALLED A REPAIR.Jun 1, 2018 · N423UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2018060601415Skin · dentedDENT FOUND IN THE LEFT LOWER FUSELAGE BETWEEN FRAMES 55 & 56 JUST ABOVE STRINGER 35L. CUT OUT THE DAMAGE & REPAIRED THE SKIN IAW SRM 53-00-11-300-042. ACCOMPLISHED HFEC OF CUTOUT & ROTO PROBE OF OPEN HOLES, NO CRACKS FOUND.Jun 1, 2018 · N423UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2018060601419Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 41R AND 42R, FRAME 33, IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED FISH PLATE IAW SRM 51-72-11-911-001, NTM 51-10-01, ER5100R01017, REV E.Jun 1, 2018 · N423UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2018060601418Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGER 43L AND 44L, FRAME 32 FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51-72-11-911-001, NTM 51-10-01, AND ER5100R01017, REV E.Jun 1, 2018 · N423UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018060601417Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGER 39R AND 40R, FRAME 32, IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE. PERFORMED A ROTO PROBE INSPECTION. NO CRACKS OR CORROSION NOTED.Jun 1, 2018 · N423UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201806059017Lens · missing4C EMERGENCY LIGHT LENS MISSING. R EPLACED THE LENS.Jun 1, 2018 · N601AW · Airbus A320232 · Emergency LightingSDR YENA2018060410233Lamp · inoperativeDURING A WEEKLY CHECK, THE R1 DOOR EXIT LIGHT WAS NOT WORKING. REPLACED THE LAMPS IAW AMM 33-51-13. OPS CHECKED GOOD.Jun 1, 2018 · N579JB · Airbus A320232 · Emergency LightingSDR CALA2018060541402Intercostal · crackedROTO PROBE INSPECTION SHOWS CRACK INDICATION 1R DOOR, FR16, DOOR STOP 1 (BOTTOM DOOR STOP) LOWER I/B HOLE AND UPPER I/B HOLE. PERFORMED ROTO PROBE INSPECTION OF SECOND HOLE ON THE INTERCOASTAL AT THE R1 DOOR STOP NR.1, FRAME 16, FOUND CRACKED AND WAS OUT OF LMay 31, 2018 · N455UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018060541401Intercostal · crackedROTO PROBE INSPECTION SHOWED A CRACK INDICATION IN HOLE AT FRAME 16, AT STOP NR .7, REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 5 1-72-11-911-001, AND AMM 52-11-31-420-051-A.May 31, 2018 · N455UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018060541400Intercostal · crackedROTO PROBE INSPECTION SHOWED A CRACK INDICATION ON THE R1 DOOR FRAME 16, AT DOOR STOP NR 7. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-72-11-911-0 01, AND SRM 52-11-31-400-002-A. RESTORED SURFACE. CRACK INDICATION FOUND ONLY ON THE INTERCOSTAL.May 31, 2018 · N455UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018060531399Plate · corrodedCORROSION ON FISH PLATE AT FRAME 31 BETWEEN STRINGERS 40 AND 41R, IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51-72-11-911-001, AND N TM 51-10-01.May 31, 2018 · N423UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018060531398Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 43L TO 43R, FRAME 33, IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51-42-11-001, NTM 51-10-01, AND SRM 51-72-11-911-001.May 31, 2018 · N423UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018060531397Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 43 AND 44R, FRAME 34, IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISHPLATE AND ANGLE IAW SRM 51-44-11-001, SRM 51-42-11-001, 51-75-12-001. ROTO PROBED THE OPEN HOLES IAW NTM 51-10-01, NO CRAMay 31, 2018 · N455UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2018060102678Unknown · odorFA REPORTED A SMOKE ODOR AFTER LIFTOFF, LASTING LESS THAN A MINUTE. SMOKE ONLY DETECTED IN THE GALLEY AND FIRST FEW ROWS. PERFORMED TSM 05-50-00-810-831-A, COULD NOT DUPLICATE THE ODOR. ACFT OK FOR SERVICE.May 31, 2018 · N625NK · Airbus A320232 · Air Distribution SystemSDR CALA2018060531393Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 41 AND 42L, FRAME 34, IN THE FWD CARGO BAY AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51-72-11-911-001. ACCOMPLISHED ROTO-PROBE OF OPEN HOLES, NO DEFECTS NOTED. REAMED UP FOUR FASTNERS HOLES TO .18May 30, 2018 · N423UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018060531392Frame · dentedAFT CARGO FRAME 53, STRINGERS 39 - 40L THE FRAME WAS DENTED. REMOVED AND REPLACED THE FRAME IAW SRM 57-72-11-911-001.May 30, 2018 · N423UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2018060501391Splice · crackedAFTER REMOVAL OF THE L2 DOOR SILL, THE FRAME 68, CROSSBEAM TO FRAME CONNECTION SPLICE WAS FOUND TO BE CRACKED. REMOVED AND REPLACED THE SPLICE IAW SRM 51-72-11-911-001.May 30, 2018 · N455UA · Airbus A320232 · Fuselage Main, Attach FittingsSDR CALA2018060501390Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 41 AND 42R, IN THE FWD CARGO BAY BILG E AREA, FRAME 32. REMOVED AND REPLACED THE FISHPLATE, HOLES ROTO PROBED, NO CRACKS, RESTORED SURFACE PROTECTION IAW SRM 51-42-11-001-2E, 51-75-12-911-002, NTM 51-1May 30, 2018 · N455UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018060501389Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGER 41 AND 42R SIDE IN THE FWD CARGO BAY BILGE AREA, FRAME 33. REMOVED AND REPLACED THE FISHPLATE HOLES ROTO PROBED, NO CRACKS DETECTED. RESTORED SURFACE PROTECTION IAW SRM 51-42-11-001-2E, 51-75-12-911-002, May 30, 2018 · N455UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018060501388Door Sill · corrodedR2 DOOR SILL CORRODED AT MULTIPLE AREAS. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11-911-001.May 30, 2018 · N455UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2018060192674Unknown · odorDESCENDING THROUGH FL 240, FIRST OFFICER SMELLED A SLIGHT CHEESE ODOR WHICH WENT STRONGER, CALLED F/A AND THEY REPORTED A SLIGHT SULFUR ODOR. RAN ODOR ELIMINATION PROCEDURE AND REMOVAL OF SMOKE BELOW 10,000. PERFORM AN ISOLATION PROCEDURE IAW TSM 05-50-00-May 29, 2018 · N902NK · Airbus A320232 · Air Distribution SystemSDR GTIA2018060192673Unknown · odorDURING DESCENT, FROM 600 FT TO THE GATE, HAD AN ODOR IN THE CABIN AND COCKPIT. BOTH PACKS AND BLEEDS ON, APPLIED TSM 05-50-810-813-A, PERFORMED GVI. CHECKED NO OIL CONTAMINATION IN THE APU IAW AMM 49-16-00. RAN BOTH PACKS WITH ENGINES ON, IAW AMM 71-00-May 29, 2018 · N902NK · Airbus A320232 · Air Distribution SystemSDR YENA201805290220Battery Pack · failedEMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED THE BATTERY ASSY AT 13WL IAW 33-51-11.May 29, 2018 · N508JL · Airbus A320232 · Emergency LightingSDR AALA2018061549025Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 212GF, FRAMES 6 TO 12, Y-765 TO Y-254. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIG 20106, AND IRM 9701 REV 71.May 28, 2018 · N679AW · Airbus A320232 · Fuselage Floor PanelSDR GTIA2018060182671Unknown · odorF/A REPORTED A STRONG ODOR IN THE MIDDLE OF THE CABIN. THE ODOR WAS GONE AFTER THE APU BLEED TURNED OFF. PERFORMED TSM 05-50-00-810-831.228789902, PERFORMED DECONTAMINATION OF THE ECS IAW AMM 21-00-00. NO ODOR NOTICED.May 28, 2018 · N638NK · Airbus A320232 · Air Distribution SystemSDR GTIA2018052802668Unknown · odorDURING DESCENT THROUGH 5,000', FA'S COMPLAINED OF STRONG ODOR IN AFT CABIN. IDLE THRUST, APU OFF (INOP). PERFORMED TSM 05-50-00-810-831 RAN EM'S AND OPERATED BOTH PACK'S, NO ODOR'S PRESENT AT THIS TIME.May 28, 2018 · N638NK · Airbus A320232 · Air Distribution SystemSDR GTIA2018052702666Generator · leakingF/A REPORT A STRONG SMELL OF DIRTY SOCKS IN THE MIDLE OF THE CABIN. THE SMELL IS GONE AFTER THE APU BLEED TURNED OFF. PERFORMED TSM 05-50-00-810-831, FOUND APU GENERATOR GENERATOR LEAKING. PERFORMED DECONTAMINATION OF THE ECS IAW AMM 21-00-00. NO SMELL NOTMay 27, 2018 · N638NK · Airbus A320232 · AC Generator-AlternatorSDR YENA201805260920Skin · dentedDURING HEAVY MAINTENANCE, DENTS WERE FOUND. REFER TO EC A18-416-01. WINGS/ RT IB FLAP/ TRAILING EDGE SKIN BTW RIB 11 & 13/ DENTS- PERMANENT REPAIR; APPROVED THIS REPAIR PER REF /2/ RDAS AND IS CLASSIFIED AS MAJOR CATEGORY 'A'.May 26, 2018 · N648JB · Airbus A320232 · Trailing Edge FlapsSDR YENA2018100560497Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y1225 AT LEVEL STR23R FR66 +5" FR67+16" AT AFT GALLEY AREA (1 EA); REF NRC 2018-159130 & W/O 909857. REPLACED FLOORBEAM -Y1225 AND FASTENERS 10 FR66 TO FR68 AT LEVEL STR 23R AFT GALLEY AREA IAW SMay 26, 2018 · N648JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2018100560496Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL AT LEVEL FR68 AND STR23R AT AFT GALLEY AREA (1EA); REF. NRC 2018-159125 W/O 909857. REPLACED LOWER SILL AT LEVEL STR23R BTW FR66 TO FR68 AFT GALLEY AREA (1EA) IAW SRM -51-72-11` AND DRAWING D5348May 26, 2018 · N648JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018100560495Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL