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 YENA2025032400304Apu · odorFLT#583, JFK-MCO.' ON DESCENT BELOW 10000 FEET NOTICED STRONG DIRTY SOCK SMELL ON SHORT FINAL FA'S CALLED TO COMPLAIN OF A POSSIBLE FUME EVENT IN PROGRESS. AFTER LANDING DISSIPATED; COMPLIED WITH INFO NOTICE 2017-T015K SECT B2. FOUND SOURCE OF SMELL TO COME FRSDR AALA202503242434Lamp · inoperativeAIRCRAFT WAS NOT GROUNDED: FORWARD CABIN EMERGENCY EXIT SIGN FACING AFT, ONE SIDE OF IT DOES NOT ILLUMINATE. MAINTENANCE RELAMPED EMERGENCY EXIT SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR AALA202503242062Handle · brokenAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS LAVATORY E DOOR HANDLE HAS BROKEN OFF, AND ARE UNABLE TO OPEN THE DOOR AFTER GETTING IT CLOSED. MAINTENANCE RESECURED AND TIGHTENED LAVATORY DOOR LATCH SCREWS AS REQUIRED..SDR AALA202503231829Elec Connector · defectiveAIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ON SEAT ROW 15ABC INOPERATIVE. MAINTENANCE FOUND BAD CONNECTOR ON 5751VC AND REPLACED THE CONNECTOR PER ESPM 20-53-29. A SATISFACTORY OPERATIONAL TEST WAS ACCOMPLISHED.SDR CALA2025032603201Door Frame · crackedLEFT HAND FWD EMER. EXIT FWD FRAME CRACKED. REMOVED AND REPLACED FWD FRAME AT LEFT HAND FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-21-11-911-001. WPB V947030. REMOVED AND REPLACED FWD FRAME AT LEFT HAND FWD EMER EXIT DOOR I AW A320 SRM 51-42-11-911-001.SDR GTIA2025032438816A/C Pack · odorHAD A FUME EVENT COMING IN TO LAND STARTED AROUND 3000. DESCRIPTION OF ODOR/FUMES: CONTINUOUS AND DISCOMFORTABLE, MUSTRY DRY AND DIRTY SOCKS SMELL. APPARENT CABIN SOURCE: UNKNOWN. FLIGHT DECK, FWD CABIN, AFT CABIN, AND MID CABIN. NO VISIBLE SMOKE/HAZE. NO MEDISDR CALA2025032403144Door Frame · crackedRH FR 66 DOORSTOP NO.1, LOWER IB HOLE HAS CRACK INDICATION IN FRAME LAYER @ 5 OCLOCK POSITION, 80% S.H. REMOVED CRACK AND FABRICATED REPAIR WASHER IAW A320 SRM 53-41-12-300-010 AND SRM 53-41-12-300-008 REMOVED CRACK AND INSTALLED REPAIR TO FR66 RH #1 DOORSTSDR CALA2025032403112Battery · faultyEPSU BATTERY EMER R INSTALLED SERVICEABLE BATTERY EPSU 12WL REF. AMM 33-51-38-400-002-A. OKAY TO CONTINUE.PARTS USED: 18-3351-3-0001, QTY :1SDR CALA2025032403100Chiller · faultedFA REPORTS BURNING SMELL IN AFT OF AIRCRAFT ADDED PHOTOS OF COMPLETED ODOR FORM. ORIGINAL COPY GIVENT TO SUPERVISOR RONNIE INSPECTED AFT GALLEY FOR OPEN CB. NONE FOUND. INSPECTED G4 AIR CHILLER. NO SMELL ORIGINATING FROM UNIT OR VENTS. INSPECTED G3 AIR CHISDR AALA202503231946Computer · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECARED AND THE AIRCRAFT DIVERTED TO DEN DUE TO THE FLIGHT CREW REPORTING A DMC 1 FAULT CONSTANTLY COMING ON ECAM AND CLEARING ITSELF EVERY 5 TO 15 SECONDS. THE EMERGENCY CANCEL BUTTON NOT WORKING TO MUTE THE REPETITIVE SDR YENA2025032600339Control Servo · faultedFLT#2466, FLL-BUF. 