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 = '402C' 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 = '402C' 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 95ZZZX5523Channel · crackedDURING INSPECTION, FOUND CHANNELS CRACKED. REMOVED AND REPLACED WITH NEW. SUSPECT CAUSE - HILOK'S BECAME LOOSE ON CHANNELS CAUSING BEND RADIUS TO CRACK.SDR 95ZZZX5028Distributor Gear · teeth missingENGINE HAD SLIGHT ROUGHNESS AND TIMING JUMP TO THE TIME OF FAILURE. FOUND DISTRIBUTOR GEAR TEETH MISSING. RECOMMEND SHIMS BE CHECKED FOR GEAR FREEDOM AND UNIT BE REPLACED AT ONE-HALF OF SPECIFIC T.B.O. OF MAGNETO.SDR 95ZZZX5115Hub · crackedINSPECTION FOUND CRACK IN THREADS OF HUB SOCKET.SDR 95ZZZX5126Uplock Hook · crackedPILOT REPORTED GEAR WOULD NOT STAY IN UP POSITION. IN INSPECTION, FOUND LEFT MAIN GEAR UPLOCK HOOK CRACKED.SDR 95ZZZX4508Switch · out of rigPILOT REPORTED WITH THE GEAR IN THE UP POSITION, THE RED UNSAFE LIGHT FAILED TO EXTINGUISH. AIRCRAFT JACKED AND GEAR OPERATED. FOUND RT GEAR UPLOCK SWITCH NEEDED ADJUSTMENT. SWITCH ADJUSTED IAW SECTION 32 OF THE CESSNA SM. GEAR OPERATED SEVERAL MORE TIMES,SDR 95ZZZX4377Pump · bearing wornFUEL PUMP REPLACED DUE TO LOW PRESSURE. THIS IS THE 3RD FAILURE IN 160 HOURS, ALL OVERHAULED BY RAPCO FLEET SUPPORT. PILOT FOUND METAL FLAKES IN FUEL SAMPLE FROM SUMP DRAIN. DISASSEMBLED PUMP AND FOUND BEARING FAILED. REPLACED WITH NEW AIRBORNE PUMP.SDR 95ZZZX3810Pump · defectiveDURING CRUISE FLIGHT, PLACED RIGHT FUEL SELECTOR TO LEFT MAIN FUEL TANK, BOTH RIGHT AND LEFT ENGINES SHOWED SIGNS OF FUEL STARVATION (ENGINES SURGING). PUT LEFT FUEL BOOST PUMP ON LOW AND WAS OK. FOUND LEFT AUXILIARY BOOST PUMP INLET CHECK BALL STUCK ON SEAT SDR 95ZZZW802Light Wire · failedMIA-MHN - FLT 102 - BURNING SMELL IN COCKPIT WITH LIGHTS AT FULL INTENSITY. AC RETURNED TO MIA WITHOUT INCIDENT. TROUBLESHOT, FOUND BURNT WIRE AT CIRCUIT BOARD SWITCH. CLEANED AREA AND RESOLDERED WIRE. OPERATIONAL CHECK GOOD.SDR 95ZZZX4203Hub · crackedPROPELLER RECEIVED FOR 5-YEAR OVERHAUL. AFTER HUB INSPECTION, HUB DISCOVERED CRACKED IN NR 2 BLADE SOCKET, BETWEEN 8 TO 9 O'CLOCK POSITIONS, 3 THREADS IN, APPROXIMATELY 1 INCH LONG. THE CRACK WAS DISCOVERED USING A 10X POWERED MICROSCOPE.SDR 95ZZZX4052Pin · shearedUPON LANDING IN CAPE HATIAN, HAITI, THE LEFT MLG TORQUE LINK, UPPER SCISSOR PIN SHEARED CAUSING AIRCRAFT TO VEER OFF THE RUNWAY. INSPECTED IAW CESSNA MM, CHAPTER 5-50-00, PAGES 1 AND 2A, AND PAGE 4, NR 2F. REMOVED AND REPLACED UPPER SCISSOR ASSEMBLY.SDR 95ZZZX3075Valve · deterioratedPILOT ABORTED TAKEOFF DUE TO ENGINE OVERBOOST. FOUND TOP SECTION OF BUTTERFLY VALVE WARPED DUE TO HEAT. FOUND THAT ON WASTEGATES OVERHAULED USING CONTINUED TIME VALVES, THIS OFTEN HAPPENS ALONG WITH VARING MANIFOLD