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 CALA2023031000688Slide · noneREOCCURRENCE OF DOOR R2 SLIDE NOT SHOWING ARMED IN FLIGHT. CREW REPORTS THAT DOOR 2R ARMING HANDLE MIGRATED SLIGHTLY OUT IN FLIGHT MULTIPLE TIMES. FLIGHT CREW CALLED AND TOLD THEM THEY GOT THE INDICATION IMMEDIATLEY WHEN THE ARMING HANDLE MIGRATED OUTWARD CHECMar 10, 2023 · N418UA · Airbus A320232 · Electrical/Electronic Compartment DoorsSDR CALA2023031000683Door · corrodedFWD CARGO DOOR CUTOUT LOWER AREA BETWEEN FR24 TO FR28 ABOVE STRI NGER 38RH SHOWS SEVERAL CORROSION AS MARKED. REMOVED CORROSION IAW SRM 51-74-00 FROM FWD CARGO DOOR CUTOUT LO STA: ST ENG BFM WER AREA BETWEEN FR24 AND FR28 L=2" W=1.1" D=0.065" FOUND TO BE OUT OMar 10, 2023 · N448UA · Airbus A320232 · DoorsSDR CALA2023031000682Flange · crackedORIGINAL LOP PAGE CLOSED IN ERROR: R/H FR68 STGR22 INNER CAP WEB FLANGE HAS A CRACK INDICATION "CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT" AD RELATED (AD 2022-15-05) PER HAECO LCQ NR 9292565/40565 GENERATED BY V061632. REFERENCE ORIGINAL Mar 10, 2023 · N447UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2023031000681Frame · noneAREA REQUIRES INITIAL INSPECTION ON FRAME REPAIR AT R/H FR68, STR22RH PER PART 2B OF THE LATEST REVISION OF ECRA5341-01371 ON OR BEFORE AIRCRAFT REACHES 79200 TOTAL FLIGHT CYCLES. OR BEFORE AIRCRAFT REACHES 79200 TOTAL FLIGHT CYCLES. INSPECTION THRESHOLD. METHMar 10, 2023 · N447UA · Airbus A320232 · Fuselage Main, FrameSDR AALA202305153439Structure · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN CENTER FUSELAGE SIDE SHELL AFT LOWER FASTENER HOLE #2 AT FR 35 AND S30L REPAIRED SIDE SHELL PER EA 343127.Mar 9, 2023 · N657AW · Airbus A320232 · Fuselage Main, Plate/SkinSDR AALA202304274094Gauge · brokenAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DAMPER AND EMERGENCY OPERATION CYLINDER GUAGE BROKEN. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14.Mar 9, 2023 · N657AW · Airbus A320232 · Passenger/Crew DoorsSDR GTIA2023031037029Strut · wornWEAR ON OB FLAP INTERCONNECTING AREA IB SIDE ON LH WING. RAF-01 2824485-02 GENERATED. REF AEROMAN NR 2023-47274.-PERFORMED PERMANENT REPAIR LOCATED ON FLAP INTERCONNECTING AREA I/B SIDE ON LH WING IAW EA # 57-0057-23 REV #1, EA # 57-0057-23 REV #2, EA # 57-00Mar 9, 2023 · N647NK · Airbus A320232 · Trailing Edge FlapsSDR GTIA2023031037028None · dentedSEVERAL DENTS WORK DECK GALLEY 4 AFT GALLEY AREA. RAF-01 2824484-01 GENERATED-REPLACED WORK DICK GALLEY 4 AFT GALLEY AREA IAW AE 25-3006-23.Mar 9, 2023 · N647NK · Airbus A320232 · Cabin Equipment/FurnishingsSDR GTIA2023031037027Battery · inoperativeEPSU - EMERGENCY POWER SUPPLY UNIT 11WL INOP - SDR REQUIRED.-SDR 2824488-2 GENERATED FOR EPSU AT POSITION 11WL. NO FURTHER ACTION REQUIRED. REFERENCE AEROMAN NR 2023-47432 ON W/O 2013 74 / 1.Mar 9, 2023 · N647NK · Airbus A320232 · Lighting SystemSDR GTIA2023031037026Strut · wornWEAR ON OB FLAP INTERCONNECTING AREA IB SIDE ON RH WING. RAF-01 2824485-01 GENERATED. REF AEROMAN NR 2023-47265.