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 EE4Y201706233815Door Sill · corrodedPAX CABIN RT AFT DOOR SILL CORRODED. REPLACED IAW SRM INSTRUCTIONS.SDR EE4Y2017062338015Seat Track · corrodedPAX CABIN SEAT TRACK CORRODED. REPLACED IAW SRM GUIDELINES.SDR EE4Y201706233811Structure · damagedRUDDER RT SIDE HOISTING POINT, 3 AREAS WITH WATER INGRESS . REPAIRED IAW EOD-32S-55-0051-R00.SDR EE4Y201706233810Bulkhead · corrodedCENTER FUSELAGE FRAME 35 BULKHEAD WITH CORROSION. REPAIRED IAW EOD-32S-53-0165-R00.SDR RJEF20170329001Brake · overheatedON ARRIVAL, THE PILOT REPORTED THE BRAKE NR 1 TEMPERATURE AFTER LANDING REACH 495 DEGREES. BRAKES NORMAL BRAKE FAULT. BRAKES ALTERNATE L RELEASED. HYD G RESERVOIR LOW LEVEL. PERFORMED INSPECTION IAW AMM 05-51-16-200-001-A, FOUND SPOTS WITH MISSING CHROME SDR RJEF20170306001Blower · failedDURING CRUISE PHASE OF FLIGHT, THE CREW REPORTED BURNING ODOR AND VIBRATION IN THE CABIN, DUE THAT SITUATION THE AIRCRAFT DIVERTED FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED A HEAVY BURNING ODOR AND STRONG VIBRATION FELT ALONG THE CABIN. ISDR SOKF20170307003Valve · failedAFTER TAKE OFF, THE AIRCRAFT RETURN TO DEPARTURE, DUE THE FAILURE OF THE VENT SKIN VALVE, ABOUT 5, 000 FT. FOLLOWED THE ECAM PROCEDURE AND THE LIMIT UP TO 10,000 FT. PERFORMED PROCEDURES IAW TSM 21-26-00-810-804-A AND FOUND THE VENT SKIN VALVE FAULTY. REMOSDR RJEF20170227001Band · missingON LANDING, THE PILOT REPORTED A WHEEL NR 2 BAND MISSING. MAINTENANCE PERSONNEL VERIFIED THAT WHEEL NR 2 HAD THE TREAD MISSING, AS A CONSECUENCE OF THE TREAD THROWN THE INBOARD FLAP LT HAS DENTS OUT OF LIMITS AND THE SIDE STAY OF LT MLG HAS SURFACE DAMAGE. SDR RJEF20170117001Adiru · malfunctionedDURING TAKEOFF PROCESS OF FLIGHT TA567 FROM JFK TO SAL, THE AIRCRAFT SHOWED FAILURE OF AIRSPEED AND ATL INDICATIONS, DUE THAT SITUATION THE TAKEOFF WAS ABORTED AND RETURNED TO THE GATE FOR MAINTENANCE. THE PILOT REPORTED "DURING T.O. ROLL, AIRSPEED AND ALT INDSDR SOKF20161023010Warning System · false activationDURING FLIGHT FROM SAL TO MDE THE AIRCRAFT RETURN TO SAL DUE ENG 1 ANTI-ICE VALVE CLOSED, IT INCLUDED AS DMI ENG 1 ANTI ICE VALVE IN OPEN POSITION. THE AIRCRAFT RETURN TO NORMAL OPERATION.SDR 5TTY201609260001Transducer · failedDURING FLIGHT, THE AIRCRAFT GENERATED THE FLT CONTROL ELAC 2 FAULT MESSAGE AND DUE TO DEFERRED ELAC 1, THE AIRCRAFT WAS DIVERTED. AFTER AN UNEVENTFULLY LANDING, MAINTENANCE REPLACED THE CAPTAIN`S TRANSDUCER UNIT 4CE1 ON CAPTAIN SIDE STICK IAW TSM 27-93-00-810SDR SOKF20160913008Carbon Seal · damagedDURING FLIGHT, THE ACFT DIVERTED DUE TO NR 2 ENGINE HAVING OIL LEAK AND WAS LANDED WITH 