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 CALA2024020500321Manifold · crackedPTU MANIFOLD 3113GM FITTING BUSTED AND LEAKING HYDRAULIC FLUID IN RIGHT WHEL WELL. SDR# 1035015 SUBMITTED. REMOVED AND REPLACED PTU MANIFOLD REF. AMM 29-13-15-400-001-A OPS CHECK LEAK CHECK GOOD PARTS USED: 31-2913-3-0022,QTY :1.SDR AALA202402054659Pin · deterioratedAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 SLIDE ASSMBLY HAS 4 EACH PIN ATTACHMENT LOCKS DETERIORATED. REPLACED SLIDE ASSEMBLY PER TASK CARD 26C83252008.SDR AALA202402060214Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 61 AND FR 64 AT +Y765. REPLACED BEAM-SEAT TRACK PER SRM 53-41-15-300-001.SDR AALA202402067709Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 56 AND FR 64 AT +Y1292. REPLACED BEAM-SEAT TRACK PER SRM 53-41-15-300-001.SDR CALA2024020500320Skin · corrodedAFT FUSELAGE TOILET WASTE DISPOSAL VENT/EXHAUST IS CORRODED 204- 05. () REPAIRED AFT TOILET WASTE VENT AREA BY DOUBLER IAW SRM 53-41-11- 300-004 MAJOR REPAIR CAT A 44-0008 ATTACHED. WORK A CCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 85591SDR CALA2024030500637Structure · corrodedUPPER FUSLAGE FR 66 AFT SURFACE HAS CORROSION. 2.5 IN INBD EDGE. 2.0 & 3.0IN FROM FLOOR SUPPORT STRUCTURE FOUND DURING COMPLIANCE OF N/R#78715.() 53-41-12-205-003 TABLE 1 INSP THRESHOLD FROM 1ST FLIGHT 2400FC, FOR THIS INSP, SRM 1.F (2) NOTES FOR TIME FOR FIRSSDR CALA2024021200404Stringer · corrodedAFT PIT FWD OF FRAME 56 STR 43LH, SPLICE ALL FATERNERS CORRODED.() REMOVED REPAIR ANGLE IAW SRM 51-42-11, PERFORMED HFEC IAW NTM 51 BFM -10-02 NO CORROSION NOTED. FABRICATED NEW SRM AND ANGLE REPAIR IAW SRM TASK 53-41-13-300-010 INSTALLED NEW SHIM AND ANGLE RESDR YENA2024020500223Unknown · odorFLT#363,BOS-UVF. ' LEVEL 1 TRANSIENT ODOR REPORTED BY AFT FA'S DURING DESCENT; COMPLIED WITH INFO NOTICE 2017 - T015 SECTION A ISOLATION FAULT TYPE 101 (A) 1X PCD TSM 05 -50 -00 -810 -085B -055D. A/C OK FOR SERVICE.'SDR CALA2024022900608Plate · corrodedA3NB-05-3-6016- FWD CARGO FLOOR BOX TOP PLATE NEXT TO DOOR SILL HAS CORROSION-DOT 45-127. W/C:78223SDR CALA2024022900607Web · corrodedA3NB-53-3-6179- AFT CARGO FLOOR BOX UPPER WEB AT DOOR SILL HAS CORROSION AROUND CENTER 2 NET TIE-DOWNS AND INTERGRANULAR CORROSION SPOT IN BETWEEN THEM - DOT-45-120. W/C:78168SDR YENA2024020600242Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH DOOR STOP Ñ7 HOLE H3 (LWR / INB), CRAC K DIRECTION AT 4 AND 6 O CLOCK. D= 0.150 INCH; REF AEROMAN NR 2023-741034 WO 2023 362/1 REMOVED AND REPLACED INTERCOSTAL FITTING BTW FR 15 LH TO FR 16 LH AT LEVEL SDR YENA2024020600241Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX, IN COCKPIT (1 EA); REFAEROMAN NR 2023-741053 REMOVED AND REPLACED CONTINUITY FITTINGS IAW RESDR YENA2024020600240Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH, DOUBLE JOGGLE AREA, HOLE C. CRACK DI RECTION AT 3 AND 10 O CLOCK. D= 0.110 INCH; REF AEROMAN NR 2023-741037 WO 2023 362/1 PERFORMED REPAIR ON HOLE C LOCATED ON FRAME 16 LH, DOUBLE JOGGLE AREA IAW REPAISDR