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 = '182L' 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 = '182L' 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 2022FA0000027Screw · missingTHROTTLE CABLE PORT THROUGH FIRE WALL OUTER SLEEVE LOST LOWER SCREW ALLOWING SHIELD FIREWALL GROMMET ATTACHMENT PART (S-352) HOUSING OF SEAL TO WEAR INTO THE CABLE ALMOST 1/2 WAY INTO INTERIOR CABLE, CAUSING INTERIOR CABLE TO BEGIN TO BIND. REPLACED CABLE WITSDR 2020FA0000500Oil Filter · looseAFTER A FLIGHT FROM CENTRAL ARKANSAS TO SOUTHERN MISSOURI WITH OVERNIGHT STAY, WHILE CONDUCTING A POST FLIGHT INSPECTION THE PILOT REPORTED EXCESSIVE OIL ON THE AIRCRAFT BELLY AND ENGINE COWLING. WHEN QUESTIONED, THE PILOT REPORTED THAT A POST FLIGHT INSPECTSDR 2020FA0000499Oil Filter · looseDURING SCHEDULED OIL CHANGE ON A CONTINENTAL O-470-R RECIPRICATING ENGINE THE MECHANIC NOTED THE TEMPEST OIL FILTER, PART NUMBER AA48110-2, HOUSING APPEARED TO SEPERATING FROM THE BASE AS INDICATED BY A LINE OF UNPAINTED METAL AT THE JUNCTURE OF THE BASE AND HSDR 2018FA0000451Pump · failedNEW VACUUM PUMP FAILURE 3P194-AFC.SDR 2016F00214Tube · brokenWHILE PERFORMING A PART 91 FLIGHT TRAINING, PILOTS EXPERIENCED CONTROL YOKE OSCILLATION. RETURNED TO AIRPORT WITHOUT INCIDENT. DURING INSPECTION, FOUND TRIM TAB TUBE BROKEN AS SECONDARY DAMAGE. BELIEVE PRIMARY FAILURE OF ELEVATOR COUNTER BALANCE WEIGHT ATTACSDR KC2R20140812002Impulse Coupling · crackedDURING ROUTINE 500 HOUR INSPECTION OF MAGNETO, THE IMPULSE COUPLING WAS FOUND TO BE CRACKED. CRACKS ORIGINATE FROM SHARP CORNERED FEATURE OF IMPULSE COUPLING FLYWEIGHT BASE PLATE. THIS CORNER FORMS THE FULL ADVANCE STOP OF THE IMPULSE COUPLING. CRACK DISCOVERESDR KC2R20140812001Impulse Coupling · crackedDURING ROUTINE 500 HOUR INSPECTION OF MAGNETO, THE IMPULSE COUPLING WAS FOUND TO BE CRACKED. CRACKS ORIGINATE FROM SHARP CORNERED FEATURE OF IMPULSE COUPLING FLYWEIGHT BASE PLATE. THIS CORNER FORMS THE FULL ADVANCE STOP OF THE IMPULSE COUPLING. CRACK DISCOVSDR 2012FA0000025Cylinder · peelingMETAL PARTICLES WERE FOUND IN OIL FILTER DURING OIL CHANGES, APPROX 100 HRS AFTER MAJOR O/H. ALL CYLINDERS WERE REMOVED AND INSPECTED. FOUND NR 5 CYLINDER NICKLE PLATING PEELING AT THE BASE OF THE CYLINDER. PISTON AND RINGS WERE SCUFFING THE PEELING AREA CRSDR MROA20102Cylinder · leakingROUTINE DIFFERENTIAL COMPRESSION TEST RESULTING IN A 48/80 READING WAS CAUSED BY A LEAKING EXHAUST VALVE. THE CYLINDER ASSY WAS R & R WITH A NEW CYLINDER ASSY.SDR 