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 = 'CJ6108' 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 = 'CJ6108' 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 2016FA0000151Tube · failedDURING A ROUTINE FLIGHT THIS TUBE RUPTURED AT THE BASE OF THE FLARE SLEEVE FOR THE B-NUT. THE RUPTURE WAS APPROXIMATELY 50 PERCENT AROUND THE TUBE. THE RUPTURED TUBE CAUSED THE ENGINE TO BE STARVED OF FUEL AND RESULTED IN THE ENGINE SHUTTING DOWN.SDR ZP7A2010F00117Engine · bird ingestionBIRD WAS INGESTED INTO LEFT ENGINE JUST AFTER V-1. ENGINE FLAMED OUT, TAKE OFF WAS CONTINUED TO A SAFE ALTITUDE. CREW DECLARED AN EMERGENCY ON CTAF AND RETURNED FOR LANDING. AIRCRAFT LANDED SAFELY, ALL PASSENGERS AND CREWMEMBERS WERE SAFE, NO INJURIES. DSDR CJP2006F00000Ball Joint · out of adjustNR 1 ENGINE FLAMED OUT WHEN THROTTLED TO IDLE FOR DESCENT. ENGINE WAS SUCCESSFULLY AIR STARTED. UPON LANDING THROTTLES WERE RETARDED AND NR 1 ENGINE FLAMED OUT AGAIN. MAINTENANCE PERSONNEL INSPECTED ENGINE INSTALLATION AND RE-RIGGED NR 1 ENGINE AIRCRAFT THRSDR 2005FA0000188Pump · flakingTHE INTERNAL COATING IN THE GEAR SECTION OF THE FUEL PUMP STARTED FLAKING OFF AND GOT INTO THE HIGH PRESSURE FUEL LINE THAT GOES TO THE JET PUMPS IN THE RT WING. THE MATERIAL CLOGGED UP THE ORIFICES IN THE JET PUMPS, NOT ALLOWING FUEL TO BE TRANSFERRED FROM SDR 4019Warning Light · illuminatedON APPROACH INTO CLT RIGHT ENGINE FIRE LIGHT CAME ON, FIRST STARTED FLICKERING THEN CAME ON STEADY. REDUCED POWER LIGHT WENT OUT, THEN CAME BACK ON AND STAYED ON. SHUT DOWN ENGINE AND BLEW BOTH BOTTLES.SDR 4020Warning Light · illuminatedON APPROACH INTO CLT RIGHT ENGINE FIRE LIGHT CAME ON, FIRST STARTED FLICKERING THEN CAME ON STEADY. REDUCED POWER LIGHT WENT OUT, THEN CAME BACK ON AND STAYED ON. SHUT DOWN ENGINE AND BLEW BOTH BOTTLES.SDR YDB2004FBBBTube · unserviceablePILOT REPORTED BRAKES WERE VERY WEAK ON LANDING ROLL OUT. FOUND LARGE AMOUNT OF HYDRAULIC FLUID ON AFT PORTION OF AIRCRAFT BELLY. T/S AND FOUND LT ENGINE HYDRAULIC PRESSURE LINE LEAKING AT SUPPORT CLAMP IN TAIL COMPARTMENT. ADEL SUPPORT CLAMP RUBBER CUSHIONSDR 2004F00045Fire Loop · dirtyFALSE FIRE WARNING DURING FLIGHT. AFTER A/C LANDED, PILOT REPORTED INDICATION WAS INTERMITTENT. COWL WAS REMOVED, ENGINE INSPECTED, NO INDICATION OF FIRE/OVERHEAT. DETECTION LOOP INTACT/NO DAMAGE. WIRING CONNECTIONS AT FIREWALL DISCONNECTED, APPEARED TO BE SDR DRU2004F00000Fire Detector · false indicationFALSE FIRE WARNING DURING FLIGHT. AFTER THE AIRCRAFT LANDED, THE PILOT REPORTED THAT THE INDICATION WAS INTERMITTENT. THE RT ENGINE COWLING WAS REMOVED, AND THE ENGINE WAS INSPECTED. THERE WAS NO INDICATION OF FIRE IN THE ENGINE AREA. THE FIRE LOOP LOOKEDSDR 2003006Engine · malfunctionedDURING FLT AT APPROXIMATELY 2:00 AM, AIRCRAFT WAS ENROUTE WHEN THE PILOT NOTICED THAT THE LT ENGINE OIL PRESSURE WAS DECREASING. THE PILOT ALSO NOTICED THAT THE LT EGT WAS CLIMBING. THE PILOT ELECTED TO SHUT DOWN THE LT ENGINE AND RETURN AT THIS TIME. NO EMSDR CJP2003F00002Control Box · intermittentFLIGHT CREW EXPERIENCED INTERMITTENT RIGHT ENGINE FIRE WARNING. AIRCRAFT LANDED AT INTENDED DESTINATION. MAINTENANCE TROUBLESHOT ENGINE PYLON WIRING WHICH IS THE USUAL CAUSE OF INTERMITTENT FIRE WARNINGS, AND COULD NOT RESOLVE PROBLEM. TROUBLESHOOTING MOVEDSDR