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 = '172R' 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 = '172R' 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 20010409CW016Cylinder · crackedAIRCRAFT WAS 4 MILES FROM AIRPORT WHEN A LOUD BANG WAS HEARD AND THE ENGINE STARTED VIBRATING AND MISSING. PILOT PULLED POWER BACK TO IDLE AND LANDED SAFELY AT AIRPORT. INSPECTED ENGINE AND FOUND NR 3 ENGINE CYLINDER WITH A CRACK, HALF AROUND CYLINDER. THISSDR 20010320CW002Bolt · mismanufacturedTHE SIX A2513-92 PROPELLER MOUNTING BOLTS ARE APPROX .250 INCHES TOO SHORT. THEY ARE THREE THREADS TOO SHORT FROM BEING FLUSH WITH THE BACK SIDE OF THE PRESSED IN NUT ON CRANKSHAFT FLANGE. A LONGER BOLT (APPROX .250 IN) WOULD CORRECT THIS PROBLEM. THIS AIRSDR 20010228CW001Resistor · defectiveDURING PHASE 1 INSPECTION, RT FUEL QUANTITY READING WAS ERRATIC. THE SHAFT BEARING OR SEAL WAS FOUND TO BE DEFECTIVE ON THE RT SENDER. THIS APPARENTLY ALLOWED GASOLINE INTO THE SENDER.SDR 20010209CW007Firewall · crackedFOUND 1.8 IN LONG CRACK IN FIREWALL. CRACK IS LOCATED BEHIND COWL SHOCKMOUNT BRACKET AT RIGHT FIREWALL STEP. REPAIRED CRACK IN ACCORDANCE WITH SB.SDR 20010302AP004Engine · malfunctionedI AM A STUDENT PILOT AND WAS AT 3000 FT AT A LEVEL CRUISE AND THE ENGINE SHUTTERED FOR APPROX. 1-3 SECONDS. WE NEVER LOST POWER AND CONTINUED ON. APPROX. 20 MINUTES LATER AT 2000'''' THE SAME CONDITION OCCURED. MY FLIGHT INSTRUCTOR FELT THAT WATER HAD PASSEDSDR CA010119007Pan · cracked(CAN) DURING A 100 HOUR INSPECTION, IT WAS OBSERVED THAT THE SEAT PAN ASSEMBLY THAT SUPPORTS THE LOWER SET CUSHION ON BOTH PILOT AND CO-PILOT SEAT HAD A CRACK APPROXIMATELY 2 1/2 INCH TO 3 INCH LONG, RADIATING FROM BOTH REAR CORNERS TO THE LIGHTENING HOLES JUSSDR 20001214SH018Bungee Cylinder · weakPILOT EXPERIENCED POOR STEERING, RAN OFF RUNWAY IN CROSSWIND CONDITION. FOUND LEFT AND RIGHT STEERING BUNGEES WEAK. PULLED TESTED BOTH ORIGINAL BUNGEES, ACTUATOR STARTED ABOUT 20 - 25 POUNDS PULL. NEW BUNGEES PULL TESTED 60 - 65 POUNDS PULL. (X)SDR 20001214SH017Bungee Cylinder · weakPILOT EXPERIENCED POOR STEERING, RAN OFF RUNWAY IN CROSSWIND CONDITION. FOUND LEFT AND RIGHT STEERING BUNGEES WEAK. PULLED TESTED BOTH ORIGINAL BUNGEES, ACTUATOR STARTED ABOUT 20 - 25 POUNDS PULL. NEW BUNGEES PULL TESTED 60 - 65 POUNDS PULL. (X)SDR 20001206SH026Crankshaft · failedTHIS ACFT RECEIVED NEW FROM CESSNA FACTORY. UPON REMOVAL OF PROPELLER TO FACILITATE INSTALL OF AFTERMARKET AIR CONDITIONERS, NOTED THAT 2 OF THE 4 PROPELLER ALIGNMENT BUSHINGS THAT ARE PRESSED INTO THE CRANKSHAFT FLANGE WERE EXTRUDED FROM THE BACKSIDE OF THE SDR 20001103SH008Gyro · fluctuatesDIRECTIONAL GYRO PRECESSES ABOUT 5 DEGREES EVERY 10 MINUTES IN-FLIGHT. WITH VACUUM SYSTEM TEST KIT INSTALLED, DG