Airbus A320-233
Service difficulty reports · 254
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 = 'A320233' 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 = 'A320233' 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 2026FA0000532Sleeve · damagedT/R ASSY OUT OF LIMIT WITH ISSUED REPAIRED. T/R ASSY LEADING EDGE SLEEVE OUT OF LIMIT WITH ISSUED REPAIRED CERTIFICATE. AFTER INSTALLATION OF NEW RECEIVED SERVICEABLE T/R HALF ASSY INCREASED CLEARANCE FOUND ON LOWER LEADING EDGE SLEEVE APPROXIMATELY 600 MM (WSDR 2023FA0000030Blower · faultedDURING CLIMB FROM MGA TO MIA THE AIRCRAFT RETURNED TO MGA DUE TO VENT SKIN VALVE FAULT. VENT EXTRACT FAULT. VENT BLOWER FAULT. AT MGA STATION WAS INCLUDED OUTLET SKIN VALVE AS DMI IAW MEL 21-26-04 CAT. CSDR SOKF20211108003None · noneDURING TAKE OFF FROM SAL TO LAX THE AIRCRAFT REJECTED THE TAKE OF DUE TO UNRELIABLE SPEED CAPTAIN SIDE FOLLOWING TSM 34-13-00-810-998-B WAS PERFORMED CLEANING OF CAPTAIN, F/O AND STANDBY PITOT PROBE IN ACCORDANCE WIH AMM 34-10-00-170-004-A REV 58 PERFORMED FUNSDR SOKF20211108002Control Valve · damagedDURING CLIMB FROM BOG TO SAL THE AIRCRAFT RETURNED TO BOG DUE TO ECAM ADVISORY PRESS VENT SKIN OULET VALVE IN AMBER, CAB PRESS SYST 1 Y 2 RESETED NO SUCCESSFUL. AT BOG STATION PERFORMED TSM TASK CARD 21-26-00-810-819, TASK CARD 21-26-00-810-804, TASK CARD 21-2SDR YENA2021092200614Unknown · odorFLT 667, HPN-PBI. DESCENDING THRU 20,000 FT, AFTER SOME LIGHT TO HEAVY RAIN STRONG MAGIC MARKER / NEW SHOW SMELL DOWN TO 1 K. CHECKED W / FA'S NO ODOR / FUMES NOTED. BOTH FO AND CA NOTICED INTENSITY. NO PHYSIOLOGICAL EFFECTS NOTED JUST THE STRONG ODOR.SDR SOKF20210608001Pitot Head · obstructedDURING TAKE OFF FROM MIA TO SAL THE TAKE OFF WAS REJECTED DUE TO AIRSPEED DISCREPANCY BETWEEN CAP PFD AND FO PFD DURING TAKE OFF ROLL. IN ACCORDANCE WITH TSM TASK 34-13-00-810-998-B PERFORMED INSPECTION IAW AMM 34-11-15-200-001. PERFORMED FLUSHING OF THE PRINSDR YENA2021040700210Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION UPPER SURFACE EXTERNAL SKIN LOCATED BTW RIB 9 TO RIB 10 ON LH WING; (REF AEROMAN WO 2021-87/1, NR 2021-115794) ACCOMPLISHED LIFE LIMIT REPAIR TOP SKIN PANEL 2 EXT SKIN LOC BTW RIB 9 TO RIB 11 LON LH WING IAW JETBLUE EC A32-3SDR RJEF20210104001Pump · warning messageDURING CRUISE FLIGHT, THE FUEL CENTER TANK PUMP 2 LO PR ACTIVATED 40 MINUTES AFTER TAKEOFF, AS PER TSM TASK TASK 28-21-00-810-826-A AND TSM TASK TASK 28-21-00-810-814-A WAS PERFORMED SUBTASK 28-21-00-710-062-C (B-1 AND 3 , FUNCTIONAL TEST OF THE CENTER TANK FUSDR SOKF2020030600000Pump · damagedDDURING FLIGHT FROM SAL TO SFO THE AIRCRAFT DIVERTED TO MEX DUE TO PILOT REPORT BLUE PUMP OVERHEAT AND BLUE HYDRAULIC SYSTEM WAS LOST AND ECAM WARNING MESSAGE CAME ON, THEN WHEN THE FAULT