DRU2003F00000Blanket · burnedDURING INSP BY MECH, A BLACK STREAK (FORE TO AFT) WAS NOTICED ON LT HORIZ STAB, THAT BOOT LOOKED BURNT ON L.E. EXAMINATION REVEALED THAT BOOT MUST HAVE SHORTED AGAINST L.E., BURNING BOTH BOOT AND HORIZ STAB CONSISTED OF NICKEL SIZE HOLE BEING COMPLETELY BURNTSDR ESUA116360Line · loosePILOT DECLARED AN EMERGENCY ON APPROACH, IT WAS DISCOVERED THAT THE HYDRAULIC PRESSURE INDICATED (0). THE GEAR WAS ABLE TO BE PLACED IN THE DOWN AND LOCKED POSITION WITH NO EMERGENCY PROCEDURES. AIRCRAFT LANDED ON 13L. THE AIRCRAFT WAS STOPPED ON THE RUNWAYSDR ESY2002F00000Engine · failedFIFTEEN MINUTES AFTER TAKE-OFF, EXPERIENCED FAILURE OF RT ENGINE, WHILE CLIMBING, LEAVING, EVERYTHING WAS NORMAL. NO PREVIOUS ENG ABNORMALITY HAD BEEN NOTED. AT APPROX 20,000 FEET, HEARD LOUD BANG AND EXPERIENCED VIBRATIONS FROM RT ENGINE. ENGINE LOST POWESDR IKM2002F00001Wheel · crackedWHEEL, CRACKED, BEAD SEAL AREA.SDR IY22002F00000Structure · corrodedDURING PREPARATION OF AIRCRAFT FOR PAINT, CORROSION WAS FOUND ON THE TOP OF THE LEFT WING BETWEEN WING STATIONS 125.00 TO 181.10 AND SPAR NR 5 TO 8 UNDER A RAISED BACK COVER. THE CORROSION IS AS MUCH AS .044 INCHES DEEP. WHEN THE COVER WAS REMOVED, NUMEROUS SDR JDMA648BLine · crackedHYDRAULIC TRANSFER LINE IN AUXILARY SYSTEM, LINE WAS FOUND BROKEN AT FLAIR CAUSING LOSS OF HYDRAULIC FLUID AND HYDRAULIC SYSTEM FAILURE. AIRCRAFT WAS REPAIRED AND RETURNED TO SERVICE.SDR 20010205CW013Hydraulic Line · chafedPILOT LOST HYDRAULIC PRESSURE IN FLIGHT. INSPECTION REVEALED HYDRAULIC PRESSURE LINE FROM LEFT ENGINE TO AUXILLARY HYDRALUIC PUMP MANIFOLD LINE, CHAFFED AT CLAMP, RECOMMENDED REMOVING CLAMPS ON THIS SPECIFIC HYDRAULIC LINE ON AIRCRAFT WITH THE SAME HYDRAULIC SDR CA001019018Accumulator · separated(CAN) AFTER FLAPS SELECTED TO 10 DEGREES HYDRAULIC PRESSURE DROPPED TO 0 PSI ALTERNATE GEAR EXTENSION USED. FOUND THRUST REVERSER ACCUMULATOR SPLIT IN TWO. WHICH DRAINED ALL HYDRAULIC FLUID AND PUT HOLE IN REAR FUSELAGE. 1. ACCUMULATOR REPLACED SYSTEM GROUND TSDR 20010117AP001Engine · flamed outENGINE FLAMED OUT DURING CRUISE-FOUND EXCESSIVE CORROSION OF COMPRESSOR CASINGSDR 20001016SH006Control Unit · malfunctionedCMH - LOST CABIN PRESSURIZATION AFTER DEPARTURE OUT OF COLUMBUS. RETURNED TO CMH. INSPECTED BLEED AIR LINES IN HEX HOSE AND IN CABIN, RAN BOTH ENGINES, NO LEAKS FOUND. TEST FLEW AIRCRAFT TO 27,000 FEET. ALL FUNCTIONS, PRESSURIZATION SYSTEM, CHECKED GOOD. SDR 20000329SH050Starter Gen · failedDURING FLIGHT ON 1-10-2000, PILOT NOTICED VIBRATION IN AIRCRAFT, SHORTLY THEREAFTER, GENERATOR OFF-LINE. PILOT LANDED AIRCRAFT AT GJT. STARTER/GENERATOR WAS REPLACED AND GROUND TESTED NORMAL. AIRCRAFT RETURNED TO BASE AT PSP. (X)SDR CA991209027Transceiver · malfunctioned(CAN) AFTER FLYING THROUGH RAIN ON APPROACH, COMMUNICATION RADIOS BECAME GARBLED/UNREADABLE. BENCH CHECK OF UNITS REVEALED TRANSCEIVER UNITS TO BE INTERNALLY CONTAMINATED WITH WATER. NO LEAKS IN THE NOSE CONE COULD BE FOUND.SDR 95ZZZX6579Hose · failedPILOT STATED LT NACELLE ANTI-ICE INOP AND TRIPPING CIRCUIT BREAKER ON LANDING. AFTER REMOVAL OF TOP COWLING, FOUND HOSE CONNECTING ANTI-ICE TUBE AND ANTI-ICE TEE TUBE WAS TORN IN HALF CAUSING EXPELLED BLEED AIR TO DISCONNECT ANTI-ICE VALVE POWER WIRE FROM CAN
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