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 = 'CF680A2' 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 = 'CF680A2' 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 DL76S020915Duct · wornAIR TURN BACK RT ENG OVERHEAT MSG AFTER TAKEOFF. FOUND 8TH STAGE DUCT SEPERATED ON NO.2 ENG. REPLCD DUCT BETWEEN CK VLV AND PRECOOLER.SDR DL76S020671Smoke · detectedAFTER T/O SMOKE IN MID CABIN WITH SMOKE DETECTOR GOING OFF IN MID CABIN. RETURNED TO LAND. LT PACK TRIPPED AND LT ENG BLEED LIGHT ILLUMINATED. ON GROUND SMOKE DISSIPATED. COMPRESSOR WASH NUMBER 1 ENGINE. AFTER WASH - RUN ENG 5 MINS AT IDLE, RUN PACKS/CYCLSDR DL76S020611Engine · unserviceableON TAKE OFF ROLL ABOUT 130 KIAS, LEFT ENGINE TEMP WENT TO 975, PULLED THROTTLE BACK TO KEEP WITHIN LIMITS, CONTINUED TAKE OFF AT 150 AGL, LEFT ENGINE ROLLED BACK TO IDLE AND TEMPWENT TO 1100. POWER CAME BACK TO IDLE AND RETURNED TO FIELD.THE ENGINE WAS NOT SSDR DL767021295Connector · shortedNR 2 ENG INFLT SHUTDOWN RT OIL FILTER LIGHT CAME ON. FOUND SHORT BETWEEN D4254P AND D4258J. REPLACED PLUG D4258J. SYSTEM CHECKS NORMAL.SDR DL76S020512Engine · failedENGINE STALLED ON TAKEOFF WITH EGT EXCEEDING REDLINE. NR 2 ENG REPLACED.SDR DL76S020446Idg · lack of lubeLT GEN DRIVE EICAS MESSAGE ILLUMINATED WHEN TAKEOFF POWER APPLIED. LIGHT WENT OUT WHEN THROTTLES RETURNED TO IDLE. TAKEOFF ABORTED BELOW 80 KTS. SERVICED IDG, RAN NR 1 ENG, PUT GEN ONLINE, LOADED GEN TO .67 PERCENT VOLTS AND FREQS CHECK NORMAL. OIL TEMP NOSDR DL76S020409Bolt · loosePILOT REPORT, SUSPECTED FUEL LEAK RIGHT ENGINE FUEL FLOW NORMAL IN FLIGHT -5700PPH, NO VISUAL LEAKAGE NOTED REQ'D REBALANCING 3 TIME IN FLIGHT. FOUND BOLTS LOOSE ON FUEL PUMP TO MEC TUBE AT MEC. REPLACED GASKETS AND RETORQUED BOLTS (P/N 731203193) GASKET TUBSDR DL767020168Smoke · detectedON TAKEOFF ROLL, SMOKE AND FUMES THROUGHOUT CABIN. PERFORMED DUCT BURN OUT FOR BOTH PACKS AND BOTH ENGINES. NO EVIDENCE OF FUMES FROM PNEU SYS AFTER DUCT BURN OUT. CONTINUE TO MONITOR AIRCRAFT.SDR DL76S020048Gasket · leakingLEFT ENGINE FAILED IN FLT ON DESCENT INTO MCO. POM PROCEDURES FOLLOWED, ONLY ABNORMAL INDICATION WAS HIGH FUEL FLOW, COMPARED TO THE RIGHT ENGINE. ON ARRIVAL FOUND LEFT ENGINE IDG FUEL/OIL COOLER GASKET CUT AND LEAKING. REPLACED SAME. FULL POWER RUN UP PERSDR DL76S020013Manifold · defectiveENGINE FLAME-OUT ON CLIMBOUT AT 34000. RETURNED FOR LANDING AT MCO. ENGINE