'DURING LEVEL FLIGHT AT FL350 A/C WOULD SHUTTER MOMENTARILY AND PITCH UP EVERY FEW MINUTES. IT DID IT WITH BOTH AUTOPILOTS 1 AND 2 AND WITH MANUAL FLYING. ALSO WAS NOTED DURING DESCENT THRU FL180; REMOVED AND REPLACED ELEVATOR SERVO CONTROL SDR YENA2025032500321Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE 1 FR16LH DOOR STOP 7 AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 5 OCLOCK; REF AEROMAN N/R 2025-133913,REMOVED AND REPLACED INTERCOSTAL FITTING LOC. AT LEVEL FR.16 LH DOOR STOP FITTING #7 I.A.W ASDR YENA2025032500320Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE 3 FR16RH DOOR STOP 7 AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 6 OCLOCK; REF AEROMAN N/R 2025- 133916, REMOVED AND REPLACED INTERCOSTAL FITTING LOC. AT LEVEL FR.16 RH DOOR STOP FITTING #7 I.A.W SDR YENA2025032500319Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE 3 FR16LH DOOR STOP 7 AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 5 OCLOCK; REF AEROMAN N/R 2025-133914, REMOVED AND REPLACED INTERCOSTAL FITTING LOC. AT LEVEL FR.16 LH DOOR STOP FITTING #7 I.A.W ASDR YENA2025032500318Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE 1 FR16RH DOOR STOP 7 AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 6 O'CLOCK; REF AEROMAN N/R 2025-133915, REMOVED AND REPLACED INTERCOSTAL FITTING LOC. AT LEVEL FR.16 RH DOOR STOP FITTING #7 I.A.W SDR YENA2025032500317Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON DOOR EMERGENCY EXIT (AFT RH EEH ) Z844 INNER FRAME SEGMENTS 1 ( FWD AND AFT ) CRACK L=0.094 INCH; REF TO AEROMAN WO 2025 47/1 NR 2025-133808, REMOVED AND REPLACED FRAME SEGMENTS ON EMERGENCY EXIT DOOR 844 FALSDR YENA2025032500316Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON DOOR EMERGENCY EXIT (AFT LH EEH ) Z834 INNE R FRAME SEGMENTS 1 ( FWD AND AFT ) CRACK L=0.105 INCH; REF TO AEROMAN WO 2025 47/1 NR 2025-133809, REMOVED AND REPLACED FRAME SEGMENTS ON EMERGENCY EXIT DOOR 834 FASDR YENA2025032500315Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON DOOR EMERGENCY EXIT (FWD LH EEH ) Z833 INNER FRAME SEGMENTS 1 ( FWD AND AFT ) CRACK L=2.218 INCH; REF TO AEROMAN WO 2025 47/1 NR 2025-133811, REMOVED AND REPLACED FRAME SEGMENTS ON EMERGENCY EXIT DOOR 833 FALSDR YENA2025032500314Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON DOOR EMERGENCY EXIT (FWD RH EEH ) Z843 INNER FRAME SEGMENTS 1 ( FWD AND AFT ) CRACK L=0.095 INCH; REF TO AEROMAN WO 2025 47/1 NR 2025-133805, REMOVED AND REPLACED FRAME SEGMENTS ON EMERGENCY EXIT DOOR 843 FOLSDR YENA2025032500313Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 66 RH DOOR STOP FITTING #7 UPPER INBOA RD HOLE. CRACK DEPTH: 0.103 INCH; REF TO AEROMAN WO 2025 47/1 NR 2025-133953, PERFORMED PERMANENT REPAIR ON FRAME 66 RH DOOR