PRESSURE. ON COMPONENTS WITH NEW VALVES INSDR 95ZZZM179Stud · brokenDEPARTED FROM INAGUA, BAHAMAS, AFTER ABOUT 20 MINUTES RT ENGINE OIL PRESSURE DROPPED TO RED LINE AND ENGINE WAS SHUT DOWN. THE AIRCRAFT RETURNED TO INAGUA. AFTER INSPECTION THE RT ENG, FOUND 4 STUDS ON NR 2 CYLINDER BROKEN. REMOVED THE CYLINDER AND REPLACEDSDR 95ZZZX2901Trunnion · crackedPILOT REPORTED RT STRUT WAS RIDING LOW. MAINTENANCE DISCOVERED A CRACK APPROXIMATELY 4 INCHES LONG ALONG SIDE THE CAST MARK OR SEAM IN THE UPPER GEAR TRUNNION. DURING DISASSEMBLY, NOTED THE STRUT BARREL WAS ALSO CRACKED. PILOT REPORTED NO UNUSUAL LANDINGS ASDR 95ZZZM148Engine · failedDURING CRUISE FLIGHT, THE LEFT ENGINE MADE A LOUD BANG. THE RPM AND POWER DECREASED, SO THE PILOT SHUT IT DOWN. THE AIRCRAFT LANDED IN LEE STOCKING ISLAND 25 MILES SHORT OF GEORGETOWN. THE CAUSE OF ENGINE FAILURE HAS NOT BEEN DETERMINED, UNTIL A MECHANIC CASDR 95ZZZX2679Breaker · failedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RECYCLED SWITCH AND CHECKED CIRCUIT BREAKERS. RECYCLED HYDRAULIC CIRCUIT BREAKER AGAIN AND GEAR WENT UP WITH NO FURTHER PROBLEMS. MAINTENANCE WAS ABLE TO DUPLICATE THE PROBLEM AND CHANGED CIRCUIT BREAKER. NO FUSDR 96ZZZX1248Switch · burnedDURING CRUISE FLIGHT, CABIN STARTED FILLING WITH SMOKE. SMOKE WAS ORIGINATING FROM AVIONICS MASTER SWITCH - UNABLE TO TURN SWITCH OFF, SO CIRCUIT BREAKERS WERE PULLED. SMOKE EVACUATION PROCEDURES WERE INITIATED AND SMOKE SUBSIDED. A NORMAL LANDING WAS MADE.SDR 95ZZZX2544Line · failedPILOT REPORTED BOTH FLOW LIGHTS CAME ON AND STAYED ON AFTER TAKEOFF. IMMEDIATELY, GEAR WAS LOWERED, MAINS LOCKED AND NOSE GEAR UNSAFE. BLEW GEAR BOTTLE, NOSE GEAR LOCKED DOWN. FOUND RT LINE FROM PUMP TO FIREWALL BLOWN, PN AE1003957G0310. REPLACED LINE WITHSDR 95ZZZX2383Switch · req adjPILOT REPORTED THAT WITH GEAR UP AND LOCKED, THE RED UNSAFE LIGHT REMAINED ON. GEAR CYCLED AND SAME PROBLEM. ALL OTHER PARAMETERS NORMAL. CYCLED GEAR ON JACKS, ADJUSTED LT UPLOCK SWITCH OUT, ONE-QUARTER TURN. OPERATED GEAR, TOTAL OF TEN TIMES, ALL NORMAL.SDR 95ZZZX2194Lifter · mismfgZERO TIME ENGINE AFTER OVERHAUL WAS INSTALLED ON THIS AIRCRAFT AND ON FIRST REVENUE FLIGHT AFTER TEST FLIGHT, THE ENGINE BEGAN RUNNING ROUGH AND LOSING OIL PRESSURE. THE AIRCRAFT LANDED AND UPON INSPECTION OF ENGINE, THE NR 2 CYLINDER EXHAUST PUSH-ROD WAS FOUSDR 95ZZZX1928Pushrod · bentON 4-1-95, A ZERO TIME OVERHAULED ENGINE WAS INSTALLED ON NR 1 POSITION. THE AIRCRAFT WAS TEST FLOWN FOR ENGINE INSTALLATION AND OPS CHECKED OKAY. THE AIRCRAFT WAS RELEASED FOR SERVICE. ON THE FIRST REVENUE FLIGHT TO TREASURE CAY, NR 1 ENGINE BEGAN RUNNING SDR 95ZZZX1869Line · failedPILOT REPORTED THAT DURING TAKEOFF ROLL, THE RIGHT MANIFOLD INDICATION DECREASED TO STATION PRESSURE, AND