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.

SDR YENA2024050200683Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON BOTH FRAME SEGMENTS (1), FWD RH EMERGENCY EX IT DOOR (843) CRACK LENGTH: 0.812 INCH; REF AEROMAN NR 2024-168773 WO 2024 45/1 REMOVED AND REPLACED FRAME SEGMENT (1) FWD RH EMERGENCY EXIT DOOR (843) IAW EC A320May 1, 2024 · N649JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024050200682Shear Tie · corrodedDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 34 BTW STR. 43R AND STR 44 IN FWD CA RGO COMPARTMENT; REF AEROMAN NR 2024-168821 WO 2024 45/1 REMOVED AND REPLACED SHEAR TIE LOC. FR34 BTW STR43R TO STR44 IN FWD CARGO COMPARTMENT IAW A320 SRM 51-72-1May 1, 2024 · N649JB · Airbus A320232 · Fuselage Internal Mounting StructureSDR YENA2024050200681Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION ON TOP EXTERNAL SKIN CENTER FUEL TANK BTW FR 41 TO FR 42 AND BTW -Y1292 TO -Y1732 PASSENGER CABIN; REF AEROMANM NR 2023-168921 WO 2024 45/1 PERFORMED PERMANENT REPAIR LOC.TOP EXTERNAL SKIN CENTER FUEL TANK BTW FR41 TO FR42 OMay 1, 2024 · N649JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2024050200680Attach Bracket · corrodedDURING HEAVY MAINTENANCE: CORROSION RETRACTION ACTUATOR ATTACHMENT BRACKET ON LH MLG. (CPCP RELATED); "REF AEROMAN NR 2024-168957 WO 2024 45/1 REPAIRED BORE, LOWER AND UPPER FACES OF RETRACTION ACTUATOR ANCHORAGE FITTING LH MLG IAW A320 SRM 57-26-13-300-008. MMay 1, 2024 · N649JB · Airbus A320232 · Wing, Landing Gear Attach FittingsSDR YENA2024050200679Skin · corrodedDURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / RH TOP SKIN BTWN FR 41-42 & BTWN BEAM -Y1292 - RIB 1 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)May 1, 2024 · N649JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2024050200696Wire Harness · damagedFLT#1036, SJU-STT. (AIRCRAFT PERFORMED AN AIR TURN BACK) 'AUTO BRAKE FAULT ( TACHOMETER ); FOUND 1M AXLE HARNESS FAULTY WHEN FLEXING CABLE. ALSO PIN GRIPS VERY WORN AND WEAK. REPLACED 1M AXLE HARNESS ON RIGHT MLG AND TESTED IAW AMM 32-11-43. OPS CHECK NORMAL. Apr 30, 2024 · N531JL · Airbus A320232 · Landing Gear System WiringSDR AALA202406219224Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND LATERAL POST WINDSHIELD FRAME UPPER ATTACHMENT CRACKED BETWEEN FR 3 AND FR 4 AT Y0. REPLACED WINDSHIELD FRAME PER EA 353864.Apr 29, 2024 · N662AW · Airbus A320232 · Fuselage Main, FrameSDR AALA202406218199Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND LATERAL POST WINDSHIELD FRAME UPPER ATTACHMENT CRACKED BETWEEN FR 3 AND FR 4 AT Y0. REPLACED WINDSHIELD FRAME PER EA 353864.Apr 29, 2024 · N662AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202406139826Fitting · noneAIRCRAFT IN BASE MAINTENANCE: THE FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0 REQUIRES REPLACEMENT DUE TO THE MAJOR REPAIRS BEING ACCOMPLISHED TO THE FLIGHT DECK CENTER WINDSHIELD FRAMING PER EA 353508. MAINTEApr 29, 2024 · N662AW · Airbus A320232 · Standard Practices/StructuresSDR AALA202406132769Fitting · noneAIRCRAFT IN BASE MAINTENANCE: THE FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0 REQUIRES REPLACEMENT DUE TO THE MAJOR REPAIRS BEING ACCOMPLISHED TO THE FLIGHT DECK CENTER WINDSHIELD FRAMING PER EA 353508. MAINTApr 29, 2024 · N662AW · Airbus A320232 · Fuselage Main, StructureSDR YENA2024050200694Unknown · odorFLT#1302, PHX-BOS. 