LIGHT WENT OFF THE BLUE HYD SYSTEM WAS RECOVERED, IN ACCORDANCE WITH TSSDR SOKF2020030200000Unknown · malfunctionedAFTER TO FROM BOG TO LIM THE AIRCRAFT RETURNED TO BOG DUE TO ECAM WARNING MESSAGE AIR ENG 1 + 2 BLEED FAULT. IN ACCORDANCE WITH AMM 36-11-52 PB 401 PRV WAS REPLACED IN LH ENGINE S/N V10892, IN ACCORDANCE WITH AMM TASK 36-11-52-790-001-A LEAK TEST OF BLEED PRESDR SOKF20191208007Fitting · wornDURING CLIMB, THE AIRCRAFT RETURN TO LIM DUE TO HIGH VIBRATION DURING CLIMB BETWEEN FL 050 AND FL 270 . SPEED BETWEEN 200-300 KTS. VIBRATION MODERATE FELT IN ALL THE AIRCRAFT. AT LIM STATION PERFOMED T/S PROCEDURE IAW TSM 05-50-00-810-801-A AND TSM 27-10-00-8SDR 5TTY20190417 0001Regulator · malfunctionedDURING CRUISE PHASE OF FLIGHT, THE AIRCRAFT WAS TURNED BACK DUE TO THE LH ENGINE AIR BLEED FAULT. THE AIRCRAFT LANDED WITH NO INCIDENT NOR WEIGHT EXCEEDANCE. AT MAINTENANCE, THE BLEED PRESSURE REGULATOR VALVE AND ITS SOLENOID ON LH ENGINE WERE REPLACED PER TRSDR RJEF20190320001Transceiver · unserviceableDURING FLIGHT TPU146 (LIM-MED) THE AIRCRAFT HAD FAILURE OF RADAR SYSTEM AND RETURNED TO LIM FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED: "RADAR INOP, GW 61500 KG, NO OVERWEIGHT LANDING", MAINTENANCE PERSONNEL PERFORMED FAULT ANALYSIS IN ACCSDR RJEF20190301001Servo Control · unserviceableDURING FLIGHT LRC638 FROM SAL TO CUN THE PILOT REPORTED AIRFRAME VIBRATION AND RETURNED TO SAL FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED: 1)"STRONG VIBRATION DURING CLIMB AND LEVEL FLIGHT", FOR THIS REPORT MAINTENANCE PERSONNEL PERFORMED SDR RJEF20190107001Unknown · malfunctionedDURING TAKE OFF PROCESS OF FLIGHT TP823 FROM LIM TO CUZ ENGINE 1 ACCELERATED LESSER IN COMPARISON WITH ENGINE 2, THE TAKE OFF WAS ABORTED AND RETURNED TO THE GATE FOR MAINTENANCE. THE PILOT REPORTED: "DURING ROLLING TAKE OFF ENG 1 DELAY ACCELERATION IN RELATIOSDR 5TTY2018110500001Hydraulic System · overservicedDURING ENGINE START, PRIOR TO THE DEPARTURE OF THE AIRCRAFT FLIGHT AV503, PILOT REPORTED LOW PRESSURE ON BLUE HYDRAULIC SYSTEM; CONSEQUENTLY, THE AIRCRAFT WAS RETURNED TO BLOCK. AT MAINTENANCE, AND PER TSM 29-12-00-860-053-C, THE BLUE HYD. SYSTEM WAS FOUND SDR RJEF20181126001Gps · failedDURING CLIMB OF FLIGHT TP831 FROM LIM TO CUZ, THE AIRCRAFT HAD FAILURE OF GPS1 AND RETURNED TO LIM FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING AT LIM THE PILOT REPORTED THE FOLLOWING TWO ITEMS: 1) "GPS1 FAULT"; AS CORRECTIVE ACTION MAINTENANCE PERSONNEL DEFERSDR SOKF20181116009Gps · faultedDURING FLIGHT FROM LIM TO CUZ THE AIRCRAFT RETURN TO LIM DUE TO ECAM WARNING MESSAGE NAV GPS 1 FAULTGPS 1. AT LIM STATION TRANSFERRED TO DMI PAGE 06571 ITEM 2 IAW MEL 34-58-01 CAT C AND RNP-AR OPERATION PROHIBITED. THE AIRCRAFT RETURN TO NORMAL OPERATION.SDR