AT LEVEL FR68 AND STR23R AT AFT GALLEY AREA (1EA); REF. NRC-2018-159125 W/O 909857. REPLACED LOWER SILL AT LEVEL STR23R BTW FR66 TO FR68 AFT GALLEY AREA (1 EA) IAW SRM 51-72-11 AND DRAWINGS D5348May 26, 2018 · N648JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018100560494Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN BTW FR69 TO FR70 AND BTW STR29R TO STR30R OUTFLOW VALVE AREA ON LOWER FUSELAGE; REF. NRC-2018-159008 W/O 909857. PERFORMED REPAIR ON EXTERNAL SKIN BTW FR69 TO 70 AND BTW STR 29R TO STR 30R OUTMay 26, 2018 · N648JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2018100560493Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM +Y1292 AT LEVEL OF FR16 AT FWD GALLEY; REF NRC 2018-159157 W/O 909857. REPLACED FLOORBEAM +Y1292 AT LEVEL OF FR16 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DRAWING D53118212May 26, 2018 · N648JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2018100560492Dummy Rail · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RAIL DUMMY Y503.2 AT LEVEL OF FR16 AT FWD GALLEY AREA; REF NRC 2018-159156 W/O 909857 CORROSION RAIL DUMMY Y503.2 AT LEVEL OF FR16 AT FWD GALLEY AREAMay 26, 2018 · N648JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA2018100560491Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF NR 2018-159128 FLOORBEAM -Y765 AT LEVEL STR 23 R FR 66 + 5 TO FR 70 AT AFT GALLEY AREA (7EA); REF NR 2018-159128 REPLACED FLOORBEAM -Y765 AND FASTENERS LOCATED AT LEVEL STR 23 R BTW FR 66 TO FR 70 AT AFMay 26, 2018 · N648JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2018100560490Dummy Rail · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RAIL DUMMY Y 503.2 AT LEVEL OF FR16 AT FWD GALLEY AREA; REF NRC 2018-159156 W/O 909857 REPLACED RAIL DUMMY Y503.2 BTW FR12 TO FR16 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DRAWING D53112825. PI LOC FR16 +0.May 26, 2018 · N648JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA2018100560489Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y765 AT LEVEL STR 23R FR66 +5" TO FR 70 AT AFT GALLEY AREA (1EA); REF. NRC 2018-159128 AND W/O 909857 REPLACED FLOORBEAM -Y765 AND FASTENERS LOCATED AT LEVEL STR 23R BTW FR66 TO FR70 AT AFT GALLEMay 26, 2018 · N648JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2018100560488Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF NR 2018-159127 FLOORBEAM +Y1292 AT LEVEL STR 23L FR 64 TO FR 66 + 5 AT AFT GALLEY AREA (1EA); REF NR 2018-159127 REPLACED FLOORBEAM +Y1292 AT LEVEL STR 23 L BTW FR 64 TO FR 66 AT AFT GALLEY AREA IAW A32May 26, 2018 · N648JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2018100526487Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NR # 2018-159126 FLOOR BEAM +Y1225 AT LEVEL STR 23 L FR 66 + 5 TO FR 67 + 16 AT AFT GALLEY AREA (1EA); REF BP NR # 2018-159126 REPLACED FLOOR BEAM +Y1225 BTW FR 66 TO FR 68 AT AFT GALLEY AREA IAW A32May 26, 2018 · N648JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018100526486Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED REF BP NR # 2018-159126 FLOOR BEAM +Y1225 AT LEVEL STR 23 L FR 66 + 5 TO FR 67 + 16 AT AFT GALLEY AREA (1EA); REF BP NR # 2018-159126 REPLACED FLOOR BEAM +Y1225 BTW FR 66 TO FR 68 AT AFT GALLEY AREA IAW A320 SMay 26, 2018 · N648JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201806129018Floor Panel · delaminatedTHE AIRCRAFT IS IN BASE MAINTENANCE. DELAMINATION FOUND ON FLOOR PANEL 231LF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 FIG 2019 IRM 9701 REVISION H.May 25, 2018 · N679AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201806079002Door Sill · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. ORIGINAL CORROSION DEFECT WAS DOCUMENTED ON LOG PAGE 5005990 AND EA 200206 29-JUN-11. R1 DOOR SILL REPLACED DURING THIS 2S CHECK AT CUSTOMER REQUEST. REPLACED LOWER SILL PER A320 SRM 51-72-11 AND DWG D53110339.May 25, 2018 · N679AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018060531361Skin · dentedA DENT WAS FOUND ON THE SKIN BETWEEN FRAMES 68-69 AND STR 41L-35L. REPAIRED IAW SRM 53-41-11-300-018.May 25, 2018 · N449UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR AALA201806049026Beam · corrodedLEFTSILL BEAM CORRODED. REPLACED THE SILL BEAM IAW SRM 51-72-11, AND DWG D53110339.May 25, 2018 · N679AW · Airbus A320232 · Fuselage Main, Structure
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