PRECESSES ABOUT ONE-HALF DEGREE EVERY 15 MINUTES. ON THE NEW CESSNA AIRCRAFT, THE INSTRUMENTS AS WELL AS THE INSTRUMENT PANEL ARE HARD MOUNTED TOSDR 20001018SH031Mount · tornCONDITION: COWLING MOUNT TORN. CORRECTIVE ACTION: REPLACED WITH NEW. (X)SDR 20001106SH087Support Fitting · groovedDURING INSPECTION, FOUND RT FLAP, INBOARD HINGE, INBOARD FLAP SUPPORT ARM WAS GROOVED BY THE AFT BEARING CHAFING ON IT. SUBMITTER STATED THIS CONDITION IS USUALLY FOUND AT THE FORWARD BEARING AREA. FIRST TIME THIS FACILITY HAS SEEN IT IN THE AFT BEARING AREASDR 20001106SH086Support Fitting · groovedDURING INSPECTION, FOUND RT FLAP, INBOARD HINGE, INBOARD FLAP SUPPORT ARM WAS GROOVED BY THE AFT BEARING CHAFING ON IT. REPLACED BOTH THE INBOARD AND OUTBOARD SUPPORT A;RMS. SEB 95-3 ADDRESSES INSPECTING THESE AREAS. (X)SDR 20001218SH033Gyro · inoperativeDIRECTIONAL GYRO REPORTED INOPERATIVE BY PILOT. DURING REPLACEMENT OF DG, NOTED THE CASE UNDER THE DATA PLATE WAS DENTED IN. SUSPECT THAT THE SERIAL NUMBER WAS STAMPED ON DATA PLATE RESULTING IN DENTED CASE. (X)SDR CA001012011Bearing Support · cracked(CAN) DURING ROUTINE INSPECTION, RUDDER PEDAL TORQUE TUBE SUPPORT BEARING FOUND CRACKED IN HALF AT APPROXIMATELY THE CENTER OF THE UPPER BEARING HALF. BEARING HALVES WERE BOTH REPLACED. BEARING FAILURE APPEARS TO HAVE OCCURED DUE TO MANUFACTURING DEFECT. (XSDR 20001101SH001Master Switch · malfunctionedWHEN AVIONICS MASTER SWITCH STARTS TO FAIL, IT WILL ONLY TURN ON THE NR 1 COM. ALL OTHER AVIONIC COMPONENTS ARE CONTROLLED BY THE BATTERY MASTER. (X)SDR 20001012SH028Reservoir · crackedPILOT REPORTED FUEL DRIPPING FROM UNDER ACFT. MECH DETERMINED IT WAS DRAIN VALVE. DRAIN VALVE REPLACED. FUEL CONTINUED TO DRIP FROM THE VALVE. INVEST SHOWED THE LEAK WAS COMING FROM THE LOWER LEADING EDGE SEAM OF THE RESERVOIR TANK. AFTER REMOVAL, 2 INCH SDR CA000926014Alternator · seized(CAN) ALTERNATOR SEIZED. BELT PULLEY SHEARED FROM MAIN DRIVESHAFT. (X)SDR 20000907SH010Mount · looseDURING ANNUAL INSPECTION, FOUND HORIZONTAL STABILIZER LOOSE AT FORWARD MOUNT BOLTS, PLAY VISIBLY NOTICEABLE AND ACCOMPANIED BY LOUD CREAKING NOISE. (X)SDR 20000821SH010Bearing · looseCOPILOT''S LEFT RUDDER PEDAL FOUND EXCESSIVLEY LOOSE AT DUAL BRAKE TUBE DURING 100-HOUR INSPECTION. FURTHER INVESTIGATION REVEALED BEARING, PN S1003-43A, NOT INSTALLED. INSTALLED NEW BEARING. SUBMITTER SUSPECTED BEARING NOT INSTALLED AT FACTORY. AIRCRAFT TSDR AU000568Engine · failed(AUS) ENGINE FAILED ON TAKEOFF RESULTING IN A FORCED LANDING. AIRCRAFT DAMAGED. GROUND RUNS ON ENGINE COULD NOT REPLICATE FAULT AND ENGINE RAN OK.SDR 20000821SH005Air Filter · deterioratedAIR FILTER IS LISTED AS A 500-HOUR REPLACEMENT ITEM. AT 100-HOUR INSPECTION, MADE AT 300 HOURS, NOTED THE INSPECTION AT 200 HOURS