SOKF20181019008Anti-Ice Valve · damagedDURING FLIGHT FROM AQP TO CUZ THE AIRCRAFT DEVERTED TO LIM DUE TO ECAM WARNING WING ANTI-ICE FAULT AND BAD WEATHER AT CUZ STATION. AT LIM STATION PERFORMED TSM 30-11-00-810-803-A, REMOVED AND REPLACED OF WING ANTI ICE CONTROL VALVE PERFORMED IAW AMM 30-11-51-0SDR SOKF2018100210006Fmc · damagedDURING TO FROM LIM TO JUL THE, TO WAS REJECTED DUE ECAM WARNING A/T OFF. REMOVED AND REPLACED FMGC IAW AMM 22-83-34-000-001-A AND AMM 22-83-34-400-001-A OP TEST AFS IAW AMM 22-96-00-710-001 TEST SATISFACTORY. THE AIRCRAFT RETURN TO NORMAL OPERATION.SDR SOKF20180927005Autothrottle Sys · malfunctionedDURING TO FROM LIM TO CUZ THE TO WAS REJECTED DUE TO A/THR INOP AND DURING T/O PWR CLB DO NOT SHOW INDICATION THRUST MODE AND FLEX TOGA. AUTO FLIGHT AUTO THRUST OFF DURING TAKE OFF ROLL. AT LIM STATION LAND CAT 3 CAPABILITY TEST PERFORMED IAW AMM 22-97-00-710-SDR 2018FA0000283Warning Message · false activationACFT RETURNED FROM FLIGHT, DECLARED IN EMERGENCY DUE TO AN ENG MESSAGE 2 EGT OVERLIMIT IN PHASE 05 SO THE CREW ACCORDING TO THEIR PROCEDURES PERFORMED A MOTOR CUT. PLANE LANDS WITHOUT PROBLEM AND ARRIVES AT THE PIER BY ITS OWN MEANS. CHECK IN AND OUT OF THE ESDR RJEF20180529001Fcu · malfunctionedDURING CLIMB, THE AIRCRAFT HAD A FAILURE OF THE KNOB SELECTORS SPEED AND HEADING OF THE FCU, LATER, THE AIRCRAFT DIVERTED, AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED THE FCU SPEED AND HEADING KNOBS BECAME INOPERATIVE WITH NO ECAM MESSAGE OR ANY APPARENT SDR RJEF20180515001Control Valve · inoperativeDURING CLIMB, THE AIRCRAFT HAD A FAILURE OF THE AIR CONDITIONING SYSTEM AND RETURNED TO DEPARTURE. UNEVENTFUL LANDING, AC SUPPLY TEMPERATURES OF 36°C AND 62°C, MAINTENANCE PERFORMED A FAULT ANALYSIS IAW TSM 21-61-00-810-803-A, REPLACED THE PACK FLOW CONTROSDR RJEF20180501001Brake Assy · overtempDURING TAKE OFF, THE PILOT REPORTED THAT THE TAKE WAS ABORTED DUE TO A STRONG VIBRATION AT LOW SPEED, THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PERFORMED A FAULT ANALYSIS IAW TSM 05-50-00-810-823-A, & 32-42-00-810-925, INSPECTED THE BRAKES ASSEMBLIES FORSDR SOKF20180430004Contactor · damagedTHE AIRCRAFT RETURN TO DEPARTURE DUE TO AN ECAM WARNING FOR THE CENTER TANK PUMP 1, LOW PRESSURE AND CENTER TANK PUMP 2, LOW PRESSURE PREVIOUSLY. REPLACED THE CONTACTOR GFI FOR THE CENTER TANK PUMP 2 SUPPLY 70QA IAW ESPM 50-46-50, INSTALLATION SATISFACTORY CSDR RJEF20180410002Egt Indication · illuminatedDURING ENGINE START, THE PILOT REPORTED THE NR 1 ENGINE EGT OVERLIMIT, DURING THE NR 1 ENGINE START, EGT INDICATION WENT TO MAX DISPLAYED EGT ON THE NEEDLE AND DIGITAL 818°C, NR 1 ENGINE MASTER WAS SET TO OFF, THEN THE NR 1 ENGINE INDICATIONS DISPLAY XX, THSDR RJEF20180309001Pcu · faultyDURING