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 = 'V2533A5' 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 = 'V2533A5' 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 RJEF20181113001Warning Light · false activationDURING CRUISE PHASE OF FLIGHT TAI523 FROM LAX TO SAL, THE AIRCRAFT DIVERTED TO MEX DUE TO A MEDICAL EMERGENCY WITH A PASSENGER. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED THE FOLLOWING 6 ITEMS: 1) APU LOW OIL LEVEL INDICATION. MAINTENANCE PERSONNEL VERIFIESDR AALA201810159041Accelerometer · faultyFAILURE OF THE NR 2 ENGINE, ACCELERATOR ON THE N1 AND N2 ON PLACARDS. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED TASK TROUBLESHOOTING MANUAL MM 77-32-00-819-828A AND REPLACED ACCELEROMETER.SDR AALA201810129014Warning Message · false activationREJECTED TAKE OFF, AT 100KTS DUE TO AN N1 EXCEEDING LIMITS. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED DFDR DOWNLOAD IAW AMM 71-00-00-860-010-B, ROTOR SPEED LIMITS FOR TRANSIENT OVER SPEED WAS LESS THAN FIVE SECONDS. NO MAINTENANCE PROCEDURE NECESSARY. DOWNLOASDR SOKF20181011007Warning System · false activationDURING T/O FROM SAL TO IAD, THE AIRCRAFT REJECTED THE T/O DUE TO ECAM WARNING N1 EXCEEDED PARAMETERS. PERFORMED TSM TASK CARD 77.00.00.810.813B, 77.00.00.810.814B AND AMM 77.00.00.860.010B AND WERE FOUND THAT THE VALUES RECORDED WERE 99.88% FOR ENGINE 1 AND 99SDR RJEF20180924001Warning System · activatedDURING CRUISE PHASE OF FLIGHT TAI369 FROM SAL TO MDE, THE AIRCRAFT HAD FAILURE INDICATION OF EPR ENGINE 2, DUE THAT REASON DIVERTED TO PTY FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING AT PTY THE PILOT REPORTED: ENG 2 EPR MODE FAULT. MAINTENANCE PERSONNEL VERIFSDR AALA2018091219008Warning Message · activatedREJECTED TAKEOFF DUE TO A LEFT ENGINE COMPRESSOR VANE FAULT MESSAGE. RETURNED TO GATE. REPLACED THE NR 1 ENGINE VSV ACTUATOR IAW MM 75-32-41. OPS AND LEAK CHECKED GOOD.SDR RJEF20180907001Actuator · faultyDURING LANDING AT MIA OF FLIGHT TAI536 COMING FROM SAP, HAD THE FOLLOWING FAILURE MESSAGE REGARDING ENGINE 2: "COMPRESSOR VANE, N2 OVERLIMIT, EGT OVERLIMIT". IAW TSM 77-00-00-810-818-B, HOT SECTION OF ENGINE 2 WAS VISUAL AND BORESCOPE-INSPECTED IN ACCORDANCE WSDR AALA201808169010Engine · stalledRIGHT ENGINE STALLED AFTER TAKEOFF. RIGHT ENGINE WAS RETURNED TO IDLE, NOT SHUTDOWN. EMERGENCY DECLARED. AIRCRAFT RETURNED TO DEPARTURE, THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED RIGHT ENGINE IAW AMM.SDR AALA201808089021Transducer · faultedDURING CRUISE, AIRCRAFT EXPERIENCED A LOSS OF BOTH PACKS. FLIGHT DESCENDED 12,000 FEET. NO EMERGENCY WAS DECLARED. QRH PROCEDURES WERE COMPLETED, AIR ENGINE 2 BLEED FAULT, ENGINE 1 BLEED VALVE FAILED AND CLOSED WITH ASSOCIATED ENGINE 1 BLEED, PACK 1, PACK 2. FSDR AALA2018071309031Engine · shutdownCLIMBING THRU 5600 FT, THE NR 2 ENGINE EGT OVERTEMP WITH BOOM AND YAW SHUTDOWN BY QRH. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. REPLACED THE NR 2 ENGINE IAW JC 26L40071004. THE AIRCRAFT WAS GROUNDED.SDR RJEF20180622002Electrical Box · contaminatedDURING ENGINE START, THE ENGINE EGT OVERLIMIT DURING START, THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PERFORMED A FAULT ANALISYS IAW TSM 77-00-00-810-930-A & 77-20-00-810-801-B, FOUND EXCESS MOISTURE ON THE EGT JUNCTION BOX, DRIED THE EGT JUNCTION BSDR RJEF20180607001Exciter · faultedDURING ENGINE START, THE AIRCRAFT HAD A FAILURE OF THE IGNITION SYSTEM ON THE NR 2 ENGINE AND RETURNED TO THE GATE FOR MAINTENANCE. MAINTENANCE PERFORMED A FAULT ANALYSIS IAW TSM 74-00-00-810-816-A, REPLACED THE NR 2 ENGINE IGNITER PLUGS A AND B IAW AMM 74-2SDR AALA2018051700000Brake Assy · damagedLEFT MAIN NR 2 TIRE APPEARS LOW. ON REMOVAL OF THE TIRE, FOUND METAL SHAVINGS FROM BRAKE ON TIRE. FOUND THE NR 2 BRAKE BUSHINGS DAMAGED. FOUND THE NR 2 TIRE ASSY DAMAGED INTERNALLY.SDR RJEF20180412001Actuator · unserviceableDURING APPROACH TO SAL AIRPORT OF FLIGHT TAI523 COMING FROM LAX, THE AIRCRAFT HAD FAILURE OF THE LANDING GEAR NORMAL EXTENSION SYSTEM, THEN, THE FLIGHT CREW EXTENDED THE LANDING GEAR BY THE GRAVITY EXTENSION SYSTEM. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTSDR RJEF20180410001Actuator · unserviceableDURING TAXING OF FLIGHT TAI581 FROM IAD TO SAL, THE PILOT REPORTED "ENG 1 COMPRESSOR VANE ON ECAM" AND RETURNED TO THE GATE FOR MAINTENANCE. MAINTENANCE PERSONNEL PERFORMED FAULT ANALYSIS IN ACCORDANCE WITH TSM 75-30-00-810-843-A, LUBRICATED THE VSV MECHANISM SDR AALA201804059006Engine · damagedORD FLT 711 EN-ROUTE ORD - PHX. AIRCRAFT WAS GROUNDED. ON TAKEOFF, JUST AFTER LIFTOFF, THE CREW HEARD A BANG, FOLLOWED BY A LOUD BUZZING VIBRATION. HIGHEST VIBRATION NOTED ON THE GAUGE WAS 6.2, #1 ENGINE. BURNED FUEL DOWN TO LAND BELOW MAX LANDING WEIGHT. THE SDR AALA201804029018Engine · failedNR 1 ENGINE FAILED, HIGH ENGINE TEMPERATURE, EGT OVER LIMIT. REPLACED THE 1 ENGINE IAW 26L40071004 AND 26L00071015. SYSTEM TESTED NORMAL. AIRCRAFT WAS GROUNDED.SDR AALA201803299018Engine · seizedTHE AIRCRAFT RETURNED TO DEPARTURE, DUE TO THE LEFT ENGINE ISSUE. DECLARED EMERGENCY AND PERFROMED UNEVENTFUL LANDING. LEFT ENGINE SEIZED, FAN WILL NOT ROTATE. FIRE DEPARMENT CONFIRMED FLAMES IN TAIL PIPE, BUT EXTINGUISHED UPON LANDING. ACCOMPLISHED A NR 1SDR 5TTY2018022800001Actuator · failedAFTER T/O POWER WAS APPLIED, THE NR 1 ENGINE COMPRESSOR VANE ECAM MESSAGE AND N2 OVERLIMIT INDICATION DISPLAYED, PROMPTING THE CREW TO REJECT TAKE OFF AND RETURN THE ACFT TO THE BLOCK. TROUBLESHOOTING MANUAL, VSV ACTUATOR ON THE NR 1 ENGINE WAS REPLACED AND VSDR AALA201802129042Fuel Control · malfunctionedDURING CRUISE, FL 330, AUTO THRUST NR 1 FAILED, THRUST LOCKED. ACOMPLISHED AN ELECTRONIC CENTRALIZED AIRCRAFT MONITOR PROCEEDURE, SWITCHED