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 AWXA200201205Warning Horn · false activationON TAKEOFF ROLL ENROUTE FOR SET N1 THRUST AT 80 KTS AND HEARD REPETITIVE "RETARD" OVER THE LOUD SPEAKER; REJECTED TAKEOFF AND RETURNED TO GATE. MAX SPEED INDICATED WAS 87 KTS. MAINTENANCE REVIEWED POST FLIGHT REPORT THAT INDICATED AIRCRAFT WENT FROM PHASE 2 TOSDR AWXA200201202Actuator · failedABORTED TAKEOFF, FLT 0045, REJECTED TAKEOFF AT APPROXIMATELY 50 KTS DUE TO NR 1 ENGINE COMPRESSOR VANE ECAM MESSAGE. MESSAGE FOLLOWED MOMENTARY SURGE OF NR1 EPR ABOVE FLEX THRUST TARGET. NO OTHER ANOMALIES NOTED, RETURNED TO GATE. REVIEWED THE LAST LOG REPOSDR AWXA200201194Battery Pack · dischargedDURING INSPECTION THE LEFT AFT DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT EMERGENCY POWER SUPPLY BATTERY PACK, OPERATIONAL CHECK WAS GOOD.SDR 2002FA0001286Seal · crackedSEAL REJECTED FOR CRACK AT 1 PLACE ON BACK WALL OF THE PILOT GROOVE SEAL AS MARKED ON THE PART.SDR 2002FA0001287Seal · crackedSEAL REJECTED AT FPI FOR VOID WITH LINEAR INDICATION ON SEAL LAND EXCEEDING 3X1 LIMIT.SDR DLM90021067Actuator · failedVSV ACTUATOR HEAD END SEPERATED FROM BODY OF ACTUATOR RESULTING IN LARGE FUEL LEAK. FOUND AT GATE PRIOR TO FLIGHT AFTER ENGINE CHANGE.SDR CA020913011Panel · delaminated(CAN) NR 1 ENGINE SUFFERED DAMAGE TO THE FRONT ANTI ICE IMPACT PANEL IN THE LOWER HALF OF THE FAN CASE. AFTER A FERRY FLIGHT TO A MAIN BASE THE DAMAGE WAS REPAIRED. A NUMBER OF DAYS LATER, THE SAME REPAIRED PANELS WERE FOUND DELAMINATED. ONE PANEL WAS REPAIRESDR AWXA200200755Smoke · detectedAFTER SHUTDOWN OF THE NR 2 ENG, EXCESSIVE SMOKE COMING FROM ENGINE.SDR AWXA200200753Tailpipe · fireAFTER ENG SHUTDOWN, RT TAIL PIPE FIRE, MOTORED ENG AND FIRE OUT. PERFORMED EXHAUST INSP & CHECK, NORM, ENG RUN ACCOMPLISHED, NORM SHUTDOWN. RETURN TO PHX, AT ENG SHUTDOWN, SMOKE COMING FROM NR 2. PERFORMED DYE PEN AND AND ENG RUN, COMPLETED, NO DEFECT NOTED.SDR AWXA200200745Line · crushedPREPARING TO TAKEOFF, WHEN STARTING TO APPLY TAKEOFF POWER PRIOR TO 1.05 EPR, THE NR 2 ENGINE MADE A COMPRESSOR STALL SOUND. IMMEDIATELY MOVED THRUST LEVERS TO IDLE AND ECAM INDICATED, ENGINE 2 COMPRESSOR VANE FAULT. EIGHT PASSENGERS ALSO REPORTED SEEING FLASDR AWXA200200718Engine · malfunctionedON TAKEOFF FROM FLL EN ROUTE FOR PHX NR 1 ENGINE HAD LOW EPR, EPR AT 1.32 CHARTED EPR WAS 1.40, ABORTED TAKEOFF. CONTRACT MAINTENANCE AT FLL PERFORMED TEST OF BOTH ENGINES, TESTS WERE NORMAL. PLACED NR 1 ENGINE ON MEL 73-20-04, COND. 