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 = '180H' 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 = '180H' 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 2018FA0000118Camshaft · making metalTHE ENGINE APPEARS TO HAVE FAULTY SET OF LIFTERS CAUSING SEVERE DAMAGE TO THE CAMS. PURCHASED WITH 20 HRS ENGINE TIME. CAMS AND LIFTERS WERE INSPECTED ON PRE-BUY AND FOUND TO BE VISUALLY NORMAL WITH BLUEING STILL PRESENT. PERSISTENT HIGH FE ON REGULAR OIL ASDR CA151117019Engine · malfunctioned(CAN) THE ACFT DESCENDED FROM FL200 WITH THE ENGINE THROTTLE AT IDLE, 61 PERCENT. BEFORE LANDING THE PILOT TRIED TO INCREASE POWER AND THERE WAS NO RESPONSE FROM THE ENGINE. HE ATTEMPTED TO CHANGE THE PROPELLER SPEED TO OBTAIN A CHANGE IN ENGINE POWER THEN THSDR CA140124005Universal Joint · cracked(CAN) WHEN CONTROL YOKE U WAS REMOVED FROM THE ACFT FOR REPAIRS TO SUPPORT STRUCTURE A CRACK WAS FOUND ON BOTH TOP AND BOTTOM SIDES OF CO-PILOT CONTROL YOKE UNIVERSAL JOINT STARTING FROM THE BOLT HOLES AND PROGRESSING TO THE AFT END OF THE U-JOINT. THESE CRACSDR 2013FA0000217Support Bracket · crackedDURING ANNUAL INSPECTION, JACKED ACFT TO CHECK MLG FREE PLAY, AND FOUND THE RT LANDING GEAR OTBD SUPPORT BRACKET RT TO HAVE SOME MOVEMENT BETWEEN ITSELF AND THE FWD AND REAR ATTACHED BULKHEADS. REMOVED GEAR LEG IAW MM AND ONLY AFTER REMOVAL, SPOTTED INTERGRANSDR 2013FA0000216Support Bracket · crackedDURING ANNUAL INSPECTION, JACKED ACFT TO CHECK MLG FREE-PLAY, AND FOUND THE RT LANDING GEAR OTBD SUPPORT BRACKET, RT TO HAVE SOME MOVEMENT BETWEEN ITSELF AND THE FWD AND REAR ATTACHED BULKHEADS. REMOVED GEAR LEG IAW MM AND ONLY AFTER REMOVAL, SPOTTED INTERGRSDR CA050316004Blade · cracked(CAN) PROPELLER, W/O T 64571, RECEIVED FOR 10 YEAR OVERHAUL. LAST OVERHAUL MAY 1996. NOW 667.9 HOUR SINCE OVERHAUL. FOUND BLADE S-90AT-2, SN B34101YS, CRACKED IN BLADE THREADS, FOUND WITH EDDY CURRENT.SDR CA040730007Trim System · contaminated(CAN) ELEVATOR TRIM WHEEL WOULD ONLY MOVE .5 INCH. FOUND DEBRIS CONSISTING OF GRASS, PEANUT SHELLS ETC. A SQUIRRELS NEST JAMMING THE CHAIN (CABLE ATTACHED TO CHAIN) ON THE GEAR WHICH ACTIVATES THE WORM GEAR TO MOVE THE ELEVATOR UP AND DOWN. BECAUSE OF THE SDR CA040527008Bulkhead · crackedBACK PLATE CRACKS FOUND RADIATING FROM RIVET HOLES. AT MANUFACTURING THE TALL SIDE OF RIVET AREAS NOT DEBURED PROPERLY. HOLES MAY HAVE BEEN PUNCH PRESSED AND SMALL AMOUNTS OF EXCESS MATERIAL REMAINED.SDR CA040825003Bracket · cracked(CAN) TAIL REMOVED TO CHANGE BROKEN BRACKETS. PN 0712302-1 LT BRACKET AND 0732101-4 REINFORCEMENT REPLACED WITH NEW PARTS. ADJACENT RIVETS REPLACED. TAIL REASSEMBLED AND DUAL INSPECTED.SDR CA040506002Bar · crackedDURING A ROUTINE, CHANGE OVER FROM SKIS TO FLOATS, IT WAS DISCOVERED THAT THE FORWARD SPREADER BAR ASSEMBLY PART NUMBER 36657-10 WAS BADLY CORRODED AND CRACKED. THE SPREADER BAR ASSEMBLY WAS REMOVED FROM EDO 249-2870 FLOATS. NEW PART NUMBER 26-32096 INSTALLESDR