STOP FITTING #7 UPPER INBOARD HOLE. I.SDR YENA2025032500312Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 68 LH DOOR STOP FITTING #1 LOWER INBOA RD HOLE. CRACK DEPTH: 0.103 INCH; REF TO AEROMAN WO 2025 47/1 NR 2025-133952, PERFORMED PERMANENT REPAIR ON FRAME 68 LH DOOR STOP FITTING #1 LOWER INBOARD HOLE. I.SDR YENA2025032500311Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE 6 FR16RH DOUBLE JOGGLE AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 2 OCLOCK; (RESOLVED ON W/O: 1353445 TASKCARD: NR-00030) REF TO AEROMAN WO 2025 47/1 NR 2025-133911, FUR-A320-53-02104, PERFORMEDSDR YENA2025032500310Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SKIN SLAT 3 OUTBOARD EDGE LH WING; REF TO AEROMAN WO 2025 47/1 NR 2025-133475, PERFORMED PERMANENT REPAIR ON UPPER SKIN SLAT #3 OUTBOARD EDGE LH WING, AS PER EA 57-0010-25 (COVER PLUS PART 1) REPAIR DRAWING R574-60332 SDR GTIA2025032438813Megaphone · inoperativeREF T/C 256551-01-1, BOTH FWD AND AFT MEGAPHONES NEED TO BE REPLACED BECAUSE OF BAD SET SCREWS.-R&R'D BOTH FWD AND AFT MEGAPHONES PER AIRCRAFT DRAWINGS A321 EMER-EQUIP-2. OPS CHK GOOD PER AMM 25-65-51.SDR GTIA2025032438812Skin · corrodedCORROSION ON TRAILING EDGE TOP SKIN LOWER SURFACE OVERHANG BTW RIB 5 TO RIB 9 ON RH WING. RAF-01 CREATED AND SDR 3563280-02 LENGTH 5.297"" AND WIDTH 2.383""-PERFORMED PERMANENT REPAIR ON TRAILING EDGE TOP SKIN LOWER SURFACE OVERHEANG BTW RIB 5 TO RIB 9 ON RH WSDR YENA2025032400303Pump · malfunctionedFLT#595, HPN-MCO. (AIRCRAFT DIVERTED TO JFK) 'UPON CLIMBOUT FROM HPN ND GEAR RETRACTION, WE RECEIVED THE ECAM L/G DOORS NOT CLOSED. WE COMPLIED WITH THE ECAM PROCEDURES AND QRH PROCEDURES, BY CLIMB THE GEAR AND DID NOT CORRECT THE ISSUE; REF L/P'S 4224961-2 (RSDR CALA2025032403096Landing Gear · malfunctionedAVIATAR REPORTING L/G GEAR NOT DOWNLOCKED, L/G DOOR NOT CLOSED ECAM, CFDS MSG STEERING ELECTRO-HYD MODULE (6GC)- VARGAS TOMC FLAGGED SDR SEE LP 4237214SDR YENA2025032400301Thermostat · failedFLT#2121, FLL-LAX. (AIRCRAFT DECLARED AN EMERGENCY).' ON CLIMB OUT 2 TIMES AIR ENG 1 BLEED ABNORMAL MSG CLEARED ITSELF 3RD TIME WE COMPLIED WITH QRH TAKEOFF WAS A TOGA BLEEDS OFF AND PSI WAS 22 / 215 C. ENG ONE #1 . WHEN WE STARTED GETTING THE BLEED ABNORMAL MSDR YENA2025032400300Hydraulic System · lowFLT#2121, FLL-LAX. (AIRCRAFT DECLARED AN EMERGENCY).' APPROX 3 HOURS INTO FLIGHT PERFORMING SYSTEMS CHECKS. THE HYD STATUS PAGE SHOWED AMBER LINE FROM GREEN SYSTEM RESERVOIR TO GREEN ENG PUMP AND RESERVOIR INDICATOR WAS AMBER 3000 GREEN; ACCOMPLISHED VISUAL ISDR AALA202503235246Swivel Fitting · brokenAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INBOUND INTO SYR DUE TO THE FLIGHT CREW REPORTING THAT UPON GEAR EXTENSION ON APPROACH A GREEN HYDRAULIC SYSTEM RESERVOIR LOW LEVEL MESSAGE