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 = '182G' 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 = '182G' 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 2018FA0000485Bolt · crackedDURING ACCIDENT INVESTIGATION OF N3267S, THE FORWARD OUTBOARD ATTACH BOLT P/N NAS147-34 HAD A PREEXISTING CRACK AT THE BEGINNING OF THE THREADS FROM THE SHAFT WITH THE PRESENCE OF CORROSION. THIS LEAD TO AN INSTANTANEOUS FAIL OF THE BOLT UPON LANDING AND SPRINSDR CA120718005Snap Ring · failed(CAN) WHILE IN CRUISE FLIGHT, PILOT NOTICED INCREASED RPM AND VIBRATION. PILOT DECREASED RMP AND CARRIED OUT A PRECAUTIONARY LANDING. PROPELLER TECH HISTORY, PROPELLER O/H 21-FEB-11 -AT 1.3 TSO PROPELLER BLADES REPAINTED DUE TO POOR ADHESION -AT 36.1 TSO ACSDR 2011FA0000675Casting · crackedCASTING CRACK FOUND BY VISUAL INSPECTION DURING COURSE OF ANNUAL INSPECTION. THE CRACK IS LOCATED ON THE FORWARD END OF THE SUPPORT CASTING AND RUNS FROM 1/4 INCH FROM MOUNT HOLES ON THE OUTBOARD SIDE TO WITHIN 1/4 INCH OF THE MOUNT HOLES ON THE INBOARD SIDE SDR 2008FA0000146Torque Link · crackedON INSPECTION, A CRACK WAS IDENTIFIED IN THE FORGING FOR THE UPPER TORQUE LINK FOR THE NOSE LANDING GEAR. THE CRACK WAS ON BOTH SIDES OF THE BEAM SECTION ADJACENT TO THE EXTENSION STOP FOR THE GEAR.(AFT SIDE)SDR 2007FA0000840Carburetor · failedPILOT REPORTED THAT AFTER A NORMAL START, HE WAS UNABLE TO ADVANCE THE THROTTLE CONTROL TO CRUISE OR TAKEOFF POWER. A PARTIAL DISASSEMBLY OF THE CARBURETOR REVEALED THAT THE AIR METERING PIN/AIR METERING JET WAS BLOCKING THE THROTTLE SHAFT TRAVEL. THE CARBURSDR CA070823010Torque Tube · loose(CAN) MINOR PLAY (UP AND DOWN) ON THE RT ELEVATOR CAUSE BY LOOSE RIVETS ON THE TORQUE TUBE (TC NR 20070823010)SDR CA060327004Torque Link · cracked(CAN) NOSE GEAR UPPER TORQUE LINK WAS FOUND CRACKED INSIDE UPPER CORNER ON THE LT SIDE. FORGING NR 0543034-497, 2014 KAE-2A (TC NR20060327004)SDR CA041108003Spring · brokenLEFT HAND MAIN LANDING GEAR SPRING ASSEMBLY BROKE OF AT FUSELAGE WHILE TAXIING FOR FLIGHT. THERE WAS NO VISUAL EVIDENCE OF A PREVIOUS CRACK. THE GEAR LEG WAS SENT TO TRANSPORT SAFETY BOARD TO BE ANALYZED.SDR AUS20030693Rivet · faulty(AUS) AILERON MASS BALANCE WEIGHT ATTACHMENT RIVETS FAULTY. APPROXIMATELY HALF OF THE RIVETS FAILED TESTING AND INSPECTION IAW AD/CESSNA180/28.SDR 2003FA0000660Bulkhead · crackedTHIS DEFECT WAS FOUND AS A RESULT OF INSPECTION REQUIRED BY AD. THIS PART WAS REPLACED AT THIS TIME JUNE 17, 2003. TT 5187.97. THIS REPORT REQUIRED BY AD PART (I).SDR 2002FA0000589Air Box · crackedSEVERAL CRACKS IN HOUSING, BOTH IN ALUMINUM AND STAINLESS STEEL. SERVICEABLE PART INSTALLED ABOUT 375 HOURS OPERATING TIME. SUGGEST MORE ATTENTION BE GIVEN THIS ITEM AND THE WAY IT IS ATTACHED, FOR SECURITY. HIGH VIBRATION AREA. CHECK