1, EPR MODE INOP. MAINTENASDR AWXA200200742Actuator · leakingDTW - FIRE - FLT 0239 - WHILE AT GATE, POST FLIGHT, A FIRE OCCURRED AT THE NR 2 ENGINE ON SHUTDOWN, NO ECAM WARNING JUST A LOT OF SMOKE, PUSHED NR 2 ENGINE FIRE BUTTON DISCHARGING BOTH FIRE EXTINGUISHER BOTTLES, FIRE WAS PUT OUT. MAINTENANCE TROUBLESHOT PROBSDR AWXA200200675Scavenge Pump · leakingPHX - FLT 0536 - WHILE AIRCRAFT WAS TAXIING TO GATE, THE AIRCRAFT TAXIING BEHIND REPORTED SEEING A TAILPIPE FIRE AT NR 1 ENGINE TAILPIPE. MAINTENANCE PERFORMED A HOT SECTION BORESCOPE PER T/C 15M72304, NO DEFECTS WERE NOTED. AS A PRECAUTION THE NR 1 ENGINE SDR AWXA200200596Engine · fireFLT 0279 - AFTER LANDING AT IAH INBOUND FROM PHX, AFTER ENGINE SHUTDOWN AT GATE, GROUND CREW OBSERVED FIRE IN THE TAILPIPE OF THE NR 1 ENGINE. FLIGHT CREW MOTORED ENGINE APPROXIMATELY 1 MINUTE BEFORE FLAME EXTINGUISHED, ESTIMATE TAILPIPE FIRE LASTED TOTAL OF 2SDR CA020620001Duct · loose(CAN) CLIMBING THROUGH 18000FT, CSM ADVISED OF SMELL OF SMOKE IN CABIN. EMERGENCY DECENT, A/C RETURNED TO HER(GREECE) PASSENGERS COMMENTED THAT SIDE WALL PANELS AROUND ROW 25 - 30 WERE HOT. T/S REVEALED THAT CLAMP HOLDING APU BLEED DUCT HAD COME LOOSE, ALLOWINSDR AWXA200200515Fire · detectedPHX - TAILPIPE FIRE - FLT 0192 - RAMP PERSONNEL REPORTED A BRIEF TAILPIPE FIRE IN NR 2 ENGINE AFTER SHUT DOWN. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE NR 2 ENGINE TAILPIPE PER MM 78-10-00-06, NO DAMAGE OR DEFECTS NOTED.SDR CA020628003Coffeemaker · burned(CAN) AT FLT.LEVEL 35000FT IN CRUISE, CABIN CREW & PASSENGERS NOTICED SMOKE IN FWD GALLEY AREA.CABIN CREW PULLED GALLEY CB'S AND NOTIFIED FLIGHT CREW WHO IN TURN PULLED MAIN GALLEY SUPPLY BREAKERS. A/C DIVERTED INTO SDL (AMSTERDAM) ON FURTHER INSPECTION NR 2SDR AWXA200200337Anti-Ice Valve · closedYKM - DIVERSION - EN ROUTE FROM PHX TO SEA LT ENGINE ANTI-ICE VALVE CLOSED, ECAM WARNING OCCURRED AFTER SELECTION OF ANTI-ICE TO ON. TRIED VARIOUS POWER SETTINGS UP TO FULL CLIMB POWER TO OPEN THE ANTI-ICE VALVE, ATTEMPTS WERE UNSUCCESSFUL, DUE TO ICING CONDISDR AWXA200200265Seal · leakingPHX - AIR TURNBACK - FLT 0001 - ON CLIMBOUT FROM PHX EN ROUTE TO ORD LT ENGINE OIL PRESSURE INDICATED 300 PSI, AIRCRAFT TURNED BACK TO PHX. MAINTENANCE TROUBLESHOT THE HIGH OIL PRESSURE INDICATION PER AWA ER 26-7920-02091-KL1, THE DIFFERENTIAL PRESSURE TRANSDSDR CA020308002Pump · failed(CAN) DURING INITIAL ROLL AT 1.2 EPR THE ECAM MESSAGE "COMP VANE NR 2" APPEARED ON THE UPPER ECAM SCREEN. THE ENGINE