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 = '182P' 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 = '182P' 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 96ZZZX4806Skin · corrodedBOTH CENTER SECTION SKIN AND CENTER SECTION DOUBLER BADLY CORRODED (WITH HOLES). CORROSION IS APPARENTLY DUE TO 'DRIZ-AIR' DESICCANT SPILLING ONTO CARPET, AND THEN FLOWING BETWEEN SKINS INTO GEARBOX.SDR EY2R9600944Hub · corrodedHUB CORRODED.SDR EY2R9600106Hub · crackedHUB CRACKED IN THREAD AREASDR 96ZZZX4783Valve Guide · oversizeCYLINDER REMOVED FOR LOW COMPRESSION. FOUND EXT VALVE GUIDE .012 INCH OVERSIZE AT ONE END ALLOWING EXT VALVE EXCESS MOVEMENT CAUSING IMPROPER VALVE SEATING. FACTORY NEW CYLINDER INSTALLED. THIS ENGINE FACTORY REMANUFACTURED 6/95.SDR 96ZZZX4765Lifter · spalledCYLINDER REMOVED FOR LOW COMPRESSION. FOUND BOTH LIFTERS STARTING TO SPALL. CHECKED ALL LIFTERS, 9 OF 12 LIFTERS SHOWED EVIDENCE OF SPALLING. FACTORY NEW LIFTERS (ALL 12) INSTALLED. CAM APPEARS OK. THIS ENGINE FACTORY REMANUFACTURED, 6/95.SDR 96ZZZX3571Line · chafedDURING WINDSHIELD REPLACEMENT, FOUND AILERON CONTROL CABLE, WHICH TRAVELS UP THE FORWARD RIGHT DOOR POST, WAS CHAFING ON THE ADJACENT FUEL LINE. ORIGINAL WALL THICKNESS IS .030 INCH AND THE DEPTH OF THE CHAFE WAS .020 INCH.SDR 96ZZZX3539Cap · water leakTHIS AIRCRAFT HAS HAD A LONG HISTORY OF WATER IN THE FUEL. AD 84-10-01 ADDRESSES HOW TO DETERMINE HOW MUCH WATER AN AIRCRAFT WILL OR IS HOLDING, BUT DOES NOT SOLVE THE PROBLEM. NEW 'ZERO' RING (SEVERAL SETS) DID NOT HELP. WATER STILL SEEPED IN AROUND THE CASDR 98ZZZX226Seal · leakSEALS FOR PLASTIC TYPE FUEL CAPS SUPPLIED WITH AIRCRAFT ARE NO LONGER AVAILABLE. DESIGN OF FUEL TANK OPENINGS (FLUSH MOUNT) ALLOWS WATER TO ENTER FUEL TANK IF SEAL INTEGRITY IS LOST.SDR AU960633Bulkhead · cracked(AUS) FORWARD DOORPOST BULKHEAD CRACKED AT RELIEF NOTCHES ON BOTH LH AND RH SIDES - CRACK LENGTH 7MM (0.275IN)SDR AU960540Seat Belt · wrong part(AUS) SEAT BELTS USED AUTOMOTIVE HARDWARE WITH NON MIL-SPEC WEBBING - UNAPPROVED PART - PERSONNEL/MAINTENANCE ERRORSDR AU960507Bulkhead · cracked(AUS) FORWARD DOOR BULKHEAD CRACKEDSDR 98ZZZX4451Valve Guide · wornDURING A ROUTINE COMPRESSION CHECK, THE EXHAUST VALVE WAS FOUND LEAKING ON THE NR 5 CYLINDER. THE REMOVED CYLINDER, EXHAUST VALVE AND GUIDE WERE FOUND WORN OUT. SUBMITTER SUGGESTED CAUSE AS DEFECTIVE PARTS AND/OR ASSEMBLY PROCESS FROM THE FACTORY.SDR 96ZZZX1546Adapter · failedWHEN STARTER WAS ENGAGED, THE PROPELLER MADE APPROXIMATELY ONE-EIGHTH REVOLUTION AND STOPPED. FURTHER ATTEMPTS WITH STARTER WOULD NOT TURN PROPELLER. PROP WAS 'STIFF' TURNING IN DIRECTION OF NORMAL ROTATION. PROP COULD NOT BE TURNED AT ALL IN OPPOSITE DIRECSDR 96ZZZX1263Seat Rail · misrepairedUPON ANNUAL