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 AALA202512127299Wire Harness · faultedAIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHT AT ROW 15ABC INOP. **SUPPLEMENTAL REPORT FOR SDR AALA202512119250 SUBMITTED 12/9/2025 BY AUS .** (CLOSED)** MAINTENANCE REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AND HARNESS IAW AMM 33-51-19.SDR AALA202512129250Light · no testAIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHT AT ROW 15ABC INOP. **SUPPLEMENTAL REPORT FOR SDR AALA202512119250 SUBMITTED 12/9/2025 BY AUS .** (CLOSED)** MAINTENANCE REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AND HARNESS IAW AMM 33-51-19.SDR GTIA2025121139197Megaphone · inoperativeAFT MEGAPHONE INOP-R/R AFT MEGAPHONE IAW SPIRIT AIRLINES DRAWING A320-EMER EQUIP REV 7SDR AALA202512119250Light · inoperativeAIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHT AT ROW 15ABC INOP. (OPEN)SDR AALA202512106543Power Supply · inoperativeAIRCRAFT IN BASE MAINTENANCE: INOP EMERGENCY LIGTHS ON PASSENGER SEAT ROW 1LH, 4LH AND 9RH IN PASSENGER CABIN. MAINTENANCE REPLACED UNIT POWER SUPPLY (10WL) IN FWD PASSENGER CABIN I.A.W.A320 AMM 33-51-38-000-001-A AND IAW A320 AMM 33-51-38-400-001-A.SDR YENA2025121001189Unknown · odorFLT 1153, JFK-PBI. STRONG ODOR EVENT DURING APPROACH PRESENT IN CABIN AND COCKPIT,. LASTED ABOUT 4 MINUTES. SMELLED LIKE CHEMICAL OR NAIL POLISH SCENT; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION B2. IDENTIFIED ODOR AS TYPE 10 (MISC, SMOKE OR FUME) DESDR YENA2025120901186Unknown · odorFLT 503, JFK-SJU. ODOR DETECTED DURING DESCENT BELOW 10,000. CONFIRMED WITH CABIN CREW. LOCATION OVERWING EXITS STRONGEST, AND FWD. LASTED A MINUTE THEN DISSAPATED. FOUL HEATED PLASTIC TYPE ODOR, FOLLOWED INFO NOTICE 2017-T015L WITH MX-270 PROVIDED. TSM 05-5SDR CALA2025120911957Profile · crackedLEFT AFT EMERGENCY EXIT HATCH RT LOAD TRANSMITTING PROFILE SUSPECTED CRACK. REMOVED AND REPLACED LT AFT EMERGENCY EXIT HATCH LOAD TRANSMITTING PROFILE SEGMENT IAW SRM 51-42-11/001, AND SRM 51-72-11-911-00 1.SDR CALA2025120911955Profile · crackedLEFT FWD EMERGENCY EXIT HATCH LT LOAD TRANSMITTING PROFILE CRACKED. REMOVED AND REPLACED SEGMENT IAW SRM 51-72-11-911-002, AND SRM 51-42-11/001.SDR CALA2025120911953Profile · crackedLEFT AFT EMERGENCY EXIT HATCH LT LOAD TRANSMITTING PROFILE SUSPECTED CRACKED. REMOVED & REPLACED SEGMENT IAW SRM 51-72-11-911-002, AND SRM 51-42-11/001.SDR CALA2025120911951Profile · crackedRIGHT AFT EMERGENCY EXIT HATCH RT LOAD TRANSMITTING PROFILE SUSPECTED CRACKED. REMOVED AND REPLACED SEGMENT IAW SRM 51-72-11-911-002, AND SRM 51-42-11/001.SDR CALA2025120911949Fuel Cap · missingFUEL CAP MISSING. APROX 1.2 LBS. APROX 22 SQ INCH. INSTALLED NEW UNDERWING FUEL CAP ASSY IAW AMM 28-25-41-400-007-A, AND AMM 28-25-41-400-006-A. NEW FUEL CAP ASSY IS FLUSH WITH SKIN AND NO LEAKS NOTED FROM THE COUPLING. PLACARD REMOVED.SDR AALA202512080090Epsu · no testAIRCRAFT IN BASE MAINTENANCE: INOP EPSU AT FWD GALLEY AREA 10WL. MAINTENANCE REPLACED EPSU AT FWD GALLEY AREA 10WL I.A.W A320 FAM AMM 33-51-38-000-001-AAND 33-51-38-400-001-A.SDR AALA202601103578Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL LOCATED FR66 RH SIDE AT AFT GALLEY AREA. MAINTENANCE PERFORMED REPAIRED LOC. ON LOWER SILL LOCATED FR66 RH SIDE AT AFT GALLEY AREA IAW A320 SRM A320 SRM 53-41-14-300-001.SDR AALA202512302480Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT SLEEVE OF LEFT PYLON (L: 7.570 IN). MAINTENANCE REPLACED SPIGOT SLEEVE ON LH PYLON IAW AMM 57-26-12-400-002-A STEP 4.A.SDR AALA202512162027Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT RECEPTACLE FITTING OF LEFT PYLON. MAINTENANCE REPLACED LOWER SPIGOT FITTING ON LH PYLON IAW A320 SRM 54-51-12-300-002.SDR YENA2025120801177Pump · failedFLT 1824, LAX-JFK, (ETOPS). REF LP 4455807 ITEM NR 1 DUE TO ENG NR 1 