DISPLAYED, FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES AND LANDED SAFELY ASDR AALA202503213135Battery · no testAIRCRAFT WAS NOT GROUNDED: AFTER MEGAPHONE WILL NOT TEST. REPLACED BATTERIES AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-65-51.SDR CALA2025032103058Fitting · crackedWINDSHIELD CENTER POST LH CONTINUITY FITTING HAS CRACK APPROX .400 INCH O/B OF CENTER POST PER HAECO LCQ N/R 9290924/38924 GEN BY V892444 REPLACED WITH NEW CONTINUITY FITTING IAW DRWG R53112919 AND SRM 51-42-11.SDR CALA2025032103055Skin · contaminatedR/H ELEVATOR HAS LIQUID INGRESS AT 146IN FROM I/B END, 5IN FROM TRAILING EDGE, 1.5IN DIAMETER.SDR CALA2025032103052Skin · contaminatedL/H AFT SIDE OF RUDDER HAS TRAPPED WATER 2 IN FROM TRAILING EDGE , 103 IN FROM BOTTOM, 8X5 IN DIAMETER, NUMEROUS SPOTS IN AREA. " REPAIR PRIOR TO NEXT FLIGHT". GENERATED BY V061632 ON HAECO LCQ NR 9290745/38745. REPAIR WAS PERFORMED IAW A320 SRM 55-41-13-300-0SDR GTIA2025032038810Power Supply · no testDURING SERVICE CHECK FOUND FAULT EPSU(10WL) FWD L/ DEU B (300RH1), WHILE DOING EPSU SYSTEM TEST. DURING EPSU BATTERY TEST, EXTERIOR LIGHTS FAULT CAME ON TEST. -FOLLOWED TSM 33-51-00-810-830-A, REPLACED POWER- EMERGENCY SUPPLY, REPLACED EPSU BATT, CHECKED WIRINSDR YENA2025032400277Unknown · odorFLT#1337, JFK-STI. 'FA REPORTS TEMPORARY SMELL DESCRIBED AS (ELECTRICAL BURNING) BETWEEN ROW 7 AND 10 DURING FINAL APPROACH ( THALES AVANT IFE (ENTIRE SYSTEM) ); REACTIVATED AVANT SYSTEM AND PERFORMED AIRCRAFT WIRING INSPECTION AND COMPONENT INSPECTION BETWEENSDR CALA2025032103063Bottle · low pressureFA REPORTS DOOR 2L SLIDE PRESSURE IN THE RED. CHECKED AND DETERMINED SLIDE 2L IN PRESSURE LIMITS PER AMM 25-62-00-210-001-A. CHECKED AND DETERMINED SLIDE 2L IN PRESSURE LIMITS PER AMM 25-62-00-210-001-A.SDR CALA2025032103062Warning Light · false activationFWD CARGO DOOR OPENINDICATION X 3 ECAM.REPEATEDLY HAPPENING. LOG PAGE 4161341 HAS BEEN REOPENED. VISUALLY CHECKED FORWARD CARGO DOOR IS CLOSED AND LOCKED (REF. AMM 52-70-00-040-001-A) AND INSTALLED INOPERATIVE STICKER ADJACENT TO LOWER ECAM DISPLAY.SDR YENA2025032000297Frame · crackedDURING HEAVY MAINTENANCE: SEVERAL CRACK INDICATIONS FOUND ON FRAME SEGMENT 1 OF THE FWD LH SIDE OVER WING EMERGENCY EXIT HATCH DOOR 833. MAXIMUM CRACK LENGTH: 0.500 I NCHES; REF AEROMAN N/R 2025- 125818, ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCYSDR YENA2025032000296Frame · crackedDURING HEAVY MAINTENANCE: SEVERAL CRACK INDICATIONS FOUND ON FRAME SEGMENT 1 OF THE FWD RH SIDE OVER WING EMERGENCY EXIT HATCH DOOR 843. MAXIMUM CRACK LENGTH: 0.450 I NCHES; REF AEROMAN N/R 2025-125819, ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY SDR YENA2025032000295Frame · crackedDURING HEAVY MAINTENANCE: SEVERAL CRACK INDICATIONS FOUND ON FRAME SEGMENT 1 OF THE AFT LH SIDE OVERWING