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 aircraft_model_key = '750' 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 aircraft_model_key = '750' 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 2001F00326Battery · overtempFOUND RIGHT BATTERY OVERTEMPED 75 DEGREES CELSIUS, SHUT OFF BATTERY AND RETURNED TO DTW. REPLACED BATTERY, CLEANED TEMP SENSOR CONNECTOR. (M)SDR 2001F00336Squat Switch · out of adjDTW - NOSE GEAR WOULD NOT RETRACT. ADJUSTED NOSE GEAR SQUAT SWITCH RAMP. (M)SDR DXT2001F00001Brake · looseSPECIAL BOLTS BETWEEN STRIKER AND PISTON HOUSING WERE LOOSE AND WERE BACKED OFF APPROX 114 INCH. BRAKE TORQUE BUTTON HAS WORN A GROOVE AROUND THE INNER CIRCUMFERENCE AT THE WHEEL.SDR 20010511CW013Alternator · failedCREW STATED RIGHT HAND WINDSHIELD HEAT INOPERATIVE. TROUBLESHOT TO FAULTY LEFT HAND ALTERNATOR. UPON ALTERNATOR REMOVAL, NOTICED THAT THE COOLING FAN BLADES ON THE ALTERNATOR WERE ALL BROKEN OFF.SDR 20010509CW003Pump · failedAC ON DECENT WHEN AMBER EICAS INDICATION OF HYD VOLUME LOW(A) ILLUMINATED. FLIGHT CREW CONFIRMED THE EICAS INDICATION WAS AN ACTUAL PROBLEM BY VIEWING EICAS WHICH SHOWED, HYD LEVEL AT 16 PERCENT AND DECREASING. PRESSURE DROPING AND FLUID TEMP INCREASING. FLIGHSDR 20010323CW018Computer · inoperativeAFTER INITIAL POWER UP OF THE AIRCRAFT THE CREW NOTED A FAILED NR 2 AHRS INDICATION ON THE COPILOTS PRIMARY FLIGHT DISPLAY. FAILED NR 2 AHRS COMPUTER. REPLACED NR 2 AHRS COMPUTER WITH SERVICEABLE UNIT AND COMPLETED OPERATIONAL CHECKS.SDR 20010208CW013Actuator · malfunctionedAFTER LANDING AT PDU THE RED GEAR UNLOCK LIGHT IN THE GEAR SELECTOR HANDLE ASSEMBLY ILLUMINATED AND THE GEAR WARNING HORN SOUNDED. WHILE TAXING TO PARKING THE GEAR WARNING INDICATIONS CEASED AND ALL INDICATIONS RETURNED TO NORMAL. AFTER PARKING THE AIRCRAFT,SDR 20001027SH001Sensor · faultyAGC - FLT 14740 - AFTER TAKEOFF WHILE IN CRUISE, CREW REPORTED THE NR 1 BATTERY AS INDICATING AN OVERHEAT CONDITION. THE CREW ISOLATED THE BATTERY WITH THE BATTERY SWITCH AND MONITORED THE TEMPERATURE PER THE EMERGENCY CHECK LIST. THE TEMPERATURE CONTINUED TSDR 20001017SH023Computer · failedKDTW - FLT 14223 - FLAPS FAILED AFTER TAKEOFF. FAILED RIGHT FLAP POSITION RESOLVER. REPLACED RIGHT FLAP RESOLVER, RIGGED AND CHECKED FLAPS IAW CESSNA CITATION X MM. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. (X)SDR 20000817SH011Control Handle · failedTHE AIRCRAFT DEPARTED ON THE MORNING OF 7-27-00. AT THIS TIME, THE CREW WAS UNABLE TO RETRACT THE LANDING GEAR AS THE HANDLE WOULD NOT MOVE FROM THE DOWN POSITION. THE LANDING GEAR CONTROL ASSY, PN 9914551-3, FAILED. TROUBLESHOOTING INCLUDED ON OPEN SAFETY SDR 20000814SH011Coupler · meltedCREW MEMBER TURNED ON CABIN COFFEEMAKER, PACIFIC SYSTEMS P/N 1322-1-55 SWITCH PANEL, SHORTLY THEREAFTER, THERE WAS SMOKE IN THE AREA OF 1322 SWITCH PANEL. CREWMEMBER REMOVED