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 = '182Q' 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 = '182Q' 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 AU990769Cylinder · separated(AUS) CYLINDER HEAD SEPARATED FROM BARREL.SDR 99ZZZX2379Bulkhead · deformedSPINNER BULKHEAD WAS ASSEMBLED INCORRECTLY DURING PREVIOUS REPLACEMENT CAUSING BULKHEAD TO BECOME DEFORMED AND SPINNER TO WOBBLE.SDR 99ZZZX2157Impulse Coupling · corrodedBOTH INMPULSE COUPLINGS ARE REJECTED DUE TO RUST ON AND AROUND THE PAWLS AND RIVETS.SDR 99ZZZX3478Pin · brokenNOSE GEAR WOULD NOT LOCK DOWN. AFTER MASTER WAS SHUT OFF, NOSE GEAR COLLAPSED CAUSING DAMAGE TO PROPELLER, NOSE GEAR DOORS, AND COWL FLAP DOORS. THE TWO LOCKING PINS ATTACHED TO ACTUATOR CYLINDER WERE LOOSE/BROKEN AND FLOATED OUT TO TOUCH THE ACTUATING CYLINSDR AU990080Seat Belt · frayed(AUS) SEAT BELT FRAYED.SDR AU990079Battery · corroded(AUS) ELT BATTERIES LEAKING. BATTERY CASE CORRODED. BATTERIES WERE TWELVE MONTHS OUT OF DATE.SDR AU990053Mount · cracked(AUS) ENGINE MOUNT CRACKED AS INDICATED IN AD/CESSNA180/4 AMDT1. PART TC: 1,880.SDR 99ZZZX338Valve Guide · wornDURING A ROUTINE 100-HOUR INSPECTION, THE NR 4 CYLINDER WAS FOUND TO HAVE LEAKAGE PAST THE EXHAUST VALVE. FURTHER INVESTIGATION REVEALED A WORN OUT EXHAUST VALVE GUIDE. REPLACING THE GUIDE AND RE-FACING THE EXHAUST VALVE RESOLVED THE PROBLEM. SUBMITTER SUGGSDR CA981022013Seal · missing(CAN) DURING FLT WITH PARTIAL CARB HEAT, EGT GAUGE DROPPED STEADILY TO MINS. ALL OTHER ENG PARAMETERS NORMAL AND UNCHANGED. FULL CARB HEAT APPLIED WITH MIX RICH PER POH AND CARB ICE, IMMEDIATE LOSS OF ENG POWER WITH ROUGH RUNNING AND ENG STOPPED DUE TO OVERRSDR 98ZZZX4466Oil Cooler · crackedDURING A ROUTINE INSPECTION, A CRACK WAS FOUND ON THE OIL COOLER NEAR THE AFT, LOWER SUPPORT, STRUT ATTACH POINT (WELD). SUBMITTER SUGGESTED POSSIBLE CAUSE AS IMPROPER WELDING DURING MANUFACTURE OR REMANUFACTURE.SDR 98ZZZX4464Intake Valve · wornDURING AN INSPECTION REQUIRED BY TCM CSB98-1B, TITLED INTAKE AND EXHAUST VALVE INSPECTION, THE INTAKE VALVE TIPS ON THE NR'S 2, 4, AND 6 CYLINDERS WERE FOUND EXCESSIVELY WORN. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PARTS INSTALLED INTO THE ENGINE AT SDR 98ZZZX3050Flap · jammedPILOT REPORTED DURING DAY VFR FLIGHT, FLAPS JAMMED WHILE IN RETRACT MOTION. INITIAL INSPECTION ON THE GROUND REVEALED THE RT FLAP COCKED SIDEWAYS AND CONTACTED THE AILERON. FLAP TRACKS AND ROLLERS HAD NO LUBRICATION AND LOWER FLAP LIMIT SWITCH WAS OUT OF ADJSDR AU981175Bearing · failed(AUS) MAIN CRANKSHAFT BEARING BROKEN. CRANKCASE THROUGH BOLT P/N 641931-10-75 BROKEN. ALL CYLINDER FLANGE NUTS LOOSE. CRANKCASE MATING FACES FRETTED AND CRANKCASE CRACKED. METAL CONTAMINATION OF OIL FILTER. PART TC: 1,618.SDR 98ZZZX2621Line · failedA HYDRAULIC INDICATOR WAS INSTALLED IN THE AIRCRAFT UTILIZING AN EXISTING 'TEE' ON THE HYDRAULIC POWER PACK. THE FLARE ON THE LINE GOING