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.

SDR AALA201805299044Tachometer · faultedAFTER TAKEOFF, ECAM MESSAGES APPEARED FOR BRAKES, AUTO BRAKE FAULT, BRAKE RELEASED. ALSO AMBER AUTO BRAKE MESSAGE WAS DISPLAYED ON THE WHEEL PAGE. REPLACED THE TACHOMETER 22GG, FOR THE NR 4 MAIN IAW AMM 32-42-57.May 25, 2018 · N656AW · Airbus A320232 · Landing Gear Brake SystemSDR AALA2018053099043Cover · brokenR2 EMERGENCY LIGHT COVER BROKEN. REPLACED THE EMERGENCY LIGHT COVERMay 25, 2018 · N654AW · Airbus A320232 · Emergency LightingSDR YENA2018052950221Unknown · odorDURING DECENT, FLT CREW WERE INFORMED BY FA1 THAT THEY SMELLED A SLIGHT MUSTY ODOR. NO ODOR DETECTED IN COCKPIT. AIRCRAFT IS OK FOR SERVICE.May 25, 2018 · N556JB · Airbus A320232 · Air Distribution SystemSDR GTIA2018052502663Seal · damagedPACK 1 INOP DUE TO ODOR EVENT REF LP 2416400-1. FAULT CAUTIONS ASSOCIATED WITH OPERATIVE SIDE NOT DISPLAYED. PREFORMED TSM 71-00-00-810-801-A FOUND DE-OILER SEAL ON ENG NR 1 TO BE LEAKING. REMOVED AND REPLACED DE-OILER SEAL ASSY IAW AMM 72-60-31. OPS CHECK ANDMay 25, 2018 · N602NK · Airbus A320232 · Turbine Engine Accessory DriveSDR YENA2018100540502Skin Panel · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LT TOP WING SKIN PANEL BTW FASTENER HEADS AT RIB 14 STR 11; PERMANENT REPAIR PERFORMED IAW EO-A32F-4656-00. FASTENER REPLACED AND OVERSIZED IAW SRM 51-42-11. WORK ACCOMPLISHED ON LHT NT 5000761250-0010May 24, 2018 · N520JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2018100540501Skin Panel · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED LT TOP WING SKIN PANEL BTW FASTENER HEADS AT RIB 8 ON STR 13; REPAIRED PERFORM IAW LPTR EO-A32F-4656-00. WORK ACCOMPLISHED ON LHT NR 5000761216-0010May 24, 2018 · N520JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2018100540500Skin Panel · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BETWEEN FASTENER HEADS ON LT WING TOP SKIN PANEL AT RIB 9 BETWEEN STR 14-15; PERMANENT REPAIR PERFORMED IAW LPTR EO-A32F057-4656-00 CORROSION REWORK IAW SRM 57-21-00-200-019-600 FASTENER REPLACE AND OVERSIZMay 24, 2018 · N520JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2018100540499Skin Panel · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BETWEEN FASTENER HEADS ON LT WING TOP SKIN PANEL UPR SURFACE AT RIB 19 +3 AND 4.92" AFT OF FRONT SPAR; CORROSION REWORKED IAW SRM 57-21-11-283-014 REV 122. WORK ACCOMPLISHED ON LHT NR 5000761256-0010May 24, 2018 · N520JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2018100540498Skin Panel · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BETWEEN FASTENER HEADS ON LT WING TOP SKIN PANEL UPR SURFACE AT RIB 19 +2 ON FRONT SPAR; PERMANENT REPAIR PERFORMED IAW LTPR EO-A32F-57-4656099. CORROSION REWORKED PER SRM TASK. 57-21-11-283-014 REV 122 WORMay 24, 2018 · N520JB · Airbus A320232 · Wing, Plate/SkinSDR AALA201806209014Hinge Fitting · damagedELONGATED AFT DOOR HINGE FITTING, RIGHT NOSE LANDING GEAR DOOR, BETWEEN FRAMES 19 TO 20, STRINGER 41R. REPLACED THE HINGE FITTING IAW CMM 52-82-32.May 24, 2018 · N679AW · Airbus A320232 · Landing Gear DoorsSDR AALA201806209013Hinge Fitting · elongatedELONGATED AFT RT DOOR HINGE FITTING, NOSE LANDING GEAR, BETWEEN FRAMES 19 TO 20, STRINGER 41R. REPLACED THE HINGE FITTING IAW CMM 52-82-32.May 24, 2018 · N679AW · Airbus A320232 · Landing Gear DoorsSDR AALA201806209012Hinge Fitting · damagedELONGATED AFT LT DOOR HINGE FITTING, NOSE LANDING GEAR, BETWEEN FRAMES 19 TO 20, STRINGER 41L. REPLACED THE HINGE FITTING IAW CMM 52-82-32.May 24, 2018 · N679AW · Airbus A320232 · Landing Gear DoorsSDR AALA201806209011Hinge Fitting · damagedELONGATED AFT DOOR HINGE FITTING, LEFT NOSE LANDING GEAR BETWEEN FRAMES 19 TO 20, STRINGER 41L. REPLACED HINGE FITTING IAW CMM 52-82-32.May 24, 2018 · N679AW · Airbus A320232 · Landing Gear DoorsSDR AALA2018061329015Support · corrodedCORROSION FOUND ON LOWER SUPPORT, STRINGER 23L, BETWEEN FRAMES 66 - 68 IN THE AFT GALLEY. REPAIRED THE SUPPORT IAW SRM 53-41-14-300-001.May 24, 2018 · N679AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201806129017Door Sill · corrodedTHE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON LOWER SILL AT LEVEL STRINGER 23R AND BETWEEN FRAMES 66-68 AT AFT GALLEY AREA. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.May 24, 2018 · N679AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201805240227Epsu · failedDURING HEAVY MAINTENANCE, OPERATIONAL TEST OF EMER LIGHTS FAILED DURING TEST. REPAIRED 3 EA EPSU'S AT (10WL-11WL AND 12WL) AND 1 BATTERY AT (10WL) IAW AMM 33-51-38-000-001-A. SYS OPS CKS NORMAL.May 24, 2018 · N520JB · Airbus A320232 · Emergency LightingSDR YENA201805240226Epsu · failedDURING HEAVY MAINTENANCE, OPERATIONAL TEST OF EMER LIGHTS FAILED DURING TEST. REPAIRED 3 EA EPSU'S AT (10WL-11WL AND 12WL) AND 1 BATTERY AT (10WL) IAW AMM 33-51-38-000-001-A. SYS OPS CKS NORMAL.May 24, 2018 · N520JB · Airbus A320232 · Emergency LightingSDR YENA201805240225Epsu · failedDURING HEAVY MAINTENANCE, OPERATIONAL TEST OF EMER LIGHTS FAILED DURING TEST. REPAIRED 3 EA EPSU'S AT (10WL-11WL AND 12WL) AND 1 BATTERY AT (10WL) IAW AMM 33-51-38-000-001-A. SYS OPS CKS NORMAL.May 24, 2018 · N520JB · Airbus A320232 · Emergency LightingSDR YENA201805294224Battery Pack · failedOPS TEST OF THE EMERGENCY LIGHTS FAILED. REPAIRED THREE POWER SUPPLIES, 10WL, 11WL, AND 12WL) AND ONE BATTERY 10WL IAW AMM 33-51-38-000-001-A. SYS OPS CHECKED NORMAL.May 24, 2018 · N520JB · Airbus A320232 · Emergency LightingSDR YENA2018052940223Skin · damagedDURING HEAVY MAINTENANCE, GOUGE & DENT FOUND ON THE SKIN AT FRAMES 61 - 62, STRINGER 40 - 42L. REPAIRED IAW SRM 53-00-11-300-043.May 24, 2018 · N520JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2018052940222Frame · damagedDURING HEAVY MAINTENANCE, FRAME 20, LT SIDE UPPER CORNER FASTENER HOLE ELONGATED. ACCOMPLISHED EC A18-418-01.May 24, 2018 · N520JB · Airbus A320232 · Fuselage Main, FrameSDR AALA2018052989019Light · damagedWALL MOUNTED EMERGENCY LIGHT AT THE R1 DOOR WAS FOUND DAMAGED. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-13.May 24, 2018 · N673AW · Airbus A320232 · Emergency LightingSDR AALA201806219002Box Beam · crackedLEFT BOX BEAM FLANGE CRACKED AT FRAME 43, -Y1650. REPAIRED THE BOX BEAM IAW EO 5315Y066.May 23, 2018 · N679AW · Airbus A320232 · Fuselage Main, StructureSDR AALA201806219001Box Beam · crackedRIGHT BOX BEAM FLANGE CRACKED AT FRAME 43, -Y1650. REPAIRED THE BOX BEAM IAW EO 5315Y066.May 23, 2018 · N679AW · Airbus A320232 · Fuselage Main, StructureSDR AALA201806069005Tray · crackedCRACKED TRAY BETWEEN FRAMES 68 TO 69, STRINGER 23L. REPLACED THE TRAY IAW SRM 51-72-11, AND DRAWING #D53480019.May 23, 2018 · N679AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA2018060529002Floor Support · corrodedCORROSION WAS FOUND ON THE FLOOR SUPPORT, -Y1162.5, BETWEEN FRAMES 68 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.May 23, 2018 · N679AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201806049025Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT, FRAMES 68 TO 69, Y1162.5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472780.May 23, 2018 · N679AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201806119020Floor Panel · delaminatedAIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION FOUND ON FLOOR PANEL 221DF LOCATED BTW FR16 TO FR21, AND BL Y-254 TO Y254. REPLACED FLOOR PANEL PER SRM 53-12-00-300-006 FIGURE 20106, IRM 9701 REV H.May 22, 2018 · N679AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201806059004Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 231YF. IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-006, PARA 2, FIGURE 20106, AND IRM 9701 REVISION H.May 22, 2018 · N679AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201806049027Floor Panel · delaminatedDELAMINTATION FOUND ON FLOOR PANEL 261PF, FRAMES 68 TO 70, Y1292 TO -Y1292. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011.May 22, 2018 · N679AW · Airbus A320232 · Fuselage Floor PanelSDR GTIA2018052202662Bottle · low pressureL1 DOOR ASSIST BOTTLE REQUIRE SERVICE. SERVICED L1 DOOR ASSIST BOTTLE AMM 52-10-00.May 22, 2018 · N634NK · Airbus A320232 · Passenger/Crew DoorsSDR YENA201805220214Battery Pack · no testEPSU BATTERY 12WL FAILED AN EMERGENCY LIGHT TEST. R & R THE BATTERY IAW AMM 33-51-38, SYSTEM OPS CHECKED NORMAL.May 22, 2018 · N590JB · Airbus A320232 · Emergency LightingSDR YENA2018052320213Battery Pack · no testEPSU 10WL FAILED AN EMERGENCY LIGHT TEST. R & R THE BATTERY IAW AMM 33-51-38, SYSTEM OPS CHECKED NORMAL.May 22, 2018 · N590JB · Airbus A320232 · Emergency LightingSDR YENA2018052320212Battery Pack · no testEPSU BATTERY 11WL FAILED AN EMERGENCY LIGHT TEST. R & R THE BATTERY IAW AMM 33-51-38, SYSTEM OPS CHECKED GOOD.May 22, 2018 · N590JB · Airbus A320232 · Emergency LightingSDR CALA20180L0531346Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 42L AND 43L IN THE FWD CARGO BILGE AREA AT FRAME 31. REMOVED AND REPLACED FWD CARGO FISH PLATE IAW SRM 51-72-11-911-001. ACCOMPLISHED ROTO PROBE OF OPEN HOLE S IAW NTM 51-10-01.May 21, 2018 · N455UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018060531345Plate · corrodedCORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 43L AND 44L IN THE FWD CARGO BILGE AREA AT FRAME 31. REMOVED AND REPLACED THE FISHPLATE IAW SRM 51-72-11-911-001. ACCOMPLISHED ROTO-PROBE OF OPEN HOLES IAW NTM 51-10-01.May 21, 2018 · N455UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018060531344Plate · corrodedCORROSION FOUND ON THE FISH PLATE, BETWEEN STRINGERS 42L AND 43L, IN THE FWD CARGO BILGE AREA, AT FRAME 28. REMOVED AND REPLACED THE FISHPLATE IAW SRM 51-72-11-911- 001, AND NTM 51-10-01.May 21, 2018 · N455UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018060531338Window Post · crackedLEFT WINDSHIELD SIDE POST LOWER ATTACHMENT, FRAME 4 AFT LOWER WEB WAS CRACKED. REPAIRED THE WINDSHIELD POST LOWER WEB IAW ECRA 5311-01939.May 21, 2018 · N449UA · Airbus A320232 · Fuselage