HYDRAULIC DRIVEN PUMP REPLACEMENT EDP REQUIRES VERIFICATION ENG RUN. REMOVED AND REPLACED ENG NR 1 EDP IAW AMM 29-11-57 OPS CHK & LEAK CHKD OK, NO FAULTS NOTED.SDR AALA202512085105Light · inoperativeAIRCRAFT IN BASE MAINTENANCE: AFT LH LAV LOWER FWD EMERGENCY LIGHT INOP. MAINTENANCE REPLACED AFT L/H LAV LOWER FWD EMERGENCY LIGHT, OPS CHECK GOOD. IAW AMM 33-51-19.SDR YENA2025120801176A/C Pack · odorFLT 547, ISP-MCO. ODOR EVENT ON DESENT 17FL DOWN TO 9K WITEN ISOLATION OF PACK 1 STOPPED SMELL MUSTY DIRTY SOCK OIL SMELL MD-27 OUT ODOR COCKPIT TO AFT CABIN. OPENSDR YENA2025120801175Unknown · odorFLT 1533, JFK-CTG. ON APPROACH TAXI IN AND DEPLANING AFT F/A COULD SMELL A DIRTY MUSTY SMELL CUSTOMER SAID SMELLED LIKE A SKUNK; PER INFO NOTICE 2017-T015L ACCOMPLISHED TSM 05-50-00-810-831-A AND INSPECTED APU COMPARTMENT PER AMM 49-00-00200-812-A FOR ANY EVIDSDR GTIA2025120839195Megaphone · inoperativeAFT MEGAPHONE INOP-R&R AFTE MEGAPHONE IAW AMM 25-64-00. OPS CK OKSDR CALA2025120811826Bottle · no discrepancyF/A REPORTED RT DOOR PRESSURE IN RED. PRESSURE NEEDLE IS STILL WITHIN GREEN BAND AT THIS TIME. BUSTLE VIEWPORT IS NOT CENTERED ON GUAGE AND DIFFICULT TO SEE WITHOUT SUFFICIENT LUMINATION. NO MAINT ACTION TAKEN.SDR AALA202512064627Plate · wornAIRCRAFT IN BASE MAINTENANCE: CRACKED CONNECTING PLATE ON LEFT MAIN LANDING GEAR DOOR HINGE FITTING ON THE KEEL BEAM BETWEEN FR 42 AND FR 43, BETWEEN S41R AND S42R. REPLACED CONNECTING PLATE PER EA 370471.SDR CALA2025120511797Fuel Cap · missingFUEL CAP MISSING. DEFERED ON LOG PAGE 7156404 FUEL CAP MISSING DEFERED ON LOG PAGE 7156404SDR CALA2025120511785Battery Pack · no testDURING THE EMERGENCY LIGHTING TEST USING PTP 110RH, RECIEVED FAULT EPSU UNIT FWD LT. REPLACED EPSU BATTERY AT L1 DOOR IAW AMM 33-51-38. OP CHECKED GOOD.SDR CALA2025120511782Chiller · odorFWD CHILLER HAD AN ODOR OF MELTED PLASTIC. FA TURNED OFF. DEFERRED PER MEL, PULLED AND COLLARED CB, INSTALLED INOP STICKER ADJ TO CB. REMOVED AND REPLACED THE FWD GALLEY AIR CHILLER IAW AMM 25-34-51. OPS CHECKED GOOD.SDR AALA202512044762Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT RECEPTACLE FITTING BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 51-51-12.SDR AALA202512034009Ground Wire · disconnectedAIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHT AT SEAT ROW 4C INOPERATIVE. MAINTENANCE FOUND GROUND WIRE DISCONNECTED AT EMERGENCY LIGHT AT SEAT ROW 4C. RECONNECTED GROUND WIRE AND ACCOMPLISHED A SATISFACTORY EMERGENCY LIGHT OPERATIONAL CHECK PER AMM 33-51-00-7SDR YENA2025120301172Unknown · odorFLT#307, BOS-BNA. "AFT CABIN INFLIGHT CREW REPORTED A DIRTY SOCK ODOR ON DESCENT. OPENSDR CALA2025120511783Wire · brokenEMERGENCY LIGHT AT ROW 35ABC IS INOPERATIVE. RELAMPED NO HELP. VERIFIED THAT NO TWO ADJACENT EMERGENCY LIGHTS ARE INOPERATIVE. VERIFIED THAT ITS THE RED LIGHT THAT WERE INOPERATIVE AND VERIFIED BLUE LIGHTS WORK CORRECLTY. DEFERED UNDER MEL 3350C, COMPLIESDR AALA202512044153Battery · no testAIRCRAFT IN BASE MAINTENANCE: BATTERY FAULT FOR EMERGENCY POWER SUPPLY UNIT 10WL DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.SDR CALA2025120211628Power Supply · faultedEPSU EXT LOAD EMER L FAULT FOUND ON EMERGENCY LIGHT BITE TEST. TESTED ALL EXTERNAL LIGHTS ON LH SIDE OF AIRPLANE. OVERWING EMERGENCY LIGHTS & LH OVERWING SLIDE (REF LP 7135969 FOR REMOVAL). ALL LIGHTS TESTED OK. REMOVED AND REPLACED EPSU POWER SUPPLY UNIT IAW SDR GTIA2025120139192Megaphone · inoperativeFWD GALLEY MEGAPHONE INOPERATIVE. R & R FWD GALLEY MEGAPHONE IAW MKS DRAWING CEO EMER EQUIP REV 7.SDR YENA2025120201167Door Actuator · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE A FR16 LH DOUBLE JOGGLE AREA, CRACK DIRECTION 3 OCLOCK AND CRACK DEPTH 0.077 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-90-00. PERFORMED PERMANENT REPAIR ON PRIMARY STRUCTURE ASDR