-PERFORMED PERMANENT REPAIR LOCATED ON OB FLAP INTERCONNECTING AREA I/B SIDE ON RH WING IAW EA # 57-0056-23 REV #1, EA # 57-0056-23 REV #2, EA # 57-Mar 9, 2023 · N647NK · Airbus A320232 · Trailing Edge FlapsSDR YENA2023031000224Fan · failedFLT#295, JFK-AUS.'DURING DESCENT INTO AUS BELOW 10000 AND AFTER PASSING THRU SEVERAL CLOUDS STRONG FUME SMELL ON FD AND IN CABIN ROW 20 FWD ( PACKS ); REFER TO L/P 3595597, ITEMS 1 (R & R COOLING IAW AMM 49-52-00. R & R APU HIGH OIL TEMP SENSOR IAW AMM 49-52-0Mar 9, 2023 · N523JB · Airbus A320232 · Air Conditioning SystemSDR CALA2023031000689Fitting · crackedORIGINAL LOP PAGE CLOSED IN ERROR: R/H FR68 STGR22 INNER CAP WEB FLANGE HAS A CRACK INDICATION "CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT" AD RELATED (AD 2022-15-05) PER HAECO LCQ NR 9292565/40565 GENERATED BY V061632. REFERENCE ORIGINAL Mar 9, 2023 · N447UA · Airbus A320232 · Fuselage Structure (General)SDR AALA202304261176Attach Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD FLAP INTERCONNECTION STRUT AFT ATTACH FITTING BEARING HAS EXCESSIVE PLAY AT RIB 24. REPLACED ATTACH FITTING PER SRM 51-42-11.Mar 8, 2023 · N657AW · Airbus A320232 · Trailing Edge FlapsSDR AALA202304251819Attach Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING FLAP INTERCONNECTING STRUT ATTACH FITTING HAS EXCESSIVE PLAY BEARING ON THE INBOARD FLAP END AT RIB 14. REPLACED ATTACH FITTING PER SRM 51-42-11.Mar 8, 2023 · N657AW · Airbus A320232 · Trailing Edge FlapsSDR GTIA2023031037022Unknown · unknownFLIGHT ATTENDANT REPORTED BURNING SMELL ON APPROACH -PERFORMED OPS TEST OF PACK 1 AND 2 TEMP CONTROL IAW AMM 21-61-00-710-001, OPS TEST GOOD, NO FURTHER DEFECTS NOTEDMar 8, 2023 · N656NK · Airbus A320232 · Air Conditioning SystemSDR YENA2023030900223Slide Raft · failedFLT#573, EWR-TPA. 'FAILED EMERGENCY LIGHT TEST ( ESCAPE SLIDE LIGHTING ); REMOVED AND REPLACED L1 DOOR SLIDE IAW AMM 25-62-44. OPS CHECK GOOD.'Mar 8, 2023 · N584JB · Airbus A320232 · Emergency LightingSDR YENA2023030900221Pressure Switch · failedFLT#698, MCO-LGA. (AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED TO JFK) 'HYD B RSVR LO LVL; INSPECTED MLG BAY NOTED BLUE SYS HYD LEAKING IN THE AREAS OF THE BLUE HYD PUMP CLEANED NOTED AFFECTED ZONE SERVICED BBLUE HYD SYS AND PRESSURIZED TO ISOLATE HYD LEAK. THMar 8, 2023 · N558JB · Airbus A320232 · Hydraulic Power SystemSDR AALA202304252669Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FRAME AFT FACE WEB ON THE HORIZONTAL FLANGE LOWER RADII CRACKED AT FR 68 AND S22L. REPAIRED FRAME PER EA 343126.Mar 7, 2023 · N657AW · Airbus A320232 · Fuselage Main, FrameSDR GTIA2023030937020Engine · stalledENG 1 COM STALL ON CLIMBOUT AIR RETURN TO MCO-PERFOMED BORESCOPE OF THE HP COMPRESSOR IAW AMM 72-00-00-200-016-B