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 = 'CF650C2' 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 = 'CF650C2' 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 20000424AP001Hydraulic System · malfunctionedMIA - FLT TA823 - AFTER TAKEOFF, THE COMPASS NR 1 FAULT AND THE BLUE ENGINE HYDRAULIC PRESSURE SHOWED 2000 PSI DUE TO THIS SITUATION THE AIRCRAFT RETURNED TO MIAMI AIRPORT. AIRCRAFT IS ON GROUND AND MX TECHS ARE PERFORMING TROUBLE SHOOTING AT THIS TIME. (M)SDR CA000322009Bolt · misinstalled(CAN) BOLT AND METAL FOUND IN THE LUBE AND SCAVANGE PUMP INLET SCREEN. BOLT ORIGINATED IN THE GEARBOX. THE BOLT CAME ADRIFT DUE TO IMPROPER TORQUEING AND LOCKING PROCEDURE.SDR AALA20000354Compressor · stalledHNL - FLT 8 - AFTER TAKEOFF, NR 2 ENGINE EXPERIENCED COMPRESSOR STALL. RETURNED AND LANDED HNL WITHOUT INCIDENT. (M)SDR CA000410013Transmitter · failed(CAN) HYDRAULIC LEAK DETECTED DURING GROUND HANDLING. INVESTIGATION REVEALED THE RT STANDBY BRAKE MANIFOLD PRESSURE TRANSMITER HAD FAILED. THE LOWER PORTION WHICH IS THREADED INTO THE MANIFOLD APPEARED TO HAVE FAILED UNDER PRESSURE LEADING TO A LOSS OF THREESDR 00FDEA00064Blade · damagedON T/O, FLEW THROUGH FLOCK OF BIRDS, NR 1 ENG START TO VIB. VIB SUBSIDE BELOW 65 DEG N1. RETURN TO SFS. *S/D* REMOVED AND REPLACED DAMAGED BLADES (5) PER MM 72-21-06-81. PERF VIB SURVEY CK AND TRIM BALANCING PER MM 72-00-00 AND DC 10 JRH. OK A/C OK FOR SDR CA000128010Smoke Detector · failed(CAN) ON TAXI AFT CARGE FIRE LIGHT ON. DISCHARGED CARGE FIRE BOTTLE NR 1, RETURNED TO GATE. REPLACED AFT NR 1 AND 2 SMOKE DETECTORS AND FIRE BOTTLE.SDR 2000UALA00026Skin · damagedON CREW WALKAROUND FOUND NUMBER 2 ENGINE AFT FAIRING TRAILING EDGE DAMAGED. *S/D* THE NR 2 ENGINE AFT FAIRING TRAILING EDGE WAS FOUND DAMAGED. CAUSED BY CRACKING OF THE SUPPORT CHANNEL AVB7021-29 AND TRAILING EDGE AVB7021-503. THE SUPPORT CHANNEL AND TRAILSDR 2000UALA00027Panel · dentedLT WING MOST I/B SLAT LARGE DENTS ON I/B END AND MID SPAN WING FILLET PANEL ON I/B END. ALSO LEFT STABILIZER HAS DEEP DENT IN LEADING EDGE IN MIDDLE OF STABILIZER. DENT IS AT RIB WITH RIVETS PULLING THROUGH SKIN. *S/D* REPAIR A WATER LEAK AT THE FILL VALVESDR 20000420AP006Blade · damagedSAP - FLT TA806 - DURING TAKEOFF, A BIRD WAS INGESTED BY ENGINE NR 2. THE TAKEOFF WAS REJECTED AND THE AIRCRAFT RETURNED TO THE CARGO GATE AFTER AN UNEVENTFUL REJECTED TAKEOFF PROCEDURE AT SAN PEDRO STATION. AT SAN PEDRO, MAINTENANCE TECHNICIANS PERFORMED INSDR