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 = '208' 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 = '208' 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 141A2026062900001Engine · faultedDURING CLIMB TO CRUISE, PASSING THROUGH 6000 TO 8000 FT THE ENGINE ITT WAS AT 740, WITH THE POWER BEING SET AT ONLY 1200LBS OF TORQUE. WE WERE ONLY ABLE TO MAINTAIN CLIMB RATE OF 200-300 FPM WITH AIRSPEED AT 95-100 INDICATED KNOTS. AT CRUISE ALTITUDE OF 8000FTSDR 141A2026011570001Unknown · odorCREW NOTICED STRONG BURNING ODOR IN COCKPIT WITH SMOKE. CONTACTED ATC AND DECLARED EMERGENCY. AFTER SAFE LANDING CREW OPENED UP COWLING AND COULD NOT FIND ANYTHING BURNINGSDR 141A2024050700003Unknown · odorDURING CRUISE FLIGHT, CA AND FO NOTICED A STRONG BURNING SMELL, LIKE BURNING RUBBER AND PLASTIC. FLIGHT WAS DIVERTED AND MADE AN UNSCHEDULED LANDING. MAINTENANCE WAS DISPATCH AND PERFORMED THE INSPECTION WITH NO DEFECTS NOTED AND A GROUND PERFORMANCE RUN. NO SSDR 2024FA0000016Inertia Reel · failedMECHANIC WAS PERFORMING A ROUTINE INSPECTION ON THE INERTIAL REELS FOR THE CREW SEATS IN THE CARAVAN. THE AIRCRAFT UNDER INSPECTION WAS PK-MAG, OUR NEWEST CARAVAN. MECHANIC INSPECTED THE BELTS FOR THEIR CONDITION AND THEN TESTED THE REELS BY PULLING THE BELT OSDR 2022F00457Radio · smokeNUMBER 1 RADIO STARTING SMOKING MID FLIGHTSDR LF1R2022101900208Flap Track · corrodedOWNER NOTED SOME DETERIORATION ON THE WING FLAP TRACKS. UPON CLOSER INSPECTION, THE TRACKS WERE NOTED TO HAVE SIGNIFICANT CORROSION. REVIEW OF THE CESSNA 208 STRUCTURAL REPAIR MANUAL DETERMINED THAT CORRODED AREA WAS WITH IN LIMITS. CORROSION WAS REMOVED AND TSDR ENHA202208150001Engine · unknownAFTER BEING CLEARED FOR TAKEOFF, PILOT LINED UP ON RUNWAY 20R IN KENAI AND ADVANCED POWER AND THEN PILOT NOTICED AN UNUSUAL SOUND COMING FROM THE ENGINE COMPARTMENT. PILOT THEN REDUCED POWER AND ABORTED THE TAKEOFF AND PROCEEDED TO TAXI BACK TO THE HANGER. MSDR ENHA202202110001Engine · flamed outDURING CRUISE FLIGHT, ENGINE SURGED, FLAMED OUT AND RESTARTED ON ITS OWN. TORQUE WENT FROM 1600 FT/LBS DOWN TO APPROXIMATELY 800 FT/LBS, AND JUMPED BACK UP TO 1600 FT/LBS. PILOT RETURNED TO BASE. NO TROUBLESHOOTING WAS BEEN PERFORMED AT TIME OF SUBMISSION.SDR CA191002038Seal · leaking(CAN) PROPELLER REMOVED FROM AIRCRAFT AND SENT TO REPAIR FACILITY. PROPELLER DISMANTLED FOR INVESTIGATION OF RED DYE OIL LEAK. LEAK FOUND TO BE FROM AFT BETA ROD TO HUB SEAL. PROPELLER REASSEMBLED AND PRESSURE TESTED. PROPELLER REINSTALLED ON AIRCRAFT AND RETUSDR CA190425034Fitting · cracked(CAN) DURING A SCHEDULED WING STRUT EDDY CURRENT INSPECTION (5-15-MA) REQUIRED EVERY 5000HRS, ONE OF THE LEFT STRUT