ABORTED THE TAKEOFF WHILE STILL ON THE RUNWAY. NO ACTUAL LOSS OF POWER WAS REPORTED. UPON INSPECTION, IT WAS FOUND THAT STEEL MANIFOLD PRESSURE LINE FROSDR 95ZZZX1600Spar · crackedON 11-24-89, CESSNA ME84-12 WAS C/W ON LT WING SPAR CARRY-THROUGH. IT WAS DONE IMPROPERLY AND HAS NOW CRACKED FURTHER THAN ALLOWED. AT SOME POINT, THE CRACKS WERE STOP DRILLED CAUSING DAMAGE TO THE CARRY-THROUGH CASTING. SUBMITTER RECOMMENDS WHEN C/W ME84-1SDR 95ZZZX1635Bolt · failedTHE LEFT GEAR SCISSOR BOLT CAME OUT ON LANDING. THE LEFT WHEEL TURNED SIDEWAYS. REPLACED WHEEL, BOLT, NUT. INSPECTED STRUT AND WHEELWELLS AND ACTUATORS. SUBMITTER STATED A PERIODIC CHANGE OF SCISSOR BOLTS WILL BE IMPLEMENTED. BOLT PN AN175-20. NUT PN AN3SDR 95ZZZW630Control Valve · failedFLT 102 - GEAR WILL NOT EXTEND HYDRAULICALLY, USED EMERGENCY BOTTLE, WORKS OK. REMOVED AND REPLACED SELECTOR VALVE, BLED SYSTEM, LEAK CHECK OPS CHECKS GOOD. BLOW DOWN SYSTEM RESERVICED. AIRCRAFT TEST FLOWN SATISFACTORY AND RELEASED TO REVENUE SERVICE.SDR 95ZZZX1276Piston Spring · brokenON LANDING, NOSE GEAR COLLAPSED. INSPECTION OF LANDING GEAR AND COMPLIANCE WITH MEB91-12 RESULTED IN NO DEFECTS NOTED IN GEAR SYSTEM. REMOVED AND SENT NOSE GEAR ACTUATOR OUT FOR INSPECTION. TEAR-DOWN REVEALED LOCK INDICATOR PISTON SPRING BROKEN.SDR 95ZZZX1204Oil Separator · frozenAIRCRAFT LEFT THE AIRPORT WITHOUT A PREHEAT AND TEMPS IN THE 20'S DEGREE FAHRENEIT. SHORTLY AFTER TAKEOFF, ENGINE STARTED SMOKING, AIRCRAFT RETURNED SAFELY TO THE AIRPORT. CAUSE OF THE PROBLEM WAS FROZEN MOISTURE IN THE OIL SEPARATOR WHICH DID NOT ALLOW CASESDR 95ZZZW149Le Skin · corrodedTOP AND BOTTOM OF BOTH RT AND LT WINGS HAVE SEVERE CORROSION AT LEADING EDGE TO FRONT SPAR AT WS 119.29 THROUGH 229.71. CORROSION AND POPPED RIVETS JUST AFT OF EXHAUST PIPE RT AND LT WINGS AT WS 119.29. DER APPROVABLE AT WS 119.29 THROUGH 229.71 337 AND 8110SDR BUHA95001Fitting · corrodedVERTICAL STABILIZER FORWARD SPAR ATTACH FITTING AT FUSELAGE, FOUND CORRODED. (X)SDR 95ZZZW150Le Skin · corrodedCORROSION ON LEADING EDGE OF WING AT TOP AND BOTTOM OF FRONT SPAR AT WS 119.29 THROUGH 229.7. CORROSION AT BOTTOM OF WING JUST AFT OF EXHAUST PIPE ON LEFT AND RIGHT WINGS AT WS 119.29. (W)SDR 95ZZZW148Le Skin · corrodedCORROSION LEADING EDGE TO FRONT SPAR RT WING TOP AND BOTTOM AT WS 119.29 THROUGH 229.71. (W)SDR 95ZZZX929Transceiver · inoperativeINOP OR FREQ 115.6 -- BRG POINTER AND ADI SCALLOP 20 DEGREES LEFT AND RIGHT EVEN AT 15 MILES FROM STATION. PROBLEM IS ONLY ON FREQ 115.B. FREQS 112.3, 112.6, 116.0, 113.3 -- OKAY.SDR 95ZZZW147Skin · corrodedCORROSION ON SKIN UNDER AND AFT OF EXHAUST PIPE RT WING. CORROSION UNDER EXHAUST PIPE LT WING. SKIN WAS REPLACED AT WS 119.29.
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