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 = 'V2500A1' 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 = 'V2500A1' 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 2026FA0000291Case · unserviceableIBERIA MAINTENANCE HAS RECEIVED A NOTIFICATION FROM AN EXTERNAL REPAIR STATION (FAA DLAY225D LUFTHANSA TECHNIK AG (“LHT”) TO INFORM OF AN OCCURRENCE STATING THAT A NUMBER OF INDIVIDUAL COMPONENTS WERE IDENTIFIED WHERE A FINAL, FULL FLUORESCENT PENETRANT INSPSDR 2025FA0000822Unknown · unknownTHE PARTS RECORDED UNDER EASA FORM 1 TRACKING NR 44543 AND 44538 HAVE BEEN DETECTED AS SUSPICIOUS. DISCREPANCY ON MISSING SIGNATURE, (SECTION 14B), APPROVAL/CERTIFICATE NO (SECTION 14C) AND ORGANIZATION NAME AND ADDRESS (SECTION 4) HAVE BEEN DETECTED. AUTHORISDR CALA2024083000519Engine · unknownREJECTED TAKE OFF AT 60 KNOTS. ON T/O ENGINES DI D NOT COME UP T OGETHER A ND WERE SPLIT AT FLEX UPON ARRIVAL TO COCKPIT, NO STATUS MESSAGE WAS PRESENT. PRINTED A PFR. FOUND FAILURE "DMC2: NO ADF1 DATA" AND "DMC3: NO EEC2B DATA SOURCE EIS 3 AT 01:31 GMT ( SAMESDR CALA2022112803241Module · damaged*EMERGENCY DECLARED* BIRDSTRIKE ENG 2 ENGINE #2 SN V10989 HAD BIRDSTRIKE ON TAKEOFF. ONLY PARAMETERS CHANGE WAS VIBRATION. ENGINE WAS NOT SHUTDOWN, BROUGHT BACK TO IDLE UNTIL LANDING. TRANSFERRED TO OFF #2 ENG SN V10989 AC 8802 LP3191823. ONLY PARAMETERS CHASDR CALA2022112503227Drain Line · damagedPDA 3 ENGINE #1 ZONE F DRAIN TUBE, APPROXIMATELY 8 INCHES, MISSING FROM AIRCRAFT. INSTALLED LH ZONE F DRAIN TUBE. REF AMM 54-51-29.SDR CALA2022112103193Harness · failedENG 2 EGT OVERTEMP ONT/O ROLL.TEMP APROX 890C 77-20-00-810-802-B. TOMC-MEREDITH UPDATED MAA CODE FIX USING VENDOR MAA SCREEN CREW REPORTED LOW SPEED ABORTED TAKEOFF AND EGT INDICATION POST FLIGHT REPORTS. SEE ATTACHED PICTURES. PLEASE CONTACT TOMC BEFORE COMMESDR CALA2022103102993Actuator · fault messageCOMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. - ENG ENG 1 ON INITIAL TO ROLL PERFORMED FADEC 1A&B BITE AND FOUND CHA AND CHB VSV ACT/HC/EEC1 REMOVED #1 ENG VSV ACTUATOR AS PER AMM 75-32-41-000-010-A. INSTALLED VSV ACTUATOR PER AMM 75-32-41-400-010..NEED TO PSDR CALA2021100601806Engine · none4285-2 ESN V10979 DUE TO IFSD ACCOMPLISH WINDMILL INSPECTION PER AMM 72-00-00-200-021 4.A.(2)(B). REPORT FINDINGS TO TOMC EMC. FLAGGING SDR FOR FLT 2369-01 PERFORMED WINDMILL INSPECTION PER AMM 72-00-00-200-0214. A (2) (B), REPLACED MAIN PUMP OIL FILTER AND SCSDR YENA2020121700606Engine · vibrationFLT 280, PBI-BOS. RETURNED TO FIELD. ABNORMAL AIRFRAME VIBRATION ON CLIMBOUT THROUGH FL250 UP TO LEVEL OFF AT FL310. ENGINE 2 N1 VIB 1.8, ENGINE 1 N1 BIV .4. FELT MORE LIKE FLT CONTROL FLUTTERING. NO