2010FA0001154Piston · crackedACFT WAS IN CRUISE FLIGHT AND EXPERIENCED AN ENGINE FAILURE. THE CASE WAS CRACKED ABOVE THE NR5 CYLINDER AND INSP THROUGH THE OIL FILLER TUBE REVEALED TNE NR5 PISTON WAS COMPLETELY DESTROYED. THIS ENGINE WAS O/H 17 YEARS AGO. INSP REVEALED THE ACFT IS CURRESDR 2009FA0000721Attach Fitting · damagedCOMPIED WITH AD72-07-09 DATED 10/17/74 BY INSP AND FOUND SIGNS OF WORKING AT LEFT SIDE AND RIGHT SIDE AFT VERTICAL FIN ATTACHMENT BOLTS. PERFORMED DYE PENETRANT INSP IAW PARA C,1, D, 1 AND 2 WITH NO CRACKS FOUND. CHECKED ATTACHMENT HOLES FOR EXCESSIVE ELONGASDR 2007FA0000334Bulkhead · crackedSMALL CRACK AT RUDDER CABLE CUTOUT IB, APPROX .2500 INCH, NO CAUSE.SDR BLB2004F00000Starter · failedTWO OVERHAULED STARTER WERE INSTALLED ON OVERHAULED ENGINE. BOTH STARTERS FAILED TO TURN OVER ENGINE, REINSTALLED OLD STARTER AND ENGINE STARTED AS NORMAL.SDR CA031015010Bulkhead · cracked(CAN) RIVETS LOOSE AT TOP OF ANCHOR DOUBLERS ON BOTH SIDES AND CRACK STARTING ON RIVET ON LEFT SIDE DOUBLER FOR ANCHOR NUT TO RECEIVE HORIZONTAL STAB FRONT ATTACH BOLTS.SDR 2003FA0000375Bulkhead · crackedTHE AFT FUSELAGE BULKHEAD WAS CRACKED IN THE RADIUS AT THE RUDDER STOP ATTACHEMENT POINTS. BLOCK RUDDER WHEN A/C IS TIED DOWN IN WINDY CONDITIONS.SDR 2003FA0000363Bulkhead · crackedTHE AFT FUSELAGE BULKHEAD WAS CRACKED IN THE RADIUS AT THE RUDDER STOP ATTACHMENT POINTS.SDR AUS20020716Piston · damaged(AUS) PISTON DAMAGED DUE TO DETONATION. PISTON RINGS BROKEN AND OIL RETURN DRAIN HOLE ENLARGED.SDR 2002FA0000751Nozzle · looseAIRCRAFT MADE AN EMERGENCY LANDING DUE TO LOSS OF POWER. FOUND CARBURETOR MAIN JET VERY LOOSE (REQUIRED TWO COMPLETE FINGER TIGHT TURNS TO TIGHTEN). THE TAB WASHER THAT LOCKS THE MAIN JET HAD NOT BEEN LOCKED, ALL THE TABS WERE FLAT IN A "AS NEW" CONDITION.SDR 2002FA0000012Valve · wornCOMPRESSION TEST INDICATED NR 1 AND NR 2 CYLINDERS HAVE EXHAUST LEAKS. REMOVED CYLINDERS AND DIMENSIONALLY INSPECTING VALVES AND GUIDES. SEVERE WEAR OF BOTH GUIDE AND VALVE.SDR 2002FA0000011Guide · wornCOMPRESSION TEST INDICATED NR 1 AND NR 2 CYLINDERS HAVE EXHAUST LEAKS. REMOVED CYLINDERS AND DIMENSIONALLY INSPECTING VALVES AND GUIDES. SEVERE WEAR OF BOTH GUIDE AND VALVE.SDR 2002FA0000010Exhaust Rocker · mismanufacturedTHE INSTALLED EXHAUST ROCKERS WERE PN 534398. THEY EXPLAINED THAT THOSE ROCKERS DID NOT HAVE THE HOLE DRILLED TO SQUIRT OIL ON THE EXHAUST VALVE STEM. THE NEW EXHAUST ROCKER HAS THAT SQUIRTER HOLE TO AID IN LUBRICATION. THIS WAS CAUSE OF