FAILED NO MORE THAN 27 MINUTES FROM LANDING. REPLACED FUEL MANIFOLDS AT 11 O'CLOCK AND 6 O'CLOCK POSITIONS RAN NR 2 ENG PER PFHB TEST 4 T/O POWER AND LEAK CK ALL PARAMETERS OK OK FORSDR DL76S011984Manifold · leakingIR - LOST R ENG OIL PRESS (PRESS INDICATING 4 PSI) ENG SHUTDOWN 20 MIN BEFORE LNDG. (4 PSI INDICATING WHILE WINDMILLING. CA - FOUND FUEL POURING FROM FUEL MANIFOLD AT 5 OCLOCK POS. FROM UPPER BRANSDR DL76S011966Fuel Line · leakingFOUND FUEL LEAK ON RT ENGINE WHEN OPENED FOR MTC, POSSIBLE FIRE CONDITION EXISTED. FOUND FUEL LINES LEAKING. REPLACED FLEX FUEL LINES FROM FUEL FILTER TO DIFF PRESSURE SWITCH AND TO HEAT EXCHANGER, LEAK CHECK FOUND OK.SDR DL76S011789Engine · damagedCLIMBING THRU 19000FT, LOUD BANG ON THE RIGHT SIDE. TEMP ONNO 2 ENG WENT TO 959 DEG. PULLED ENG TO IDLE. SUBSEQUENT ENG OIL EICAS MSG. SHUT DOWN ENG. ON ARRIVAL AT GATE, MTC FOUND OIL DRAINING FROM COWL, METAL IN TAIL PIPE AND FAN DIFFICULT TO TURN. SDR DL76S011516Engine · unserviceableON CLIMB OUT RIGHT ENGINE STALLED. ACCOMPLISHED POM "ENGINE SURGE OR STALL" PROCEDURE. THROTTLE REDUCED TO IDLE. ENGINE SHUT DOWN AFTER LANDING. EGT MAX 895 FOR 1.4 SECONDS. FOUND METAL IN EXHAUST. REPLACED ENGINE.SDR DL767011455Mec · defectiveNR 2 ENGINE SHUT DOWN BY CREW ON APPROACH TO PBI. DURING CRUISE NOTICED RT THROTTLE/ENGINE WAS NOT RESPONDING TO MOVEMENT, COMMAND BAR WAS PRESENT. DURING DESCENT GOT EICAS R ENG SPEED CARD. REPLACED ENGINE MEC.SDR DL767011350Fuel Line · crackedFLUID LEAKING FROM RIGHT ENGINE ON PUSHBACK AFTER START. T/S LEAK PER M/M FOUND FUEL TUBE ON FUEL NOZZLE FEEDER MANIFOLD AT 5'OCLOCK POSITION CRACKED. REPLACED SAME, RAN ENG PERPFHB, LEAK CKS GOOD.SDR DL76S011205Engine · overtempRT ENG OVERTEMP ON T/O. EGT943 T/O DISCONTINUED AT 90K. CHECKED INLET AND EXH, RAN ENG PER PFHB MAX PWR ASSURANCE TEST. CLEARED EICAS COMPUTER, MSG 943 FOR 3 SEC OVERTEMP AREA A-MCC ADVISED.SDR DL76S011153Engine · malfunctionedRT ENG EGT EXCEEDED 979 DURING T/O. N2 VIBS 5.0 AND RT HP BLEED LIGHT ON. AIRCRAFT RETURNED TO ATL AND ON APPROACH INTO ATL RT ENG WAS SHUTDOWN BY CREW DUE EGT CONTINUING TO RISE. REMOVED AND REPLACED NR 2 ENG.SDR DL76S011074Harness · burnedWORKING MCO APU ELEC INOP. FOUND GENERATOR FEEDER CABLE BURNT. CABLE SENT TO SHOP WITH OLD GENERATOR. REPLACED CABLE.SDR DL76S011008Mec · malfunctionedDURING FLIGHT NR 2 ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. ENGINE