Main, StructureSDR GTIA2018052102661Unknown · odorFUME EVENT NOTED IN AFT LAV AREA REPORTED BY LEAD FA. PERFORMED TSM 05-50-00810-831-A, PERFORMED TSM 71-00-00-810-801-A, FOR BOTH ENGINES, NO LEAKS NOTED. PERFORMED ENGINE RUN & BLEED AIR TEST, ALL RESULTS SATISFACTORY, NO ODOR NOTED. PERFORMED TSM 49May 21, 2018 · N612NK · Airbus A320232 · Air Distribution SystemSDR AALA201805239004Light · malfunctionedAIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT REPORTS EMERGENCY EXIT LIGHTS ARE ILLUMINATED WHEN EMERGENCY EXIT SWITCH FLIGHT DECK ARMED - ANN LIGHTS BLANK. RESET CIDS PER AMM 23-73-00.May 21, 2018 · N658AW · Airbus A320232 · Emergency LightingSDR YENA2018052210209Connector · brokenROW 1 FLOOR EMERGENCY LIGHT INOPERATIVE. REPLACED A BROKEN CONNECTOR IAW AMM 33-51-19. OPS CHECKED OK.May 21, 2018 · N588JB · Airbus A320232 · Light System WiringSDR CALA2018060531330Cover · corrodedAFT CARGO TORSION BOX COVER HAS SEVERAL AREAS OF CORROSION, BLENDED OUT CORROSION, AND FOUND TO BE 100% MATERIAL LOSS. REMOVED AND REPLACED TORSION BOX COVER, RESTORED SURFACE PROTECTION IAW SRM 51-72-11-911-001.May 20, 2018 · N423UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018060531328Intercostal · crackedROTO PROBE SHOWED A CRACK INDICATION AT FRAME 16, NR 7 DOOR STOP, ON THE INTERCOSTAL ONLY, REMOVED AND REPLACED THE INTERCOSTAL IAW IAW SRM 51-72- 11-911-001.May 20, 2018 · N423UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018060531327Cover · crackedTHE LT OVERWING SLIDE COVER WAS CRACKED.May 20, 2018 · N449UA · Airbus A320232 · Escape SlideSDR CALA2018060531326Cover · crackedTHE RT OVERWING ESCAPE SLIDE COVER WAS CRACKED AND SEPERATING. REMOVED & REPLACED THE OVERWING ESCAPE SLIDE IAW AMM 25-62-42-400-001-A.May 20, 2018 · N449UA · Airbus A320232 · Escape SlideSDR CALA2018060531331Plate · corrodedLAVATORY EXHAUST VENT HAD CORROSION ON THE INSIDE REINFORCEMENT PLATE, ON THE SKIN IN THE AFT WET AREA. REMOVED AND REPLACED REINFORCEMENT PLATE IAW SRM 51-42-11-001.May 20, 2018 · N423UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018052100208Sign · malfunctionedEMERGENCY EXIT SIGN AFT INOPERATIVE. PERFORMED EMERGENCY LIGHTS RESET AS REQUIRED IAW AMM 32-20-00. OPS CHECKED GOOD.May 20, 2018 · N580JB · Airbus A320232 · Emergency LightingSDR YENA201805190919Not Reported · crackedDURING HEAVY MAINTENANCE, CRACKS WERE FOUND. REFER EC A18-414-01. FUSELAGE/ CENTER FUSELAGE/ ALI 521110-01/ FR16LT & FR20LT FASTENER HOLES/ MULTIPLE CRACKS- PERMANENT REPAIR; APPROVED THIS REPAIR PER REF /3/ RDAS AND IS CLASSIFIED AS MAJOR CATEGORY 'B'.May 19, 2018 · N569JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201805190477Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LT DADO PANEL SUPPORT FLOOR BEAM AT FR 66 3" FWD OF GIRT BAR FITTING HAS BIG AREA OF CORROSION. REMOVED CORROSION ON L2 DOOR SILL, FOUND TO BE OUT OF LIMITS IAW 53-00-14-283-002 FIG 101 PG 4, REQUIRED NEW LMay 19, 2018 · N569JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201805190476Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT AFT CABIN R2 DOOR I/B SILL 1 INCH AFT OF FRAME 66. REMOVED AND REPLACED R2 DOOR SILL PN D5348004320701 PO 1041397.7 IAW SRM 51-72-11-911-001.May 19, 2018 · N569JB · Airbus A320232 · Fuselage Miscellaneous Structure
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