Airbus A320-232
Service difficulty reports · 32,653
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 CALA2018071101600Spring · brokenR1 DOOR, FWD GIRT BAR LATCH BROKEN. REMOVED AND REPLACED R1 DOOR FWD GIRT FITTING LATCH SPRING IAW AMM 52-13-31-400-003.SDR CALA2018071101599Spring · brokenBROKEN SPRING IN L2 AFT GIRT BAR FITTING. REMOVED AND REPLACED L2 DOOR AFT GIRT FITTING LATCH SPRING IAW AMM 52-13-31-400-003.SDR AALA2018070539029Stringer · corrodedCORRODED STRINGER 42L, BETWEEN FRAMES 58 & 59. REPLACED THE STRINGER IAW SRM 53-00-13-300-001, FIT 20101, SHEET 2-6.SDR CALA2018070301562Spring · brokenL1 DOOR FWD GIRT BAR LATCH SPRING BROKEN. REMOVED AND REPLACED L1 DOOR FWD GIRT FITTING LATCH SPRING IAW AMM 52-13-31-400-003.SDR CALA2018070301560Hinge Fitting · wornR1 DOOR UPPER HINGE BEARING WORN - SPUN. REMOVED AND REPLACED SUPPORT ARM UPPER HINGE FITTING IAW AMM 52-11-31-400-002, AND 52-11-12-400-001, AND 52-11-11-000-0 01 ON R1 DOOR.SDR CALA2018070301559Spring · brokenL1 DOOR AFT GIRT BAR LATCH SPRING BROKEN. REMOVED AND REPLACED L1 DOOR AFT GIRT FITTING LATCH SPRING IAW AMM 52-13-31-400-003.SDR CALA2018070301556Spacer · missingL2 DOOR FLEX CABLE LOWER EYE BOLT MISSING SPACER. REPLACED SPACER ON L2 DOOR AT FLEX CABLE LOWER EYE BOLT IAW AMM 52-13-22-400-001.SDR CALA2018070301554Wire Harness · damagedEEPL HARNESS ROWS 29-31 DAMAGED. REMOVED AND REPLACED EEPL CABLE AT SEAT ROW 29-31 IAW AMM 33-51-22-400-802C1.SDR YENA201806290930Pressure Panel · crackedDURING HEAVY MAINTENANCE, SEVERAL CRACKS WERE FOUND AT SUBJECT LOCATION. REFER TO EC A18-517-01. FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FR 35-36 / LT & RT SIDES / PRESSURE PANEL ATTACHMENT HOLES / CRACK DAMAGE – PERMANENT REPAIR; THIS TIME LIMITED REPASDR YENA201806290928Stiffener · crackedDURING HEAVY MAINTENANCE, A CRACK WAS FOUND ON LATERAL WINDOW FRAME STIFFENER RT SIDE. REFER TO EC A18-507-01. FUSELAGE/ NOSE FWD FUSELAGE/ RT SIDE/ LATERAL WINDOW FRAME (FR 4)/ UPPER STIFFENER AREA / CRACK DAMAGE - PERMANENT REPAIR (FRAME REPLACEMENT); THIS CSDR AALA201807029026Stringer · corrodedCORROSION FOUND ON STRINGER 43L FRAMES 56 - 57. REPLACED THE STRINGER SECTION IAW SRM 53-00-13-300-001.SDR AALA201807239013Threshold · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON THRESHOLD SHEET AT FR 52A TO FR56, STRINGER 38R. REPLACED THRESHOLD SHEET PER 51-72-11 AND DRAWING D53475500.SDR AALA201807239010Threshold · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON THRESHOLD SHEET AT FR 52A TO FR56, STRINGER 3R. REPLACED THRESHOLD SHEET PER 51-72-11 AND DRAWING D53475500.SDR AALA201807239005Stringer · corrodedCORROSION WAS FOUND ON STRINGER 42L, BETWEEN FRAMES 58 - 59 IN THE AFT CARGO BAY. REPAIRED THE STRINGER IAW SRM 53-00-13-201.SDR AALA201807239003Stringer · corrodedCORROSION WAS FOUND ON STRINGER 43L BETWEEN FRAMES 56 TO 57, CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-13-201.SDR AALA201807169005Structure · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON COVER SHEET AT FR 52A TO FR 56 AND STRINGER 38R. REPAIRED DAMAGED AREAS ON COVER SHEET PER SRM A320 53-41-49-283-004.SDR AALA201807129005Floorbeam · corrodedTHE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON FLOORBEAM -Y765 LOCATED BETWEEN FRAMES 64-66 AT AFT GALLEY AREA. REPLACED FLOORBEAM PER SRM 51-72-11 AND DRAWING D53472816.SDR AALA2018071099023Seat Track · corrodedCORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 64 & 66. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DWG D53472816.SDR AALA201807099011Floor Support · corrodedCORROSION FOUND ON THE FLOOR SUPPORT, -Y1162.5, BETWEEN FRAMES 68 TO 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472780.SDR AALA201807109028Seat Track · corrodedTHE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON SEAT TRACK +Y765 LOCATED BETWEEN FRAMES 64-66 AT AFT GALLEY AREA. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING D53472815.SDR AALA201807109027Floorbeam · corrodedTHE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON FLOORBEAM +Y1162.5 BETWEEN FRAMES 68-69 AT AFT GALLEY AREA. REPLACED FLOORBEAM PER SRM 51-72-11 AND DRAWING D53472780.SDR AALA201807099018Seat Track · corrodedCORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 64 TO 66. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING D53472815.SDR CALA2018070301544Window · scratchedWINDOW AT 37A HAS LARGE SCRATCH. REMOVED AND REPLACED CABIN WINDOW REF AMM 56-21-13.SDR AALA201806299011Cylinder · low pressureAIRCRAFT WAS IN BASE MAINTENANCE. L-2 DOOR EMERGENCY ASSIST/DAMPER CYLINDER PRESSURE LOW. SERVICED DOOR EMERGENCY ASSIST/DAMPER CYLINDER PER AMM 52-10-00.SDR GTIA2018062802721Oxygen Gen · detachedPASSENGER OXYGEN GENERATOR UNIT HAS BROKEN OUT OF CELLING AND IS HANGING BY A STRING ABOVE SEATS 11 DEF. INSTALLED THE OXYGEN CONTAINERS IAW AMM 35-21-41. OPS CHECKED GOOD IAW 35-23-00SDR AALA201807279011Web · corrodedTHE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON WEB LOCATED BETWEEN FRAMES 69-70 AT LEVEL STRINGER 23R, LOWER POSITION AT AFT GALLEY AREA. REPLACED WEB PER SRM 51-72-11 AND DRAWING 53474180.SDR AALA201807239012Skin · saturatedAIRCRAFT IN BASE MAINTENANCE: TRAPPED WATER INDICATION ON RIGHT HAND ELEVATOR UPPER SURFACE SKIN BETWEEN RIB 5 AND RIB 6, AT 5.28 INCHES FROM RIB 5 AND 4.22 INCHES FROM TRAILING EDGE ON RIGHT HAND HORIZONTAL STABILIZER. REPAIRED RIGHT HAND ELEVATOR UPPER SURFASDR AALA201807249042Shear Plate · crackedA CRACK INDICATION WAS FOUND ON THE SHEAR PLATE BETWEEN FRAMES 69 - 70, STRINGER 23L. REPLACED THE SHEAR PLATE IAW SRM 51-72-11, AND DRAWING D53474180.SDR AALA2018071329007Tray · crackedCRACKED TRAY, FRAMES 68 TO 69, STRINGER 23L. REPLACED THE TRAY IAW SRM 51-72-11, AND DRAWING D53480019.SDR AALA201807129008Tray · crackedAIRCRAFT WAS IN BASE MAINTENANCE. CRACK INDICATED ON THE FLOOR STRUCTURE (TRAY) BETWEEN FR 68 & 69 AT LEVEL STR 23R OF THE AFT GALLEY AREA. REPLACED FLOOR STRUCTURE (TRAY) PER SRM 51-72-11 DRAWING D53480019.SDR AALA2018071099012Web · corrodedCORROSION FOUND ON THE WEB BETWEEN FRAMES 69 TO 70. REPLACED THE WEB IAW SRM 51-72-11, AND DWG D53474180.SDR AALA2018071099013Shear Plate · corrodedCORROSION FOUND ON THE SHEAR PLATE BETWEEN FRAMES 69 TO 70. REPLACED THE SHEAR PLATE IAW SRM 51-72-11, AND DWG D53474180.SDR AALA2018070969010Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 261BG IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, FIGURE 20109, AND IRM 9701.SDR AALA2018070969009Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 261PF AT AFT GALLEY. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-011, FIGURE 20109, AND IRM 9701.SDR AALA2018070969008Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 262BG AT AFT GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, FIGURE 20109, AND IRM 9701 REVISION H.SDR AALA2018070969007Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 261AG AT AFT GALLEY AREA. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION H.SDR AALA2018070969006Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 231FF IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701 REVISION H.SDR YENA201807020273Light · inoperativeFLT 1905, EWR-FLL. EMERGENCY LIGHTING ON SEAT 1C & 19C INOP (FLOOR PROX EMERG ESCAPE PATH MARK SYS - INCANDESCENT LIGHTING SYS - NOT APPLICABLE TO (N703 AND UP). REPLACED ESCAPE LIGHT ROW 1L AND 19R HARNESS REF ESPM 20-70-00. OPS CHECK GOOD.SDR YENA201806260924Skin · damagedDURING CURRENT (6/2018) C-9 HEAVY CHECK AT GSO, WAS REPORTED WITH FRAYING DAMAGE COMMON TO THE LT OUTBOARD FLAP (PN D5757420200400/ SN TB-12720) AT THE UPPER SKIN AROUND A FILLED PRODUCTION INSPECTION HOLE (SE REF /1/ REO FOR DETAILS). CONTACTED AND INSTRUCTSDR YENA2018100860537Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT STATION 16Y+25CM; REPLACED BEAM PER DWG D53911757 AND SRM 51-42-11SDR YENA2018100860536Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT STATION 16 Y +104CM; ALL WORK ACCOMPLISHED ON NR 40484 REMOVED AND REPLACED FLOORBEAM AS PER SRM 51-42-11 AND DRWG D53112812SDR YENA2018100860535Door Frame · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN FRAME 66R CHORD AT R2 DOOR SURROUND; ALL WORK ACCOMPLISHED ON NR 40765 REMOVED CORROSION ORIG MAT .150,REMOVED .090, REMAINING .060 FOUND TO BE OUT OF LIMITS PER SRM 53-41-14; FABRICATED, LOCATEDSDR YENA2018100860534Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO PIT LOWER ENTRY SILL. HAS MULTIPLE AREAS OF CORROSION; ALL WORK ACCOMPLISHED IN NR 40795 REMOVED AND REPLACED PLATE (SILL) PER SRM 51-42-10 ALODINE PRIMED AND PAINTED AREA PER SRM 51-21-10 P/N D5SDR YENA2018100860533Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM JUST I/B OF L2 DOOR PAN AT FR 68; ALL WORK ACCOMPLISHED ON NR 40835 REMOVED CORROSION, PART BEYOND REPAIR, RECEIVED NEW REPLACEMENT. INSTALLED BEAM IAW SRM 51-42-11 AND DRAWING D53472188SDR YENA2018100860532Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT STA 20 Y-25CM; ALL WORK ACCOMPLISHED ON NR 40505 REMOVED CORROSION 0.020 ,ORIG MAT 0.063 ; REMAINING MAT 0.043 AND IS FOUND TO BE OUT OF LIMITS PER SRM 53-11-14. REMOVED AND REPLACED NEW BEAM ASDR YENA2018100860531Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FOUND ON FLOORBEAM AT STA 16 Y-155CM; ALL WORK ACCOMPLISHED ON NR 40471 REMOVED CORROSION 0.050, ORIG MAT 0.080. REMAINING MAT 0.030 AND IS FOUND TO BE OUT OF LIMITS PER SRM 51-74-00. REMOVED AND REPLACED NSDR YENA2018100860530Panel Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CORROSION L1 SURROUND FWD PANEL SUPPORT; ALL WORK ACCOMPLISHED ON NR 40485 REMOVED AND REPLACED WEB PER SRM 51-42-11 AND DRWG 53114110SDR YENA2018100860529Pan · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON L-2 FWD GIRT BAR FITTING ATTACH PAN; ALL WORK WAS ACCOMPLISHED ON NR 40780 REMOVED AND REPLACED L2 DOOR SILL PER SRM 51-42-11 AND DRW 53480505 PN D5348004320601SDR YENA2018100860528Fitting · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON R2 FWD GIRT BAR FITTING HOLES; ALL WORK ACCOMPLISHED ON NR 40779 REMOVED CORROSION, ORIG MAT THICKNESS .0217, REMOVED .068, REMAINING MAT THICKNESS .149 FOUND TO BE OUT OF LIMITS PER SRM 53-41-14 FABBED LOCSDR YENA2018100860527Pan · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON R-2 DOOR AFT GIRT BAR ATTACH FLOOR PAN; REF NR 40778 REMOVED CORROSION, ORIG MAT THICKNESS .0217, REMOVED .083, REMAINING MAT THICKNESS .134 FOUND TO BE OUT OF LIMITS PER SRM 53-41-14 FABBED LOCATED AND D
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