Airbus A320-232
Service difficulty reports · 32,652
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 AALA202510022918Power Supply · no testAIRCRAFT WAS GROUNDED: FWD LEFT EPSU BATTERY FAILS BITE TEST. MAINTENANCE REPLACED FWD LEFT ESPU BATTERY. OPS TEST GOOD. REF AMM 31-51-38/402A.SDR AALA202510025630Power Supply · no testAIRCRAFT WAS GROUNDED: RH EMERGENCY EXIT EPSU FAILS TEST. MAINTENANCE REPLACED 12WL ESPU AND BATTERY REF AMM 33-51-38/401 & 402A.SDR AALA202510022414Wire Harness · inoperativeAIRCRAFT WAS GROUNDED: ROW 9DEF UNDER SEAT 2EACH WIRES DISCONNECTED TO LIGHT HOUSING. MAINTENANCE REPLACED SEAT MOUNTED EMERGENCY LIGHT HARNESS FROM SIDEWALL REF AWM 33-51-07.SDR YENA2025100100987Coffeemaker · odorFLT#451, BOS-MCO. LEVELING OFF AT FL 300 INFLT CALLED AND SAID THEY HAD SMELLED A SMOKEY ODOR. THEY SHUT OFF THE COFFEE MAKERS AND THE SMELL SEEMED TO DISSAPATE. WE TOLD THEM TO ALSO PULL THE GALLEY BREAKERS AS A PRECAUTION. NO ODOR WE ENCOUNTERED AFTERWARDS;SDR YENA2025093000986Unknown · odorFLT#499, LGA-MCO. FUME EVENT DURING DESCENT AT APPROX 12000 FEET UNTIL LANDING CHECMICAL SMELL,HP BLEED OPEN,BOTH PACKS ON, BURNING EYES, FLIGHT DECK. OPENSDR AALA202510068809Handle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON HANDLE SLIDING WINDOW CAPTAIN SIDE IN COCKPIT. MAINTENANCE REPLACED HANDLE ASSEMBLY SLIDING WINDOW CAPTAIN SIDE IN COCKPITIAW CMM 56-12-12. RSDR AALA202510025465Door · obstructedAIRCRAFT WAS GROUNDED: ECAM: DOOR AFT CARGO AFTER TAKEOFF. RETURNING TO CLT, EMERGENCY DECLARED LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AFTER CARGO NET BETWEEN CARGO DOOR SEAL REMOVED NET AND PERFORMED OPS CHK OF AFT CARGO DOOR IAW AMM 52-30-00.SDR YENA2025093000978Unknown · odorFLT#2465, BUF-FLL. STRONG ODOR IN THE REAR OF THE CABIN; ACCOMPLISHED INSPECTION OF APU AND APU COMPARTMENT IAW AMM 49-00-00. NO LEAKS NOTED. ACCOMPLISHED DVI OF FUSELAGE + WHEEL WELLS FOR LEAKS IAW AMM 53-00-00. NO LEAKS NOTED ACCOMPLISHED DVI OF ENG 1 + 2 IASDR AALA202509307006Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: OUT LIMIT RH AFT DOOR (6MM) IAW JC 26C71032007 IN NOSE WHEEL WELL. MAINTENANCE REPLACED AFT AND FWD HINGE FITTINGS ON NLG AFT DOOR RH IAW CMM 52-82-32-000-801-B01; CMM 52-82-32-000-803-C01; CMM 52-82-32-400-802-C01 AND CMM 52-82SDR AALA202509300309Hinge · excess playAIRCRAFT IN BASE MAINTENANCE: OUT LIMIT LH AFT DOOR (6MM) IAW JC 26C71032007 IN NOSE WHEEL WELL. MAINTNENANCE REPLACED AFT AND FWD HINGE FITTINGS ON NLG AFT DOOR LH IAW CMM 52-82-32-000-801-B01; CMM 52-82-32-000-803-C01; CMM 52-82-32-400-802-C01 AND CMM 52-82-SDR CALA2025093009425Cover · misinstalledDOOR L FWD EMER EXIT ON ECAM SCREEN AT 16000 FT VERIFIED LH FWD EMERGENCY EXIT HATCH HANDLE FLAP COVER IS IN ITS CORRECT INSTALLATION POSITION, LOWER ECAM EMERGENCY EXIT SYMBOL LIGHT EXTINGUISHED AND NO ACTIVE FAULTS PRESSENT. REF TSM 52-21-00-810-801-A.SDR GTIA2025092939108Unknown · odorAT 3000 AGL ON ILS FLT ATTENDANT REPORTED ODOR DESCRIBED AS DIRTY SOCKS PER ELIMINATION ODOR PROCEDURE PACK 2 OFF X BLEED SHUT. DESCRIPTION OF ODOR/FUMES: TEMPORARY, DIRTY SOCKS/MOLDY SMELL. APPARENT CABIN SOURCE: UNKNOWN. AFT CABIN AND MID CABIN. NO