CLIMB, THE AIRCRAFT HAD A FAILURE MESSAGE, FLAPS LOCKED, RETURNED TO DEPARTURE. UNEVENTFUL LANDING. MAINTENANCE PERFORMED A FAULT ANALYSIS IAW TSM 27-51-00-810-820-A, REPLACED THE FLAP PCU IAW AMM 27-54-51 PB401. REMOVED AND REPLACED THE BLOCK-VALVESDR SOKF20180304002Actuator · damagedDURING TO FROM LIM TO AQP THE TO WAS REJECTED DUE TO ECAM MSG ENG 2 COMPRESSOR VANE. AT LIM STATION PERFORMED TSM 75-30-00-810-853-A REMOVED AND REPLACED OF THE VSV ACTUATOR AS PER AMM 75-32-41-000-010-A A01 AND AMM 75-32-41-400-010-A01 PERFORMED IDLE LEAK CHESDR RJEF20180219001Actuator · malfunctionedDURING CLIMB, HAD A WARNING MESSAGE OF THE NR 2 THRUST REVERSE UNLOCKED, RETURNED TO DEPARTURE. UNEVENTFUL LANDING. PERFORMED FAULT ANALISYS IAW TSM 78-30-00-810-844-A, REPLACED THE HCU, REPLACED THE NON-LOCKING ACTUATORS FOR THE NR 2 THRUST REVERSER IASDR 5TTY2018012900001Controller · faultedAFTER T/O, THE AIRCRAFT WAS TURNED BACK TO DEPARTURE BASE DUE TO PRESSURE SYS 1 FAILURE AND UNABLE TO CONTROL PRESSURIZATION AFTER SWITCHING TO SYS 2. LANDING IN MANUAL MODE WITH NO INCIDENTS. FUEL AUTO FEED FAULT WAS REPORTED. PRESSURIZATION SYSTEM 1 FAILUSDR RJEF20180110001Engine · malfunctionedDURING FLIGHT, THE NR 1 ENGINE HAD A STALL CONDITION AND EGT OVERLIMIT, DUE THAT SITUATION THE AIRCRAFT DIVERTED. UNEVENTFUL LANDING. CARRIED OUT THE CORRESPONDING FAILURE ANALYSIS. FOLLOWED THE INSTRUCTIONS OF TSM 71-00-00-810-808-A, PERFORMED BORESCOPE SDR RJEF20171208001Pitot Head · damagedAFTER ARRIVAL TO MIA OF FLIGHT AVA008 COMING FROM BOG, THE PILOT REPORTED: "DURING INITIAL CLIMB POSSIBLE BIRD STRIKE ON THE F/O PITOT PROBES (WRONG SPEED AND ALTITUDE INDICATION ON F/O PFD)". DUE THAT SITUATION THE AIRCRAFT WAS HELD ON GROUND AT MIA, MAINTENASDR SOKF20171122012Tank · contaminatedDURING MAYOR CHECK, MANUALLY OPERATED THE TRANSFER SYSTEM DISCHARGE CHECK VALVE, BETWEEN RIB 1 AND RIB 2 WERE FOUND MATALLIC PARTICLES AND DEBRIS. LT AND RT ENGINE FUEL FILTER ELEMENTS WERE REMOVED AND REPLACED IAW AMM 73-12-42, REVISION 42, AMM 57-27-11, SDR RJEF20171110001Outflow Valve · malfunctionedAFTER TAKEOFF, THE PILOT REPORTED THE CABIN PRESSURE SYSTEM 1 & 2 FAULTED. NR 1 ENGINE COMPRESSOR VANE DUE TO THAT SITUATION THE AIRCRAFT RETURNED TO DEPARTURE FOR MAINTENANCE. MAINTENANCE PERFORMED FAULT ANALYSIS IAW TSM 21-31-00-810-807-A, REPLACED THSDR RJEF20171027001Pin · brokenDURING PREPARATION FOR PUSHBACK, THE FLIGHT CREW REPORTED SOMETHING ABNORMAL FELT DURING TOW TRUCK COUPLE. DUE THAT SITUATION THE AIRCRAFT WAS HELD ON GROUND, MAINTENANCE PERSONNEL PERFORMED VISUAL INSPECTION OF NOSE LANDING GEAR IAW AMM 32-21-00-200-002-A, ALSDR RJEF20171012001Thermocouple · faultyDURING THE NR 1 ENGINE START, EGT ROSE TO 780°C, INDICATION ON RED. DUE TO THAT SITUATION THE AIRCRAFT RETURNED