6.5 QT AND 10.5 WHEN SHUTDOWN, AT STATION PERFORMED TSM 79-30-00-810-806A AND FOUND SIGNS OF OIL LEAK FROM CARBON SEAL OF THE STARTER DRIVE. PERFORMED REPLACEMENT OF THE CSDR SOKF20160902006Servo Control · faultyDURING CLIMB, THE ACFT RETURN TO DEPARTURE DUE TO ECAM WARNING FLIGHT CONTROL ELAC 2 PITCH FAULT, AT STATION, PERFORMED TSM 27-93-00-810-867-A. R & R ELEVATOR SERVO CONTROL LT SIDE, 34 CE1 IAW AMM 27-34-51-000-001-A AND 27-34-51-400-001-A. ADJUSTMENT TEST OFSDR RJEF20160708001Lever · faultyDURING CLIMB OF FLIGHT TP803, THE LANDING GEAR CONTROL LEVER DID NOT MOVE UP, DUE THAT REASON THE AIRCRAFT RETURNED TO DEPARTURE FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING MAINTENANCE PERSONNEL PERFORMED FAULT ANALYSIS IN ACCORDANCE WITH TSM 32-31-00-810-88SDR SOKF20160704004Valve · damagedDURING TAKE OFF FL 803, THE AIRCRAFT REJECTED TAKE OFF DUE NR 2 ENGINE COMPRESOR VANE MAINTENANCE REQUIERED AS PER TSM 75-30-00-810-853-A AND TSM 75-30-00-810-844-A PERFORMED REMOVAL AND REPLACED VSV ACTUATOR (4022KS) IAW AMM 75-32-41-00-010-A AND AMM 75-32-4SDR RJEF20160621001Probe · faultyDURING TAKEOFF OF FLIGHT, THE ACFT LOST THE AIR SPEED INDICATION ON CAPTAIN´S SIDE, THE TAKEOFF WAS ABORTED AND RETURNED TO THE GATE FOR MAINTENANCE. NO AIR SPEED INDICATION ON CAP SIDE, RTO, BRAKE TEMPERATURE 420 DEGREES C". MAINTENANCE PERSONNEL PERFORMED SDR RJEF20160422001Sensor · faultyDURING LANDING PROCEDURES, THE FLAPS BECAME JAMMED, THE PILOT ASKED FOR THE ACTIVATION OF THE EMERGENCY PROTOCOL AND LANDED WITHOUT INCIDENT IN THAT CONFIGURATION. ONCE THE ACFT ARRIVED TO THE GATE THE PILOT REPORTED: LANDING WITH FLAPS JAMMED BETWEEN 0 AND SDR RJEF20160419001Fcu · faultyDURING CLIMB OF FLIGHT TA588, THE PILOT REPORTED FCU ALTITUDE UNABLE TO CHANGE ALTITUDES. DUE THAT SITUATION THE ACFT RETURNED. AFTER AN UNEVENTFUL LANDING, ONCE THE ACFT PARKED AT THE GATE, PERFORMED FAULT ANALYSIS IAW TSM 22-81-00-810-801-A. REPLACED THE SDR RJEF201603220001Check Valve · failedDURING TAKEOFF, THE PILOT REPORTED OVERHEAT YELLOW HYDRAULIC RESERVOIR ECAM WARNING; HENCE THE ACFT TURN BACK TO AIRPORT. AT LANDING, THE PILOT REPORTED NO OVERWEIGHT LANDING. AFTER AN UNEVENFUL LANDING AND FOLLOWING TSM 29-13-00-810-802-A, IT WAS DETERMINEDSDR SOKF20160310001Warning System · false activationDURING CLIMB, THE ACFT RETURNED, DUE ECAM WARNING MSG DOOR FWD CARGO OPEN, DURING INITIAL CLIMB, NEVER PRESSURIZED. PERFORMED IAW TSM 21-31-00-810-809-A, TEST TO MEASURE THE STRUCTURAL LEAKAGE WITH THE AIDS PERFORMED IAW AMM 05-53-00-780-003-A01, PRESSURIZATISDR RJEF20160118001Warning System · false activationDURING PUSHBACK OF FLIGHT TA561, AT