VISIBLE SSDR AALA202509296900Hinge Fitting · excess playEXCESSIVE PLAY FWD BEARING MAIN DOOR ON LH MAIN LANDING GEAR. MAINTENANCE REPLACED HINGE FITTING ASSY OF RH MLG DOOR IAW AIRBUS CMM 52-81-18, A319 SRM 51-44-11-801, A319 SRM 51-21-11-801 PMS 01-05-26 AND NTM 51-90-00.SDR AALA202510207376Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM END FITTING #1 ON LH ELEVATOR.MAINTENANCE REPLACED HINGE ARM END FITTING #1 ON LH HORIZONTAL STABILIZER IAW A320 FAM AMM 55-16-42-000-001-A AND IAW A320 FAM AMM 55-16-42-400-001-A.SDR AALA202510142177Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM END FITTING #6 ON LH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #6 ON LH ELEVATOR IAW A320 FAM AMM 55-16-42-000-001-A. AND A320 FAM AMM 55-16-42-400-001-A.SDR AALA202510140836Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM END FITTING #5 ON LH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #5 ON LH ELEVATOR IAW A320 FAM AMM 55-16-42-000-001-A. AND A320 AMM 55-16-42-400-001-A.SDR AALA202510143908Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM END FITTING #4 ON LH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #4 ON LH ELEVATOR IAW A320 FAM AMM 55-16-42-000-001-A. AND A320 AMM 55-16-42-400-001-A.SDR AALA202510143666Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM END FITTING #3 ON LH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #3 ON LH ELEVATOR IAW A320 FAM AMM 55-16-42-000-001-A. AND A320 AMM 55-16-42-400-001-A.SDR AALA202510142300Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM END FITTING #2 ON LH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #2 ON LH ELEVATOR IAW A320 FAM AMM 55-16-42-000-001-A. AND A320 AMM 55-16-42-400-001-A.SDR CALA2025093009426Tire · bulgedNR 3 MLG TIRE FOUND BEYOND AMM LIMITS. MUST BE REPLACED PRIOR TO T HE NEXT FLIGHT. RAMP REPORT: NR 3 TIRE HAS A LARGE BULGE AT THE 6 O'OCLOCK POSITION. WILL NEED REPLACEMENT REPLACED #3 MLG TIRE REF. AMM 32-41-11-400-006-A.SDR YENA2025093000985Smoke Warning · false activationFLT#8650, SAL-FLL. "LAV B SMOKE ECAM SMOKE LAVATORY SMOKE NO SMOKE WAS PRESENT IN LAV B; RESET CIDS 1 & 2 PER A320 AMM 23-93-01 OPS CHECKS OK OF LAV B SMOKE DETECTOR OKSDR YENA2025093000984Fitting · crackedDURING HEAVY MAINTENANCE: CONTINUITY FITTTING CRACKED & RH FWD WINDSHIELD CENTER POST; REF AEROMAN NR 2025-506691 & NR 2025-530843 WO 2025 282/1 FOR WORK ACCOMPLISHED & JB EC A22-921-02 & AIRBUS RDAF 81136833/040/2025."SDR YENA2025093000983Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED BTW FR 79 AND FR 80 AND BTW STRINGER 2LH A ND STRINGER 2RH ON UPPER FUSELAGE; (RESOLVED ON W/O: 1409303 TASKCARD: NR-00057) REF AEROMAN W/O 2025 282/1 NR 2025-505895. PERFORMED PERMANENT REPAIR LOCATED ON EXSDR YENA2025093000982Hinge Fitting · corrodedDURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION FOUND ON THE BORE OF HINGE N7 VERTICAL STABILIZER; REF AEROMAN WO 2025 282/1 NR 2025-530866. REMOVED AND REPLACED HINGE #7 VERTICAL STABILIZER IAW AMM 27-21-41-400-001-A STEP 2 (A). TOOL USED EDDY CURRESDR AALA202509291459Flashlight · missingAIRCRAFT WAS NOT GROUNDED: FAS REPORT FLASHLIGHT MISSING FROM REAR OF AIRCRAFT. MAINTENANCE