PROPELLER FOR BALANCESDR 20010320CW006Hub · crackedEDDY CURRENT INSPECTION REVEALED A CRACK IN THREADS OR NR1 BLADE HUB SOCKET AT APPROX 7 OCLOCK POSITION WHEN VIEWED FROM SIDE WITH CYLINDER END POINTING UP AND APPROX 1.25 INCH IN LENGTH HUB WAS NOT MODIFIED TO OIL FILL CONFIGURATION.SDR CA001103009Generator · failed(CAN) 4 GENERATORS WERE TRIED ON THIS AIRCRAFT OVER A PERIOD OF 15 - 18 MONTHS, THE END RESULT WAS INSTALLING AN ALTERNATOR KIT, AS THE COMPANY OVERHAULED THE GENERATOR WAS DOING SUBSTANDARD WORK.SDR 20000505SH019Muffler · deterioratedDURING ANNUAL INSPECTION, THE LT INTERNAL BAFFLE WAS FOUND TO HAVE SEPARATED AND WAS PARTIALLY BLOCKING THE EXHAUST PORT IN THE MUFFLER. UPON REMOVAL, THE RT EXHAUST STACK WAS FOUND BADLY DETERIORATED WITH SEVERAL PIECES MISSING. ONLY MINOR EXHAUST LEAK WASSDR 20000505SH018Muffler · separatedDURING ANNUAL INSPECTION, THE LT INTERNAL BAFFLE WAS FOUND TO HAVE SEPARATED AND WAS PARTIALLY BLOCKING THE EXHAUST PORT IN THE MUFFLER. UPON REMOVAL, THE RT EXHAUST STACK WAS FOUND BADLY DETERIORATED WITH SEVERAL PIECES MISSING. ONLY MINOR EXHAUST LEAK WASSDR AU000015Fuel Cell · contaminated(AUS) FUEL SYSTEM CONTAMINATED WITH ETHYLENE DIAMINE. MOBIL BRAND FUEL WAS USED OUTSIDE OF PUBLISHED DATES. CARBURETTOR ALSO CONTAMINATED.SDR 99ZZZX4154Data Plate · detachedPARTIAL POWER LOSS AT FULL THROTTLE WAS EXPERIENCED ON ACFT REGISTERED, 6Y-JDK, PRIOR TO THE COMMENCEMENT OF TAKEOFF ROLL AT KIRKVINE AERODROME IN JAMACIA. SEVERAL FULL POWER CHKS ACHIEVED ONLY 2,350 RPM INSTEAD OF THE REQUISITE 2,600 RPM. ACFT RETURNED TO RSDR 99ZZZX3192Fitting · crackedFOUND CRACK IN LOWEST (AS INSTALLED) RIVET HOLE. INSPECTING SIMILAR (1963-1974) 182'S, SUBMITTER HAS FOUND 3 CRACKS IN A MONTH.SDR 98ZZZX3306Drain Valve · malfunctionedOWNER STATED ONE VALVE WOULD NOT OPEN AND A 'GREENISH STICKY' SUBSTANCE WAS FOU ND IN THE OTHER. REPLACED BOTH WING TANK DRAIN VALVES. CHECKED AND CLEANED ALL FUEL SYSTEM SCREENS AND FILTERS. NO DEFECTS NOTED. DRAINED 5 GALLONS FROM EACH TANK, NO DEBRIS NOSDR CA980814005Skin · wrinkled(CAN) ON LANDING OF FLOAT EQUIPPED AIRCRAFT HIT LARGE WAVE. ON RETURN TO DOCK, INVESTIGATON FOUND THE SIDE SKINS AND LOWER COWL WERE WRINKLED. FURTHER EXAMINATION FOUND THE FIREWALL AND BELLY SKINS WERE ALSO WRINKLED. NEW REINFORCED FIREWALL AND TUNNEL INSTSDR 98ZZZX2449Chain · failedTHE ELEVATOR TRIM BECAME INOPERATIVE WHEN INSPECTED. THE LAST PIVOT PIN OF THE CHAIN WAS FOUND SEPARATED FROM THE SIDE LINK. THIS IS DIFFICULT TO INSPECT BECAUSE IT IS LOCATED INSIDE THE CENTER CONSOLE.SDR 97ZZZX4959Piston · crackedSIX ENGINE PISTONS FOUND CRACKED IN PISTON PIN BOSS. CRACKS WERE ALL IN SAME AREA, UPPER PIN BOSS RUNNING PARALLEL TO PISTON PIN. ONE PISTON HAD LOST ONE-FOURTH OF THE CASTING AROUND PIN. THIS CONDITION DID NOT