EMERGENCY EXIT HATCH DOOR 834. MAXIMUM CRACK LENGTH: 0.400 INCHES; REF AEROMAN N/R 20250125820, ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXSDR YENA2025032000294Frame · crackedDURING HEAVY MAINTENANCE: SEVERAL CRACK INDICATIONS FOUND ON FRAME SEGMENT 1 OF THE AFT RH SIDE OVER WING EMERGENCY EXIT HATCH DOOR 844. MAXIMUM CRACK LENGTH: 0.400 I NCHES; REF AEROMAN N/R 2025-125821, ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY SDR YENA2025032000293Skin · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE C FR16LH DOUBLE JOGGLE AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 3 OCLOCK; (RESOLVED ON W/O: 1353243 TASKCARD: NR-00019) FUR-A320-53-02089, REF AEROMAN N/R 2025- 125698, PERFORMED PERMANENTE RESDR YENA2025032000292Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE C FR16LH DOUBLE JOGGLE AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 3 OCLOCK; REF AEROMAN N/R 2025- 125698, PERFORMED PERMANENTE REPAIR ON HOLE C FR16LH JOGGLE AREA I.A.W A320 SRM 53-11-12-300-012SDR YENA2025032000291Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE D FR16LH DOUBLE JOGGLE AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 9 OCLOCK; (RESOLVED ON W/O: 1353243 TASKCARD: NR-00021) FUR-A320-53-02090, REF AEROMAN N/R 2025-125700, MESURE OF DIAMETER ON OPESDR YENA2025032000290Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE D FR16LH DOUBLE JOGGLE AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 9 OCLOCK; REF AEROMAN N/R 20250125700, PERFORMED PERMANENTE REPAIR ON HOLE D FR16LH JOGGLE AREA I.A.W A320 SRM 53-11-12-300-012 FSDR YENA2025032000289Skin · abnormalDURING HEAVY MAINTENANCE: DENT OB FLAP EXISTING REPAIR LOWER SURFACE ON RH WING; REF AEROMAN N/R 2025-125365, PERFORMED VISUAL AND TAP TEST INSPECTION ON EXISTING REPAIR ON O/B FLAP LOWER SURFACE ON RH WING AS PER A320 NTM 51-10-03 AND A320 NTM 51-90-00. REPAISDR YENA2025032000288Stop Fitting · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE 3 FR68RH DOOR STOP 1. CRACK DEPTH 0.100 INCH, CRACK DIRECTION 6 OCLOCK; (RESOLVED ON W/O: 1353243 TASKCARD: NR-00024) REF AEROMAN W/O:2025 84/1 NR 2025 - 125682, PERFORMED REPAIR ON FRAME 68 RH SIDESDR YENA2025032000287Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE LOC. BTW FR64 TO FR 65 AND BTW STR 30R T O STR 31R IN AFT CARGO COMPARTMENT. (SKIN); (RESOLVED ON W/O: 1353243 TASKCARD: NR-00025) REF AEROMAN W/O:2025 84/1 NR 2025 - 125815; PERFORMED PERMANENT REPAIR LOCSDR YENA2025032000286Battery · no testDURING HEAVY MAINTENANCE: DONT PASS OPERATIONAL TEST EMERGENCY EXIT LIGHTS ON PASSENGER CABIN; REF AEROMAN W/O:2025 84/1, NR 2025 - 125236; REMOVED AND REPLACED THE BATTERY OF EPSU 11WL I.A.W AMM 33-51-38-000-002-A AND I.A.W AMM 33-51-38-400-002-A AND PERFORME
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