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 = 'CJ6106' 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 = 'CJ6106' 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 KC8A20121116001Engine · flamed outDURING CLIMBOUT FROM KOSC EN ROUTE TO KJFK THROUGH FLIGHT LEVEL 390, THE RIGHT ENGINE FLAMED OUT. ATC WAS CONTACTED, A LOWER ALTITUDE AND RETURNED TO KYIP WAS REQUESTED. DURING DESCENT THROUGH THE RE-LIGHT ENVELOPE, THE ENGINE WAS RE-STARTED AND THE AIRCRAFTSDR 2011F00033Filter · contaminatedCABIN WAS PRESSURIZING BUT PILOT REPORTED ERRATIC CABIN RATE OF CLIMB AND ELECTED TO RETURN TO BASE. MX CHECKED TAILCONE FOR PRESSURE LEAKS NONE FOUND. MX CHECKED PRESSURE CONTROLLER AND FOUND CONTAMINATION IN THE FILTER WHICH APPEARED TO BE AN INSECT. REPLSDR KC8AN76CKEngine · flamed outLT ENGINE FLAMED OUT AT 40,000FT, DURING CRUISE IN TURBULENT AIR. PILOT DESCENDED TO A LOWER ALTITUDE AND PERFORMED A SUCCESSFUL RELIGHT OF THE ENGINE. NO ABNORMAL ENGINE PERFORMANCE ISSUES NOTED. ACFT CONTINUED TO THE INTENDED DESTINATION. THE ACFT LANDED, WSDR HAEA200800205APump · failedENGINE RPM ROLLED BACK FL430 PLUS 30 MINUTES. AIRCRAFT DESCENDED TO FL 150 AND DIVERTED TO GSP. MAINTENANCE DISCOVERED ENGINE DRIVEN FUEL PUMP FAILED. REPLACED FUEL CONTROL/FUEL PUMP ASSY. NO FURTHER DEFECTS.SDR G41A2007003Engine · flamed outLEARJET N26AT WAS ON THE WAY FROM ELP TO LAX AT FL 410, THE CREW WAS EXPERIENCING SEVERE WEATHER AND REQUESTED TO GO TO FL 450. DURING THE CLIMB THEY HIT TURBULENCE AND THE LT ENGINE FLAMED OUT. THEN REQUESTED TO GO DOWN TO FL 250, RELIT THE LT ENGINE, THEN SDR N76CK80606Engine · fodCREW REPORTED RT FIRE WARNING LIGHT FLICKERING WHEN POWER LEVER WAS PULLED BACK TO THE IDLE POSITION. NO SECONDARY INDICATIONS NOTED. FOUND EXHAUST CASE LEAKING AT A FLANGE BOSS. FURTHER INVESTIGATION AFTER REMOVAL OF THE EXHAUST CASE, FOUND SLIGHT TURBINE FODSDR KC8A0608001Gasket · blownPILOT REPORTED RT ENGINE FIRE WARNING LIGHT FLICKERING ON DESCENT WITH POWER LEVER REDUCED TO IDLE SPEED. FOUND EXHAUST CASE, CENTER BODY, UPPER RIGHT STRUT SUPPORT FLANGE GASKET BROKEN. REPLACED GASKET WITH NEW GASKET. PERFORMED ENGINE RUN UP AND LEAK-CHECK OSDR HAEA200600191Engine · power lossAIRCRAFT ENCOUNTERED TURBULENCE AT FL430 AND RT ENGINE LOST POWER. AIRCRAFT DESCENDED AND ENGINE REGAINED POWER AT FL250. MAINTENANCE PERFORMED POST OPERATION INSPECTION. NO VISIBLE INTERNAL/EXTERNAL DAMAGE OR FLUID LEAKAGE EVIDENT ON ENGINE OR COMPONENTS. SDR 4262006N236CACompressor Wheel · fodAT 285 KNOTS AT FL270 THE LT ENGINE WENT DOWN TO 20 PERCENT N1. THE AIRCRAFT DIVERTED AND