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 engine_model_key = 'V2527EA5' 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 engine_model_key = 'V2527EA5' 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 YENA2024122301578Actuator · failedFLT#8523, EWR-RDU. (AIRCRAFT DIVERTED TO JFK) 'DURING CLIMB OUT ENG 2 COMPRESSOR VANE ECAM MSG FOLLOWED BY ENG 2 STALL. BANG/THUD HEARD DURING STALL. ENGINE 2 RECOVERED BEFORE ECAM ACTIONS STARTED; REMOVED AND REPLACED #2 ENG LOW PRESS COMPRESSOR BLEED MASTER SDR YENA2024030600360Engine · stalledFLT#621, BOS-PBI. (AIRCRAFT DECLARED AN EMERGENCY). '#1 ENGINE, ENGINE STALL ENGINE EGT 765 - SHUT DOWN.' (SUPPLEMENTAL INFORMATION TO FOLLOW)SDR 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 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 YENA2020082500433Seal · leakingFLT 206, BNA-BOS. LEVEL 1 ODOR EVENT SEE CABIN ODOR FOR DETAILS; TROUBLE SHOT PER TSM 71-00-00-810-801-A, FOUND DE-OILER CARBON SEAL LEAKING. R & R DE-OILER CARBON SEAL REF AMM 72-61-49. LEAK CHECK GOOD. COULD NOT SMELL ANYTHING IN COCKPIT OR CABIN. A/C OK FORSDR 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 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 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 YENA2018121014838Pump · failedFT # 1735, BOS-MSP. DIVERTED TO BUF. #2 ENG LO OIL PRESS NO SECONDARIES; REMOVED + REPLACED #2 ENG OIL PRESSURE PUMP ASSY PER AMM 79-21-41 LEAK/OPS GOOD ALSO FOUND REAGS CLOGGING STRAINER REMOVED AND INSP OIL TANK FOR OTHER RAGS- NO DEFECT FOUND.SDR 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 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 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 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 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 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 YENA201704300320Engine · failedAT TOP OF DESCENT, THERE WAS A BURNED MATERIAL ODOR IN THE COCKPIT. SOON DISSAPATED, AT 2200 MSL ON APPROACH A VERY STRONG DIRTY SOCK ODOR PERMEATED THE FLIGHT DECK & DID NOT GO AWAY UNTIL ENGINE SHUTDOWN. R & R THE NR 1 ENGINE.SDR 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 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 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 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 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 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 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 YENA20140918200Engine · failedAIR RETURN TO DEPARTURE DUE TO ENGINE NR 2 FAILURE AND FIRE CLIMBING THROUGH 8000'. NR 2 ENGINE WAS R & R IAW AMM 71-00-20. ENGINE RUN OK.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 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 ENGI
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