TO AUTO PILOT NR 2 FOR THE REMAINDER OF THE FLIGHT. RESET THE NR 1 & 2 FUEL CONTROL UNITS, FLIGHT MANAGEMENT, AND GUIDASDR GTIA2017122002299Seal · leakingAT 400 FT ON FINAL, AN ODOR WAS DETECTED. WITH PACK 1 OFF, THE ODOR DISAPATED. ACCOMPLISHED GVI APU BLEED-AIR DUCT, INLET GUIDE FANES, ETC. NO EXTERNAL LEAKS NOTED IN APU AREA. IAW TSM 21-00-00-810-801-A. PERFORMED ENGINE RUNS & FOUND THE NR 1 ENG DESDR AALA201711239001Turbine · damagedEMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE, DURING CLIMB OUT AT APPROXIMATELY 16,000 FT, THE RIGHT ENGINE WAS SHUTDOWN. LANDING WAS UNEVENTFUL. MAINTENANCE NOTES MOST OF DAMAGE IS IN THE TURBINE SECTION WITH NO VISIBLE DAMAGE TO THE FAN, THE FAN WASSDR 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 AALA201711209034Plug · faultyAIRCRAFT WAS GROUNDED: TAKE OFF ABORTED DUE TO SEVER LAG ON THE NR 2 ENGINE. MAINTENANCE SCHEDULED TO REPLACE NR 2 ENGINE FMU PER MCM CARD 73-94-12. REPLACED LEFT HAND DATA ENTRY PLUG PER MM 73-22-35. SEE ALSO AALA201711169016, AALA201711219053, AALA2017112190SDR AALA201711169016Fmu · slowAIRCRAFT WAS GROUNDED: TAKE OFF ABORTED DUE TO SEVERE LAG ON THE NR 2 ENGINE. MAINTENANCE SCHEDULED TO REPLACE NR 2 ENGINE FMU PER MCM CARD 73-94-12. REPLACED RIGHT HAND ENGINE FMU PER MCM 73-94-12. SEE ALSO AALA2017111209034, AALA201711219053, AALA20171121905SDR AALA201711219053Thermocouple · faultyAIRCRAFT WAS GROUNDED: TAKE OFF ABORTED DUE TO SEVER LAG ON THE NR 2 ENGINE. MAINTENANCE SCHEDULED TO REPLACE NR 2 ENGINE FMU PER MCM CARD 73-94-12. REPLACED RIGHT HAND FUEL TEMPERATURE SENSOR (THERMOCOUPLE) PER MM 73-35-15. SEE ALSO AALA201711169016, AALA2017SDR AALA201711219054Eec · faultyAIRCRAFT WAS GROUNDED: TAKE OFF ABORTED DUE TO SEVER LAG ON THE NR 2 ENGINE. MAINTENANCE SCHEDULED TO REPLACE NR 2 ENGINE FMU PER MCM CARD 73-94-12. REPLACED RIGHT HAND ENGINE EEC PER MCM 73-94-02. SEE ALSO AALA2017111209034, AALA201711169016, AALA201711219053SDR AALA201711219055Fuel Filter · faultyAIRCRAFT WAS GROUNDED: TAKE OFF ABORTED DUE TO SEVER LAG ON THE NR 2 ENGINE. MAINTENANCE SCHEDULED TO REPLACE NR 2 ENGINE FMU PER MCM CARD 73-94-12. REPLACED RIGHT HAND ENGINE FUEL FILTER PER MM 73-12-42. SEE ALSO AALA2017111209034, AALA201711169016, AALA20171SDR AALA201711219016Engine · stalledCLIMBING THROUGH 20,000 FT MSL THE NR 2 ENGINE STALLED, LOST THRUST, AND SHOWED OVERHEAT. THRUST LEVERS REDUCED TO IDLE POWER BUT THE ENGINE DID NOT HAVE ANY THRUST OR RPM. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. ON LANDING BOTH THRUST REVSDR GTIA2017110902235Seal · leakingDIRTY SOCK ODOR REPORTED IN AFT CABIN. PERFORMED SUPPLEMENTARY PROCEDURE 3.266.1. NR 2 PACK WAS SHUTDOWN AND ODOR WENT AWAY, STARTED OUR DECENT, AND THE ODOR CAME BACK WITH PACK 2 ISOLATED, IDLE POWER.. IAW TSM 05-50-00-810-831, FOUND SIGNS OF OIL ON THE NRSDR AALA20171006003Bleed Valve · warning messageAFTER TAKEOFF ENGINE BLEED NR 2 ABNORMAL ILLUMINATED. ENGINE BLEED RESET WAS UNSUCCESSFUL. ACCOMPLISHED ECAM CHECKLIST RETURNED TO DEPARTURE FOR LANDING, REMOVED AIRCRAFT FROM SERVICE FOR TROUBLE SHOOTING OF RIGHT ENGINE BLEED SYSTEM. MAINTENANCE REPLACED PRESDR AALA201710109002Solenoid · failedAFTER TAKEOFF NR 2 ENGINE BLEED ABNORMAL LIGHT ILLUMINATED. ENGINE BLEED RESET WAS UNSUCCESSFUL. ACCOMPLISHED ECAM CHECKLIST RETURNED TO DEPARTURE FOR LANDING, REMOVED AIRCRAFT FROM SERVICE FOR TROUBLE SHOOTING OF RIGHT ENGINE BLEED SYSTEM. MAINTENANCE REPLSDR AALA201710059010O-Ring · leakingUNUSUAL ODOR DETECTED NEAR MID CABIN LAVATORY ROWS 18 TO 22 AT LEVEL OFF AND CRUISE. SLOWLY DISSIPATED. ODOR RESUMED DURING DESCENT AND POWER CHANGES. FOUND THE NR 1 ENGINE SERVICE COUPLING LEAKING. REMOVED AND REPLACED THE O-RING, CLEANED AND RE-INSTALLEDSDR AALA201710059008Thermocouple · faultyDURING IDLE DESCENT, THE NR 1 ENGINE CARRIED BETWEEN 9 AND 15 PERCENT HIGHER N1 THAN THE NR 2 ENGINE AUTOTHROTTLE ON OR OFF, MADE NO DIFFERENCE. WHEN POWER WAS ADDED FOR LEVEL OFF, ENGINES MATCHED PERFECTLY. MAINTENANCE REPLACED THE NR 1 ENGINE FUEL THERMOCSDR AALA20170921002Probe · failedNR 2 ENGINE NOT PRODUCING FLEX POWER DURING TAKEOFF IN FLEX DETENT MOST POWER 1.2 EPR. MAINTENANCE REPLACED P2/T2 INLET PROBE IAW AMM 73-22-11. ACCOMPLISHED SATISFACTORY OPS CHECK. AIRCRAFT WAS GROUNDED.SDR AALA201709129025Oil Filter · cloggedNR 1 ENGINE MASTER CAUTION ALERT FOR A CLOGGED OIL FILTER. ACCOMPLISHED TSM 79-30-00 AND FOUND THE SCAVENGE OIL FILTER CONTAMINATED. REMOVED AND REPLACED THE NR 1 ENGINE SCAVENGE OIL FILTER, RAN ENGINE, LEAK AND OPS CHECKED IAW MM 79-22-44.SDR AALA201708239018Filter · cloggedDURING DESCENT, THE NR 2 ENGINE WOULD NOT COME BACK TO IDLE. AT IDLE, THE NR 1 ENGINE READS: FUEL FILTER 680, N1 41PERCENT, N2 71 PERCENT. THE NR 2 ENGINE READINGS: FUEL FILTER 1360, N1 57 PERCENT, N2 77 PERCENT.. REPLACED THE NR 2 ENGINE FUEL FILTER IAW AMMSDR AALA201708229004Engine · overspeedREJECTED TAKE OFF AT 100 KNOTS DUE TO THE FLIGHT CREW OBSERVING THAT THE N1 OVERSPEED LIMITS HAD BEEN EXCEEDED ON BOTH ENGINES. AIRCRAFT RETURNED TO GATE AND WAS REMOVED FROM SERVICE. . PERFORMED DOWNLOAD OF FDR AND ENGINEERING DETERMINED NO MAINTENANCE ACTSDR AALA201708229019Engine · overspeedREJECTED TAKE OFF AT 100 KNOTS DUE TO THE FLIGHT CREW OBSERVING THAT THE N1 OVERSPEED LIMITS HAD BEEN EXCEEDED ON BOTH ENGINES. AIRCRAFT RETURNED TO GATE AND WAS REMOVED FROM SERVICE. MAINTENANCE ACCOMPLISHED HIGH ENERGY STOP INSPECTION PER MCM 05-96-10. PERFOSDR AALA201708099017Thermocouple · faultyAIRCRAFT WAS NOT GROUNDED. NOTICABLE DIFFERENCE IN ENGINE PERFORMANCE. IDLE: 1 EPR (.91) 2 (.94), 1 ENGINE FF (760) 2 (1280). EGT 1 (422) 2 (407). N2 1 ENGINE (64.9 ) 2 (73.5). N1 1 ENGINE (30.3) 2 (41.2). AT 10000 SAT, SPEED 250 KDS. ECAM MAINTANENCE MESSAGE,SDR