FOUND DAMAGE ON THE 5TH STAGE OF THE HPC.Mar 7, 2023 · N621NK · Airbus A320232 · Engine (Turbine/Turboprop)SDR AALA202305051256Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.Mar 6, 2023 · N657AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202305045526Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.Mar 6, 2023 · N657AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202304203081Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON LEFT HAND FRAME DOOR STOP FITTING #1 INBOARD LOWER FASTENER HOLE AT FR 66. REPAIRED FRAME PER SRM 53-41-12-300-011.Mar 6, 2023 · N657AW · Airbus A320232 · Fuselage Main, FrameSDR AALA202304199164Unknown · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPLACED LOWER SILL PER SRM 51-72-11.Mar 6, 2023 · N657AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202304122840Unknown · crackedAIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 834 DOOR FRAME, EDGE CURVED LOWER CRACKED AT FR 38. REPLACED DOOR FRAME, EDGE CURVED LOWER PER SRM 51-42-11.Mar 6, 2023 · N657AW · Airbus A320232 · Emergency ExitsSDR AALA202304069352Unknown · crackedAIRCRAFT IN BASE MAINTENACNE: EMERGENCY EXIT DOOR 834 INTERNAL SEGMENT ANGLE CRACKED BETWEEN DOOR BEAM 2 AND BEAM 3. REPLACED SEGMENT PER SRM 51-72-11.Mar 6, 2023 · N657AW · Airbus A320232 · Emergency ExitsSDR AALA202304057498Unknown · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUT OUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23R. REPLACED LOWER SILL PER SRM 51-42-11.Mar 6, 2023 · N657AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202304046532Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK AT FR 66 AND -Y765. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.Mar 6, 2023 · N657AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202304047172Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 64 AND FR 66 AT -Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.Mar 6, 2023 · N657AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202303224983Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK AT FR 66 AND +Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.Mar 6, 2023 · N657AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202303179778Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON WEB AT FR 20 AND S23R. REPLACED WEB PER SRM 51-42-11.Mar 6, 2023 · N657AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2023030900643Beam · corrodedA3NB-53-3-6038 CABIN FLOOR SUPPORT AND ATTACHED BRACKET JUST O/B OF -Y1292 FR16 HAVE CORROSION CABIN FLOOR SUPPORT REMOVED AND REPLACED FOR NEW FLOOR SUPPORT IAW SRM 51-42-11. WC:50689 EMP:V936191 STA:ST ENG BFMMar 6, 2023 · N451UA · Airbus A320232 · Fuselage Main, StructureSDR YENA2023030600206None · noneFLT#87, ALB-FLL. 