'INFLIGHT REPORTED ODOR IN CRUISE. STRONGEST IN AFT GALLEY WHILE IN FLIGHT. ODOR REPORT FORM COMPLETED; REMOVED AND INSTALLED RECIRCULATION FILTERS IAW AMM 21-21-41. OPS NORMAL COMPLIED WITH INFORMATION NOTICE 2017-T015J SECTION A, ISOLATEDApr 29, 2024 · N705JB · Airbus A320232 · Air Distribution SystemSDR YENA2024042900672Lgciu · failedFLT#593, EWR-STI. (AIRCRAFT DIVERTED TO FLL) .'AFTER TAKEOFF ECAM LGCIU 2 FAULT ( 2ND WRITEUP); REF TSM 32-31-00-810-823-A. VISUALLY INSPECTED DNLK SENSOR 17GA, NO DEFECT NOTED. GAP WITHIN LIMITS. REMOVED AND REPLACED LGCIU2 IAW AMM 32-31-71.OPS CHECK OK. NO FApr 29, 2024 · N653JB · Airbus A320232 · Landing Gear Position and WarningSDR AALA202405158927Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT OPEN HOLE OF DOOR STOP FITTING #1 LOWER INBOARD POSITION AT FR 68 AND S23R. REPAIRED FRAME PER EA 354083.Apr 28, 2024 · N669AW · Airbus A320232 · Fuselage Main, FrameSDR AALA202405076986Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BOLT ATTACHMENT SLAT TRACK 2 (MID FORWARD BOLT) ON LEFT-HAND WING. REPLACED BOLT PER JOB CARD 26C51057005.Apr 28, 2024 · N662AW · Airbus A320232 · Leading Edge DevicesSDR CALA2024042901254Lamp · missingPDA 2 AIRCRAFT ARRIVED AND TECH DISCOVERED RH RETRACTABLE LANDING LIGHT AND RETAINING RING MISSING. ITEM IS CLASS 2 PDA AND LAMP WEIGHT IS 2.0LBS. SDR REPORT # 1035963 SUBMITTED. TOMC MX CNTL HILL. FOND RH LANDING LIGHT MISSING. THE WIRE EXPOSED. TOMC NOTIFIEDApr 28, 2024 · N447UA · Airbus A320232 · Exterior LightingSDR CALA2024042901259Bulb · missingPDA 2 REF LOG 7799106 - RIGHT RETRACTABLE LANDING LIGHT BULB AND RETAINER MISSING (DEPARTED AIRCRAFT). PARTS MISSING ARE BULB, RETAINER & GASKET. REF. IPC 33-42-11-01A ITEMS 20, 30 & 40. RETERMINATED REF. TO AWM 33-42-00 AND ESPM 20-48-19. INSTALLED NEW LANDINApr 28, 2024 · N483UA · Airbus A320232 · Exterior LightingSDR GTIA2024042838092Megaphone · inoperativeAFT MEGAPHONE INOP-R/R AFT MEGAPHONE IAW CMM 25-60-01.Apr 27, 2024 · N629NK · Airbus A320232 · Emergency EquipmentSDR YENA2024042900669Apu · contaminatedFLT#469, BOS-FLL. 'STRONG LEVEL 2 DIRTY SOCK. DESCENDING FROM 4K TO 3K ON APPROACH. PILOTS THOUGHT IT SOMEWHAT DISSIPATED. FLIGHT ATTENDANT'S DID NOT; FOUND SOURCE OF SMELL: APU HAS OIL SATURATION. "COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION B2. DECONApr 26, 2024 · N630JB · Airbus A320232 · APU Oil SystemSDR GTIA2024042838089Bottle · low pressureFOUND DURING SERVICE CHECK L2 DOOR ASSIST BOTTLE PRESS LOW-SERVICED L2 DOOR ASSIST BOTTLE TO REQUIRED PRESSURE. IAW AMM 12-14-00. OPS CHECK GOODApr 26, 2024 · N690NK · Airbus A320232 · Emergency EquipmentSDR GTIA2024042838088Bottle · low pressureUPON WALK AROUND FOUND DOOR