AND THE INSPECTION AT 300 HOURS THE PAPER ELEMENT OF THE FILTER ASSY HAD BADLY ERODED ON APPROXIMATELY 40 PERCENT OF THE FORWARD SDR 20000508SH007Light · chafedPILOT REPORTED THE RADIO LIGHTS WERE FLICKERING WHILE ENGINE WAS RUNNING. UPON INSPECTION, WIRING BUNDLE THAT RUNS HORIZONTALLY ACROSS BOTTOM OF INSTRUMENT PANEL WAS FOUND CHAFING ON ''''RADIO INSTRUMENT LIGHT POTENTIOMETER'''' PN S2091-9 (REF: R1002 I CESSNSDR AU000120Contactor · burned(AUS) IGNITION SWITCH CONTACTS BURNT/DAMAGED. AIRCRAFT IS NOT SUBJECT TO AD/ELECT/59.SDR 20000427SH019Elt · failedDURING 100-HOUR INSPECTION, ELT SYSTEM WAS TESTED FOR OPERATION. UPON ACTIVATING PANEL MOUNTED REMOTE CABIN SWITCH, PN 2019-10, ELT WOULD NOT TRANSMIT. AFTER REPEATED ATTEMPTS, ELT WOULD SOMETIMES TRANSMIT. ELT WAS REPLACED WITH A SERVICEABLE UNIT, PN 3000-SDR 20000328SH001Engine · malfunctionedENGINE RAN ROUGH AND ALMOST SHUT DOWN DURING DESCENT. (X)SDR 20000329SH048Pump · inoperativeTHE CREW REPORTED THE ELECTRIC BOOST PUMP INOPERABLE. THE PUMP WAS REPLACED. THIS PUMP ROUTINELY FAILS IN THIS FLEET OF 172R AIRCRAFT, AND IN MOST CASES, PRODUCES METAL THAT CONTAMINATED THE FUEL INJECTION COMPONENTS. (X)SDR 20000331SH021Engine · roughTHE ENGINE WAS REPORTED ROUGH IN CRUISE. CORRECTIVE ACTION WAS TAKEN AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X)SDR 20000407SH030Engine · malfunctionedWHILE IN THE PATTERN ON A DUAL FLIGHT, THE ENGINE BEGAN TO RUN ROUGH ON THE CROSS-WIND LEG. IT CONTINUED DOING SO ON DOWN-WIND. AN EMERGENCY WAS DECLARED AND A SUCCESSFUL LANDING WAS MADE. (X)SDR 20000407SH029Engine · malfunctionedDURING FINAL APPROACH, THE ENGINE STUMBLED AND RAN ROUGH. (X)SDR 20000328SH004Rod End · shearedBEARING ROD END THAT ATTACHES STEERING BUNGEE TO STEERING COLLAR SHEARED AT PREVIOUS CRACK AT THE FIRST THREAD. SUBMITTER STATED MAY HAVE HAPPENED AS A RESULT OF ACCIDENT RATHER THAN CAUSE. (X)SDR 20000328SH007Seat · crackedREFERENCE DRAWING 0514222 (SEAT BACK ASSY, AFT BENCH 172) VIEWING THE -1 SEAT BACK ASSY. AT THE LOWER RIGHT HAND CORNER OF THE SEAT BACK THRE IS A -11 FRAME END THAT WELDS TO THE -4 FRAME UPPER. THE WELD IS APPROXIMATELY 7.30 INCHES UP FROM THE BOTTOM OF THESDR 20000427SH014Switch · failedONE-HALF OF SPLIT AVIONICS MASTER BUS SWITCH FAILED. DEFECTIVE HALF OF SWITCH WILL NOT TURN OFF LEAVING SOME AVIONICS SYSTEMS POWER CONTROLLED BY A/C MASTER SWITCH. SWITCH FAILED UNDER NORMAL OPERATING PARAMETERS. POSSIBLE CAUSE OF FAILURE IS DUE TO POOR SWSDR 20000329SH007Flow Divider · malfunctionedDURING FLIGHT, THE PILOT REPORTED ROUGH ENGINE OPERATION FOR A FEW SECONDS. THE FUEL FLOW DIVIDER WAS REPLACED AND THE NR 1 NOZZLE WAS REPLACED. (X)SDR 20000329SH006Spark Plug · dirtyDURING FLIGHT, PILOT REPORTED ROUGH ENGINE OPERATION FOR A FEW