CA000215027O-Ring · split(CAN) LOSS OF GREEN SYSTEM HYD FLUID LED TO LANDING. INVESTIGATION REVEALED A DAMAGED O-RING ON THE PRESSURE MANIFOLD. O-RING REPLACED.SDR 20000424AP006Cooler · crackedMIA - FLT TA807 - DURING CRUISE, THE NR 2 ENGINE HIGH TEMPERATURE LIGHT CAME ON AND PACK NR 2 AUTOMATICALLY CLOSE. WHEN CROSS BLEED VALVE WAS OPENED NR 1 BLEED AIR TEMPERATURE STARTED TO RISE. BOTH ENGINES BLEED WERE CLOSED AND THE AIRCRAFT RETURNED TO MIAMISDR CALA9901649Liner · failedTHE NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED DURING CLIMBOUT. THE FIRE WARNING LIGHT WAS ACCOMPANIED BY EGT GOING FULL SCALE. THE ENGINE THROTTLE WAS RETARDED AND THE FIRE LIGHT WENT OUT. AN ATTEMPT TO THROTTLE UP WAS MADE, BUT N1 WOULD NOT ACCELERATE. TSDR 99UAL900628Light · inoperativeTHE 3L SLIDE PRESS TO TEST LIGHT INOP.SDR CA991230003Bolt · broken(CAN) WHEN ASSEMBLING WHEEL BOLTS STRETCHED BEFORE REACHING SPECIFIED TORQUE.WHEEL TIE BOLTS STRETCHED AT 180 FT/LBS TORQUE.SDR CA991208061Harness · separated(CAN) FUEL QUANTITY INDICATION BLINKING. FUEL QUANTITY WIRES IN UPPER AUXILIARY TANK HAVE INSULATION SEPARATION. WIRES DAMAGED LOCATED BETWEEN FUEL QUANTITY JUNCTION PROBE AND AFT FUEL TANK BULKHEAD. WIRES REPLACED.SDR 20000424AP007Transmitter · inoperativeSAL - FLT TA821 - DURING CRUISE, THE WEATHER RADAR SYSTEM FAULT, DUE TO THIS SITUATION THE AIRCRAFT DIVERTED TO EL SALVADOR STATION FOR MAINTENANCE. AT SAL, MAINTENANCE TECHS PERFORMED TROUBLE SHOOTING OF THE WEATHER RADAR SYSTEM AND WAS FOUND RADAR TRANSCEIVSDR 20000424AP008Antenna · inoperativeSAL - FLT TA821 - DURING CRUISE, THE WEATHER RADAR SYSTEM FAULT, DUE TO THIS SITUATION THE AIRCRAFT DIVERTED TO EL SALVADOR FOR MX. AT SAL, MX TECHS PERFORMED TROUBLESHOOTING OF THE WEATHER RADAR SYSTEM AND FOUND RADAR TRANSCEIVER/RECEIVER AND ANTENNA INOPERASDR CA991027001Battery Charger · failed(CAN) AT CRUISE, BATTERY AND LEFT EMERGENCY AC BUS WERE PULSATING. RESET BATTERY CHARGER CIRCUIT BREAKER, PROBLEM STILL EVIDENT. CHARGING STOPPED COMPLETELY, VOLTAGE DROPPED TO 20 VOLTS. AFTER STARTING DIVERSION CHARGING STARTED TO CYCLE FOR APPROXIMATELY 5SDR CA991007016Stringer · cracked(CAN) FOUND LEFT WING STRINGER 41 CRACKED. AIRCRAFT FERRIED FOR REPAIR.SDR CA991007096Bolt · failed(CAN) WHEEL TIE BOLTS STRETCHED AT 180 FEET/POUNDS TORQUE. REF: MESSIER BUGUATTI SL C20195-32-799.SDR CA991007097Bolt · broken(CAN) WHEEL TIE BOLTS STRETCHED AT 180 FEET/POUNDS TORQUE. REF: MESSIER BUGUATTI SL C2 195-32-799.SDR