SHUT DOWN, LANDED SINGLE ENGINE. CHECKED THROTTLE CABLES, ALL SECURE. REMOVED AND REPLACED MECPRE M/M. LEAK AND RUN CHECK GOOD.SDR DL76S010934Gasket · leakingLT ENG FIRE INDICATIONS SHORTLY AFTER TAKEOFF THROTTLE. RETARDED TO IDLE AND FIRE INDICATION WENT OUT. FOUND ALL THERMOCOUPLE GASKETS LEAKING. REPLACED GASKETS, CK OK ON RUN.SDR DL767002274Idg · lack of lubeON T/O ROLL, LT GEN DRIVE EICAS MSG CAME ON. ABORT T/O AT 100 KNTS. BPCU INDICATES SERVICE IDG. SERVICED IDG AND RAN ENGINE.SDR DL76S002234Engine · fodNR 1 ENGINE SUSTAINED DAMAGE TO 7 FANS BLADES DURING TAKEOFF FROM PBI. DEPARTMENT OF AIRPORTS FOUND 2 PARTIAL REMAINS OF TURKEY VULTURES NEAR END OF RUNWAY. ENGINE WAS NOT SHUT DOWN IN FLIGHT. ENGINE WILL REQUIRE REPLACEMENT BEFORE FURTHER FLIGHT.SDR DL767002283Engine · leakingSMOKE IN CABIN SOURCE UNKNOWN SMOKE CLEARED AFTER PERFORMINGSMOKE AND FUME REMOVAL CHK LIST._HAPPENED AT FL370 DESCENDED TO FL230 ALSO SMOKE ALARM IN MID LAV WENT OFF. FLL MTC WAS SENT TO INVESTIGATE AFTER CONTRACT MTC WAS UNABLE TO DUPLICATE PROBLEM WITH RSDR DL76S002032Engine · leakingLOSS OF OIL QTY DURING FLT WITH DECREASING OIL PRESSURE. AT TOP OF DESENT WITH THROTTLE TO IDLE OIL PRESSURE WENT THRU 10 PSI INTO RED AREA AND CREW SHUT DOWN ENG. ENG WINDMILLED FOR 15 MIN WITH ZERO OIL PRESSURE. REPLACED ENGINE.SDR DL76S001531Engine · leakingFULL PWR TAKEOFF RIGHT AFTER LIFTOFF SMOKE FILLED THE ENTIRE AFT CABIN C ZONE AND SET OFF THE LAV SMOKE DETECTORS. NO SOURCE COULD BE IDENTIFIED. LAVS AND GALLEYS WERE CHECKED, SMOKE APPEARED TO BE UNIFORM THROUGHOUT THE CABIN IN C ZONE. REPLACED NR 2 ENGINSDR DL76S001537Engine · odorFULL POWER T/O, GOT STRONG ACRID SMELL IN THE MID AND AFT CABIN RIGHT AFTER LIFTOFF. SMELL WENT AWAY RAPIDLY WHEN CLIMB POWER WAS SELECTED. NO SMOKE OBSERVED. IT SMELLED HOT, WAS VERY PUNGENT AND MAY HAVE HAD A BURNT OIL SMELL. FOUND OIL PUDDLING IN FAN EXSDR DL76S001528Engine · leakingSTRONG SMELL IN A/C PACKS T/O MADE AFT SMOKE DET GO OFF BRIEFLY, NO SMOKE. CLEARED UP A FEW MINS LATER. REPLACED NR 2 ENGINE FOR OIL LEAK.SDR DL76S001124Line · wornDURING CLIMB FROM DFW, HYD QTY EICAS MSG WITH DECREASING QTY LEFT HYD INDICATED. ONCE LEFT ENG PRIMARY PUMP WAS TURNED OFF LEFT HYD QTY STABILIZED AT .40. FOUND HYD LINE OFF OF EDP WORN THROUGH. REPLACED AND REPOSITIONED LINE SVC SYSTEM, OPS CHECK NORMAL. SDR DL76S000831Fire Detector · chafedAFTER TAKEOFF, RECEIVED LT ENG FIRE LOOP 1 EICAS MSG FOLLOWED BY LT ENG FIRE WARNING. REPLACED UPPER AFT LOOP AND REPAIRED CHAFED WIRING.SDR DL76S000798Engine · odorON TAKEOFF, F/A CALLED AND REPORTED SMOKE AND FUMES IN THE CABIN. RETURNED FOR LANDING. F/A THEN REPORTED ONLY FUMES. PRIOR TO LANDING FUMES HAD DISAPPEARED. FOUND DETERGENT SMELL NR 2 ENGINE. PERFORMED ENGINE RUN FOR 20 MINUTES. NO FUMES NOTICED.SDR DL767000263Turbine · damagedNR 1 ENG HIGH VIBS 5.0 N-2 WITH HUM AND VIBRATION. FOUND DAMAGE TO TURBINE. REPLACING ENGINE.SDR DL767992558Engine · failedON TAKOFF ROLL, RT ENG COMPRESSOR STALL AND EGT WENT TO 1081 DEG CELSIUS. ICING CONDITIONS PRESENT, ANTI ICE ON. ENGINE HAD METAL IN TAILPIPE ON GATE RETURN. REPLACED ENGINE.SDR DL76S992416Compressor · damagedON ARRIVAL FLT 1814 BOS, FOUND FOD DAMAGE TO MULTIPLE FAN BLADES AND ACCOUSTICAL LINER. REPLACED FAN.SDR DL76S992002Starter · failedAPU INOP, WILL NOT START. FOUND APU STARTER OVERHEATED AND BURNED ON OUTER CASE. REPLACED STARTER, APU OPS NORMAL.SDR AALA991329Manifold · defectiveGIG - FLT 972 - ON INITIAL ENGINE START UP ON RAMP DURING PUSH OUT, FUEL LEAK NOTED FROM RIGHT ENGINE. ENGINE WAS SHUTDOWN WITHOUT FURTHER INCIDENT. FOUND RIGHT ENGINE UPPER FUEL NOZZLE MANIFOLD LEAKING. REPLACED RIGHT ENGINE UPPER FUEL NOZZLE MANIFOLD AND SDR DL76S991585Compressor · dirtyACRID SMOKE SMELL WITH SMOKE DETECTORS GOING OFF ON TAKEOFF TO WT 314,000 LAND WEIGHT 310,000, OVERWEIGHT LANDING, DETECTORS SOUNDED APPROX THIRTY SECONDS THEN OFF. A/C RETURNED TO GATE. NO VISIBLE SMOKE IN CABIN OR COCKPIT. SMELL DETERMINED COMING FROM BOTSDR DL767991497Engine · failedNR 1 ENG SLOW TO ACCELERATE, SEVERAL RED LINES. REPLACED ENGINE.SDR DL76S991016Engine · failedLEFT ENGINE FAILED AT 6,000 FT. CLIMBOUT EGT REACHED 1,100, LITE ENGINE VIBRATION FELT FOLLOWED BY EGT SPIKE. REPLACED ENGINE.SDR DL76S990785Fitting · leakingAT TOP OF DESCENT, NR 1 ENGINE ROLLED BACK AND OIL PRESSURE STARTED TO DECAY WITH N1 AND N2 STILL INDICATING DOUBLE DIGITS. REPLACED T-BONE FITTING AT 10 O'CLOCK POSITION.SDR DL76S982011Line · wornRIGHT HYDRAULIC SYSTEM QUANTITY INDICATED ZERO SOON AFTER TAKEOFF. COMPLETED POM PROCEDURES AND RETURNED FOR LANDING. PER CREW COMMENT ENGINE HYD PUMP DID NOT RUN DRY. NO PRESSURE LOSS NOTED. ENGINE PUMP SHUT DOWN PRIOR TO PRESSURE LOSS. FOUND NR 2 ENGINE SDR DL767981374Engine · failedAS POWER CAME