LOWER FITTINGS WAS FOUND CRACKED AND SEPARATED AT TIME OF STRUT REMOVAL PREPARING FOR THE INSPECTION. THE LAST COMPLIANCE OF THIS INSPECTION WASSDR CA190412011Return Spring · broken(CAN) PILOT REPORTED CLICKING NOISE FROM R/H BRAKE PEDAL. FOUND RETURN SPRING BINDING, BRAKE PEDAL STICKING. BRAKE RETURN SPRING REPLACED WITH NEW. FUNCTION TESTED SERVICEABLE. (TC# 20190412011)SDR CA190329031Transponder · failed(CAN) TRANSPONDER SMOKING IN FLIGHT. PILOT REMOVED ELECTRICAL POWER TO THE TRANSPONDER. (TC# 20190329031)SDR CA180822010Gyro · failed(CAN) DURING CRUISE FLIGHT WITH AUTOPILOT ENGAGED, AUTOPILOT DISCONNECTED AND SMELL OF SMOKE/BURNING WIRES DETECTED AND THE AVIONICS BUS 1, HSI 1 CIRCUIT BREAKER TRIPPED. PILOT RETURNED TO POINT OF DEPARTURE/MAIN BASE. (TC# 20180822010)SDR LU4R2017102418840Beta Ring · damagedDURING PREFLIGHT, DISCOVERED THAT THE CARBON BLOCK WHICH RIDES IN THE CHANNEL OF THE PROPELLER BETA FEEDBACK COLLAR WAS DAMAGED BY A SMALL FAILURE OF THE SECTION OF THE FEEDBACK COLLAR CHANNEL WALL DIRECTLY UNDER ONE OF THE MOUNTING STUDS. ONE POSSIBILTY THSDR P9KA17020803Torque Tube · corrodedDURING A ROUTINE ANNUAL INSPECTION, THE RUDDER TORQUE TUBE WAS FOUND TO HAVE CORROSION ON MULTIPLE AREAS INSIDE THE RUDDER. RUDDER TORQUE TUBE CORROSION IS ADDRESSED IN CAB06-2, BUT THERE ARE 2 PROBLEMS WITH THAT CAB. FIRST, THERE IS NO INSTRUCTION IN THE CAB SDR P9KA2017020801Actuator · corrodedDURING ROUTINE INSPECTION, THE LEFT ELEVATOR TRIM ACTUATOR WAS FOUND TO HAVE MULTIPLE PARTS CORRODED BEYOND LIMITS. THE ACTUATOR HAD APPROXIMATELY 800 HOURS AND 12 MONTHS SINCE LAST DISASSEMBLY, INSPECTION, AND LUBRICATION.SDR 2017F00000O-Ring · cutLEFT BRAKE CALIPER, BRAKE PUCK O-RING FAILED, CUT. AIRCRAFT LOST BRAKING CONTROL TO THE LEFTSDR HYIA20161020001Strut · separatedPILOT REPORTED "NO INDICATION ON POSITION OF RIGHT MAIN GEAR. HAD TO CONDUCT A LANDING ON THE AIRCRAFT FLOAT SKIDS ON A HARD SURFACE RUNWAY." UPON INSPECTION, MAINTENANCE DISCOVERED THE RIGHT MAIN GEAR STRUT INNER PISTON & OUTER CYLINDER HAD SEPARATED. THIS SDR HYIA09102016001Attach Bolt · backed outWHILE TURNING LEFT FOR FINAL APPROACH TO LAND, THE CREW FELT AND HEARD A SMALL THUD IN THE AIRCRAFT WING AREA. THE CREW REPORTED THE AIRCRAFT BEGAN A SLOW ROLL TO THE LEFT AND THAT THEY WERE ABLE TO CORRECT WITH OPPOSITE AILERON DEFLECTION. THE AIRCRAFT LANDSDR HYIA02202016001Attach Fitting · crackedDURING A ROUTINE INTERVAL INSPECTION, RT FLOAT PYLON ATTACH FITTING WAS FOUND TO BE CRACKED AT THE 12 O CLOCK POSITION OF THE THIRD INBD LUG. WITH SUPPORT FROM THE FLOAT STC OEM, THIS ACFT WAS REPOSITIONED UNDER SFP TO THE FLOAT STC OEM FACILITY, FOR EVALUATISDR