FAILURE, PER MFG. SDR 2001FA0000078Bulkhead · crackedCRACKS IN THE UPPER OUTBOARD CORNERS OF THE RUDDER CABLE CUT-OUTS ON THE 0712616-1 BULKHEAD ASSEMBLY. AREA IN WHICH CRACK OCCURS IS RELATIVELY THIN GAUGE MATERIAL THAT APPARENTLY PROVIDES LITTLE STRUCTURAL STRENGTH. THE FLANGES IN THIS AREA DO LITTLE MORE THSDR 20010511CW008Bulkhead · crackedFAILED INSPECTION DUE TO CRACKS IN CRITICAL AREAS, REPLACED.SDR CA000414011Hub · damaged(CAN) PROP HUB DAMAGED IN RETENSION AREA.SDR 98ZZZX2230Muffler · failedTHE MUFFLER WAS OBTAINED FROM THE MANUFACTURER IN JUNE, 1996. IT WAS INSTALLED ON THE AIRCRAFT JUNE 5, 1996. MAY 30, 1998, AT ANNUAL INSPECTION, THIS MUFFLER WAS FOUND TO HAVE ONE OF THE INTERNAL CONES MORE THAN 50 PERCENT BURNED OUT. THE CALENDAR TIME WAS SDR 98ZZZX1178Bulkhead · crackedBULKHEAD FOUND CRACKED AT RIGHT RUDDER STOP APPROXIMATELY .50 INCH LONG. REMOVED AND REPLACED BULKHEAD ASSY. THIS REPORT SUBMITTED IN C/W AD 72-07-09.SDR 97ZZZX4872Points · weakFOUND POINTS WITH VERY LOW SPRING TENSION. CAUSED ENGINE TO RUN ROUGH AND QUIT IN FLIGHT AT HIGHER RPM'S.SDR 96ZZZX5913Mount · corrodedDURING ANNUAL INSPECTION, FOUND HEAVY CORROSION AT FORWARD END OF ENGINE MOUNT MAIN BEAMS AND DIAGONAL BRACE TUBES ON BOTH SIDES. CAUSE OF CORROSION-PROXIMITY OF EXHAUST COLLECTORS TO MOUNT. CORRECTIVE ACTION-INSTALL HEAT SHIELDS AFTER PAINTING WITH HEATPROOSDR 96ZZZX3206Fuel Cap · water leakFUEL CAPS LEAKING WATER INTO FUEL TANKS WHEN EXPOSED TO RAINY WEATHER. CORRECTED BY INSTALLING CESSNA 182L, SN 59229, (WW OVAL PLATES) FROM MONARCH AIR AND DEVELOPMENT, INC.SDR 95ZZZX4473Reinforcement · corrodedANNUAL INSPECTION FOUND SEVERE CORROSION AT STA 65.33 BELOW FLOORBOARDS. STEEL REINFORCEMENT HAD CORRODED BADLY. SURROUNDING STRUCTURE STARTED TO CORRODE. REINFORCEMENT IS MAJOR STRUCTURE FOR LANDING GEAR BULKHEAD, PN 0710600, AND IS FASTENED WITH HI-SHEAR SDR 95ZZZX4431Cylinder · crackedCYLINDER SHOWED LOW COMPRESSION. DETAILED INSPECTION REVEALED CRACK IN EXHAUST VALVE AREA ON HEAD NEAR VALVE EXHAUST PORT. CYLINDER WAS PREVIOUSLY WELDED IN THIS AREA. CYLINDER SCRAPPED. EXCHANGE UNIT INSTALLED. NO WAY OF KNOWING TIME SINCE NEW ON THIS CYSDR 95ZZZX4429Bulkhead · crackedDURING ANNUAL INSPECTION OF AIRCRAFT, NOTED WHAT APPEARED TO BE VERY SMALL CRACKS RADIATING FROM PROP SPINNER BULKHEAD FASTENER HOLES. CRACKS VERY SMALL. CONFIRMED USING EDDY CURRENT INSPECTION AND ZYGLO. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA. N
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