ASSIST ACCUMLATORS LOW-SERVICED DOOR ASSIST ACCUNULATORS TO REQUIRED PRESSURE IAW AMM 29-10-00. OPS CHECK GOODApr 26, 2024 · N690NK · Airbus A320232 · Emergency EquipmentSDR GTIA2024042938105Pressure Blkhd · corroded"CORROSION AND PRESSURIZATION LEAK FOUND AT APU DUCT FAIRLEAD ON AFT PRESSURE BULKHEAD FR. 70 RAF-01 3420898-01 GENERATED-COMPLIED WITH EA 5351-2440"Apr 25, 2024 · N643NK · Airbus A320232 · Fuselage Main, BulkheadSDR GTIA2024042938104Counter · damagedREF SPIRIT W/O 297693 J/C TR-2533-015-1-NKS. G4 GALLEY WORKDECK REPAIR. RAF 3420896-02 GENERATED. SDR GENERATED.-COMPLIED WITH TR 2533-015Apr 25, 2024 · N643NK · Airbus A320232 · Buffet/GalleysSDR GTIA2024042938103Counter · damaged"ON CALL REPAIR OF G4 GALLEY WORKDECK REQUIRED PER TR 2533-015-1. RAF-01 3316180-02 GENERATED-REMOVED AND REPLACED BY NEW ONE DUE TO NOT FOUND ALLOWABLE DAMAGE IAW SAFRAN CMM 25-31-605. FOR STEPS PROCEDURE REFER TO CARD EC TR 2533-015"Apr 25, 2024 · N615NK · Airbus A320232 · Buffet/GalleysSDR GTIA2024042938102Release Cable · disengagedDURING THE INCOMING INSPECTION THE RH OVERWING SLIDE INFLATION RELEASE CABLE WAS FOUND DISENGAGED AT THE EMERGENCY DOOR-TRANSFERRED TO AEROMAN W.O. 2024-98/1 NR 2024-188541Apr 25, 2024 · N615NK · Airbus A320232 · Escape SlideSDR GTIA2024042938101Skin · wornREF SPIRIT W/O 293812 TC 534148-01-1-NKS. WEAR ON EXTERNAL SKIN LOACTED AT FRAME 34 BETWEEN STRINGER 43L TO STRINGER 43R AT LOWER FUSELAGE. LENGTH OF 60.70 MM, WIDTH OF 48.514 MM, AND DEPTH OD 0.78 MM. RAF-01 3316183/2 GENERATED. SDR GENERATED.-PERFORMED PApr 25, 2024 · N615NK · Airbus A320232 · Fuselage Main, Plate/SkinSDR GTIA2024042938100Skin · scratchedREF SPIRIT W/O 293812 T/C ZL-500-03-1-L-NKS. SCRATCH LEADING EDGE SKIN SLAT 1 ON L/H WING. SEVEN SCRATCHES MEASURING LENGTH 5.017 IN DEPTH 0.002 IN, LENGTH 6.141 IN DEPTH 0.003 IN, LEGTH 7.663 IN DEPTH 0.005 IN, LENGTH 22.017 IN DEPTH 0.005 IN, LENGTH 3.462 Apr 25, 2024 · N615NK · Airbus A320232 · Leading Edge DevicesSDR GTIA2024042938099Access Panel · damaged"ELONGATED HOLE CUT OUT ON FUEL TANK ACCESS PNL 640K BTW RIB 15 AND RIB 16 RH WING. RAF-01 3316188-01 GENERATED-REPLACED ACCESS PANEL 640KB FUEL TANK ON RH WING PER SRM 51-72-11--911-001 REFER TO JOB CARD CL- Z2640-NKS FOR INSTALLATION OF THE NEW ACCESS PANELApr 25, 2024 · N615NK · Airbus A320232 · Wing, Plate/SkinSDR GTIA2024042938098Access Panel · damaged"DELAMINATED ACCESS PNL 481AL RAF-01 3316187-01 GENERATED-PERFORMED PERMANENT REPAIR ON RH PYLON ACCESS PANEL 481AL AS PER EC EA 5453-2419 AND EA#54-0082-24 REV 0."Apr 25, 2024 · N615NK · Airbus A320232 · Nacelle/Pylon Miscellaneous StructureSDR GTIA2024042938097Access Panel · damaged"ELONGATED HOLE CUT OUT ON FUEL TANK LOWER EXTERNAL SKIN BTW RIB 16 AND RIB 17 LH WING. RAF-01 3316188-02 GENERATED-PERFORMED PERMANENT REPAIR ON COI-00T OF RIB 16 AND RIB 17 ON LH WING OF FUL TANK PANEL AS PER SRM 57-21-11-300-002.. THIS REPAIR IS CATEGORY BApr 25, 2024 · N615NK · Airbus A320232 · Wing, Plate/SkinSDR GTIA2024042938096Access Panel · damaged"ELONGATED HOLE CUT OUT