SECONDS. THE INJECTOR NOZZLES WERE CLEANED, THE SPARK PLUGS WERE SERVICED, AND THE ELECTRIC BOOST PUMP WAS REPLACED. (X)SDR 20000329SH005Spark Plug · dirtyDURING FLIGHT, THE PILOT REPORTED ROUGH ENGINE OPERATION FOR SEVERAL SECONDS. THE SPARK PLUGS WERE SERVICED. (X)SDR 2000ZZZX713Injector Nozzle · failedPILOT EXPERIENCED A BRIEF ROUGHNESS IN CRUISE. THREE FUEL INJECTOR NOZZLES WERE CHANGED.SDR 20000405SH017Spark Plug · failedENGINE HAD MOMENTARY ROUGHNESS DURING CRUISE. CHANGED ONE SPARK PLUG. INSTALLED NEW SPARK PLUGS. (X)SDR 20000405SH016Nozzle · failedENGINE HAD MOMENTARY ROUGHNESS WHILE IN CRUISE FLIGHT. REPLACED NR 3 CYLINDER NOZZLE. (X)SDR 20000405SH015Spark Plug · failedDURING NORMAL CRUISE, ENGINE RAN ROUGH FOR SEVERAL SECONDS. THE SPARK PLUGS WERE SERVICED. (X)SDR 20000405SH014Manifold · malfunctionedENGINE HAD MOMENTARY ROUGHNESS DURING CRUISE. REPLACED FUEL MANIFOLD. (X)SDR 20000405SH013Spark Plug · failedENGINE HAD MOMENTARY ROUGHNESS WHILE IN CRUISE FLIGHT. REPLACED ALL SPARK PLUGS. (X)SDR 20000405SH012Spark Plug · malfunctionedENGINE HAD MOMENTARY ROUGHNESS DURING CRUISE. CHANGED ONE SPARK PLUG. (X)SDR 20000405SH011Nozzle · malfunctionedENGINE HAD MOMENTARY ROUGNESS WHILE IN CRUISE FLIGHT. REPLACED NR 2 CYLINDER INJECTOR NOZZLE. (X)SDR 20000405SH010Nozzle · dirtyENGINE HAD MOMENTARY ROUGHNESS WHILE IN CRUISE FLIGHT. CLEANED ALL FUEL NOZZLES. (X)SDR 20000405SH009Flow Divider · malfunctionedENGINE HAD MOMENTARY ROUGHNESS WHILE IN CRUISE FLIGHT. REPLACED FUEL FLOW DIVIDER, FUEL SERVO, AND ELECTRIC BOOST PUMP. (X)SDR 2000ZZZX170Control Unit · failedPILOT DETECTED ALTERNATOR OUT LIGHT IN-FLIGHT AND NO OUTPUT ON METER. CYCLED ALT SWITCH AND ALTERNATOR OUT LIGHT STAYED OFF, BUT METER WENT TO FULL CHARGE DEFLECTION. PILOT LANDED WITH NO PROBLEMS. UPON INVESTIGATION, FOUND ALT CONTROL UNIT MELTED INTO AREASDR 20000406SH054Pin · shearedPIN SHEARED. FOUND RT DOOR FORWARD SKIN AT LOWER HINGE AREA IMPROPERLY TRIMMED, EXTENDED TOO FAR FORWARD, CAUSING DOOR TO UNDER-LAP FUSELAGE SKIN AT THE HINGE STRESSING HINGE PIN. NOTE: SUBMITTER STATED LOSS OF THIS LOWER HINGE INTEGRITY IN-FLIGHT COULD LEASDR 99ZZZX4638Pump · failedTHE PILOT REPORTED ZERO FUEL PRESSURE WHEN THE BOOST PUMP WAS TURNED ON. INVESTIGATION REVEALED IT HAD FAILED IN THE PUMP SECTION. THE METAL PARTICLES HAD MIGRATED THROUGHOUT THE FUEL SYSTEM REQUIRING THE INSPECTION, CLEANING, AND REPLACEMENT OF COMPONENTS ASDR 99ZZZX4637Engine · malfunctionedTHE PILOT REPORTED A BRIEF POWER LOSS. THOROUGHLY INSPECTED ENGINE AND COMPONENTS. CLEANED AND INSPECTED SPARK PLUGS, FLOW DIVIDER, INSPECTED FUEL STRAINER AND SERVO SCREEN, CLEANED AND INSPECTED FUEL NOZZLES. A POST-MAINTENANCE GROUND RUN INDICATED NORMAL
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