TO THE HYDRAULIC PRESSURE GAUGE FAILED CAUSING THE LINE TO BLOW OUT OF ITS 'B' NUT. THE HYDRAULIC FLUID SUPPLY WAS SUBSEQSDR 98ZZZX1019Skin · corrodedFOUND CORROSION UNDER FACTORY INSTALLED BLACK INSULATION PADS BONDED TO FUSELAGE BELLY SKINS UNDER CABIN FLOOR AND FUSELAGE SIDE SKINS. RECOMMEND REMOVAL OF ALL PADS AND TREAT CORROSION IAW SM AND AC 43-13-1A.SDR 98ZZZX4469Crankcase · crackedDURING A ROUTINE OIL CHANGE, A CRACK WAS FOUND IN THE CRANKCASE THAT RADIATES ABOUT ONE INCH TOWARDS THE CENTER OF THE ENGINE STARTING FROM THE FORWARD UPPER HOLD DOWN STUD ON THE NR 5 CYLINDER. THE ENGINE WAS RETURNED TO THE FACTORY FOR A CRANKCASE REPLACEMESDR 98ZZZX4493Lifters · pittedDURING A ROUTINE COMPRESSION CHECK, THE NR 2 CYLINDER EXHAUST VALVE WAS FOUND LEAKING. AFTER THE CYLINDER WAS REMOVED, ALL CAM LIFTERS FOUND PITTED AND THE NR 5 CYLINDER INTAKE CAM LOBE FOUND SCOURED. THE ENGINE REMOVED FROM SERVICE. SUBMITTER SUGGESTED POSSDR 98ZZZX824Cylinder Assy · wornDURING ANNUAL COMPRESSION CHECK, FOUND CYLINDERS COMP LOW. INSPECTED CYLINDERS, FOUND INTAKE VALVES SEAT EXCESSIVELY WORN. FURTHER INSPECTION FOUND ALL CERMACHROME ON CYLINDERS WORN AWAY. ALL CYLINDERS REPLACED WITH FACTORY NEW CYLINDERS.SDR CA971223011Carburetor · failed(CAN) SEVERE CARBURETOR FLOODING ON GROUND RUN-UP, HARD STARTING AND FOULING OF SPARK PLUGS. FUEL WAS SEEN LEAKING FROM THE CARBURETOR. ENGINE FAILED TO SHUTDOWN USING MIXTURE CONTROL AND SEVERE BACKFIRING OCCURRED. THE CARBURETOR WAS REPLACED AND THE PROBSDR 98ZZZX762Flap · jammedON APPROACH, PILOT SELECTED THE FLAP POSITION. THE RIGHT FLAP JAMMED AND TWISTED INTERFERRING WITH CONTROL OF THE RIGHT AILERON. PILOT LANDED WITHOUT INCIDENT. SUSPECT CAUSE WAS THE WING ATTACHING POINT SHOWED THE ROLLERS BEING LUBRICATED, BUT WERE WORN; THSDR AU971365Transponder · failed(AUS) TRANSPONDER FAULTY. FOUND DURING TEST IAW AD/RAD/47 AND AD/RAD/43SDR 97ZZZX4669Valve · wornINSPECTION FOUND THE NITRALOY GUIDES WORE THE EX VALVE STEMS LEAVING STEPS IN THE STEM AT THE ENDS OF TRAVEL IN THE GUIDE. ONE VALVE HAD .070 INCH WEAR. SUBMITTER STATED CONTINENTAL SHOULD ISSUE A BULLETIN OR SERVICE LETTER ALERTING MECHANICS OF THIS PROBLEMSDR 97ZZZX4525Drain Tube · leakingWHILE PERFORMING 100-HOUR INSPECTION, NOTICED DRAIN TUBE FROM BATTERY BOX HAD BEEN LEAKING ACID INTO REAR FUSELAGE. SUBMITTER STATED THIS BATTERY BOX IS MOUNTED RIGHT OVER CONTROL CABLES AND CABLES COULD BE DAMAGED.SDR 97ZZZX4268Carburetor · not markedCARBURETORS BEING PRODUCED BY PRECISION AIRMOTIVE ARE NOT IN COMPLIANCE WITH MARVEL-SCHEBELER AD 63-22-03. THE LETTER 'V' IS NOT STAMPED UNDER THE SERIAL NUMBER. SUBMITTER STATED REQUIRE PRECISION AIRMOTIVE TO RECTIFY ALL THE CARBURETORS THEY HAVE PRODUCED TSDR 97ZZZX3903Carburetor · stuckPILOT REPORTED AT CRUISE, PREPARED FOR DESCENT, THROTTLE STUCK FUEL OPEN. AIRCRAFT LANDED AND SHUT OFF ENGINE WITH MIXTURE. UPON INSPECTION, DISCONNECTED THROTTLE, FOUND PROBLEM