EXPERIENCED A LIGHT COMPRESSOR STALL. THE TAKE-OFF WAS REJECTED AT 50 KTS AND THE AIRCRAFT RETURNED TO THE GATE WITH BOTH ENGINES RUNNING. MAINSDR CA020204001Hose · ruptured(CAN) LOST HYDARULIC QUANTITY IN GREEN SYSTEM AND LOW PRESSURE WARNING ON ENGINE 1 HYDRAULIC SYSTEM(GREEN). CREW SWITCHED OFF THE EDP AND PTU AT FIRST INDICATION OF FLUID LOSS AND USED THE EMERGENCY FREE FALL GEAR EXTENSION HANDLE. MAINTENANCE FOUND A RUPTUREDSDR CA020118006Handle · malfunctioned(CAN) AT APPRXIMATELY 10,000 FT ALTITUDE THE FWD CARGO DOOR INDICATED UNSAFE ON ECAM. THE AIRCRAFT DIVERTED AND WAS INSPECTED BY A COMPANY ACA. THE DOOR HANDLE WAS FOUND TO BE OUT OF THE DETENT BY ABOUT 1/4 OF AN INCH. THE HANDLE ASSY AND DOOR LOCKING MECHANISSDR CA020109008Brake · overheated(CAN) SHORTLY AFTER POWER WAS APPLIED AT TAKEOFF, BOTH BRAKE TEMPERATURE INDICATIONS ON LEFT SIDE EXCEEDED 300 DEG.C, FLIGHT CREW REJECTED TAKEOFF. MAX BRAKE TEMP INDICATION ON LEFT SIDE WAS 610 DEG.C. BRAKES STARTED TO SMOKE. REJECTED TAKEOFF INSPECTION SDR MZA2002F00000Sensor · failedAFTER ROTATION LANDING GEAR HANDLE COULD NOT PHYSICALLY BE MOVED. ECAM 4G SHOCK ABSORBER FAULT. FOUND LGCIV AND GROUND PROX. SENSOR BAD.SDR AWXA200100512Nipple · loosePHX - ENG FIRE/SMOKE - FLT 14 - "C" - AFTER LANDING, WHEN TAXING OFF RUNWAY, ECAM MESSAGE APPEARED, NO. 2 ENG. FIRE AND CREW SHUTDOWN #2 ENG. OVERHEAD #2 FIRE PUSHBUTTON DID NOT ILLUMINATE. ALL ENG PARAMETERS WERE NORMAL, SMOKE WAS OBSERVED BY THE FIRE DEPT FRSDR CA010823005Tire · deflated(CAN) L/H NOSE WHEEL ASSEMBLY DEFLATED DURING TAXI TO GATE. MECHANICS ON SITE NOTED, OVER PRESSURE VALVE WAS LOOSE WHICH CONTRIBUTED TO THE LOSS OF PRESSURE IN THE TIRE. L/H AND R/H NOSE WHEEL ASSEMBLIES WERE CHANGED.SDR AWXA0001966Turbine · damagedSEA - ENGINE FAILURE - DIVERTED FLIGHT. EN ROUTE FROM YVR TO PHX THE NR 2 ENGINE EXCEEDED EGT LIMITS FOLLOWED BY ENGINE STOPPAGE. THE AIRCRAFT DIVERTED TO SEA MAKING AN UNEVENTFUL LANDING. IN SEA THE ENGINE WAS INSPECTED AND FOUND TO HAVE EXTENSIVE TURBINE SDR 20010612CW002Seal · crackedPART REJECTED A F.P. I. FOR LINEAR INDICATIONS ON BOSSES.SDR 20010511CW003Seal · crackedPART RECEIVED FOR PENETRANT INSPECTION. PART REJECTED AT PENETRANT INSPECTION FOR INDICATION IN COUNTERBORE.SDR AWXA0001598Fmu · failedSEA - ABORTED TAKEOFF - 4/2/01 - NR 2 ENGINE FLAMEOUT. ON TAKEOFF AFTER SETTING TAKEOFF POWER AND ABOUT 60 KTS THERE WAS A SURGE ON NR 2 ENGINE AND IT SHUT DOWN; THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. THE