'INFLIGHT ADVISED DURING DESCENT THAT THERE WAS A STRONG AND PERSISTENT DIRTY SOCK ODOR. MX -270 FILLED OUT; PERFORMED LEVEL B REMOVAL OF THE CONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM (ECS) IAW AMM 21-00-00-615-803A. REMOVED AND REPLACMar 6, 2023 · N559JB · Airbus A320232 · Air Conditioning SystemSDR CALA2023030600637Floor Support · corrodedA3NB-53-3-6038 CABIN FLOOR SUPPORT AND ATTACHED BRACKET JUST O/B OF -Y1292 FR16 HAVE CORROSION CABIN FLOOR SUPPORT REMOVED AND REPLACED FOR NEW FLOOR SUPPORT IAW SRM 51-42-11. WC:50689 EMP:V936191 STA:ST ENG BFMMar 6, 2023 · N451UA · Airbus A320232 · Fuselage Main, StructureSDR YENA2023030600205None · noneFLT#771, BOS-CUN. 'DIRTY SOCK SMELL ON DESCENT REPORTED BY IN FLIGHT AFTER FLIGHT; PERFORMED PACK BURN WITH ENG #2 IAW INFO NOTICE 2017-T015J. NO MORE ODOR WAS DETECTED. CLEAR.'Mar 4, 2023 · N504JB · Airbus A320232 · Standard Practices/StructuresSDR CALA2023030600631Flange · crackedDURING HMV4 VISIT AT BFM ACCOMPL''G EA5341-01231 (B) CRACKS WERE FOUND AT FR68 LH STGR 22 WEB HORIZ FLANGE UPPER & LWR BOTTOM RADIUS. ADDITIONALLY, WHILE ACCOMPL''G EA5340-01724(C) OP2 A CRACK WAS NOTED AT FR68 LH DOOR STOP FITTING #1 WORK ACCOMPLISHED ON VTAEMar 4, 2023 · N448UA · Airbus A320232 · Fuselage Main, Attach FittingsSDR CALA2023030600630Frame · corrodedRH FWD EMERGENCY EXIT DOOR LOWER FRAME CORROSION PER HAECO LCQ N R 9292717/40717 GENERATED BY V798788 REMOVED AND REPLACED DOOR FRAME AND EDGE CURVE ON R/H FWD EMERGE NCY EXIT DOOR IAW A320 SRM 51-72-11-911-001 & SRM 51-42-11-001 B Y MECH V061737 INSP V079881Mar 4, 2023 · N447UA · Airbus A320232 · DoorsSDR CALA2023030600629Seat Track · corrodedCABIN SEAT TRACK -Y1292 FR20 HAS CORROSION. REMOVED AND REPLACED, CABIN SEAT TRACK -Y1292 FROM FR12 TO FR24 I.A.W. SRM 51-42-11.- EMP: V936191 WC: 50692 STA: ST ENG BFMMar 4, 2023 · N451UA · Airbus A320232 · Fuselage Main, StructureSDR GTIA2023030637010None · noneSTRONG ELECTRICAL SMOKE SMELL COMING FROM ROE 16.-PERFORMED IDENTIFICATION FOR CAUSE OF CABIN ELECTRIC SMELL PER TSM 05-50-00-810-831-A TYPE 9.REMOVED ALL CEILING & SIDEWALL PANELS AROUND ROW 16 & PERFORMED INSPECTION. NO ELECTRICAL SMELL AT THIS TIME. RE-INSMar 3, 2023 · N695NK · Airbus A320232 · Standard Practices/StructuresSDR GTIA2023030637009Flashlight · no testREF DMI # 3058072 R2 FLASHLIGHT WONT TEST-R/R R2 F/A FLASHLIGHT IAW CMM 25-60-13. OPS CHECK GOOD THIS CLEARS DMI # 3058072 PLACARD REMOVED MOC NOTIFIED.Mar 3, 2023 · N642NK · Airbus A320232 · Escape SlideSDR AALA202303060503Battery · no testAIRCRAFT WAS NOT GROUNDED: OVERHEAD EMERGENCY LIGHT AT SEAT ROW 18 INOPERATIVE. MAINTENANCE REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.Mar 3, 2023 · N601AW · Airbus A320232 · Emergency LightingSDR AALA202303067182Power Supply · no testAIRCRAFT WAS NOT GROUNDED: OVERHEAD EMERGENCY LIGHT AT SEAT ROW 26 INOPERATIVE. MAINTENANCE REPLACED AFT EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.Mar 3, 2023 · N601AW · Airbus A320232 · Emergency LightingSDR CALA2023030300597Seat Track · corrodedCABIN SEAT TRACK -Y1292 FR20 HAS CORROSION. REMOVED AND REPLACED, CABIN SEAT TRACK -Y1292 FROM FR12 TO FR24 I.A.W. SRM 51-42-11.