REPLACED FLASHLIGHT AFT CABIN AS REQUIRED OK FOR SVC IAW AMM 25-63-00.SDR CALA2025093009439Intercostal · crackedLEFT FRAME 16 DOUBLE JOGGLE AREA HOLE 18 HAS CRACK INDICATION IN FRAME LAYER AT 5 O`CLOCK, DIRECTION 50%. REMOVED FASTENERS COMMON TO #18 (LEADER), #19 (ASSOCIATED). REF SRM 51-42-11/001. HOLE #18, #19 DIA. = NOMINAL. REAMED HOLE 18 TO MAX DIA. OF .34220? INSDR YENA2025093000972Unknown · odorFLT#1229, EWR-CUN. TRANSIENT ODOR EVENT DURING TAKEOFF, MODORATE NURNING SMELL THROUOUT CABIN. BEGAN TO DISIPATE DURING CLIMBOUT. ( THALES-AVANT IFE (ENTIRE SYSTEM) ); REACTIVATED AVANT IFE SYSTEM IAW AVANT AMMS 44-21-00. NO HAZARDOUS CONDITION NOTED. PERFORMESDR YENA2025093000971Coffeemaker · odorFLT#1307, BOS-BNA, ODOR EVENT ON DESCENT INTO BNA 2-3 MINUTES IN DURATION FROM APPOX 17000 TO 14000 FT COCKPIT NOTICED FOR 2 MINUTES AFT GALLEY NOTICED FOR 3 MINTUES WAS WORST IN AFT GALLEY ELECTRICAL SMELL MIST OR SMOKE VISABLE EYE IRRATION AND HEADACHE SYMPSDR GTIA2025092939103Adr · malfunctionedADR 1 FAULT INCRUISE, PREFORMED OPS TEST IAW AMM 34-13-00 OPS CHECK GOOD NO FAULT MSGS MOC 69661SDR GTIA2025092939102Actuator · faultedUNCOMMANDED RUDDER MOVEMENTS BACK AND FORTH. SMALL MOVEMENTS OF PEDALS AND BLUE RUDDER TRIM INDICATOR. NO FAILURE MESSAGES. STARTED AT ABOUT 4000FT DURING CLIMB OUT-REF TSM 22-62-00-810-809-A. FOUND RUDDER TRIM ACTUATOR AT FAULT. R&R RUDDER TRIM ACTUATOR IAW ASDR AALA202509290999Bottle · low pressureAIRCRAFT IN BASE MAINTENANCE: LOW PRESSURE INFLATION RESERVOIR EMERGENCY EXIT RH DOOR 844. MAINTENANCE REPLACED INFLATION RESERVOIR EMERGENCY EXIT RH DOOR 844 IAW AMM 25-62-46-000-001-A AND AMM 25-62-46-400-001-A.SDR CALA2025092909374Pin · corrodedNUMBER 2 ENG AFT MOUNT INNER AND OUTER PINS ARE PITTED. REMOVED AND REPLACED NR 2 ENGINE AFT MOUNT INNER AND OUTER PINS IAW AMM 71-22-11-000-803-A/400-803-A.SDR CALA2025092909373Pin · corrodedNUMBER 1 ENG AFT MOUNT INNER AND OUTER PINS ARE PITTED. REMOVED AND REPLACED #1 ENGINE AFT MOUNT INNER AND OUTER PINS IA W A320 AMM 71-22-11-000-803-A/400-803-A.SDR CALA2025092909360Girt Bar · obstructedDOOR 2L SLIDE WILL NOT ARM. CHECK GIRT BAR FOR OBSTRUCTION. REMOVED OBSTRUCTION FROM GIRT BAR FITTING. NO DEFECTS NOTED IAW AMM 52-13-00.SDR AALA202512119444Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R BTW FR 69 TO FR 70 AT AFT GALLEY AREA MEASURE OF CRACK IS L= 1.043 IN . MAINTENANCE REPLACED SHEAR PLATE LOCATED STR 23RH BTW FR69 AND FR70 AT AFT GALLEY AREA IAW A320 SRM 51-42-11-801 SRM 51-72-11-911-0SDR AALA202512040529Shear 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.SDR AALA202512032631Profile · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN EMERGENCY EXIT DOOR 843 RIGHT HAND LOAD TRANSMITTING PROFILE SEGMENT. REPLACED SEGMENT PER EO 5210Y228-001.SDR AALA202512031389Profile · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN EMERGENCY EXIT DOOR 833 RIGHT HAND LOAD TRANSMITTING PROFILE SEGMENT. REPLACED SEGMENT PER EO 5210Y228-001.SDR AALA202511286704Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INTERNAL STRUCTURE FR68 UPPER CORNER LH SIDE MEASURE CRACK L : 0.388 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR LOC ON