POST FLIGHT REPORT FAULTED THE NR 2 ENGINSDR CA010426008Terminal Block · melted(CAN) THE FORWARD GALLEY OVENS WERE FOUND TO BE INOPERATIVE BY THE FLIGHT ATENDANTS ON THE FLIGHT. THE ENGINEERS TROUBLESHOOTING THE DEFECT FOUND FWD GALLEY FEEDER D BREAKER POPPED. FURTHER INVESTIGATION FOUND TERMINAL BLOCK 2752VT STUD 8 MELTED, AND THE TERMISDR 20010504CW003Seal · crackedPART REJECTED AT PENETRANT INSPECTION FOR INDICATIONS AS MARKED ON AREA ADJACENT TO BOSS.SDR AWXA0001451Fire Loop · chafedPHX - AIR TURNBACK - 2/22/01 - DURING CLIMB THE CREW GOT A CLASS I ECAM MESSAGE, ENG 2 FIRE DET FAULT AND RETURNED TO PHX. IN PHX MAINTENANCE FOUND THE NR 2 ENG LOWER CORE FIRE LOOP CHAFED; THE LOWER CORE FIRE DETECTOR ASSY WAS REPLACED AND FUNCTIONALLY CHECKSDR 20010504CW002Seal · crackedPART REJECTED AT PENETRANT INSPECTION FOR INDICATIONS AS MARKED ON BOTTOM OF PART (SIDE OF BOSS).SDR AWXA0001281Fmu · malfunctionedPHX - AIR TURNBACK - 2/3/01 - DURING INITIAL CLIMB, LEFT ENG UNCOMMANDED THRUST INCREASE ABOVE CLIMB EPR LIMIT WITH DEFINITE YAW TO THE RIGHT; EVENT WAS MOMENTARY AND LEFT EPR WAS NOTICED DECREASING THRU 1.5 BACK TO CLIMB EPR OF 1.3, OTHER PARAMETERS NORMAL. SDR AWXA0001282Resolver · malfunctionedMAINTENANCE TROUBLESHOT IAW TSR 73-22-00-810-851 AND IAE TELEX; CELL CODE FAULT OF 59 ON FMU/HC/EEC 1 MESSAGE; (WFXCF) FUEL FLOW RESOLVER FAULT; CH B ON CONNECTOR J8 HAD HIGH RESISTANCE OF 104 OHMS BETWEEN PINS I & J (NORM: 15-78 OHMS); WIRING CHECKED GOOD; RASDR 20010312CW003Seal · crackedPART RECEIVED FROM REPAIR STATION FOR PENETRANT INSPECTION. PART REJECTED 2ND TIME AT PENETRANT INSPECTION FOR INDICATIONS AS MARKED IN RADIUS ADJACENT TO MACHINED FACES OF OIL PASSAGES.SDR 20010312CW004Seal · crackedPART RECEIVED FOR PENETRANT INSPECTION. PART REJECTED AT PENETRANT INSPECTION FOR TWO INDICATIONS AT BOTTOM OF COUNTERBORES ON ID OF PART.SDR 20010312CW005Seal · crackedPART RECEIVED FOR PENETRANT INSPECTION. PART REJECTED AT PENETRANT INSPECTION FOR INDICATIONS AS MARKED IN RADIUS ADJACENT TO MACHINED FACES OF OIL PASSAGES.SDR 20001214SH014Seal · crackedPART RECEIVED FROM WESTFIELD GAGE CO (WESTFIELD GAGE REPAIR STATION NR WNFR711K) FOR FPI IAW IAE V2500 PROPULSION SYSTEM ENGINE MANUAL, REV 45, SECT 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501. PART REJECTED AT FPI DUE TO A CRACK ON THE OUTSIDE DIAMESDR 20001212SH010Seal · crackedPART RECEIVED FOR FPI IAW IAE V2500 PROPULSION SYSTEM ENGINE MANUAL, REV 45, SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501. PART