- EMP: V936191 WC: 50692 STA: ST ENG BFMMar 3, 2023 · N451UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2023030300610None · noneLEFT OVERWING AFT EXITINDICATION SHOWS COVERHAS BEEN REMOVED WIT HPRESSURIZATION NORMAL COVER FOR AFT OVERWING EXIT HATCH FOUND INSTALLED. EMER EXIT SLIDE INDICATION LIGHT OPS CHECKED GOOD REF MM25-62-44-420-064-A STEP 10.Mar 3, 2023 · N423UA · Airbus A320232 · Emergency EquipmentSDR CALA2023030300599Sensor · faultedDURING FADEC FAULT CODES TASK CARD 18-73-22-1-7905 FADEC 1B SHOWED A FAULT. P2 T2 SENS/HC/EEC1. ON ENGINE 1. ACCOMPLISHED TSM 73-22-00-810-871-A, AND PERFORMED INSPECTION OF THE P2/T2 SENSOR IAW AMM 73-22-11-200-010, AND THE P2/T2 HAS BEEN TESTED IAW AMM 73-22Mar 3, 2023 · N471UA · Airbus A320232 · Fuel Controlling SystemSDR AALA202303157304Rudder · unknownAIRCRAFT IN BASE MAINTENANCE: TRAPPED WATER INDICATION FOUND ON RUDDER SIDE PANEL LEFT HAND HONEYCOMB CORE STRUCTURE BETWEEN RIB 6 AND RIB 7 AND 4.75 INCH FROM RIB 7 AND FASTENER 27 TO 28 AND 2.88 INCH FROM THE TRAILING EDGE. MAINTENANCE REPAIRED RUDDER PER SRMar 2, 2023 · N657AW · Airbus A320232 · Rudder, Plate/SkinSDR CALA2023030300618Frame · crackedWHILE PERFORMING INSPECTIONS ON LH CONTINUITY FITTING, A CRACK W AS FOUND. CRACK FINDINGS CALL FOR REPLACEMENT OF LH/RH CONTINUIT Y FITTINGS. CRACKS WERE ALSO FOUND IN THE LH/RH WINDSHIELD FRAME S HOLES COMMON TO CONTINUITY FITTING HOLES AT 2 O?CLOCK AND 7-8 OMar 2, 2023 · N427UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2023030300617Frame · corrodedRH AFT EMERGENCY EXIT DOOR LOWER FRAME CORROSION PER HAECO LCQ N ON ROUTINE 9292719/40719 GENERATED BY V798788 REMOVED AND REPLACED DOOR FRAME AND CURVE EDGE ON R/H EMERGENCY EXIT DOOR I/A/W A320 SRM 51-72-11-911-001 PER MECH V075620Mar 2, 2023 · N447UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2023030300594Frame · noneFOR THE REPAIR PERFORMED AT FRONT WINDSHIELD FRAME AND LH/RH CONTINUITY FITTINGS ? PLANNING TO CONTACT ENGINEERING AFTER 63,104 TFC BUT BEFORE 64,104 TFC FOR ECRA 5311-02954 PART 2 INSPECTION REQUIREMENTS. REF LP 3976500. 63,104 TFC BUT BEFORE 64,104 TFC FOR EMar 2, 2023 · N427UA · Airbus A320232 · Fuselage Main, StructureSDR AALA202304250452Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD CENTER POST LEFT HAND FRAME UPPER RADII UPPER FASTENER HOLE CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 342932Mar 1, 2023 · N657AW · Airbus A320232 · Fuselage Main, FrameSDR AALA202304253267Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD CENTER POST LEFT HAND CONTINUITY FITTING CRACKED AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 342932Mar 1, 2023 · N657AW · Airbus A320232 · Fuselage Structure (General)
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