YENA2024020600239Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH, DOUBLE JOGGLE AREA, HOLE Ñ6. CRACK D IRECTION AT 1 O CLOCK. D= 0.130 INCH; REF AEROMAN NR 2023-741038 WO 2023 362/1 PERFORMED REPAIR ON HOLE #6 LOCATED ON FOR 16 RH, DOUBLE JOGGLE AREA, IAW REPAIR INSTSDR YENA2024020600238Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH, DOUBLE JOGGLE AREA, HOLE A. CRACK DI RECTION AT 9 O CLOCK. D= 0.160 INCH; REF AEROMAN NR 2023-741039 WO 2023 362/1 PERFORMED REPAIR ON HOLE #A LOCATED ON FOR 16 RH, DOUBLE JOGGLE AREA, IAW REPAIR INSTRSDR YENA2024020600237Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH, DOUBLE JOGGLE AREA, HOLE C. CRACK DI RECTION AT 9 O CLOCK. D= 0.150 INCH; REF AEROMAN NR 2023-741040 WO 2023 362/1 PERFORMED REPAIR ON HOLE C LOCATED ON FRAME 16 RH, DOUBLE JOGGLE AREA, IAW REPAIR INSTSDR YENA2024020600236Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBOA RD AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 12 OCLOCK, AT A FT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1254356 TASKCARD: NR-00013) REF AEROMAN NR 2023-741SDR YENA2024020600235Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 2 POSITION, CRACK DIRECTION IS 6 OCLOCK, AT AF T GALLEY AREA (1 EA); (RESOLVED ON W/O: 1254356 TASKCARD: NR-00014) REF AEROMAN NR 2023-7412SDR YENA2024020600234Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 OCLOCK, AT AF T GALLEY AREA (1 EA); (RESOLVED ON W/O: 1254356 TASKCARD: NR-00015) REF AEROMAN NR 2023-7412SDR YENA2024020600233Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTIONS ARE 3 AND 6 OCLOC K, AT AFT GALLEY AREA (2 EA); (RESOLVED ON W/O: 1254356 TASKCARD: NR-00016) REF AEROMAN NR 2SDR YENA2024020600232Flange · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ONN FR68 LH SIDE HORIZONTAL FLANGE RADIUS AT STR 22LH, CRACK LENGTH .300 INSCH APPROX, AT AFT GALLEY AREA; REF AEM WO: 2023 362/1, NR 2023-741036. ACCOMPLISHED REPAIR ON RADIAL FLANGE STOP FITTING AT FR68,STR22LSDR YENA2024020600231Flange · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AO FR 68RH HORIZONTAL FLANGE RADIUS AT STR22RH. CRACK LENGTH 300 INCH, AT AFT GALLEY AREA; REF AEM WO: 2023 362/1, NR 2023-741035. ACCOMPLISHED REPAIR ON HORIZONTAL FLANGE FR 68RH AT STR 22RH. PER JB EC: A24-111SDR YENA2024020600230Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION ON LH WING TOP SKIN LOWER SURFACE OVERHANG AT TRAILING EDGE AREA BTW RIB 6 AND RIB 7; ACCOMPLISHED THE REPAIR OF CORROSION ON LH WING TOP SKIN PANEL 2 FALSE REAR SPAR TE OVERHANG LOWER SURFACE BETWEEN WX3622-WX4013 IN ACCORSDR YENA2024020600229Stop Fitting · crackedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 RH & STR 22 / DOOR STOP FITTING #1 / RADIAL FLANGE FILLET RADIUS / CRACK DAMAGE - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR YENA2024020600228Stop Fitting · crackedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 LH & STR 22 / DOOR STOP FITTING #1 / RADIAL FLANGE FILLET RADIUS / CRACK DAMAGE - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR CALA2024020500316Skin · corrodedCORROSION NOTED ON THE RH PYLON AFT FIXED FAIRING I/B SKINSDR AALA202402021313Battery · inoperativeAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT FLASHLIGHT AT POSITION 3 INOPERATIVE. REPLACED FLASHLIGHT BATTERY.SDR YENA2024020200222Converter · failedFLT#1759, JFK-KIN. 