REJECTED AT FPI DUE TO CRACKS IN TWO AREAS ON OUTSIDE DIAMETER OF PART. (X)SDR 20001212SH011Seal · crackedPART RECEIVED FOR FPI IAW IAE V2500 PROPULSION SYSTEM ENGINE MANUAL, REV 45, SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501. PART REJECTED AT FPI FOR CRACKS IN TWO AREAS ON OUTSIDE OF PART. (X)SDR 20001129SH003Seal · crackedPART RECEIVED FOR FLUORESCENT PENETRANT INSPECTION IAW IAE V2500 PROPULSION SYSTEM ENGINE MANUAL, REV 44, SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501. PART REJECTED AT FPI DUE TO TWO CRACKS ON OUTSIDE DIAMETER OF PART (AREAS MARKED ON PART). SDR 20001101SH028Seal · crackedPART RECEIVED FOR PENETRANT INSPECTION IAW THE IAE V2500 PROPULSION SYSTEM ENGINE SYSTEM MANUAL, REV 44, SECT 70-23-01, TASK 70-23-01-230-501. PART REJECTED DUE TO CRACKS ON TOP SURFACE. (X)SDR 20001011AP015Eec · inoperativeFLT 8169 - DECLARED AN EMERGENCY AIR TURN BACK IN CUN, ENGINE NR 1 HAD STALL INDICATION ON ELECTRONIC CENTRALIZED AIRCRAFT MONITORING, ENGINE WOULD SURGE. REPLACED ELECTRONIC ENGINE CONTROL. PERFORMED FULL AUTHORITY DIGITAL ENGINE CONTROL OPERATIONS TEST ANDSDR 20000524SH008Seal · crackedPART RECEIVED FROM WESTFIELD GAGE (WNFR711K) FOR FPI PER V2500 ENGINE MANUAL REV 42, SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501). PART REJECTED AT FPI DUE TO A CRACK, 0.180 INCH ON TOP SURFACE,SDR 20000524SH009Seal · crackedPART RECEIVED FROM WESTFIELD GAGE (WNFR711K) FOR FPI PER V2500 ENGINE MANUAL REV 42, SECTIO 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501). PART REJECTEDAT FPI DUE TO A CRACK 0.325 INCH ON TOP SURFACE. (X)SDR 20000524SH002Seal · crackedPART RECEIVED FROM WESTFIELD GAGE (WNFR711K) FOR PENETRANT INSPECTION PER V2500 ENGINE MANUAL SECTION 70-23-01, TASK 70-23-01-230-501, INSPECTION CHECK-01. PART REJECTED AT PENETRANT INSPECTION DUE TO A CRACK ON OUTSIDE TOP OF PART APPROXIMATELY .250 INCH LOSDR 20000517SH003Bearing · spalledENGINE REMOVED FOR ''''PERFORMANCE DETERIORATION''''. THE NR 4 BEARING EXHIBITED AXIAL SCORING OF THE ROLLERS AND OUTER RACE. MINOR FATIGUE SPALLING WAS PRESENT AT THE DAMAGE SITES ON BOTH THE RACE AND ROLLERS. INVESTIGATION IS IN PROGRESS AT GE ENGINE SERVSDR 20000517SH004Bearing · making metalENGINE WAS REMOVED FOR ''''''''METAL IN NR 4 MCD''''''''. THE NR 4 BEARING EXHIBITED A REGION OF FATIGUE BREAK-UP ON THE OUTER RACE. INVESTIGATION IS IN PROGRESS AT GE ENGINE SERVICES - DALLAS. (X)
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