LANDED UNEVENTFUL. MAINTENANCE FOUND FOD ON THE 1ST STAGE OF THE COMPRESSOR.SDR CED2006F00000Rudder Pedal · stiffTHE FLIGHT CREW ABORTED TAKEOFF ROLL. THE FLIGHT CREW NOTICED ON TAKEOFF ROLL THAT THE RUDDER PEDALS FELT STIFF AND HAD VERY LITTLE MOVEMENT. MAINTENANCE INSPECTED AIRCRAFT RUDDER CONTROL CABLE SYSTEM AND FOUND NO DEFECTS. (K)SDR CED2006F00021Engine · shutdownTHE NR 2 ENGINE SHUTDOWN. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND DIVERTED WITHOUT INCEDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. ADDITIONAL INFORMATION WILL BE SUPPLIED AT YOU REQUEST AFTER MAINTENASDR CED2006F00020Indicator · defectiveTHE AIRCRAFT ABORTED TAKEOFF ROLL, THE NR 2 ENGINE WAS NOT MAKING TAKEOFF EPR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A DEFECTIVE EPR GAUGE. MAINTENANCE REPLACED THE DEFECTIVE GAUGE. (K)SDR CED2006F00005Altimeter · failedON DEPARTURE, THE CAPTAIN`S ALTIMETER FAILED. REMOVED AND REPLACED ALTIMETER. SYSTEM OPS CHECK GOOD. (K)SDR CED2006F00010Engine · malfunctionedHAD TO ABORT THE TAKEOFF WHILE ATTEMPTING TO DEPART. THE REASON FOR THE ABORT WAS THAT THE NR 2 ENGINE WOULD NOT PRODUCE TAKEOFF FOR THE CONDITIONS. MAINTENANCE CHECKED AIRCRAFT AND FOUND IT TO MAKE TAKEOFF EPR ON PERFORMANCE RUN. (K)SDR CED2006F00018Insulator · dirtyWHILE DESCENDING THROUGH FL 220 FOR APPROACH INTO AIRPORT, THE NR2 FIRE LIGHT CAME ON MOMENTARILY. IMMEDIATELY REDUCED THE RT THRUST LEVER TO IDLE. MAINTENANCE INSPECTED AIRCRAFT AND FOUND BAD FIRE LOOP CONNECTION. (K)SDR CED2006F00023Engine · malfunctionedON TAKEOFF ROLL, THE NR 2 ENGINE WOULD NEVER PRODUCE TAKEOFF . THE CREW ABORTED TAKEOFF ROLL AND EXITED THE RUNWAY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS. ALL ENGINE PARAMETERS WERE WITHIN NORMAL LIMITATIONS. (K)SDR 7032005N213CAHose · kinkedENROUTE, UPON THE AIRCRAFT REACHING ITS ASSIGNED LEVEL OF FL 430 POWER WAS REDUCED FOR CRUISE AND THE NR 2 ENGINE QUIT. AIRCRAFT DESCENDED TO FL 250 AND THE ENGINE WAS RESTARTED. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. (K)SDR 6252004N8005YCabin Pressure · malfunctionedWHILE ENROUTE, AT FLIGHT LEVEL 410 THE CABIN ALTITUDE EXCEEDED 10000 FT, THE FLIGHT CREW FOLLOWED THE CHECKLIST PROCEDURES AND DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. I WSDR 6242004N238CAFire Loop · out of positionON DECENT, THE FLIGHT CREW RECEIVED INDICATION OF FIRE IN THE NR1 ENGINE. THE FLIGHT CREW PERFORMED THE CHECKLIST AND COULD NOT CANCEL THE FIRE LIGHT. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE CREW INSPECTED THE AIRSDR 2006FA0000120Static Line · looseWHILE ENROUTE, CABIN ALTITUDE EXCEEDED 10,000 FT. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES BUT WAS UNABLE TO RETURN THE CABIN PRESSURIZATION WITHIN NORMAL PIRAMETERS. THE FLIGHT CREW DECIDED TO DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. UPON INSPECTSDR CED2006F00007Tire · destroyedON TAKEOFF ROLL THE AIRCRAFT BLEW THE LT MAIN GEAR TIRES IN ELP. (K)SDR CED2006F00019Fire Detector · false activationWHILE ENROUTE, THE CREW EXPERIENCED INDICATION OF FIRE ON THE NR2 ENGINE. THE CREW THEN FOLLOWED THE EMERGENCY CHECK LIST AND COULD NOT EXTINGUISH THE FIRE LIGHT. THE CREW THEN DECLARED AN EMERGENCY AND LANDED AT THEIR DESTINATION WITHOUT FURTHER INCIDENT. SDR CED2006F00014Element · false indicationAFTER TAKEOFF AT FLIGHT LEVEL 220, THE CREW OBSERVED A FIRE INDICATION LIGHT ON THE NR 1 ENGINE. THE FLIGHT CREW FOLLOWED STANDARD EMERGENCY PROCEDURES AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. ONCE BACK, MAINTENANCE FOUND THE FIRE LOOP ELEMENT TOUSDR CED2006F00008Case · crackedWHILE ENROUTE, AT FLIGHT LEVEL 390, FLIGHT CREW OBSERVED A FIRE INDICATION ON THE NR 2 ENGINE. THE FLIGHT CREW WAS ABLE TO EXTINGUISH THE FIRE INDICATION LIGHT USING STANDARD EMERGENCY PROCEDURES. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND RETURNED TO DESDR CED2006F00017Plate · malfunctionedON DESCENT, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LT THE ENGINE RUNNING AT IDLE AND LANDED WITHOUT INCIDENT. (K)SDR 2004F00421Engine · shutdownAT FL370, THE NR 2 ENGINE SHUTDOWN. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND DIVERTED TO LIT WITHOUT INCIDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. ADDITIONAL INFORMATION WILL BE SUPPLIED AT YOUR REQUSDR 2004F00338Control Cable · brokenTHROTTLE CABLE BROKEN 12 INCHES FROM END OF CABLE. BROKEN AT AFT END OF FORWARD CABLE WHERE FORWARD CABLE ATTACHES TO AFT CABLE. (SO13200405891)SDR HAEA200400165Landing Gear · lack of lubeLANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. AIRCRAFT RETURNED TO BASE. MAINTENANCE LUBED LANDING GEAR AND PERFORMED GEAR SWING. CYCLED GEAR AT LEAST 20 TIMES WITH NO FAILURE. MAINTENANCE ITEM CLEARED. [CLOSED]SDR CED2004F00004Fire Warning · false activationWHILE ENROUTE, THE CREW EXPERIENCED INDICATION OF FIRE ON THE NR 2 ENGINE. THE CREW THEN FOLLOWED THE EMERGENCY CHECK LIST AND COULD NOT EXTINGUISH THE FIRE LIGHT. THE CREW THEN DECLARED AN EMERGENCY AND LANDED AT THEIR DESTINATION WITHOUT FURTHER INCIDENT. SDR 00141Engine · flamed outAIRCRAFT ENCOUNTERED TURBULENCE AT FL390K. LT ENGINE FLAMED OUT. ENGINE RELIGHT NORMAL.SDR CED2004F00003Fuel Sys · leakingON TAKEOFF ROLL AND INITIAL CLIMB OUT, FUEL WAS OBSERVED LEAKING FROM THE LEFT WING TIP. ATC INFORMED THE CREW OF THE LEAK AND INSTRUCTED THEM TO COME AROUND AND LAND. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LT FUEL VENT AND FOUNSDR CED2004F00002Fire Detector · malfunctionedAFTER TAKEOFF AT FLIGHT LEVEL 220 THE CREW OBSERVED A FIRE INDICATION LIGHT ON THE NR 1 ENGINE. THE FLIGHT CREW FOLLOWED STARNDARD EMERGENCY PROCEDURES AND RETURNED WITHOUT FURTHER INCIDENT. ONCE BACK IN MAINTENANCE FOUND THE FIRELOOP ELEMENT TOUCHING THE COSDR CED2004F00001Case · crackedWHILE ENROUTE, AT FLIGHT LEVEL 390 FLIGHT CREW OBSERVED A FIRE INDICATION ON THE NR 2 ENGINE. THE FLIGHT CREW WAS ABLE TO EXTINGUISH THE FIRE INDICATION LIGHT USING STANDARD EMERGENCY PROCEDURES. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND RETURNED WITH NSDR 00140Engine · flamed outPILOT REPORTED LT ENGINE FLAMED OUT AT FL430 IN SEVERE TURBULANCE ON TRIP FROM HKS TO LRD. ENGINE RELET NORMALLY AT FL 250. CONTINUED TRIP TO LRD. MAINTENANCE PERFORMED INSPECTION IN ACCORDANCE WITH GE M/M 77-00. AIRCRAFT RETURNED TO SERVICE.SDR 2004F00424Engine · stalledON DESCENT INTO MEMPHIS, TN, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LEFT THE ENGINE RUNNING AT IDLE AND LANDED WITHOUT INCIDENT. (M)SDR 00133Engine · flamed outPILOT REPORTED, LT ENGINE FLAMED OUT CLIMBING THRU FL38.5, ENGINE RELET AT FL25. CONTINUED FLIGHT WITH NO FURTHER PROBLEM, PILOT INSPECTED ENGINE AT DESTINATION NO FOD DAMAGE OR LEAKS, AIRCRAFT ROUTED TO MAINTENANCE BASE. YIP, MAINTENANCE PERFORMED FLAMEOUT SDR 00132Engine · flamed outPILOT REPORTED RT ENGINE FLAMMED OUT CLIMBING THROUGH FL 39.5 AIRCRAFT DIVERTED TO GRI. MAINTENANCE DISPATCHED FROM ADS, FOUND NO FOD DAMAGE OR LEAKS, RESTRICTED AIRCRAFT 39K ALT AND HAD AIRCRAFT FLOWN TO ADS. WILL UPDATE AFTER FURTHER MAINTENANCE. CORRECTION SDR 00131Engine · flamed outPILOT REPORTED LT ENGINE FLAMED OUT CLIMBING FROM FL 370. WILL UPDATE THIS SDR AFTER MAINTENANCE. LT ENGINE REMOVED FOR HSI INSPECTION NO ABNORMAL WEAR REPORTED, PERFORMANCE RUN COMPLETED, ENGINE AND AIRCRAFT RETURN TO SERVICE.SDR CED2004F00000Tire · separatedON CLIMB OUT, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR NUMEROUS TIMES WITH NO CHANGE IN THE UNSAFE INDICATION, THEY THEN RETURNED WITHOUT INCIDENT AND NOTICED THE NOSE WHEEL TIRE WAS MISSING TREAD. UPON INSPECTION OF THE AIRCRAFT, FOUSDR 2004F00223Nozzle · damagedBRO - ON CLIMB-OUT, THE NR 1 ENGINE FLAMED OUT AT 39,600 FEET. THE AIRCRAFT DESCENDED TO FLIGHT LEVEL 25,000 FEET AND RESTARTED THE ENGINE. THE AIRCRAFT THEN DIVERTED