ABNORMAL ECAMS. HYD, FLT CONTROLS READ NORMAL. SUPPLESDR AALA202011149001Beam · crackedAIRCRAFT IN BASE MAINTENANCE. NR 1 ENGINE PYLON AFT BEAM HANGER IS CRACKED. REPLACED NR 1 ENGINE PYLON AFT INBOARD HANGER BEAM, PER AMM 54-51-17.SDR AALA202011149002Beam · crackedAIRCRAFT IN BASE MAINTENANCE. NR 1 ENGINE PYLON CENTER INBOARD BEAM HANGER IS CRACKED. REPLACED NR 1 ENGINE PYLON CENTER INBOARD HANGER BEAM, PER AMM 54-51-17.SDR AALA202011149003Beam · crackedAIRCRAFT IN BASE MAINTENANCE. NR 1 ENGINE PYLON AFT OUTBOARD BEAM HANGAR IS CRACKED. REPLACED NR 1 ENGINE PYLON AFT OUTBOARD BEAM HANGER, PER AMM 54-51-17-401.SDR AALA2019120549008Actuator · faultyAIRCRAFT WAS GROUNDED: PILOT REPORTS APPLIED T/O POWER ENG 2 COMPRESSOR VANE FAULT. EXIT RWY AND SHUTDOWN. CLASS 2 MESSAGE, ENGINE 2 FADEC. MAINTENANCE PERFORMED REMOVAL AND INSTALLATION OF ENGINE 2 VSV ACTUATOR IAW JOB CARD 26T40075005 AND 26L00071014. OKAY FSDR YENA2019120280685Relay · failedFT # 1416, LGB-AUS. RETURNED TO FIELD. ENG 2 EPR MODE FAULT ON CLIMBOUT; R & R RELAY BOX 4100KS ENG #2 AS PER AMM 71-51-49. IDLE RUN NO FAULT BITE PASS.SDR GTIA2016072101511Seal · leakingODORIN CABIN AND COCKPIT DURING TAXI IN ON NR 1 ENGINE, COCKPIT CREW SMELLED EXHAUST FUMES, ASKED FA'S ABOUT ODORS. THEY ALL SAID THEY SMELLED ODORS OF MUSTY, DIRTY SOCKS. THE 2 AFT F/A'S THEN SAID THAT DURING CLIMBOUT, THERE WAS A MUSTY ODOR. DE-BRIEFED CAPSDR GTIA2016070101497Packing · leakingAFT F/A REPORTS BURNING RUBBER ODOR IN CABIN. ODOR DISAPPEARED ONLY WHEN NR 2 BLEED CLOSED. RAN NR 1 & 2 ENGINES WITH BOTH PACKS ON AND CYCLED BOTH ENGINE BLEEDS. NO ODOR NOTICED AT THIS TIME. AFTER SHUTTING DOWN ENGINES, NOTICED EXCESSIVE POOLING OF OIL SDR USAA2014080400012Door · looseON REACHING LEVEL OFF AT 35000 FT, NR 1 ENGINE VIBRATION EXCEEDED 5.0 N1, IT REACHED A MAXIMUM OF 6.2. REDUCED POWER TO KEEP VIBRATION BELOW 5.0 IAW TSM 77-30-00-810-826A. FOUND NR 1 ENG OIL SERVICE DOOR LOOSE & HAS PLAY. REPLACED ENGINE OIL SERVICE DOOR &SDR IU5R2014032800001Fuel Nozzle · crackedDURING INVESTIGATION ON FUEL NOZZLES IAW CMM 73-13-41. ENGINEERING REVIEW PRIOR REPAIR CONDITIONS OF CIRCUMFERENTIAL CRACKS, CC ON THE OUTER AIR SWIRLER, OAS, SIDE OF EB WELD JOINT TO THE END CAP BAFFLE, ECB, IT WAS APPARENT BY OAS ADJACENT MATERIAL CONDITIONSDR USAA2013121600018Unknown · odorFLT 657, VERY STRONG ODOR IN CABIN MAKING FLIGHT ATTENDANT ILL WITH RESPIRATORY IRRITATION. COMPLIED WITH JOB CARD 26L00021001 TROUBLE SHOT CABIN AIR QUALITY. FINDINGS ARE IN COMPLIANCE WITH JOB CARD.SDR USAA2013121600015Actuator · inoperativeNR 1 ENGINE FAILURE AND SHUTDOWN ON DESCENT INTO IAH. RELIGHT ATTEMPTED, UNSUCESSFUL AND ENGINE SECURED FOR