CABIN POWER AND SMOKE CEASED. ACFT CONTINUED TO ITS DESTINATION AND LANDED NORMALLYSDR 20000802SH019Tube · brokenSHORTLY AFTER TAKEOFF, THE FLIGHT CREW NOTICED A SUDDEN INCREASE IN THE RIGHT ENGINE ITT (50-60 DEGREES) AND IT BECAME TEMPERATURE LIMITED. ALL OTHER ENGINE PARAMETERS APPEARED NORMAL SELECTING THE OTHER FADEC IN CONTROL HAD NO EFFECT. THE START BLEED CONTRSDR 20000626SH016Module · failedWITH GEAR SELECTED DOWN WITH INDICATION OF ALL THREE GEAR DOWN AND LOCKED ON FINAL INTO KIAD, THE GEAR UNLOCKED LIGHT CAME ON AND LANDING GEAR HORN SOUNDED. MADE UNEVENTFUL LANDING AND TAXI TO FBO PARKING. NO OBSERVED DISCREPANCY TO GEAR OR ELECTRICAL EQUIPMSDR 20000512SH007Retainer · worn**TONY, ENG IN SYS****THE LEFT ENGINE ALTERNATOR CARBON SEAL WAS REPLACED. A SATISFACTORY LEAK CHECK WAS PERFORMED DURING THE GROUND ENGINE RUN CHECKS. THE ENGINE DEVELOPED A LARGE OIL LEAK DURING A TEST FLIGHT AND IT WAS LATER DISCOVERED THE CARBON SEAL RETSDR 20000511SH008Trunnion · looseLEFT NOSE LANDING GEAR TRUNNION LOOSE. THIS IS THE THIRD OCCURRENCE IN A FLEET OF APPROXIMATELY 25 AIRCRAFT. (X)SDR 20000511SH007Trunnion · crackedNOSE GEAR TRUNNION MOUNT PLATES CRACKED OR MISSING FASTENERS. SUBMITTER STATED THIS IS THE THIRD OCCURRENCE OF THIS TYPE IN A FLEET OF APPROXIMATELY 25 AIRCRAFT. (X)SDR 20000511SH006Trunnion · crackedNOSE GEAR TRUNNION MOUNT PLATES CRACKED. THIS IS THE THIRD OCCURRENCE OF THIS TYPE IN A FLEET OF APPROXIMATELY 25 AIRCRAFT. (X)SDR CA991230015Screw · out of position(CAN) THE FLGHT CREW WAS REQUESTED TO TURN RIGHT BY ATC AND FOUND THE AILERON CONTROLS JAMMED. AFTER TRYING TO MANEUVER THE AIRCRAFT, THE CONTROLS RETURNED TO NORMAL WITH A LOUD SNAP. MAINTENANCE FOUND THE LOCK SCREW AND NUT ASSEMBLY, SECURING THE AILERON CABLSDR CA991103057Fgc · failed(CAN) DURING CRUISE FLIGHT, FLIGHT GUIDANCE CONTROLLER A FAIL LIGHT CAME ON.SDR 99ZZZX4324Pump · leakingHYDRAULIC VOLUME LOW 'A' SYSTEM IN-FLIGHT AT FL 410, SHUT DOWN 'A' HYDRAULIC SYSTEM. FOUND 3 EACH SMALL PIN HOLES IN HYDRAUIC PUMP HOUSING. REPLACED ENGINE DRIVEN HYDRAULIC PUMP.SDR 99ZZZX1010Switch · failedDUE TO A NO TAKEOFF WARNING ILLUMINATING AT 90 KNOTS, THE CREW REJECTED TAKEOFF. MAINTENANCE DISCOVERED A LOOSE PROXIMITY SWITCH AT THE AILERON/SPOILER DISCONNECT HANDLE. ADJUSTED PROXIMITY SWITCH AND PERFORMED OPS CHECK. MAINTENANCE RETURNED AIRCRAFT TO SESDR 99ZZZX428Resolver · failedKLGB - AFTER TAKEOFF, PILOT NOTICED FLAP FAIL MESSAGE. DIVERTED AIRCRAFT, RETURNED FOR INVESTIGATION. FLAP OPERATIONAL CHECK PERFORMED. FOUND DEFECTIVE RESOLVER BY COLD SOAKING THE RIGHT WING FLAP RESOLVER. REPLACED RESOLVER AND PERFORMED RIGGING CHECK. SDR 99ZZZX427Resolver · failedKIAD - AFTER TAKEOFF, PILOT NOTICED FLAP FAIL MESSAGE. DIVERTED AIRCRAFT, RETURNED FOR INVESTIGATION. FLAP OPERATIONAL CHECK PERFORMED. FOUND DEFECTIVE RESOLVER LOCATED RIGHT WING FLAP. REPLACED