TO BE IN CARBURETOR. BUTTERFLY VALVE STUCK FULL, WILL NOT CLOSE. CARBURETOR RESDR 20010417AP001Knob · backed outCLIMBING VFR OUT OF KLAS, NOTED VVI AND AIRSPEED INDICATING ZERO, AND ALTIMITER FROZEN. PULLED ALTERNATE STATIC KNOB AND INDICATIONS RETURNED TO NORMAL. AFTER LANDING, FOUND RUBBER TRIM PIECE AROUND ALTERNATE STATIC KNOB HAD COME UNGLUED FROM METAL MOUNTING SDR 98ZZZX4465Valve Guide · wornDURING A ROUTINE COMPRESSION CHECK, LEAKAGE WAS FOUND PAST THE EXHAUST VALVE ON THE NR 3 CYLINDER. THE REMOVED CYLINDER, EXHAUST VALVE AND GUIDE WERE FOUND WORN OUT. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PARTS AND/OR ASSEMBLY PROCESS FROM THE FACTOSDR AU970549Cylinder · broken(AUS) NO4 CYLINDER HEAD SEPARATED FROM THE BARREL - INVESTIGATION FOUND THAT THE FAILURE OCCURRED AT THE TOP OF THE THREADED SECTION OF THE HEAD TO BARREL JUNCTIONSDR AU970540Crankshaft · cracked(AUS) CRANKSHAFT CONTAINED TWO CRACKS IN NO6 CONNECTING ROD WEB - CRANKCASE BEARING TUNNEL OUT OF LIMITS - DAMAGE CAUSED BY HEAVY LANDING AND PROPELLER STRIKESDR 97ZZZX1843Stiffener · crackedSTIFFENER HAS BEEN REPLACED 4 TIMES IN APPROXIMATELY 90 HOURS. EACH TIME IT CRACKS IN THE SAME AREA IN THE SAME WAY. ALL OTHER ATTACHING PARTS ARE NEW. IT APPEARS METAL IS TOO LIGHT OF A GAUGE OR IT IS BEING IMPROPERLY HEAT TREATED OR BOTH. CESSNA OFFERS CSDR AU970315Pipe · damaged(AUS) LH BRAKE LINE PUNCTURED BY `PK' TYPE SCREW FITTED FOLLOWING REPAINTING - LOSS OF BRAKE FLUID - PERSONNEL/MAINTENANCE ERRORSDR CA970421009Fitting · broken(CAN) NOSE GEAR FAIRING REMOVED. THE LOWER NOSE GEAR FITTING WAS FOUND BROKEN. NEW FITTING ORDERED.SDR AU970356Actuator · seized(AUS) ELEVATOR TRIM TAB ACTUATOR SEIZED - INVESTIGATION FOUND THE ACTUATOR JACK SCREW TO BE CORRODED (RUSTY) OVER THE ENTIRE LENGTH WITH NO EVIDENCE OF LUBRICATION - CAUSED BY A COMBINATION OF HIGH PRESSURE WASHES REMOVING GREASE FROM THE JACK AND OPERATIONS ISDR AU970359Bearing · damaged(AUS) NOSE AND MAIN WHEEL BEARINGS SEIZED - ALL BEARINGS WERE DRY AND THE LITTLE GREASE REMAINING WAS ALSO HARD AND DRY - SUSPECT CAUSED BY USE OF HIGH PRESSURE WATER DURING PAINT STRIPPINGSDR AU970888Roller · worn(AUS) LH FLAP ROLLERS PNO T-1221010-5 AND PNO R-0523921X3 WORN - FLAP JAMMED ON TRACK SUPPORT BRACKETSSDR AU970117Connecting Rod · failed(AUS) CONNECTING ROD END CAP SEPARATED - PRELIMINARY INVESTIGATION INDICATES FAILURE IN AREA APPROXIMATELY 10MM (0.393IN) ABOVE THE BOLT SHOULDER ON THE CAMSHAFT SIDE BEHIND THE HARD FACE FOR THE BEARING SHELL PROGRESSING OUTWARDS UNTIL FAILURE FROM OVERLOAD -SDR AU971218Bulkhead · cracked(AUS) FUSELAGE DOOR POST BULKHEAD CRACKED IN AREA OF STRESS RELIEF NOTCH. CRACK LENGTH 3.175MM (0.125IN). FOUND DURING INVESTIGATION IAW AD/180/75 AMDT1.SDR AU970084Cylinder · worn(AUS) ENGINE CYLINDER BORES EXCESSIVELY WORN IN TOP AND BOTTOM AREAS OF THE CYLINDER. PISTON RING CAUGHT IN WORN GROOVE CAUSING IT TO BREAK. ENGINE HAS CHROMED