LANDING. PERFORMED IAW A320 TSM 71-00-00-810-808-A. REPLACED E1 VSV ACTUATOR, REPLACED 10TH STAGE SOLENOID VALVE.SDR USAA2013121300011Vane · faultedNUMBER 1 ENG COMPUTER VANE FAULT. VSV LUBE & FORCE CHECK PERFORMED IAW JOB CARD 26T40075001. ADDITIONAL TROUBLESHOOTING BEING ACCOMPLISHED IAW A320 TSM TASK 75-30-00-810-821-A. SUPPLEMENTAL TO FOLLOW FINAL CORRECTIVE ACTION.SDR USAA2013022200001Engine · vibrationIN CRUISE FL 340 NR 2 N1 VIRBRATION BRIEFLY EXCEEDED 5 UNITS, THRUST REDUCED TO KEEP VIBRATION BELOW 5. VIBRATION LEVELS RETURNED TO NORMAL AT 11-12 THOUSAND FEET. PERFORMED VIBRATION SUMMARY, NO DEFECTS NOTED, INSPECTED FOR FOD DAMAGE, NONE FOUND, INSPECTEDSDR USAA2012022800009Solenoid Valve · faultyREJECTED TAKEOFF AT 70-80 KNOTS DUE TO ENGINE 1 SYSTEM FAULT AND APPROX 645 EGT. AIRCRAFT HAD ANOTHER REJECTED TAKEOFF ON THE SAME FLIGHT JUST PRIOR TO THIS TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE HPC STAGE 10 SOLENOID VALVE (4023KS) IAW AIRBUS MAINTENSDR USAA2012011700023Pump · failedENGINE NR 2 MOMENTARILY FAILED DURING IDLE DESCENT AT FL200, 280 KNOTS. CREW FELT AIRCRAFT YAW AND REPORTED N2 AT APPROXIMATELY 30 PERCENT. UPON IGNITION ACTIVATION, ENGINE RELIT ITSELF AND CONTINUED TO OPERATE NORMALLY. MAINTENANCE REMOVED AND REPLACED THESDR USAA2012011000022Actuator · failedUPON THRUST REDUCTION TO CLIMB, NR 2 ENGINE HAD TWO COMPRESSOR STALLS BEFORE THRUST LEVER COULD BE MOVED TO IDLE. EGT EXCEEDED LIMITS; ENG 2 FAIL ON ECAM. NR 2 ENGINE WAS SHUTDOWN IAW ECAM ACTIONS, FIRE BOTTLE WAS DISCHARGED AND AIRCRAFT DIVERTED, (EMERGENCYSDR USAA2012061900022Actuator · failedUPON THRUST REDUCTION TO CLIMB, NR 2 ENGINE HAD TWO COMPRESSOR STALLS BEFORE THRUST LEVER COULD BE MOVED TO IDLE. EGT EXCEEDED LIMITS; ENG 2 FAIL ON ECAM. NR 2 ENGINE WAS SHUTDOWN IAW ECAM ACTIONS, FIRE BOTTLE WAS DISCHARGED AND AIRCRAFT DIVERTED TO LAX, (EMSDR USAA2012010400021Transducer · failedAFTER TAKEOFF PRIOR TO 1000', ENGINE NR 1 SURGED TWICE AND SELF-RECOVERED WITH NORMAL INDICATIONS. ON LANDING ROLLOUT, RECEIVED ECAM MESSAGES FOR ENG 1 COMPRESSOR VANE AND FADEC MX. TWO SUBSEQUENT EVENTS FOR NR 1 ENGINE SURGE ON TAKEOFF ON 1/3/12 AND 1/4/12.SDR USAA2011090600025Pressure Switch · defectiveCREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM ON DESCENT INTO PDX. CONDUCTED GRAVITY EXTENSION OF LANDING GEAR AND DECLARED AN EMERGENCY; PASSENGERS WERE NOT INSTRUCTED TO BRACE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP IAW AIRBUS MAINTENANSDR USAA2011090600028Pump · defectiveCREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM ON DESCENT INTO PDX. CONDUCTED GRAVITY EXTENSION OF LANDING GEAR AND DECLARED AN EMERGENCY; PASSENGERS