AALA201708109013Fuel Filter · faultyAIRCRAFT WAS NOT GROUNDED. NOTICEABLE DIFFERENCE IN ENGINE PERFORMANCE. IDLE: 1 EPR (.91) 2 (.94), 1 ENGINE FF (760) 2 (1280). EGT 1 (422) 2 (407). N2 1 ENGINE (64.9 ) 2 (73.5). N1 1 ENGINE (30.3) 2 (41.2). AT 10000 SAT, SPEED 250 KDS. ECAM MAINTENANCE MESSAGESDR AALA201708079022Engine · slowAIRCRAFT WAS NOT GROUNDED. WHEN THROTTLES ADVANCED FOR TAKE OFF THE NR 2 ENGINE WAS SLOW TO SPOOL CAUSING A LARGE YAW TO THE RIGHT. TAKE OFF WAS ABORTED BELOW 80 KNOTS. CREW REACCOMPLISHED CHECKLIST AND SUBSEQUENT TAKE OFF WAS UNEVENTFUL.SDR AALA201707319001Probe · failedLOSS OF THRUST ON CLIMB OUT PASSING 5000 FEET, LEFT ENGINE EPR AT 1.44 - EPR INSTANTLY (1 SECOND) WENT TO 1.42, THEN BACKTO CLIMB (1.44) PERFORMED NORMAL REST OF FLIGHT. MAINTENANCE ACCOMPLISHED MULTIPLE ENGINE TESTS. ACCOMPLISHED VIBRATION SURVEY TEST 8 IAWSDR AALA201707269037Fault Light · false activationMOMENTARY ECAM ENGINE STALL ALL PARAMETERS NORMAL. HIGH POWER ASSURANCE TEST ACCOMPLISHED, SYSTEM CHECKED NORMAL. NO FAULTS NOTED, AIRCRAFT RETURNED TO SERVICE. PERFORMED TASK 71-00-00-810-809-A AND 71-00-00-710-013C. AIRCRAFT WAS GROUNDED.SDR AALA201707069004Warning Message · false activationDURING CLIMB, ECAM DISPLAYED A NR 1 ENGINE BLEED FAULT MESSAGE. EMERGENCY DECLARED. RETURNED TO DEPARTURE. MAINTENANCE PERFORMED A BITE CHECK OF BMC 1 AND 2 IAW AMM 36-11-00-740-001-A. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.SDR AALA20170627013Pump · faultedREJECTED TAKE OFF AT 76 KNOTS, NR 2 ENGINE DID NOT ACHIEVE FULL POWER. N2 IDICATION TURNED RED, AMBER CAUTION LIGHT FLICKERED ON/OFF. NO ECAM MESSAGES DISPLAYED. MAINTENANCE REPLACED RIGHT ENGINE FUEL PUMP PER AMM 73-21-41. ACCOMPLISHED MCM 71-95-02 FOR RIGHT SDR AALA201706299020Fmu · faultedAIRCRAFT WAS GROUNDED. REJECTED TAKE OFF AT 76 KNOTS, #2 ENGINE DID NOT ACHIEVE FULL TOGA POWER. N2 IDICATION TURNED RED, AMBER CAUTION LIGHT FLICKERED ON/OFF. NO ECAM MESSAGES DISPLAYED. MAINTENANCE REPLACED RIGHT ENGINE FMU PER AMM 73-94-12. ACCOMPLISHED MCMSDR AALA201706279013Eec · faultedDIVERTED, EMERGENCY DECLARED. NR 2 ENGINE THRUST REVERSER FAULT AT FL300. REPLACED THE NR 2 ENGINE EEC IAW AMM 73-22-34-000-010-A. AIRCRAFT WAS GROUNDED.SDR AALA201706199024Filter · faultyRIGHT ENGINE IDLED 12 PERCENT HIGHER THAN LEFT AT IDLE POWER DURING DESCENT (36-48 PERCENT). ENGINES SURGED AFTER AUTOTHROTTLE DISCONNECT. MAINTENANCE REPLACED THE NR 2 ENGINE FUEL FILTER IAW 73-12-42. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. AIRCRAFTSDR GTIA2017060601969Seal · leakingDURING TAKEOFF ROLL, A SLIGHT OIL ODOR WAS IN THE CABIN AND COCKPIT. COM PROCEDURE WAS COMPLETED AND THE NR 2 PACK SHUT OFF FOR REMAINDER OF FLIGHT. PERFORMED TSM 05-50-810-831-A, FOUND THE NR 1 ENGINE DEOILER OVERBOARD VENT LEAKING OIL, R & R MATING RING &
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