CAUSE ANY OPERATIONAL PROBLEMS. JUDGING FROM SDR 97ZZZX4798Torque Link · crackedDURING AN ANNUAL INSPECTION, THE UPPER TORQUE LINK OF THE NOSE LANDING GEAR WAS FOUND CRACKED IN THE RADIUS OF THE UPPER FORGED RIB ADJACENT TO THE ATTACH BOLT HOLE. BOTH SIDES WERE CRACKED.SDR CA970609023Blade · stone damage(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE ON FACE AND LEADING EDGE OF PROPELLER BLADES. DAMAGE REPAIRED AND CYLINDER SUPPORT REPLACED.SDR 97ZZZX1861Gear Leg · rustedDURING ANNUAL INSPECTION, RUST WAS NOTICED ON THE LANDING GEAR LEGS (MAIN GEAR) MOST SEVERE RUST WAS FOUND UNDER STOP. METAL WAS RUSTED TO THE POINT OF 'DELAMINATION'. THE RUST APPEARED TO HAVE BEEN CAUSED BY THE GLUE THAT WAS USED BY CESSNA TO HELP ATTACH THSDR 97ZZZX1860Gear Leg · rustedDURING ANNUAL INSPECTION, RUST WAS NOTICED ON THE LANDING GEAR LEGS (MAIN GEAR) MOST SEVERE RUST WAS FOUND UNDER STOP. METAL WAS RUSTED TO THE POINT OF 'DELAMINATION'. THE RUST APPEARED TO HAVE BEEN CAUSED BY THE GLUE THAT WAS USED BY CESSNA TO HELP ATTACH THSDR 97ZZZX867Bulkhead · crackedBULKHEAD WAS FOUND CRACKED AT LEFT RUDDER STOP BOLT AREA. THIS INSPECTION IS REQUIRED BY AD 72-07-09. THE CRACK WAS NOT IN THE AREA CALLED OUT IN THE AD. THE BULKHEAD IS CALLED OUT FOR REPLACEMENT IF FOUND CRACKED.SDR 96ZZZX4985Line · chafingINSPECTION FOUND THE PINS ON THE JUMP DOOR THAT EXTEND INTO THE DOOR POSTS WERE HITTING THE FUEL LINES THAT RUN PARALLEL WITH THE DOOR POST, BOTH FORWARD AND AFT, ON THE RIGHT SIDE. SPLICED IN A NEW SECTION OF TUBING AND ROUTED THE LINES OUT AND AROUND THE PISDR 96ZZZX4984Line · chafingINSPECTION FOUND THE PINS ON THE JUMP DOOR THAT EXTEND INTO THE DOOR POSTS WERE HITTING THE FUEL LINES THAT RUN PARALLEL WITH THE DOOR POST, BOTH FORWARD AND AFT, ON THE RIGHT SIDE. SPLICED IN A NEW SECTION OF TUBING AND ROUTED THE LINES OUT AND AROUND THE PISDR CA960126035Cylinder · cracked(CAN)IN CRUISE ENGINE BEGAN TO RUN ROUGH, AIRCRAFT LANDED AT NEAREST AIRPORT AND GROUND INSPECTION FOUND #5 CYLINDER CRACKED AT THE EXHAUST VALVE & SPARKK PLUG HOLE. CYLINDER REPLACED & AIRCRAFT RETURNED T O SERVICE.SDR 95ZZZX6564Fuel Cap · leakingFUEL CAPS BEGAN LEAKING CAUSING LOSS OF FUEL DURING FLIGHT. REPLACED WITH FUEL CAPS BY MONARCH AIR TYPE SA2376CE.SDR 95ZZZX5957Generator · shortedINVESTIGATION FOR COCKPIT ODOR FOUND UPON OPENING THE BATTERY COMPARTMENT, THE BATTERY WAS EXTREMELY HOT AND MOST OF THE ELECTROLYTE HAD BOILED OUT. TROUBLESHOOTING REVEALED THE FIELD COIL HAD GROUNDED OUT IN THE GENERATOR.SDR 95ZZZX2317Bracket · brokenDURING ANNUAL INSPECTION, GENERATOR BELT WAS FOUND LOOSE. INVESTIGATION SHOWED THE REAR BRACKET OF THE GENERATOR WAS BROKEN. THE BRACKET WAS REPLACED. A/C TOTAL TIME 4,645 HRS. TIME ON PART UNKNOWN.
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