CYLINDERS INSTALLED AND IT IS SUSPECTED THAT THE ENGINE WAS OPERATING WITHOUT ADEQUATE LUBRICATION.SDR 97ZZZX1101Adapter · leakPILOT REPORTED LOW OIL PRESSURE IN-FLIGHT. UPON INSPECTION, FOUND OIL LEAKING FROM OIL FILTER ADAPTER. REMOVED ADAPTER, INSTALLED NEW O-RING AND REINSTALLED. NO FURTHER LEAKS FOUND.SDR 97ZZZX511Nipple · failedWHILE CHANGING FUEL LINE CONNECTION HOSES ON LT AND RT FUEL BLADDER, NIPPLES BROKE OFF, NO EVIDENCE OF CRACKING OR PREVIOUS LEAKAGE NOTED. SUSPECT CAUSE OLD AGE?SDR 97ZZZX510Nipple · failedWHILE CHANGING FUEL LINE CONNECTION HOSES ON LT AND RT FUEL BLADDER, NIPPLES BROKE OFF. NO EVIDENCE OF CRACKING OR PREVIOUS LEAKING NOTED. SUSPECT CAUSE - OLD AGE?SDR 98ZZZX4467Camshaft · scoredA ROUTINE OIL CHANGE AND OIL FILTER INSPECTION REVEALS EXCESSIVE METAL. FURTHER INVESTIGATION FINDS THE CAMSHAFT HAS FAILED ON CERTAIN CAM LOBES. ENGINE IS REMOVED FROM SERVICE. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PART.SDR 96ZZZX5405Duct Adapter · door brokenDURING AN INVESTIGATION FOR DAMAGE FROM AN INTAKE FIRE, THE ALTERNATE AIR DOOR WAS FOUND BROKEN LOOSE FROM THE FIBERGLASS AIR DUCT. THIS AIRCRAFT HAS BEEN MODIFIED IAW A PETERSON 260 SE/STOL CONVERSION. THIS DOOR COULD BLOCK THE AIR FLOW TO THE INTAKE SYSTEMSDR 96ZZZX5223Support · crackedINSPECTION FOUND BATTERY SUPPORT CRACKED. SUSPECT CAUSE IS TIME IN SERVICE. SHOULD BE THICKER MATERIAL.SDR 98ZZZX4470Valve Guide · wornDURING A ROUTINE COMPRESSION CHECK, LEAKAGE WAS FOUND ON THE EXHAUST VALVES ON THE NR 1 AND NR 3 CYLINDERS. THE REMOVED CYLINDERS, EXHAUST VALVES AND GUIDES WERE FOUND WORN OUT. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PARTS AND/OR ASSSEMBLY PROCES FRSDR 96ZZZX4756Balance Tube · chafedBOTTOM COWL SHOCK MOUNT WAS FOUND CHAFING AGAINST INTAKE BALANCE TUBE ON THE ENGINE. THIS WOULD CAUSE AN INDUCTION LEAK. SAME CONDITION NOTICED ON SEVERAL 182'S. ACTT: 1,281 HOURS. SHOCK MOUNT, P/N S1115-29.SDR CA960808101Metering Pin · worn(CAN) PILOT HAD PROBLEM WITH THROTTLE STICKING. CARBURETOR HEAT WAS APPLIED AND THE PROBLEM WAS RECTIFIED. AS CARBURETOR ICING WAS SUSPECTED THE PROBLEM WAS NOT REPORTED. ON THE RETURN FLIGHT THE THROTTLE STUCK AGAIN, AND COULD NOT BE FREED. POST FLIGHT INSDR 96ZZZX3885Fuel Cap · seal failedFUEL CAP ASSY HAD TO BE REPLACED WITH MONARCH AIR AND DEVELOPMENT FUEL CAP AND INLET ASSY DUE TO THE UNAVAILABILITY OF REPLACEMENT PARTS. LEAKING SEALS.SDR 96ZZZX3679G Switch · failedDURING 100-HOUR INSPECTION, PULLED ELT FOR FUNCTION CHECK, G-SWITCH WOULD NOT TRIGGER ON IMPACT. ELT WOULD FUNCTION IN ON POSITION. ELT REPLACED.SDR 96ZZZX3448Support · crackedTHIS AIRCRAFT IS MODIFIED PER STC SA00152W1 AND THE ITEM IS PART OF THE MODIFICATION. THIS SUPPORT WAS CRACKED TWO-THIRDS THE WAY THROUGH; AND, IF HAD BROKEN OFF, WOULD HAVE LET THE FUEL CONTROL UNIT SLIP DOWN AND CAUSE A VERY LEAN MIXTURE AND A POSSIBLE ENGI
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