ON FUEL TANK LOWER EXTERNAL SURFACE BTW RIB 14 AND RIB 15 LH WING RAF-01 3316189-02 GENERATED-PERFORMED PERMMANENT REPAIR ON COT-OUT OF RIB 14 AND RIB 15 ON LH WING OF FUEL TANK PANEL AS PER SRM 57-21-11-300-002. THIS REPAIR IS CATEGORApr 25, 2024 · N615NK · Airbus A320232 · Wing, Plate/SkinSDR GTIA2024042938095Access Panel · damaged"DELAMINATED ACCESS PNL 471AR RAF-01 3316187-02 GENERATED-COMPLIED WITH EA 5453-2418"Apr 25, 2024 · N615NK · Airbus A320232 · Standard Practices/StructuresSDR GTIA2024042938094Hinge Arm · damagedREF SPIRIT W/O 293812 T/C 553006-01-2-NKS. ELONGATED HOLE HINGE ARM 7 ON VERTICAL STABILIZER. REF-01 3316184-02 GENERATED. SDR GENERATED.-REPLACED HINGE ARM # 7 AS PER EA#55-0096-24 AND SRM A320 55-36-42-300-003. THIS REPAIR IS CATEGORY A.Apr 25, 2024 · N615NK · Airbus A320232 · Vertical StabilizerSDR YENA2024042900668Unknown · odorFLT#1173, EWR-TPA. 'ODOR/FUME EVENT REPORTED BY INFLIGHT DURING DECENT AT 6K FEET; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION, ISOLATED FAULT TO TYPE 10,(A)1,C PER TSM 05-50-00-810-085-B / TSM 05-50-00-810-085-D. AIRCRAFT IS OK FOR SERVICE.'Apr 25, 2024 · N564JB · Airbus A320232 · Air Distribution SystemSDR GTIA2024042838084Carpet · contaminatedDURING CRUISE AN ODOR WAS NOTICED BY BOTH FAS A AND B AND PASSENGERS IN FIRST TWO ROWS. NO ODOR NOTICED ON FLT DECK OR IN REAR OF A/C.-PERFORMED TSM 05-50-00-810-831 C.O.S. IS A TYPE 10 MISCELANEOUS. SMELL IS BETWEEN ROW 1-3 MORE ON THE LEFT SIDE & FWD LAV.CLEApr 25, 2024 · N626NK · Airbus A320232 · Passenger Compartment EquipmentSDR AALA202404262182Sign · missingAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 4R DOOR IS MISSING AN EXIT SIGN. MAINTENANCE REPLACED EXIT SIGN AT 4R DOOR PER AMM 25-10-00.Apr 25, 2024 · N663AW · Airbus A320232 · Emergency LightingSDR CALA2024052901611Doubler · gougedL/H WING SLAT #3 INBD UPPER TE HAS A WEAR MARK. FABRICATED AND INSTALLED LEG DOUBLER 2EA FILLERS ON L/H WING SL AT 3 I/B UPPER T/E IAW A320 SRM 57-44-21-300-001- THIS IS CAT A REPAIR PERMAMENT NO INSPECTION REQUIRED.Apr 24, 2024 · N456UA · Airbus A320232 · Wing, Plate/SkinSDR YENA2024050200701Windshield · leakingFLT#149, JFK-GND. (AIRCRAFT PERFORMED AN AIR TURN BACK) 'CAPTAINS FIXED WINDSHIELD LOUD SQUEAL AT 9:00 POSITION. WOULD NOT SEAL AT HIGHER CABIN DIFF PRESSURE. WENT AWAY AT 5000 FT ALTITUDE WITH 2.5 PRESSURE DIFFERENTIAL; ACCOMPLISHED CAPT'N WINDSHIELD REPLACApr 24, 2024 · N708JB · Airbus A320232 · Flight Compartment WindowsSDR CALA2024050201301Doubler · damagedEA 5300-02120 FR 34 B/W STR43L AND 43R HAS PREVIOUSLY INSTALLED DOUBLER THAT IUS CHAFED AND HAS ENLONGATED FASTENER HOLE "REMOVE DAMAGED DOUBLER, MAP DAMAGE OF SKIN PANEL, REMOVED AND REPLACED DISCREPANT DOUBLER AT FR34 STR 43L-43R IAW ECRA 5331-02271.Apr 24, 2024 · N456UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2024042901258Floorbeam · crackedFR11 BEAM -765 HAS CRACKED WEB GENERATED BY ON HAECO LCQ NR9296834/30834 REMOVED AND REPLACED CRACKED WEB AT FR11 ON FLOOR BEAM -765 IAW H-320 SRM 51-42-11/001Apr 24, 2024 · N456UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2024042901257Floor Support · corrodedAFT PIT TORSION BOX COVER CORRODED IN SEVERAL PLACES GENERATED B Y V061642 ON HAECO LCQ NR 9296422/30422 REMOVED AND REPLACED AFT CARGO TORSION BOX COVER SHEET IAW A320 SRM 51-72-11-911-001 ACMP BY MECH V061737 INSP BY N078570Apr 24, 2024 · N456UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202404255722Brake · abnormalAIRCRAFT WAS GROUNDED: LEFT BRAKE DIFFICULT TO MODULATE. GRABBY WHEN APPLYING AND RELEASING. MAINTENANCE REPLACED THE #1 (AALA202404253384) AND #2 (AALA202404255722) MAIN LANDING GEAR BRAKES PER AMM 32-42-27.Apr 24, 2024 · N651AW · Airbus A320232 · Landing Gear Brake SystemSDR AALA202404253384Brake · abnormalAIRCRAFT WAS GROUNDED: LEFT BRAKE DIFFICULT TO MODULATE. GRABBY WHEN APPLYING AND RELEASING. MAINTENANCE REPLACED THE #1 (AALA202404253384) AND #2 (AALA202404255722) MAIN LANDING GEAR BRAKES PER AMM 32-42-27.Apr 24, 2024 · N651AW · Airbus A320232 · Landing Gear Brake SystemSDR AALA202405134579Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT-HAND PYLON SPIGOT FITTING RECEPTACLE BORE LOCATED BETWEEN WS 679 AND WS 706 AND RIB 4 TO RIB 5 ON LEFT-HAND PYLON. REPLACED LOWER SPIGOT FITTING PER SRM 54-51-12-300-002.Apr 23, 2024 · N662AW · Airbus A320232 · Nacelle/Pylon, Main FrameSDR AALA202405135476Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT PYLON SPIGOT RECEPTACLE BORE LOCATED BETWEEN WS 679 AND WS 706 AND RIB 4 TO RIB 5 ON LEFT-HAND PYLON. REPLACED LOWER SPIGOT FITTING PER SRM 54-51-12-300-002.Apr 23, 2024 · N662AW · Airbus A320232 · Nacelle/Pylon Miscellaneous StructureSDR CALA2024042601248Spoiler · vibrationAIRFRAME VIBRATION NOTICED AT SPEEDS GREATER THAN 290 KIAS. NUMBER 5 SPOILER VIBRATING.Apr 23, 2024 · N439UA · Airbus A320232 · SpoilersSDR AALA202404297856Splice · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPLICE COUPLING UPPER SIDE OUTBOARD LOCATED ON FR 66 AT STR 23L. REPLACED SPLICE COUPLING PER SRM 51-72-11-911-001.Apr 22, 2024 · N660AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202404293318Splice · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPLICE LOCATED ON FR 66 AT S23L UPPER SIDE INBOARD. REPLACED SPLICE COUPLING PER SRM 51-72-11.Apr 22, 2024 · N660AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202404246898Handle · lack of lubeAIRCRAFT WAS NOT GROUNDED: FLIGHTDECK DOOR HARD TO OPEN FROM INSIDE THE FLIGHTDECK. HANDLEEXTREMELY DIFFICULT TO TURN AND OPEN. LUBED DOOR HANDLE PER MM 52-51-11. OPS CHECK GOOD ON GROUND.Apr 22, 2024 · N647AW · Airbus A320232 · Fixed Inner DoorsSDR YENA2024042300655Power Supply · faultedDURING HEAVY MAINTENANCE, EPSU EXT LOAD FWD L AND EPSU INT LOAD FWD L. R & R L1 DOOR RAFT SLIDE IAW AMM 25-62-00.Apr 22, 2024 · N510JB · Airbus A320232 · Escape SlideSDR GTIA2024042338077Bottle · low pressureR2 DOOR ASSIST BOTTLE LOW.-SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00Apr 21, 2024 · N692NK · Airbus A320232 · Emergency Equipment
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