ENG STARTING THE PILOT REPORTED, ECAM WARNING ANTI-ICE FIRST OFFICER & STANDBY PITOT, DUE THAT SITUATION THE ACFT RETURNED TO THE GATE. PERSONNEL PERFORMED FAULT ANALYSIS IAW TSM 30-31-00-810-812-A, TESTED THE FIRST OFFICERSDR RJEF20151105001Computer · malfunctionedDURING CLIMB, THE PILOT REPORTED FLIGHT CONTROL RT & LT AILERON FAULT, FLIGHT CONTROL ALTN LAW & HENCE THE ACFT WAS RETURNED, LANDING WITH NO INCIDENTS. ONCE ON GND THE ACFT, BOTH ELAC 1 & ELAC 2 WERE RESET IAW TSM 27-93-00-810-949-A. PERFORMED OPERATIONAL TSDR RJEF20150928001Actuator · faultyPREVIOUS TO DEPART AS FLIGHT TA561. THE ACFT SHOWED THE FOLLOWING NO DISPATCH FAILURE MSGS. FLIGHT CONTROL RUDDER TRAVEL LIMIT 2 FAULT MSG ON ECAM. FOR THIS FAILURE IT WAS PERFORMED FAULT ANALYSIS IAW TSM 22-61-00-810-804-A BY RESETTING THE FAC 2 & TESTING SDR RJEF20150613001Control Lever · faultyDURING THE DESCENT OF THE ACFT FLIGHT TA-397, THE LG LGCIU 1 & 2 FAULT MSG WAS TRIGGERED ON THE ECAM DISPLAY. THEREFORE, THE ACFT WAS DIVERTED TO ITS ALTERNATE AIRPORT. THE ACFT LANDED WITH LG`S EXTENDED BY GRAVITY WITH NO INCIDENT & NO ADDITIONAL REPORTS. SDR RJEF20150321001Actuator · leakingPRIOR TO ITS DEPARTURE, FOUND HYD LEAK FROM THE ENG 1 RT THRUST REVERSER LOCKING ACTUATOR. THE ACFT WAS HELD ON GND FOR THE ACTUATOR REPLACEMENT IAW AMM 78-32-43 PB 401 WITH NO LEAK NOR FAULT. THE ACFT WAS RETURNED TO SERVICE ONCE THE MENTIONED CORRECTIVE ACSDR ANCF201412121Actuator · faultyDURING FLIGHT RUDDER TRIM LIMITER FAULT 1 & UNCOMMANDED RUDDER TRIM INPUTS. IAW AMM 27-22-51-000-001-A THE RUDDER TRIM ACTUATOR WAS REMOVED & IAW AMM 27-22-51-400 001-A THE RUDDER TRIM ACTUATOR WAS REPLACED. OPERATIONAL TEST OK. ACTUATOR RUDDER TRIM PN 6137SDR RJEF20141211001Unknown · smokeAFTER TAKEOFF, THE PILOT REPORTED SMOKE IN PAX CABIN SO THE ACFT WAS RETURNED TO AIRPORT. AFTER LANDING, THE PILOT REPORTED OVERWEIGHT LANDING 66.6 TONS. IAW TSM 05-50-00-810-831-A & CABIN ODOR OR SMOKE COS REPORTING SHEET, IT WAS FOUND BOTH A/C PACKS AS THESDR RJEF20141031001Engine · stalledAFTER ARRIVAL, THE PILOT REPORTED A NR 2 ENGINE STALL. PERFORMED ENG 2 FULL TROUBLESHOOTING PROCEDURE DESCRIBED ON TSM 71-00-00-810-809-A WITH NO DISCREPANCIES FOUND. THE ACFT WAS RETURNED TO SERVICE AFTER A SUCCESSFUL POWER ASSURANCE TEST.SDR RJEF20140901001Elevator System · vibrationDURING CLIMB, THE PILOT REPORTED STRONG FUSELAGE VIBRATION DURING CLIMB, FLIGHT LEVEL 250, AIS 320 KTS & 0.74M, DIMINISH BY LOWERING AIS 270 KTS. THE ACFT RETURNED FOR MAINTENANCE WHERE LANDED WITHOUT INCONVENIENCE. IAW TSM 05-50-00-810-801-A WAS FOUND PLASDR RJEF20140818012Wire Harness · faultyDURING TAKEOFF PROCEDURES