WERE NOT INSTRUCTED TO BRACE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP IAW AIRBUS MAINTENANSDR EE4Y20110382Strap · wornENGINE NR 2, FAN COWL, AIR INTAKE COWL, CAPPING STRAP UPPER AREA LT AND RT CORNERS WITH WEAR. NOTE: THE CAPPING STRAP WEAR REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.SDR EE4Y20110384Fitting · crackedENGINE NR 1, PYLON AFT FIXED FAIRING, LOWER FWD SUPPORT FITTING WITH CRACK. MAJOR REPAIR IAW SRM.SDR USAA2011032591231Compressor Blade · damagedFLT 51 - PHX - RTO - ON TAKEOFF ROLL AT ABOUT 110 KNOTS, CREW REPORTED A LOUD BANG AND THE AIRCRAFT VEERED SHARPLY TO THE RIGHT - TAKEOFF WAS REJECTED. PASSENGERS REPORTED SEEING FLAMES COMING OUT OF THE RIGHT ENGINE. MAINTENANCE FOUND NR 2 ENGINE HIGH PRESSDR USAA2011031491044Actuator · stalledFLT 88 - CREW REPORTED NR 1 ENGINE COMPRESSOR STALL ON CLIMB WITH MAX EGT 720+ FOR ONE MINUTE. SHUT DOWN ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. THE ROOT CAUSE WAS IDENTIFIED AS THE VSV ACTUATOR WHISDR USAA2010092392080Lanyard · frayedL2 DOOR SLIDE YELLOW COVER TIE CORDS FRAYED IN SVERAL SPOTS. REPLACED L2 DOOR SLIDE.SDR USAA2009090892391Filter · contaminatedFLT 128 - PHX - CABIN ODOR - NR 1 ENGINE IS PUTTING OILY SMELL IN THE AIRCRAFT - SMELLS LIKE DIRTY SOCKS. IT'S NOT BEING FILTERED OUT AND FLIGHT ATTENDANTS ADVISED SMELL IS REALLY BAD IN BACK OF AIRCRAFT. MAINTENANCE PERFORMED COMPRESSOR WASH AND REPLACED RESDR USAA2009090892404Filter · contaminatedFLT 128 - PHX - CABIN ODOR - NR 1 ENGINE IS PUTTING OILY SMELL IN THE AIRCRAFT - SMELLS LIKE DIRTY SOCKS. IT'S NOT BEING FILTERED OUT AND FLIGHT ATTENDANTS ADVISED SMELL IS REALLY BAD IN BACK OF AIRCRAFT. MAINTENANCE PERFORMED COMPRESSOR WASH AND REPLACED RESDR USAA2009090892405Filter · contaminatedFLT 128 - PHX - CABIN ODOR - NR 1 ENGINE IS PUTTING OILY SMELL IN THE AIRCRAFT - SMELLS LIKE DIRTY SOCKS. IT'S NOT BEING FILTERED OUT AND FLIGHT ATTENDANTS ADVISED SMELL IS REALLY BAD IN BACK OF AIRCRAFT. MAINTENANCE PERFORMED COMPRESSOR WASH AND REPLACED RESDR USAA2009081892154Engine · bird ingestionFLT 407 PHX-ATL - DIVERSION / BURNING SMELL - DIVERTED INTO MEMPHIS DUE TO STRONG BURNING PLASTIC SMELL IN CABIN THROUGHOUT CLIMB AND INTO CRUISE. MAINTENANCE FOUND EVIDENCE OF BIRD INGESTION IN NR 1 ENGINE ON STAGE 3 HIGH PRESSURE COMPRESSOR. PERFORMED COMPSDR USAA2009062491571Bottle · lowEMERGENCY EGRESS SYS - R-2 DOOR ASSIST BOTTLE NEEDS SERVICING. MX SERVICED R-2 DOOR ASSIST BOTTLE IAW MM 52-10-00-614-001. (K)SDR USAA2009062291536Unknown · unknownREJECTED TAKEOFF AT 80 KTS DUE TO THRUST ASYMMETRY - LT INDICATION 1.390 RT 1320 - NO THRUST ASYMMETRY FELT IN LATERAL CONTROL INPUTS, ECAM WARNING. MX