CA991007098Bolt · failed(CAN) WHEEL TIE BOLTS STRETCHED AT 180 FEET/POUNDS TORQUE. REF: MESSIER BUGUATTI SL C2 195-32-799.SDR CA991004020Valve · failed(CAN) ON CLIMB, NR 3 PNEUMATIC MANIFOLD FAIL LIGHT ILLUMINATED, INDICATED 90 PSI AND 220 DEGREE TEMPERATURE. ACCOMPLISHED CHECK LIST. THROTTLE BACK NR 3 TO BRING PRESSURE AND TEMP BACK. ENGINE PRESSURE VALVE REPLACED.SDR DHL99366002Fuel Line · crackedAT STABILIZED CRUISE, FL 350, NR 1 ENGINE ROLLED BACK TO APPROX 87 PERCENT N1. THROTTLE RETARDED TO DETERMINE IF RPM WOULD FOLLOW. ENGINE THEN ROLLED BACK TO 38 PERCENT, FUEL FLOW TO 1700 AND ENGINE CEASED TO FOLLOW THROTTLE INPUTS. ENGINE SHUTDOWN PER PROSDR 99UAL900462Audio Box · failedELECTRICAL SMELL AROUND SEAT 33, 32, 34 LEFT SIDE OF AC. PAX CLAIMS SMELLS WAS STRONG FOR FEW SECONDS THEN DISAPPEARED. PAX 32C LOOSE OVERHEAD LIGHTS AND AUDIO. *S/D* SEAT ELECTRONIC BOX FAILED AT SEAT 32C. REPLACED SEAT ELECTRONIC BOX AT 32C, OPS CHECK NSDR CA990915037Hose · damaged(CAN) LOUD NOISE WITH HEAT REPORTED BEHIND SEAT 36A. FLOOR BECAME TOO HOT TO TOUCH. NR 2 PNEUMATIC SYSTEM SELECTED OFF, NOISE STOPPED, BUT AREA BETWEEN 36A AND LAVATORY BECAME HOTTER. PNEUMATIC ISOLATION VALVE 1-2 IN THE NORMAL POSITION (CLOSED). OVER A PESDR 99UAL900449Clamp · brokenAFTER T/O DURING CLIMBOUT, FIRE WARNING NR 1 ENGINE. SHUTDOWN PER SOP, DUMPED FUEL, RETURNED TO SFO. *S/D* FOUND FAILED V-CLAMP (P/N 9130M36P240) ON REVERSER DRIVE SUPPLY DUCT (P/N 9057M85G02). ALSO, DUCT WAS DAMAGED. DUCT AND CLAMP WERE REPLACED.SDR CA990804007Fire Detector · loose(CAN) LEVELING OUT AT 32,000 FEET, FIRE WARNING ACTIVATED FOR NR 3 ENGINE. ENGINE THROTTLED BACK TO IDLE AND FIRE WARNING WENT OUT. ALL ENGINE PARAMETERS OK. FOUND BIRD CAGE COOLING MANIFOLD ADRIFT ON NR 3 ENGINE REPAIRED.SDR CA990804006Cit Sensor · failed(CAN) ON ROLLING TAKEOFF, NR 3 ENGINE APPEARED TO BE SLOW TO SPOOL AND HUNG AT 102 PERCENT. ENGINE FAIL LIGHT ILLUMINATED AND TAKEOFF ABORTED. BORESCOPE INSPECTION REVEALED NO FAULTS. REPLACED NR 3 ENGINE FUEL FILTER AND FUEL PUMP DEBRIS FILTER, ENGINE RUN SDR 9902761233Engine · malfunctionedDURING TAKEOFF ROLL (DEL), CREW OBSERVED THE NR 1 ENGINE WAS NOT PRODUCING TAKEOFF POWER WITH EGT AT REDLINE. THE TAKEOFF WAS ABORTED AT 130 KTS AND THE AIRCRAFT RETURNED TO THE GATE. AFTER A BORESCOPE, FOUND NO DEFECTS AND AND MEC CHANGE DID NOT CORRECT THESDR AALA990953Filter · defectiveHNL - FLT 72 - DURING CLIMB-OUT, NR 2 ENGINE STRAINER CLOG LIGHT ILLUMINATED INTERMITTENTLY