INTERNAL STRUCTURE FR68 UPPER CORNER LH SIDE THIS REPAIR IS CATEGORY B IAW A320 SRM 53-41-12-300-012 SDR AALA202511243952Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INTERNAL STRUCTURE FR68 UPPER CORNER RH SIDE AT AFT GALLEY AREA. CRACK. L=0.141 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOC ON FR68 BTW S-8RH/S-9RH-AFT UPPER CORNER IAW EA# 368628 AND A320 SRM 53-41-12-300-012.SDR AALA202510303899Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23R. REPLACED LOWER SILL PER SRM 51-42-11.SDR YENA2025093000981Hinge Fitting · corrodedDURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ3 VERTICAL STABILIZER; REMOVED AND REPLACED #3 VERTICAL STABILISER FITTING ALL WORK DONE BY O. FLORES 8621011 AND QC RII. C. PORTILLO # 230. ALL WORK EMBODIED ON AEROMAN SDR YENA2025093000980Bearing · corrodedDURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ4 VERTICAL STABILIZER; REMOVED AND REPLACED HINGE ARM FITTING 4 AND FASTENERS ON VERTICAL STABILIZER I.A.W A320 SRM 55-36-42-300-008 STEP 2.A AND A320 SRM 51-72-11 AND DWSDR YENA2025093000979Hinge Arm · corrodedDURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ1 VERTICAL STABILIZER; (RESOLVED ON W/O: 1401080 TASKCARD: NR-00014) REMOVED AND REPLACED HINGE ARM FITTING 1 AND FASTENERS ON VERTICAL STABILIZER I.A.W A320 SRM 55-36-42SDR GTIA2025092939101Bushing · corrodedAFTER BUSHINGS REMOVAL CORROSION WAS FOUND ON INNER BORE HINGE FITTING Ñ3 AT RH ELEVATOR (2EA) RAF 3589623-01 CREATED-REPAIRED BOTH BORES AND REPLACED BUSHINGS (2 EA) ON HINGE FITTING #3 AT RH ELEVATOR IAW SRM 55-26-41-300-004 THIS REPAIR IS CATEGORY B INSPECTSDR GTIA2025092939100Bushing · corrodedAFTER BUSHINGS REMOVAL CORROSION WAS FOUND ON INNER BORE HINGE FITTING Ñ4 OB LUG AT RH ELEVATOR (1 EA) RAF 3589622-02 CREATED -REPAIRED BOTH BORES AND REPLACED BUSHING (1 E/A) ON HINGE FITTING #4 OUTBOARD LUG AT RH ELEVATOR IAW SRM 55-26-41-300-005 THIS REPAIRSDR GTIA2025092939099Bushing · corrodedAFTER BUSHINGS REMOVAL CORROSION WAS FOUND ON INNER BORE HINGE FITTING Ñ6 AT RH ELEVATOR (2EA). RAF 3589622-01 CREATED-REPAIRED BOTH BORES AND REPLACED BUSHINGS (2 E/A) ON HINGE FITTING #6 AT RH ELEVATOR IAW SRM 55-26-41-300-006 THIS REPAIR IS CATEGORY B INSPESDR GTIA2025092939098Bushing · corrodedAFTER BUSHING REMOVAL CORROSION WAS FOUND ON INNER BORE HINGE FITTING #1, 2, AND 3 AT LH ELEVATOR RAF 3589621-02 CREATED SEE APPENDIX 3589621-02-REPAIRED BOTH BORES AND REPLACED BUSHINGS (2 EA) ON HINGE FITTING #1,2 AND 3 AT LH ELEVATOR IAW SRM 55-26-41-300-00SDR GTIA2025092939097Skin Panel · crackedCRACK INDICATION FOUND IN FASTENER HOLE (LOWER INBOARD POSITION) LOCATED AT FR 68 DOOR STOP FITTING 1 RH SIDE. RAF 3589624-01 GENERATED -PERFORMED REPAIR ON FASTENER HOLE (LOWER INBOARD POSITION) LOCATED AT FR.68 DOOR STOP FITTING #1 RH SIDE SRM 53-41-12-300-0SDR GTIA2025092939096Skin Panel · crackedCRACK INDICATION FOUND IN FASTENER HOLE ( LOWER INBOARD POSTION) LOCATED AT FR 68 DOOR STOP FITTING 6 LT SIDE. RAF 3589623-02 GENERATED -PERFORMED REPAIR ON FASTENER HOLE (LOWER INBOARD POSITION) LOCATED AT FR.68 DOOR STOP FITTING #6 LH SIDE IAW SRM 53-41-12-3
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