INSPECTION, FOUND SEAT RAILS INSTALLED BY PERSONS UNKNOWN. RAILS WERE INSTALLED WITH MANY MIS-SIZED RIVETS AND SEVERAL WERE NOT BUCKED. TWO FLANGES OR RIBS WERE SMASHED OUT OF PLACE DUE TO PUNCHING OUT THE OLD RIVETS, AND NOT REPAIRED. UPON REMOSDR 96ZZZX2555Valve Guide · looseVALVE GUIDE LOOSENED IN CYLINDER HEAD ALLOWING CYLINDER TO MISFIRE. NOTE: DIFFICULT TO DIAGNOSE. COMPRESSION WAS 55/80 UNTIL SPRING ASSY WAS MOVED. SUBMITTER RECOMMENDS CHECKING SPRING ASSYS FOR SIDE PLAY WHEN VALVE COVERS REMOVED FOR ANY REASON.SDR 98ZZZX4473Valve Guide · wornDURING A ROUTINE COMPRESSION CHECK, THE EXHAUST VALVE ON THE NR 2 CYLINDER WAS FOUND LEAKING. THE REMOVED CYLINDER, EXHAUST VALVE AND GUIDE WERE FOUND WORN OUT. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PARTS OR ASSEMBLY PROCESS AT THE FACTORY.SDR AU960085Bulkhead · cracked(AUS) LH LOWER FORWARD DOORPOST BULKHEAD CRACKED FROM BEND RELIEF NOTCH- FOUND DURING INSPECTION IAW AD/C180/74 AMDT1 AND CESSNA SEB95-19SDR 96ZZZX584Cylinder Assy · boss brokeFOUND NR 5 CYLINDER ROCKER ARM BOSSES BROKEN OFF ON EXHAUST VALVE.SDR 96ZZZX352Switch · failedELT G-SWITCH FAILED CRASH TEST IN ARM POSITION. CHECKED OK IN 'ON' POSITION.SDR 96ZZZX353Cap · defectiveREPLACED DEFECTIVE STOCK GAS CAPS WITH MONARCH AIR AND DEV. CO., INC.'S CAPS.SDR EY2R9600196Retain Bearing · corrodedPROP ASSY RETAIN BEARING CORRODEDSDR EY2R9600195Cylinder · corrodedPROP ASSY CYLINDER CORRODEDSDR EY2R9600194Split Retainer · corrodedPROP ASSY SPLIT RETAINER CRACKEDSDR EY2R9600193Piston Rod Pin · corrodedPROP ASSY PISTON ROD PIN ASSY CORRODEDSDR AU960024Exhaust Valve · worn(AUS) ENGINE CYLINDERS HAD WORN EXHAUST VALVES PN 646286 AND VALVE GUIDES PN 643767 - VALVE STEMS ALSO NECKED - SUSPECT CAUSED BY USE OF MOGASSDR 98ZZZX4522Guide · wornDURING A ROUTINE COMPRESSION CHECK, THE EXHAUST VALVE WAS FOUND LEAKING ON THE NR 1 CYLINDER. THE REMOVED CYLINDER HAD A WORN OUT EXHAUST VALVE AND GUIDE. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PARTS OR ASSY PROCESS AT THE FACTORY.SDR 98ZZZX4521Valve · wornDURING A ROUTINE COMPRESSION CHECK, THE EXHAUST VALVE WAS FOUND LEAKING ON THE NR 1 CYLINDER. THE REMOVED CYLINDER HAD A WORN OUT EXHAUST VALVE AND GUIDE. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PARTS OR ASSY PROCESS AT THE FACTORY.SDR 95ZZZX1737Cell · deterioratedFUEL BLADDERS DETERIORATED AND LEAKING, CAUSING SEVERE LEAKAGE, RT WING ROOT.SDR 95ZZZX2039Buss · miswiredDURING TROUBLESHOOTING A FLASHING BEACON PROBLEM, FOUND BEACON WIRED TO AVIONICS SPLIT BUSS AND WOULD NOT WORK UNTIL AVIONICS MASTER WAS TURNED ON (2ND AIRCRAFT IN 1 MONTH). THIS SITUATION COULD BE A PROBLEM IF THE AIRCRAFT WAS IFR AND LOSE THE POWER RELAY OR
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