RESOLVER AND PERFORMED RIGGING CHECK. PERFORMED OPERATIONAL SDR 98ZZZX3336Flexshaft · brokenFLAPS FAILED DURING EXTENSION. SLATS EXTENDED. FLAPS MOVED ABOUT .50 INCH, BOTH FLAPS FAIL CAS MESSAGE. FOUND BROKEN RIGHT HAND INBOARD FLEXSHAFT.SDR 98ZZZX2708Beam · looseDURING C/W SB 750-27-11, BOTH AILERON PCU'S WEEPING HYD FLUID. PCU'S REPLACED AND SB ACCOMPLISHED. ACFT RIGGED AND TESTED IAW CE750 MM. ON NEXT FLT, COCKPIT EICAS MESSAGES INDICATED AILERON PCU RIGGING INADEQUATE. HYD SERVICE UNIT RE-INSTALLED, RIGGING RSDR 98ZZZX1732Switch · looseWHEN RETRACTING LANDING GEAR, (GEAR UNLOCKED) LIGHT STAYED ILLUMINATED ON CLIMB-OUT. INSPECTED LANDING GEAR AND PERFORMED FUNCTIONAL HYDRAULIC TEST ON JACKS. (GEAR UNLOCKED) LIGHT STAYED ILLUMINATED ON FIRST RETRACTION. TIGHTENED BACKSHELL ON LT UPLOCK SWITSDR 98ZZZX1930Pitot Mast · obstructedAT EIGHTY KNOTS, THE NR 1 ADC (AIR DATA COMPUTER) FAILED AND THE FLIGHT CREW ABORTED TAKEOFF. THE AIRCRAFT RETURNED TO THE RAMP AND MAINTENANCE CONFIRMED THE NR 1 PITOT TUBE WAS OBSTRUCTED. REPLACED THE PITOT TUBE MAST.SDR 98ZZZX1102Steering Unit · malfunctionedDURING TAXI AFTER LANDING, AIRCRAFT STARTED TO TURN LEFT WITHOUT INPUT TO TILLER OR RUDDER PEDALS. AIRCRAFT EXAMINED AND NO APPARENT CAUSE WAS IDENTIFIED. CONTACTED CESSNA AND REQUESTED A REPLACEMENT STEERING UNIT. TECHNICIANS FOR ICT AND LGB CAME TO PHX ANSDR 98ZZZX558Strut · frozenOPERATOR REPORTED UPON DEPARTURE, ACFT GEAR HANDLE COULD NOT BE PUT UP TO RETRACT GEAR. ACFT RETURNED AND LANDED SAFELY. OUTSIDE AIR TEMPERATURE WAS BELOW ZERO AT DEPARTURE TIME. WHEN THE ACFT WAS JACKED UP, THE NOSE GEAR STRUT FAILED TO EXTEND ALL THE WAY SDR 98ZZZX455Nose Gear · malfunctionedTHE AIRCRAFT DEPARTED DTW AND ON CLIMB-OUT, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION. THE AIRCRAFT RETURNED TO DTW AND MAINTENANCE WAS ABLE TO DUPLICATE. UNDER CESSNA'S RECOMMENDATION, NEW SB 750-32-05 AND SB 750-32-10 INCORPORATED TO ESDR 98ZZZX340Strut · malfunctionTHE AIRCRAFT DEPARTED DTW AND ON CLIMB-OUT, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION. THE AIRCRAFT RETURNED TO DTW AND MAINTENANCE WAS UNABLE TO DUPLICATE. GALLING WAS DETECTED IN THE CHROME SECTION OF THE STRUT ASSY AND THE UNIT WAS SESDR 98ZZZX339Strut · malfunctionTHE AIRCRAFT DEPARTED DTW AND ON CLIMB-OUT, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION. THE AIRCRAFT RETURNED TO DTW AND MAINTENANCE WAS ABLE TO DUPLICATE. UNDER CESSNA'S RECOMMENDATION, NEW SB 750-32-05 AND SB 750-32-10 INCORPORATED TO ESDR 97ZZZX4494Feel Bungee · freeze upPILOT REPORTED RECEIVING 'TRIM LEFT AILERON WARNING' AT FL 41,000, 20,000, AND A FINAL WARNING AFTER LEVELING OFF JUST BELOW 11,000. AFTER EACH OF THE 2 WARNINGS, PILOT DISCONNECTED AUTOPILOT AND FOUND NO DISCREPANCIES. WHEN PILOT DISCONNECTED AUTOPILOT AFTE
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