AND THEY STAYED ON. FLIGHT CREW ACCOMPLISHED SHUT DOWN PROCEDURES CHECKLIST AND RETURNED AND LANDED HNL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NR 2 ENGINE OISDR CALA9900710Fuel Line · brokenTHE NR 3 ENGINE FLAMED OUT DUE TO LOSS OF FUEL FLOW WHILE EN ROUTE FROM GUM TO HNL. ALL OTHER ENGINE PARAMETERS WERE IN NORMAL RANGE AT TIME OF FAILURE. THE AIRCRAFT WAS RETURNED TO GUM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE EDUSDR UIEA9915Manifold · crackedFLT 322 - BOG/MIA-IFSD - NR 1 ENGINE FUEL FLOW FLUCTUATED ERRATICALLY, NO OTHER ENGINE PROBLEMS. AFTER APPROX 5 MINUTES ENGINE FLAMED UNEVENTFULLY. DECIDED NOT TO ATTEMPT A RELIGHT. CONTINUED TO MIA, DECLARED AND EMERGENCY AND LANDED. DURING TROUBLESHOOTINSDR CA990330044Wire · failed(CAN) FORWARD LOWER CARGO COMPARTMENT WIRING CHAFED ON CLAMP ABOVE CEILING LINER, LEADING TO ARCING, BURNING AND TRIPPED CIRCUIT BREAKER. WIRING REPAIRED.SDR 99ZZZX1375Cdp Line · contaminatedTEN MINUTES AFTER T/O OUT OF NARITA ON CLIMBING TO 10,000 FEET, CREWS NOTICED NR 3 ENGINE POWER LAGGING BEHIND COMPARED WITH ENG 1 AND ENG 2. ATTEMPTS TO RESTORE NORMAL POWER TO THAT ENGINE FAILED AND ACFT MADE AN ATB. DURING T/S, CHECKED MAIN FUEL FILTER ANSDR CALA9900196Frame · crackedTHE NR 3 ENGINE A AND B FIRELOOP LIGHTS ILLUMINATED AND THE FIRE HANDLE FLASHED AFTER TAKEOFF FROM HNL. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO HNL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE 13TH STAGSDR CA990226007Smoke Detector · failed(CAN) AFT BULKHEAD SMOKE WARNING ILLUMINATED, AIRCRAFT SAFELY LANDED. INVESTIGATION REVEALED CONDENSATION IN SMOKE DETECTOR DUCT LEADING TO FAILURE OF UNIT.SDR 99UAL900155Airspeed Ind · malfunctionedAIRSPEED FLAG ON SIDE AT 90 KTS, 0 AIRSPEED AND AIRSPEED FLAG. ABORTED TAKEOFF 110 TO 115 KTS. PRIOR TO TURN OFF, FLAG WENT AWAY. *S/D* UNABLE TO DUPLICATE INDICATOR PROBLEM ON THE GROUND. REPLACED MACH/AIRSPEED INDICATOR PRECAUTIONARY.SDR CA990310063Refueling Door · separated(CAN) FUEL HANDLER FOUND STARBOARD WING REFUELING PANEL MISSING. NEW PANEL INSTALLED.SDR CA990310054Crank · cracked(CAN) DURING INSPECTION, FOUND CRACK IN FORWARD CARGO DOOR SUPPORT CRANK ASSY CAUSED BY USE OF EXTERNAL POWER SOURCE WHICH OVERRIDES THE LIMIT SWITCHES. REPLACED.SDR CA990119013Smoke Detector · failed(CAN) SMOKE WARNING INDICATION FROM AFT CARGO COMPARTMENT ON OUTBOUND DEPARTURE. CARGO HOLE AND SYSTEM CHECKED, SECURED IAW MEL. SMOKE DETECTOR REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR 9900161232Cit Sensor · malfunctionedDURING TAKEOFF ROLL, THE NR 3 ENGINE HAD LAGGING N1 INDICATION AND LOW FUEL FLOW INDICATION. THE TAKEOFF WAS ABORTED AT 110 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE CHECKED THE COMPRESSOR DISCHARGE LINE FOR LEAKS AND CLEANED THE LINE. ALSO, THSDR CA990310053Turbine Wheel · cracked(CAN) DURING LANDING ROLL, AFTER THRUST REVERSER CANCELLED, SPARKS WERE SEEN FROM REAR OF NR 1 ENGINE. INSPECTION REVEALED METAL IN THE EXHAUST. DISASSEMBLY FOUND LP TURBINE ASSEMBLY DAMAGED. DISCOURAGER LEG OF NR 1 AIR SEAL HAD PIECES MISSING WITH CRACKINGSDR 98UAL900619Wire · failedNR 1 AC BUS CIRCUIT BREAKERS POPPING. *S/D* FOUND BURNED WIRES IN CEILING OF FWD COMPARTMENT LOCATED AT FWD WALL, APPROX STA 595 LHS. REPLACED ALL THE WIRES/CABLES THAT WERE INVOLVED.SDR 98UAL900630Bolt · failedFRACTURE OF THE OUTBOARD RIGHT HAND MAIN LANDING GEAR ATTACH FITTING ATTACH BOLT. THE WASHER ALSO FAILED IN THE AREA OF THE BOLT FRACTURE. *S/D* FAILED WASHER SHOWS EVIDENCE OF MOISTURE ENTRAPMENT. BOLT FAILED AS A RESULT OF CORROSION INDUCED STRESS. BOLT, SDR 98UAL900598Valve · malfunctionedON DESCENT AT 19000 FEET HEARD A LOUD BANG. *S/D* AFTER INSPECTION A DENT WAS FOUND ON THE NR 1 RT SLAT DUE TO THE BUILD UP OF ICE ON THE POTABLE WATER SYSTEM DRAIN PORT. REPLACED DRAIN VALVE AND TESTED SYSTEM FOR LEAKS. CONFIRMED CONFIGURATION AND PERFORMSDR CA990310038Circuit Breaker · tripped(CAN) AIRCRAFT DIVERTED DUE LEFT EMERGENCY BUS FEED CIRCUIT BREAKER TRIPPED, UNABLE TO RESET. REPLACED B1-136 RCCB.SDR 98UAL900516Light · inopEEL PATH LIGHTING INOP ON ENTIRE RIGHT SIDE OF ZONE A CABIN. FLEXIBLE EEL LAMP BENEATH AND JUST FORWARD OF VIDEO SYSTEM CABINET INOP. FOUND FEEDER DAMAGED. SPLICED IN NEW SECTION OF FEEDER AND SECURED WITH TAPE. REPLACED ENTIRE EEL LAMP ASSEMBLY WITH ATTACSDR WRLA98095Engine · malfunctionedDURING INITIAL CLIMB OUT, 800 FT AGL, NR 2 ENGINE BEGAN SURGING. FLT CREW RETARDED THROTTLE FROM 95 PERCENT N1 TO FLIGHT IDLE. SURGING DISCONTINUED. UPON REACHING ASSIGNED ALTITUDE, FLIGHT CREW ADVANCED THROTTLE TO 75 PERCENT N1, AND SURGING RETURNED. THROSDR 98ZZZX4012Fan Frame · crackedTHE NR 1 ENGINE REVERSER SEAL SUPPORT RING, LEFT, WAS FOUND CRACKED AT ALL FIVE FORWARD ATTACH POINTS. THE FLANGE SECTIONS HAD BROKEN COMPLETELY AWAY FROM THE TWO BOLT ATTACHMENTS IN AN ARC THE CRACK PASSING THROUGH THE TOP ROW OF TWO ATTACHMENT RIVETS OF A S
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