REPORTED ALL PARAMETERS NORMAL - NO MESSAGES AND NO SUBSEQUENT ISSUES TO DATE. (K)SDR USAA2009042891000Blade · separatedFLT 500 YYC-PHX - COMPRESSOR STALLS - NR 2 ENGINE EXPERIENCED TWO RAPID COMPRESSOR STALLS CLIMBING THROUGH FL340 IN SMOOTH AIR, VCM. TEMPORARILY LOST POWER. ENGINE QUICKLY SELF RECOVERED. NO LIMITS EXCEEDED. ENGINE CONTINUED NORMAL POWER THEREAFTER. RAN 3SDR USAA2009030290477Blade · failedFLT 180 - WHILE CLIMBING THROUGH 23,000 FT THE FLIGHT CREW FELT 6 TO 12 STRONG JOLTS AND RECEIVED ECAM MESSAGES "NUMBER 1 ENGINE FAIL" THEN "NUMBER ONE ENGINE STALL". THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO MCI FOR MAINTENANCE. COMPLIED WITH (DSDR GTIA0900006Floorbeam · corrodedFR68 - FR70 FLOORBEAM CORRODED AT Y765.SDR USAA920080920Bleed Valve · inoperativeFLT NR 455 PHX-SLC - ATB - ON CLIMB-OUT AT ABOUT 7500 FT, CREW REPORTED TWO AUDIBLE LOUD BOOMS FROM THE NR 1 ENGINE. NO ECAM WARNINGS CAME UP. REDUCED POWER TO IDLE, ALL PARAMETERS REMAINED NORMAL INCLUDING OIL PRESSURE AND TEMPERATURE. AIRCRAFT RETURNED TOSDR USAA920071255Metering Unit · faultyFLT NR 9205 - TPA-PHX - IFSD - LEVEL OFF AT 5000' ON APPROACH TO PHX, RIGHT ENG DID NOT RESPOND TO AUTOTHRUST. ENGINE INDICATIONS WERE LESS THAN IDLE. PERFORMED ECAM ACTIONS TO SHUT DOWN NR 2 ENGINE. FUEL CONTROL DID NOT RESPOND TO NR 2 ENG MASTER. PUSHED SDR GTIA200700017Power Supply · no test14WL EMERGENCY LIGHTING SYSTEM POWER SUPPLY UNIT FAILED TEST. REPLACED SAME.SDR AWXA200700720Engine · flamed outEWR - PHX - IFSD - CREW REPORTED HEARING A "BANG" FOLLOWED BY THE NR 1 ENGINE SHUTTING DOWN. CREW INITIATED AN IN-FLIGHT RESTART OF THE NR 1 ENGINE, ENGINE STARTED AND UPON APPLICATION OF POWER ANOTHER BANG WAS HEARD FOLLOWED BY THE NR 1 ENGINE SHUTTING DOWN.SDR YENA2007019A/C Pack · odorAPRX 1645Z, NO VISIBLE SMOKE (BURNING RUBBER SMELL) DURING APPROACH QRH COMPLIED WITH MID CABIN. EMERGENCY DECLARED. SMELL SUBSIDED UPON EXITING TAXIWAY. EVACUATION WAS DEEMED NOT REQUIRED. PERFORMED TROUBLESHOOTING IAW TSM 24-00-00-810-823 AND TSM 23-39-00-81SDR AWXA200700390Engine · fireLAS - ESD - CREW REPORTED DURING CLIMB THEY HEARD A LOUD BANG FOLLOWED BY A RISING EGT INDICATION ON THE RIGHT ENGINE. THE FLIGHT ATTENDANTS REPORTED SPARKS AND FLAMES COMING FROM THE RIGHT ENGINE. THE ENGINE SHUT DOWN AND THE CREW DISCHARGED THE FIRE BOTTLESDR AWXA200601837Fuel Control · failedFLIGHT 430: PHL - LAS - DURING CRUISE AT FL340, ECAM MESSAGE. ENGINE NR 1 FUEL CONTROL FAULT APPEARED ON ECAM. NR 1 ENG THRUST HAD RETARDED TO IDLE, ALL OTHER PARAMETERS NORMAL. ECAM MESSAGE ENG FAIL APPEARED AND ENGINE SHUT DOWN. ACCOMPLISHED ENG NR 1 REL
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