OF FLIGHT LR625 THE ACFT HAD THE FAILURE MSG ENG 1 SENSOR FAULT & AIR PACK 1 & 2 FAULT. THE TAKEOFF WAS REJECTED & THE ACFT RETURNED TO THE GATE FOR MX, THE BRAKE TEMP WAS 300°C AT BRAKE 2. THE ACFT WAS HELD ON GND & PERFORMED FAULTSDR SOKF20140812006Computer · faultyDURING CLIMB THE ACFT RETURNED DUE ELAC 2 FAULT. IAW TSM 27-93-00-810-967-A PERFORMED R & R OF ELAC 2 IAW AMM 27-93-34-000-001 & AMM 27-93-34-400-001. PERFORMED OPERATIONAL TEST IAW AMM 27-93-00-710-001 & LAND CAT III CAPABILITY TEST IAW AMM TASK 22-97-00-71SDR SOKF20140730005Servo Control · damagedVIBRATION AFTER TAKEOFF & CLIMB IAW TSM 05-50-00-810-802-A. PERFORMED CHECK OF THE LOAD REPORT PARAMETER AFTER HARD & OVERWEIGHT LANDING IAW AMM 31-37-00-200-001-A & NO OVERWEIGHT LANDING CONDITION WAS FOUND. CHECKED OK IAW TSM 05-50-00-810-801-A & TSM 27-2SDR RJEF20140623007Thermocouple · faultyWHEN ARRIVING THE PILOT REPORTED THAT ENG 2 HAD ABNORMAL EGT INDICATION AROUND 220°C DIFFERENCE. DUE THAT REASON THE ACFT WAS HELD ON GND FOR MX. PERFORMED A FAULT ANALYSIS IAW TSM 77-20-00-810-802-B FINDING THAT THE THERMOCOUPLES OF POSITIONS B & C OF ENG 2SDR RJEF20140527006Wire Harness · cutPIC REPORTED DURING TAKEOFF BRAKE RELEASE MSG APPEARS THEREFORE, THE TAKEOFF WAS ABORTED. PIC REPORTED THRUST REVERSERS WERE USED BELOW 70 KNOTS. PERFORMED TSM TASL 32-32-00810-815-A & FOUND HARNESS 2M MLG RT CUT. THE HARNESS 2M WAS REPLACED IAW AMM 32-11-43SDR RJEF20140110002Handle · malfunctionedON ARRIVAL, PILOT REPORTED THAT THE LANDING GEAR LEVER STUCK IN DOWN POSITION UNTIL 1000 FT AFTER TAKEOFF. PERFORMED A FUNCTIONAL TEST OF THE LANDING GEAR, RETRACTION & EXTENSION IAW AMM 32-31-00-720-002 OBTAINING NORMAL RESULTS. R & R LANDING GEAR CONTROLSDR RJEF20140108001Engine · vibrationDURING CLIMB, PILOT REPORTED INTERMITTENT ADVISORY OF NR 1 ENGINE HIGH N1 VIBRATION, REACHED 7.2 UNITS, N2 VIBRATION REACHED 4.2 UNITS. AN OIL ODOR DETECTED. ACFT RETURNED DEPARTURE FOR MAINTENANCE. UNEVENTFUL LANDING. BORESCOPIC INSPECTIONS TO NR 1 ENGISDR RJEF20131011009Coffeemaker · odorDURING FLIGHT, PILOT REPORTED ELECTRICAL FUMES DETECTED FWD AND AFT GALLEY, ACFT DIVERTED AND DECLARED AOG. MAINTENANCE PERFORMED TSM 05-50-00-810-831-A. FOUND FWD COFFEE MAKER RESPONSIBLE.SDR SOKF20130828012Solenoid Valve · malfunctionedNR 2 ENGINE EGT OVER LIMIT DURING CLIMB, THRUST EGT EXCEEDED LIMITS. EGT WENT CLOSE TO 670 CELSIUS DEGREES FOR 10 SECONDS THEN REDUCED TO LOWER EGT. R & R HPC 10 STAGE SOLENOID VALVE IAW AMM 75-32-53. PERFORMED FUNCTIONAL TEST IAW AMM 75-32-53-700-010A ANDSDR SOKF20130605003Check Valve · failedLOSS OF HYD YELLOW SYS DUE TO RESERVOIR LOW LEVEL. FOLLOWED