YENA2025120201166Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE 7 FR16 LH DOUBLE JOGGLE AREA, CRACK DIRECTION 3 OCLOCK AND CRACK DEPTH 0.107 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9SDR YENA2025120201165Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE D FR16 LH DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK AND CRACK DEPTH 0.101 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9SDR YENA2025120201164Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE B FR16 RH DOUBLE JOGGLE AREA, CRACK DIRECTION 3 OCLOCK AND CRACK DEPTH 0.081 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9SDR YENA2025120201163Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE C FR16 RH DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK AND CRACK DEPTH 0.102 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9SDR YENA2025120201162Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE A FR16 RH DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK AND CRACK DEPTH 0.086 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9SDR YENA2025120201161Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE A FR16 RH DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK AND CRACK DEPTH 0.086 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9SDR YENA2025120201160Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 E/A) (CRACK INDICATION FOUND OPEN HOLE B FR16 LH DOUBLE JOGGLE AREA) PERFORMED PERMANENT REPAIR ON PRIMARY STRUCTURE AT HOLE B FR16 LH DOUBLE JOGGLE AREA IAW SRM 53-11-12-300-012.SDR YENA2025120201159Support · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC. STR23L AND FR68 AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON LOWER SILL LOC. STR23L AND FR68 AT AFT GALLEY AREA IAW SRM A320 53-41-14-300-001 THIS REPAIR IS CATEGORY A AND FURTHER INSPECTION.
;SDR YENA2025120201158Skin · no discrepancyDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE OF TOP SKIN LOC. REAR SPAR BTW RIB18 AND RIB19 ON LH WING; EVALUATED REWORK AREA ON UPPER SURFACE OF TOP SKIN REAR SPAR BTW RIB18 AND RIB19 ON LH WING AND FOUND WITHIN LIMITS IAW SRM 57-21-11-283-007.SDR YENA2025120201157Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16 LT SIDE DOOR STOP 7 LOWER OUTBOARD HOLE AT 12 OCLOCK, CRACK LENGTH 0.078 INCH APROX; PERFORMED PERMANENT REPAIR OUTBOARD HOLE ON FR 16 LH SIDE DOOR STOP 7 LOWER IAW SRM 53-11-12-300-010 AND DWG D531354SDR YENA2025120201156Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHIELD IN COCKPIT (1 EA) (CRACK INDICATION FOU ND CONTINUITY FITTING WINDSHIELD RH SIDE.. CRACK DIRECTION VERTICAL. CRACK LENGTH 0.200 INCH.); PERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAMING CENTERSDR YENA2025120201155Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST, LOWER ATTACHMENT ARE A, INBOARD LOWER RADIUS LH SIDE, CRACK LONGITUDINAL DIRECTION, LENGTH= 0.120 INCHES APPROX; PERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAMING CENTER POSTSDR YENA2025120201154Skin · dentedDURING HEAVY MAINTENANCE: SEVERAL DENTS ON ACCESS PANEL 341BB LEADING EDGE ON RH HORIZONTAL STABILIZER; EVALUATED DENTS ON ACCESS PANEL 341BB LEADING EDGE ON RH HORIZONTAL STABILIZER AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS AS PER A320 SRM 55-12-11-283-003 PASDR YENA2025120201153Shear Plate · crackedDURING HEAVY MAINTENANCE: CRACK SHEAR PLATE STR 23R FR 69-FR 70; R & R SHEAR PLATE STR 23R FR 69-FR 70 IAW A320 SRM 51-72-11, SRM 51-42-11 & DWG D53474180.SDR YENA2025120201152Shear Plate · crackedDURING HEAVY MAINTENANCE: CRACK SHEAR PLATE STR 23L FR69-FR70; R& R SHEAR PLATE STR 23L FR 69-FR 70 IAW A320 SRM 51-72-11, 51-42-11 & DWG D53474180.SDR YENA2025120201151Fitting · crackedDURING HEAVY MAINTENANCE: NOSE FWD FUSELAGE RACK 10VU LUGS SEVERAL FINDINGS WITH CRACKED OR BROKEN FITTINGS.
Back to Airbus A320-232