CA030703005Hose · failed(CAN) NYLON STATIC HOSE CATCHING ON LT CONTROL COLUMN UNIVERSAL JOINT ATTACH BOLT. STATIC HOSE NOT TIED OFF PROPERLY, WHICH RESTRICTED FORWARD MOVEMENT OF CONTROL WHEEL.SDR CA021122003Bulkhead · cracked(CAN) DURING SCHEDULED MAINTENANCE, IT WAS DISCOVERED THAT THE ANGLE TAILCONE REINFORCEMENT LT IN THE TAILCONE BULKHEAD ASSEMBLY WAS CRACKED.SDR CA030709005Bushing · worn(CAN) ENGINE REMOVED FROM VIBRATION. ENGINE COUNTERWEIGHT BUSHINGS WORN OUT.SDR CA011116016Tail Wheel · separated(CAN) AFTER TAKEOFF FROM ROUGH STRIP ON HERSEL ISLAND, PILOT HEARD LOUD BANGING SOUND. HE WAS ABLE TO SEE TAIL WHEEL MISSING. ON LANDING AT AKLAVIK, STEERING CONTROL LOST. MINOR DAMAGE TO TAIL STRINGER. NEW TAIL WHEEL ASSEMBLY INSTALLED WITH PROPER AIRCRAFT BSDR CA000925032Pulley Bracket · broken(CAN) A BROKEN FLAP CONTROL CABLE PULLEY BRACKET CAUSED THE RIGHT FLAP EXTEND CABLE TO GO SLACK, RESULTING IN THE RIGHT FLAP PANEL PARTIALLY RETRACTING. THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL TO THE RIGHT AND THE PILOT HAD TO RETRACT THE FLAPS TO RECOVSDR CA030709004Mount · broken(CAN) CROSS TUBE ON ENGINE MOUNT BROKE ON TAKEOFF, DURING THE APPLICATION OFF POWER.SDR CA000801015Hinge Bracket · failed(CAN) THE REINFORCEMENT STABILIZER HINGE (BOX) ON THE HORIZONTAL STABILIZER WAS CHANGED. P/N 0732101-4 WAS REPLACED WITH NEW PART USING EXISTING RIVET SIZE AND PATTERN.SDR CA000801014Bracket · cracked(CAN) THE BRACKET ON THE LEFT STABILIZER WAS CHANGED AS IT WAS FOUND TO BE CRACKED. P/N 0712302-1 WAS REPLACED WITH NEW PART USING EXISTING RIVET SIZE AND PATTERN.SDR CA000713013Bracket · cracked(CAN) THE ANGLE TAIL CONE REINFORCEMENT WAS CHANGED AS IT WAS CRACKED. P/N 0712048-7 WAS REPLACED WITH NEW PART USING EXISTING RIVET SIZE AND PATTERN. THE BRACKET ON THE LEFT STABILIZER WAS CHANGED AS IT WAS FOUND TO BE CRACKED. P/N 07123021 WAS REPLACED WISDR 20000721SH017Elt · inoperativeDURING ANNUAL INSPECTION, CHECKED ELT FOR OPERATION AND CONDITION. ELT DID NOT OPERATE. EITHER INERTIA SWITCH OR MANUAL SWITCH. CHANGED BATTERY, AS SUGGESTED BY MFG. NO CHANGE. SENT UNIT TO MFG FOR REPLACEMENT. PART TT: 18 MONTHS. (X)SDR CA991028011Bracket · cracked(CAN) DURING SCHEDULED MAINTENANCE, STABILIZER APPEARED LOOSE. FURTHER INVESTIGATION REVEALED A CRACKED HINGE BRACKET.SDR CA990817029Alternator · failed(CAN) ALTERNATOR REAR BEARING FAILURE. SYSTEM NOT CHARGING.SDR CA981027010Bracket · cracked(CAN) DURING CHANGE OVER FROM FLOATS TO WHEEL GEAR, THE LEFT MAIN LANDING GEAR OUTBOARD SUPPORT BRACKET FOUND CRACKED.SDR CA981027009Bracket · cracked(CAN) DURING CHANGE OVER FROM FLOATS TO WHEEL GEAR, BOTH THE LEFT AND RIGHT MLG OUTBOARD SUPPORT BRACKETS WERE FOUND CRACKED. LEFT P/N 0713495-61 AND RIGHT HAND P/N 0713495-62.SDR CA981027001Fitting · worn(CAN) RIGHT HAND WING FOUND MOVING EXCESSIVELY AT ALL ATTACH POINTS. FITTINGS FOUND WORN TO .016 INCH PLAY. FITTINGS BUSHED IAW CESSNA INSTRUCTIONS AND NAS CLOSE