TSM 29-13-00-810-016 WAS R & R CHECK VALVE (3050GM) PERFORMED IDLE LEAK TEST OK NORMAL IAW AMM 29-13-36. THE ACFT RETURN TO NORMAL OPERATION.SDR SOKF20130207001Warning System · activatedECAM WARNING ENGINE 1 AND ENGINE 2 EPR MODE FAULT NI DEGRADED MODE. ENTER AS DD ITEM MEL REFERENCE 73-20-04 CATEGORY C.SDR RJEF2013020768701Tachometer · defectiveON ARRIVAL OF AIRCRAFT FLIGHT TAI-396 TO MGA FROM SAL, THE PILOT REPORTED AUTO BRAKE SYSTEM FAILURE, THE AIRCRAFT WAS DECLARED AOG. PER TSM 32-42-00, FOUND TACHOMETER NR 3 INOPERATIVE. REPLACED AND PERFORMED OPERATIONAL TEST AS PER AMM 32-42-00 WITH NO DUPLISDR RJEF2013010768201Cover · missingAT THE ARRIVAL OF THE AIRCRAFT AS FLIGHT TAI-9951 FROM SAP TO SAL, IT WAS FOUND THAT COVER 622WB ON PANEL 622AB ON RIGHT WING WAS MISSING. THE AIRCRAFT WAS INSPECTED AND NO OTHER DAMAGE WAS FOUND. AS PER AIRBUS REPAIR APPROVAL REF:70571449/003/2013 AND ENGINSDR RJEF2012081004Proximity Sensor · defectiveAFTER TAKEOFF OF THE AIRCRAFT AS FLIGHT TAI-561 FROM SFO TO SAL, THE PILOT IN COMMAND REPORTED A L/G SHOCK ABSORBER FAULT, FUEL AUTO FEED FAULT AND LOSS OF AUTO PILOT; CONSEQUENTLY, THE AIRCRAFT WAS RETURNED TO SFO AIRPORT FOR MAINTENANCE. AFTER LANDING OF THSDR UALA2012040202029Connector · damagedPAX REPORTED SPARKING AND A ODOR OF SMOKE. FOUND CONNECTOR ON SEU AT ROW 29ABC BURNED. REPLACED SEU AT 29ABC, CHECK GOOD.SDR MU1Z2011020200004Strut · bentFLAP INTERCONNECTING STRUT ON BOTH LT AND RT SIDES PROXIMITY SENSORS BENT.SDR MU1Z2011020200005Skin · dentedFUSELAGE SKIN - DENT LOCATED IN RT SIDE BETWEEN FR 2 AND FR 3 AND STR Z508.SDR MU1Z2011020200003Frame · dentedFUSELAGE DENT BETWEEN FR 6 AND FR 7 APROX 6.5" DOWN RT SIDE STRINGER. DEPTH 1.57MM A= 21.97MM.SDR SOKF20041118Engine · fodDURING LANDING, CAPTAIN REPORTED (FOD ON ENGINE NR 2, NO ABNORMAL INDICATION DURING TAXI). MAINT PERFORMED INSPECTION OF ENGINE NR 2 IAW MM AND FOUND SOME DAMAGES LOCATED ON ATTRITION LININGS AT 5 OCLOCK, ACOUSTIC PANEL AT 4:30, (ENGINE, FROM THE FRONT), SOMESDR 2004F00413Transceiver · malfunctionedAFTER TAKEOFF, WEATHER RADAR 1 INOPERATIVE, NAV GPWS TERR DET FAULT AND NAV PRED W/S DET FAULT MESSAGES CAME ON ECAM. AIRCRAFT RETURNED TO IAH STATION. THE AIRCRAFT LANDED WITHOUT INCIDENT AND ON GRUOND IT WAS PERFORMED TEST OF THE WEATHER RADAR AND W/S SYSTSDR 2004F00408Radar · failedSJO - FLT 631 - DURING CLIMB, THE WX RADAR WAS INOPERATIVE AND AIRCRAFT WAS RETURNED TO SAN JOSE STATION FOR MAINTENANCE. AFTER LANDING, IT WAS FOUND UNSERVICEABLE THE TRANSCEIVER WEATHER RADAR, IT WAS REPLACED PER AMM 34-41-33 AND GROUND FUNCTIONAL CHECKS WE
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