CA160229006Antenna · no test(CAN) UPON DOING THE SELF TEST TO ASSESS SYSTEM FUNCTION AN ERROR CODE CAME UP SHOWING A PROBLEM WITH THE ANTENNA CIRCUIT. UPON REPLACING THE ANTENNA THE SYSTEM TESTED FINE.SDR P9KA2015103001Governor · leakingPILOT REPORTED ENG OIL DOWN BELLY OF ACFT. FIRST TROUBLESHOOTING WAS TIGHTENING AN OIL FLEX HOSE THAT WAS SLIGHTLY LOOSE, NO CHANGE. FURTHER INSPECTION REVEALED OIL LEAKING AT BASE OF PROPELLER GOVERNOR. GOVERNOR WAS REMOVED & GOVERNOR BASE GASKET CHANGED, SDR P9KA2015091601Antenna · failedNEITHER GPS WOULD ACQUIRE POSITION. TROUBLESHOOTING REVEALED THAT THE NR 2 GPS ANTENNA WAS FAILED & RADIATING ON GPS FREQUENCY, CAUSING INTERFERENCE FOR NR 1 GPS. IT IS APPARENT THAT THIS ANTENNA FAILURE MODE IS NOT UNCOMMON. CONSIDERING THAT THE EFFECTED GSDR CA150904005Spring · broken(CAN) SPRING WAS FOUND SEPARATED FROM MOUNTING TANG, LOOSE IN CONTROL QUADRANT. POTENTIAL EXISTS FOR LOOSE PARTS IN THIS AREA TO JAM THE ENGINE CONTROLS.SDR CA150818004Engine · power loss(CAN) AFTER A RAPID DESCENT FROM ALTITUDE, DURING SKYDIVE OPERATIONS, THE ENGINE FAILED TO RESPOND TO POWER LEVER INPUT AND WAS FOUND TO HAVE FLAMED OUT. AFTER DESCENDING FROM 15000` THE PILOT ATTEMPTED TO INTRODUCE POWER AT 2000` DURING APPROACH AND THE ENGINSDR 2015F00099Boot · debondedALL 3 PROPELLER DE-ICE BOOTS DEBONDED FROM BLADE IN FLIGHT CAUSING A SEVERE VIBRATION. LANDED AT NEAREST AIRPORT WITH OUT INCIDENT. VISUAL INSPECTION REVEALED DEBONDING OF MOST OF THE BOOTS APPEARS TO BE A POORLY APPLIED BONDING APPLICATION.SDR CA150520004Line · damaged(CAN) FLARE ON HYDRAULIC LINE FAILED AT THE CONNECTION TO THE GEAR SELECTOR ASSY. FAILURE CAUSED LOSS OF HYDRAULIC FLUID AND SUBSEQUENT EMERGENCY LANDING ON A GRASS FIELD. INSPECTION DETERMINED THAT THE FLARE HAD SUBSTANDARD MANUFACTURING QUALITIES. UPON INSPSDR CA150506013Spar · corroded(CAN) INSTALLATION OF FINLETS DEVIATED FROM DWG CAUSING CORROSION WHICH LED TO THE HORIZONTAL STABILIZER AFT SPAR REPLACEMENT. DWG 6R1-2017, 8000 SERIES FLOATS, THE AFT ATTACHMENT FOR THE FINLET CALLS FOR A NUTPLATE NAS696 BUT A MS21044N3 NUT WAS INSTALLED INSDR 2015FA0000040Spacer · wrong partSPACER IS RIVETED TO RUDDER PEDAL BRACKET ITEM 18 AS INDICATED BY IPC 27-20-02, FIGURE 2, ITEM 19, AND IS SUPPOSED TO BE SIZED TO ALLOW BRAKE MASTER CYLINDER CLEVIS ITEM 21 TO FIT OVER WITH ADEQUATE CLEARANCE TO PREVENT BINDING. CLEVIS OPENING IS .250", THICKNSDR CA141217019Control Arm · stiff(CAN) AFTER START UP AND DURING TAXI THE PILOT NOTED THAT THE IDLE NG SPEED WAS ERRATIC AND TAXIED BACK TO BASE. MAINTENANCE RUN CONFIRMED THE ERRATIC IDLE SPEED. UPON INSPECTION IT WAS NOTED THAT THE FUEL CONTROL ARM WAS STIFF AND