TO THE GATE FOR MAINTENANCE. MAINTENANCE PERFORMED FAULT ANALYSIS IAW TSM 77-20-00-810-801-B, INSPECTED THE NR 1 ENGINE THERMOCOUPLES, AND FOUNSDR RJEF20171005002Indication Sys · malfunctionedDURING TAXI, THE PILOT REPORTED THE NR 1 ENGINE EGT EXCEEDED DURING TAXI TO 720°C, THEN THE TEMPERATURE DROPS TO -10°C, AFTER THAT INDICATION STABILIZED, THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PERFORMED FAULT ANALYSIS IAW TSM 77-00-00-810-934-A, INSPSDR RJEF20170914001Warning Light · false activationDURING CRUISE PHASE OF FLIGHT. THE AIRCRAFT DISPLAYED THE FAILURE MESSAGE FOR HYD Y RSVR LO LVL, DUE THAT SITUATION THE PILOT RETURNED TO DEPARTURE FOR MAINTENANCE. UNEVENTFUL LANDING, MAINTENANCE PERSONNEL PERFORMED FAULT ANALYSIS IAW TSM 29-13-00-810-80SDR ANCF2017091001Actuator · faultyDURING T/O ENGINE 2 SINGLE CHIME ANNOUNCE WAS PRESENTED T/O REJECTED AND N2 EXCEEDANCE ON ENG2 SHOWN ON EWD. IN ACCORDANCE WITH AMM 77-00-810-816-B AND 71-00-00-860-010-B FIG 71 (AIE) ENG 2 N2 MORE THAN THE LIMIT CHECK WAS PERFORMED, N2 MAX REACHED=100% . VSVSDR SOKF20170818008Filter · contaminatedDURING MAJOR CHECK, PERFORMED TASK CARD 731000-11-1, FOUND FUEL FILTER CONTAMINATED. FUEL FILTER ELEMENT WERE EVALUATED IAW AMM 73-12-42-210-061-A PARAGRAPH A ITEM (2)REV.40 01. LT AND RT ENGINE FUEL FILTERS ELEMENT WERE REPLACED. LT FUEL COOLED OIL COOLER SDR SOKF20170721007Warning Message · illuminatedDURING FLIGHT, THE AIRCRAFT RETURN TO DEPARTURE DUE TO AN ECAM WARNING MESSAGE FOR FLT CONTROL LT AILERON FAULT. INCLUDED IN THE MEL 27-14-01. THE AIRCRAFT RETURNED TO NORMAL OPERATION.SDR EE4Y201706263824Cowling · delaminatedENGINE NR 2, OUTBOARD FAN COWL, FWD EDGE WITH DELAMINATION. REPAIRED AS STATED IN ENGINEERING ORDER NR EOD-32S-54-0159-R00.SDR EE4Y201706243823Skin · dentedENGINE 1 RT THRUST REVERSE C-DUCT PERFORATED SKIN WITH DENT AND DELAMINATION. REPAIRED AS STATED IN ENGINEERING ORDER NR EOD-32S-54-0161-R00.SDR EE4Y201706233822Sleeve · damagedNR 1 ENGINE THRUST REVERSER, TRASLATING SLEEVE SKIN OUTER LOWER FORWARD SPLIT LINE, ENLARGER FASTENER HOLE. REPAIRED IAW REPAIR INSTRUCTIONS.SDR EE4Y201706233821Skin · dentedLEFT INBOARD FLAP, TRAILING EDGE LOWER SKIN DENTED. REPAIRED IAW REPAIR INSTRUCTIONS.SDR EE4Y201706233820Stringer · corrodedFRAME 32-33, STRINGER 41R CORRODED. REPAIRED IAW REPAIR INSTRUCTIONS.SDR EE4Y201706233819Stringer · corrodedFRAMES 54-56, STRINGER 42R WITH CORROSION. REPAIRED IAW REPAIR INSTRUCTIONS.SDR EE4Y201706233817Stringer · corrodedFRAMES 61 - 63, STRINGER 41R CORRODED. REPAIRED IAW REPAIR INSTRUCTION, AND EOD-32S-53-0158-R00.SDR EE4Y201706233816Structure · contaminatedRIGHT ELEVATOR UPPER SURFACE AREA WITH WATER INGRESS INDICATION. REPLACED IAW INSTRUCTIONS.
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