TOLERANCE BOLTS INSTALLED.SDR 98ZZZX3305Bolt · missingAIRCRAFT EXPERIENCED A LEFT MAIN GEAR FAILURE SHORTLY AFTER LANDING. INVESTIGATION DISCLOSED THAT THE LEFT MLG INBOARD BOLT P/N AN7-20-A W25 MISSING. ALSO, THE BOLT HOLE WAS ELONGATED. SUBMITTER RECOMMENDS SPECIAL EMPHASIS BE PLACED ON THIS AREA DURING INSPSDR CA980504013Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADES AND FERRULES (P/N 3054) WERE FOUND CORRODED. THE PROPELLER BLADES WERE TRIMMED AND THE FERRULES WERE REPLACED.SDR 98ZZZX2117Piston · failedABOUT 15 SECONDS AFTER TAKEOFF, ENGINE BEGAN TO RUN ROUGH AND LOSE POWER. PILOT COULD NOT MAINTAIN ALTITUDE, AND MADE AN UNEVENTFUL LANDING. INSPECTED ENGINE, FOUND NR 5 PISTON BROKEN AND NO LONGER IN THE CYLINDER; ALSO, A 2 INCH CRACK FROM BASE OF NR 5 PISTSDR CA970508014Cylinder · scored(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER CYLINDER WAS SCORED AND WORN AND HAD TO BE REPLACED.SDR CA970429010Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. TEN YEARS SINCE LAST OVERHAUL. INSPECTION FOUND BLADES CORRODED. TIP ANGLES OUT. FACE ALIGNMENT OUT. ONE ACTUATING PIN; TWO PISTON PINS AND CYLINDER CORRODED. REPAIRS MADE AND CORRODED PARTS REPAIRED OR REPLACSDR CA970421081Blade · spray cut(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. BLADE HAD SPRAY CUT DAMAGE.SDR CA970310004Bearing · warped(CAN) THE C3411-2 BEARING RACE WAS INSTALLED DURING THE ASSEMBLY STAGE OF THE OVERHAUL AND DURING THE BEARING SEATING INSPECTION IT WAS FOUND THAT THE BEARING SEATING AREA WAS NOT CONTACTING THE PROPELLER HUB. THE BEARING WAS REMOVED AND CHECKED FOR FLATNESS OSDR 97ZZZX5Valve · leakCONTINENTAL CYLINDER ASSY PN 653443A13. 2 OUT OF 6 CYLINDERS HAD UNACCEPTABLE LEAKS FROM INTAKE VALVES. ABOUT 1 DROP LIQUID SOLVENT PER MINUTE WITH VALVE SPRINGS INSTALLED. ALSO, VALVE GUIDES ARE HOURGLASS SHAPED. ABOUT .002 INCH SMALLER IN CENTER THAN ON SDR EY2R9601073Hub · corrodedHUB CORRODED.SDR 96ZZZX5290Impulse Coupling · spring brokenFOUND IMPULSE COUPLING, SPRING BROKEN DUE TO CORROSION.SDR 96ZZZX5289Impulse Coupling · spring brokenFOUND IMPULSE COUPLING, SPRING BROKEN DUE TO CORROSION.SDR CA961011002Float · badly worn(CAN) PILOT COMPLAINED OF INTERMITTENT FUEL LEAK FROM CARBURETOR. DISASSEMBLY OF CARBURETOR REVEALED FLOAT HINGE BADLY WORN ALLOWING CONTACT OF FLOAT WITH SIDES OF FLOAT CHAMBER RESULTING IN SEVERE WEAR ON SIDES OF METAL FLOATS. FUEL VALVE RETAINER CLIP WORN ISDR EY2R9600943Hub · corrodedHUB CORRODED.SDR 96ZZZX4234Lines · chafedIN LT DOOR POST, THE AILERON CABLE WAS RUBBING ON THE FUEL LINE. UNDER THE FLOOR, THE FUEL LINES WERE CHAFING ON THE BULKHEADS WHERE THEY PENETRATED. SUBMITTER RECOMMENDS CLOSE INSPECTION OF THESE AREAS WITH A MIRROR AND LIGHT. INTERIOR PANELS MUST BE MOVEDSDR CA960102103Float Assembly · broken(CAN)SEPARATION OF FLOAT CHAMBER FROM FRAME. SOLDERING OF JOINT APPEARS TO BE IMPROPERLY PERFORMED.
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