WOULD STAY IN WHATEVER POSITSDR CA141030014Spring · broken(CAN) PART WAS FOUND SEPARATED FROM MOUNTING TANG, LOOSE IN CONTROL QUADRANT. POTENTIAL EXISTS FOR LOOSE PARTS IN THIS AREA TO JAM THE ENGINE CONTROLS. PART REPLACED.SDR FVAA2014090300150Clamp · brokenDURING CRUISE FLIGHT, THE PILOT REPORTED HEARING A LOUD BANG, FOLLOWED BY A GENERATOR FAIL ANNUNCIATION AND A STBY PWR ON ANNUNCIATION. A FEW MINUTES LATER, THE STBY PWR FAIL ANNUNCIATION ILLUMINATED AS WELL, AND THE PILOT MADE A NORMAL LANDING AND SHUTDOWN ASDR CA140804010Engine · flamed out(CAN) CUSTOMER REPORTED THAT THEY HAD A "POWER FLUCTUATION DURING TAKEOFF ". FURTHER INVESTIGATION IDENTIFIED THAT IT WAS IN FACT A FULL FLAMEOUT AND FEATHER OF THE PROP RT AFTER ROTATION DURING THE TAKEOFF. THE PILOT LANDED THE ACFT WITHOUT FURTHER INCIDENT.SDR 2014FA0000496Gust Lock · damagedRUDDER GUST LOCK TUBE ASSY SHEARED IN FLIGHT AND CAUSED A MALFUNCTION IN THE FLIGHT CONTROL/RUDDER SYS. PILOT STATED HE HAD TO USE EXCESSIVE FORCE TO MOVE THE YOKE AFT OF ITS NEUTRAL POSITION. UPON LANDING THE ACFT, THE AIRCRAFT WAS INSPECTED AND THE RUDDER GUSDR CA140612005Wheel Half · cracked(CAN) OUR CARAVAN ON AMPHIBIOUS FLOATS WIPLINE 8000S, WAS LANDING JUNE 11 AT THE COMPANIES HOME BASE WHEN ON LANDING & TAXIING NOTICED A VIBRATION COMING FROM THE FRONT WHEELS. TAXIED TO THE COMPANY RAMP & NOTED THE FRONT RIGHT TIRE WAS FLAT. UPON FURTHER INSDR 2014FA0000253Compressor · seizedODOR DETECTED RESEMBLING BURNING RUBBER AND / OR PLASTIC. AIR CONDITIONING COMPRESSOR SEIZED CAUSING DRIVE BELT TO BE DAMAGED. THE COMPRESSOR WAS REMOVED AND REPLACED IAW THE MANUAL.SDR CA131113006Fitting · cracked(CAN) DURING A SCHEDULED EDDY CURRENT INSPECTION OF THE LOWER WING STRUT LUGS IAW INSPECTION 57-60-01. THE LT AFT LUG ON THE LOWER WING STRUT WAS FOUND CRACKED.SDR CA131113002Shroud · migrated(CAN) DURING A SCHEDULED BORESCOPE INSPECTION OF THE HOT SECTION IT WAS NOTICED THAT 2 CT SHROUD SEGMENTS HAD SHIFTED SLIGHTLY AXIALLY. HOT SECTION WAS REMOVED AND PROBLEM WAS VERIFIED. THE SEGMENT CONTAINMENT RING WAS FOUND SLIGHTLY WARPED AND SHIFTED. THESDR 2014F00009Belt · brokenDURING DEPARTURE, CAPTAIN DETECTED A BURNING ODOR. ELECTED TO RETURN AND LAND. MX FOUND AIR CONDITIONER BELT BROKEN AND RUBBING ON THE AIR CONDITIONING COMPRESSOR PULLEY, CAUSING THE ODOR. REMOVED BROKEN BELT. ACFT RETURNED TO SERVICE.SDR 2013F00172Fire Warning · false indicationFIRE WARNING INDICATION IN FLIGHT NOTED BY CREW. FLIGHT DIVERTED TO CLOSEST AIRPORT. UPON FURTHER INVESTIGATION IT WAS DISCOVER THAT THE THE FIRE WARING WAS A FALSE ALARM, CAUSED BY A WIRE SHORTED TO GROUND IN THE ACFT OVERHEAD PANEL. ACFT WAS REPAIRED AND SDR 