UP FROM IDLE A BANG WAS HEARD AND LT ENG REMAINED AT IDLE PWR. NO CONTROL OF LEFT ENG FROM COCKPIT. NO ENG EXCEEDANCE NOTED AND NO INDICATIONS IN COCKPIT OF ENG FAILURE. ENG WAS NOT SHUTDOWN FOR EMERG LANDING AT JFK. FOUND METAL IN TAILPIPESDR DL767981067Engine · failedIN DESCENT, NR 2 ENG SHOWED NO OIL QTY AND 10 PSI PRESS. SHUT DOWN ENGINE PER POM. MAINTENANCE IN PROGRESS. FOUND METAL ON CHIP DETECTOR, REPLACED ENGINE.SDR DL76S980333Fuel Line · looseON DESCENT AT FL200 WITH ENGINE ANTI-ICE TURNED ON AND AUTO THROTTLES ENGAGED RT ENGINE ADV TO FULL POWER AND LT ENGINE REMAINED AT IDLE. N1 COMMAND BUG SHOWED FULL POWER REQUESTED ENGINE STAYED AT IDLE. MAINT FOUND FUEL LINE CONN AT FUEL FLOW METER LOOSE ANSDR DL767972679Bracket · brokenDURING MTC, AFTER OPERATING THE RT ENG TO IDLE FOR HIGH OIL CONSUMPTION CHECKOUT, FOUND FUEL RUNNING FROM RT ENG STRUT DRAINLINE. INSPECTED AREA, FOUND ENG FUEL FEED LINE COUPLING AT THE TOP OF THE STRUT JUST FWD OF THE WING LE CHAFFED THRU DUE TO A BROKEN HYSDR DL76S972455Clamp · looseAIRCRAFT 133 EXPERIENCED AN IN FLIGHT SHUTDOWN DUE TO A LEFT ENGINE FIRE WARNING ON CLIMBOUT FROM PDX. PILOTS FOLLOWED POM PROCEDURES. MAINTENANCE FOUND A LOOSE HIGH PRESSURE VALVE INBOAD CLAMP AFTER BACK PRESSURIZING USING APU. RESECURED CLAMP AND RELSDR DL767971914Hose · chaffedAPPROX 30 MIN AFTER ENGINE START-R HYD SYS QTY EICAS MSG. SELECTED STATUS PAGE AND RT HYD QTY SHOWED .05. S/O RT PRIMARY AND DEMAND PUMP OFF. FOUND ENG HYD PUMP PRESS HOSE WORN THROUGH. HOSE WAS RUBBING BRACKET BOLT HEAD JUST BELOW TOP GANG CLAMP. REPLACEDSDR DL757971915Oven · failedSTRONG ELECTRICAL SMELL IN MID GALLEY AREA. REPLACED MID GALLEY DOUBLE OVEN OPERATED ALL MID GALLEY EQUIP VIDEO EQUIP AS WELL AS AIR COND SYS ALL NORMAL, NO FURTHER ODOR.SDR DL76S971834Engine · failedPASSING FL 23500 ABOUT 10 SEC AFTER SELECTING CLB PWR, LEFT ENG COMPRESSOR STALL (5 BANGS). PULLED TO IDLE MAX TEMP 928 FOR 4 SEC, INDICATED AIRSPD 310 KTS. BEGAN DESCENT, LEFT ENG COMPRESSOR STALLED AGAIN 3 TIMES AS PWR WAS REDUCED. SHUTDOWN ENG PASSING 8SDR DL767970788Idg · failedON TAKEOFF, LOST 'L' GEN FOLLOWED BY AC L BUS OFF. STARTED APU DID NOT GET L BUS BACK. FOLLOWED BY 'L' GEN DRIVE LIGHT. APU WAS RUNNING OK. NO ISOLATION LIGHT. REPLACED NR 1 IDG AND GARLOCK SEAL. OPS CHECK GOOD. BPCU FAULTED LT GCU, REPLACED GCU. CHECK
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