TO ADS, AND LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS INSPECTED AND THE EXHAUST NOZZLE SDR 2004FA0000020Pump · leakingINSTALLED OVERHAULED FUEL PUMP FROM MFG ON 4NOV03. DURING AIRCRAFT INSPECTION 22DEC04 HAD FUEL SEEP FROM WIRES ON PUMP.SDR CED2003F00000Filter · inoperativeON NOV 20, 2003, THE AIRCRAFT EXPERIENCED LOW FUEL PRESSURE WARNING LIGHTS. UPON INVESTIGATION OF THE DISCREPANCY WE CHANGED THE FUEL FILTERS BECAUSE THE FELT SEAL HAD CONE UNGLUED AND CLOGGED THE FILTER. THE AIRCRAFT WAS IN FOR A INSPECTION OF THE 15 NOV 20SDR 00117Engine · flamed outPILOT REPORTED LT ENGINE FLAMED OUT WHILE CLIMBING TO FL410 IN CONTINOUS LIGHT TO MODERATE TURBULANCE, NO EMERGENCY WAS DECLARED, RELIGHT NORMAL AT FL250, CLIMB TO FL390 FOR REMAINDER OF TRIP, INSPECTION OF ENGINE CONDUCTED AT THE COMPLETION OF TRIP NO FOD OR SDR 00107Engine · flamed outPILOT REPORTED LT ENGINE FLAMED OUT CLIMBING FROM FL400 TO FL410 NORMAL RESTART PERFORMED AND RETURN TO FL410 FOR REMAINDER OF FLIGHT WITH NO FURTHER PROBLEM, ENGINE INSPECTED IAW MM AT YIP BASE REPLACED T2 LINE AND OPS CHECKED GOOD.SDR 2003FA0001156Starter · vibrationWHILE IN CRUISE FLIGHT AT 370, THE FLIGHT CREW HEARD TWO FLUTTERING VIBRATION SOUNDS. THE VIBRATION NOISES BECAME LOUDER AND LOUDER. ADJUSTING THE THROTTLE ISOLATED THE VIBRATION TO THE NR 1 ENGINE. THE PILOTS DESCENDED TO FL 250 AND SHUT DOWN THE NR 1 ENGISDR 00100Uplock Switch · inoperativePILOT REPORTED GEAR WOULD NOT RETRACT AFTER DEPARTING YIP, CREW RETURNED TO YIP WITH GEAR DOWN AND LOCKED INDICATION. MAINTENANCE CLEANED LUBED AND ADJUSTED ALL UPLOCK SWITCHES IAW LEAR M/M AIRCRAFT RETURNED TO SERVICE.SDR 00098Engine · flamed outPILOT REPORTED RT ENGINE FLAMED-OUT CLIMBING THRU FL410 FOR FL430. DESCENDED AND RELIGHT NORMAL, CLIMB BACK TO FL410 FOR REMAINDER OF LEG. UPDATE AFTER MAINTENANCE. AIRCRAFT RESTRICTED TO FL410.SDR 00096Engine · flamed outPILOT REPORTED LT ENGINE FLAMED-OUT WHILE CLIMBING FROM FL42.5 FOR FL430, DESCEND AND RELIGHT. WILL UPDATE AFTER MAINTENANCE. MAINTENANCE PERFORMED ENGINE INSPECTION AND GROUND RUNS IAW WITH GE M/M AIRCRAFT RETURNED TO SERVICE.SDR 00095Engine · flamed outPILOT REPORTED WHILE CLIMBING FROM 410 TO 430 THE LT ENGINE FLAMED-OUT. DESCEND TO RELIGHT ALTITUDE, RELIGHT AND CLIMB BACK TO 410 FOR THE REST OF FLIGHT. WILL UPDATE AFTER MAINTENANCE. NO DEFECTS NOTED. RESTRICTED AIRCRAFT TO FL410.SDR 00094Engine · flamed outPILOT REPORTED LT ENGINE FLAME-OUT WHILE CLIMBING THRU 41,300 FT. DESCEND AND RELIGHT PERFORMED. UPDATE AFTER MAINTENANCE.
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