2013F00171Fire Warning · false indicationFIRE WARNING INDICATION IN FLIGHT NOTED BY CREW. FLIGHT DIVERTED TO CLOSEST AIRPORT. UPON FURTHER INVESTIGATION IT WAS DISCOVER THAT THE THE FIRE WARING WAS A FALSE ALARM, CAUSED BY A WIRE SHORTED TO GROUND IN THE ACFT OVERHEAD PANEL. ACFT WAS REPAIRED AND SDR 2013F00170Fire Warning · false indicationFIRE WARNING INDICATION IN FLIGHT NOTED BY CREW. FLIGHT DIVERTED TO CLOSEST AIRPORT. UPON FURTHER INVESTIGATION IT WAS DISCOVER THAT THE THE FIRE WARING WAS A FALSE ALARM, CAUSED BY A WIRE SHORTED TO GROUND IN THE ACFT OVERHEAD PANEL. ACFT WAS REPAIRED AND SDR CA130807005Seal · degraded(CAN) OIL PRESSURE LOSS DURING FLIGHT. UPON INSPECTION CARRIER, OIL SEAL, FCU DRIVE FOUND DEGRADED OIL THEN STARTED FLOWING OVERBOARD.SDR OZTA2013F00143Water Rudder · missingUPON TAKEOFF FROM THE EAST RIVER , THE WINDS WERE OUT OF THE WEST RESULTING IN A RT CROSSWIND TAKEOFF. WATER RUDDERS WERE LT DOWN, IAW SOP, TILL ON STEP TO PREVENT A WEATHERCOCK TENDENCY. THE CREW HAD TROUBLE RAISING THE WATER RUDDERS BUT ON BECOMING AIRBORNSDR CA130715006Hose · leaking(CAN) UPON PARKING THE A/C AFTER A SCHEDULED COMMUTER FLIGHT, FUEL WAS SEEN DRIPPING FROM THE ENGINE COWL. NO ABNORMAL INDICATIONS OR PERFORMANCE ISSUES WERE NOTED DURING THE FLIGHT. SUBSEQUENT GROUND RUN REVEALED FUEL LEAKING FROM THE TUBE BETWEEN THE FUEL SDR CA130605004Cylinder · rough(CAN) SHARP EDGES ON A NEW CYLINDER CAUSED DAMAGE TO A PISTON SEAL DURING ASSY AT FACTORY. OVER TIME THE SEAL STARTED TO SEPARATE AND THEN TO START BEING FORCED OUT OF THE PISTON WHICH CAUSED OIL TO START LEAKING ALL OVER THE PROPELLER ASSY.SDR CA130531006Cable · damaged(CAN) LT WATER RUDDER DIRECT CABLE FAILED WHILE TAXING. CABLE FAILED AT PLASTIC CONDUIT TERMINATION, AFT AND PULLEY JUNCTION.SDR CA130516011Support Bracket · cracked(CAN) FLAP ACTUATOR BRACKET ASSY FOUND CRACKED AT LIGHTING RELIEF HOLES AND ACROSS DOUBLER, PN 2611144-5 FROM FLANGE TO LIGHTING HOLE DURING PHASE INSPECTION. SERVICE KIT 208-158 INSTALLED TO RECTIFY PROBLEM.SDR CA130416006Line · failed(CAN) THE PILOT REPORTED AN OIL PRESSURE DROP AND PERFORMED AN IFSD. THE ACFT GLIDED SAFELY TO THE GROUND. THE ON GROUND INVESTIGATION REVEALED OIL LOST DUE TO A BROKEN RGB OIL PRESSURE TRANSFER TUBE AT A FLANGE. THE ACFT SUFFERED MINOR AIRFRAME STRUCTURAL DASDR CA130204005Connector · mismanufactured(CAN) FLAP ACTUATOR ASSY. HAS 2 MOTORS, A PRIMARY AND STAND-BY, WHICH OPPOSE EACH OTHER AT TRANSMISSION, THEREFORE THEY ARE WIRED OPPOSITE EACH OTHER TO FUNCTION NORMAL. RECEIVED NEW FLAP ACTUATOR ASSY. THE PRIMARY MOTOR WIRE CONNECTOR WAS FOUND WIRED BACKWA
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