'AFTER SHUTDOWN THE #4 IN FLIGHT CREW MEMBER REPORTED A MUSTY SMELL FROM VENTILATION SYSTEM ON FINAL DESCENT; REF LOGPAGE 3790470 ITEMS 1 (REMOVED AND REPLACED OZONE CONVERTER PER AMM 21-58-42. LEAK CHECK GOOD ) AND 2 (ACCOMPLISHED SETION B2SDR CALA2024020200291Frame · crackedR/H FWD EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY FWD OF WINDOW. RMVD AND RPLD FWD SEGMENT FRAM P/N D5227902620451 PO: 1144987.3 AT RH FWD EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11/001.SDR CALA2024020200289Frame · crackedL/H FWD EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY FWD OF WINDOW. RMVD AND RPLD FWD SEGMENT FRAME P/N D5227902670551 PO: 1145288.4 AT LH FWD EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11-001.SDR CALA2024020200288Frame · crackedL/H AFT EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY FWD OF WINDOW. RMVD AND RPLD FWD SEGMENT FRAM PN D5227902620451 PO: 1144987.3 A T LH AFT EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11/001.SDR CALA2024020200287Frame · crackedL/H FWD EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY AFT OF WINDOW. RMVD AND RPLD AFT SEGMENT FRAME AT LH FWD EMERGENCY EXIT DOOR AS SY IAW SRM 51-42-11-001.SDR CALA2024020200286Frame · crackedL/H AFT EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY AFT OF WINDOW. RMVD AND RPLD AFT SEGMENT FRAME P/N D5227902620551 PO: 1145288.4 AT LH AFT EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11-001.SDR CALA2024020200285Frame · crackedR/H AFT EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY FWD OF WINDOW. RMVD AND RPLD FWD SEGMENT FRAME P/N D5227902628451 PO: 1144987.3 AT RH AFT EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11.SDR CALA2024020200284Frame · crackedR/H AFT EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY AFT OF WINDOW. RMVD AND RPLD AFT SEGMENT FRAME P/N D5227902620551 PO: 114987.4 AT RH AFT EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11.SDR CALA2024020200292Frame · crackedR/H FWD EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY AFT OF WINDOW. RMVD AND RPLD AFT SEGMENT FRAME P/N D522790260551 PO: 1144987.4 AT RH FWD EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11/001.SDR AALA202402018982Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING OPEN HOLE 3 AT FR 16 RIGHT AND DOOR STOP FITTING #1. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.SDR AALA202402012493Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.SDR AALA202402013169Slide · overservicedAIRCRAFT WAS NOT GROUNDED: R4 SLIDE OVERSERVICED. GAUGE SHOWING IN RED ABOVE GREEN BAND. REMOVED AND REPLACED R4 SLIDE ASSEMBLY.SDR YENA2024013000169Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN BOTH FRAME SEGMENT (1) OF THE EMERGENCY EXIT HATCH DOOR 844 CRACK L= 0.380 IN; REF: ARM W/O 2023 363/1 N/R 2023-749600 ACCOMPLISHED REINFORCEMENT DOOR STRUCTURE MODIFICATION IAW EC A320-52-1144, R&R SEGMSDR YENA2024013000168Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN BOTH FRAME SEGMENT (1) OF THE EMERGENCY EXIT HATCH DOOR 834 CRACK L=0.300IN; REF: ARM W/O 2023 363/1 N/R 2023-749598 ACCOMPLISHED REINFORCEMENT DOOR STRUCTURE MODIFICATION IAW EC A320-52-1144, R&R SEGMENSDR YENA2024013000167Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN BOTH FRAME SEGMENT (1) OF THE EMERGENCY EXIT HATCH DOOR 833 CRACK L=0.375 IN; REF: ARM W/O 2023 363/1 N/R 2023-749595 ACCOMPLISHED REINFORCEMENT DOOR STRUCTURE MODIFICATION IAW EC A320-52-11444, R&R SEGMSDR YENA2024013000166Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN BOTH FRAME SEGMENT (1) OF THE EMERGENCY EXIT HATCH DOOR 843 CRACK L=0.365; REF: W/O 2023 363/1 N/R 2023-749593 ACCOMPLISHED REINFORCEMENT DOOR STRUCTURE MODIFICATION IAW EC A320-52-1144, R&R SEGMENTS IAWSDR YENA2024013000165Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 AT AFT GALLEY AREA (FR 68 LH STOP DOOR 1, INBOARD/ LOWER HOLE , DIRECTION OF CRACK IS 6 OCLOCK, LENGTH OF CRAC K IS: 0.118 INCHES APPROX); (RESOLVED ON W/O: 1256626 TASKCARD: NR-00011) REF: ARM W/O 2023 36SDR YENA2024013000164Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 AT AFT GALLEY AREA FR 68 RH STOP DOOR 1 I/B LOWER HOLE CRACK INDICATION IS 5 O'CLOCK, NENGTH OF CRACK IS .127 INCHES; (RESOLVED ON W/O: 1256626 TASKCARD: NR-00009) REF: ARM W/O 2023 363/1 N/R 2023-749785 PSDR YENA2024013000163Door Sill · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC. FR61 PLUS 9 INCHES ON DOOR CUT OUT IN BULK CARGO COMPARTMENT; REF.AERO W/O 1256621 / 2023-749879 - PERFORMED PERM REPAIR LOC. FR61 PLUS 9.510" ON LOWER SILL, BULK CARGO COMPT, IAW A320 SRM 53-41-49-300-003. PSDR YENA2024013000162Door Sill · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC FR60 PLUS 11 INCHES ON DOOR CUTOUT IN BULK CARGO COMPARTMENT; REF: ARM W/O 2023 363/1 N/R 2023-749877 PERFORMED PERMANENT REPAIR LOC. FR 60 PLUS 10.908 INCHES ON LOWER SILL BULK CARGO COMPARTMENT IAW A320 SRM SDR YENA2024013000161Door Sill · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC. BTW FR66/FR68 AT LEVEL STR23R AFT GALLEY ARE A (1 EA) (CPCP RELATED, REFER TO MPD TASK 534195-01); PERFORMED PERMANENT REPAIR LOC. LOWER SILL AT LEVEL STR23R BTW FR 67 TO FR 68 AFT GALLEY AREA IAW A320 SRM 53SDR YENA2024013000160Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE OVERHANG LOC. AT LEVEL BTW RIB 7 TO RIB 8 ON RH WING; REF AEROMAN W/O 2023 363/1 N/R 2023-749626 EVALUATED REWORKED AREA AND FOUND WITHIN LIMITS ON TRAILING EDGE TOP SKIN LOWER SURFACE OVSDR YENA2024013000159Web · corrodedDURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE WEB LOC. BTW FR69/FR70 AT LEVEL STR23R AT AF T GALLEY AREA (1 EA) (CPCP RELATED, REFER TO MPD TASK 534195-01); REF AEROMAN WO 2023 363/1 NR 2023-749950 REMOVED AND REPLACED STRUCTURE WEB (FRAME SUPPORT) LOC.
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