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 = 'T182T' 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 = 'T182T' 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 2025FA0000198Actuator · faultedPILOT REPORTED: WHILE ON DESCENT INTO KPWG I DISCONNECTED THE AUTOPILOT AT 500 FT AGL. I WENT TO MAKE A MANUAL ADJUST OF THE TRIM USING THE HAND TRIM WHEEL AND FOUND IT DIFFICULT TO MOVE. I ALSO ATTEMPTED TO USE THE ELECTRIC TRIM BUT FOUND IT TO BE INEFFECTIVESDR 2024FA0000740Intake Pipe · looseMY SHOP HAS SEEN TWO OF THESE ISSUES IN A VERY SHORT TIME ON TWO DIFFERENT AIRCRAFT. THE FIRST WAS THE LISTED AIRCRAFT (N2155J), THE SECOND IS ON N406CV. SAME ENGINES (TIO-540-AK1A) WITH APPROXIMATELY THE SAME TIME SINCE OVERHAUL (1200 HOURS) FROM TWO DIFFERENSDR 2023FA0000017Tube · puncturedON DEC 18 I WAS NOTIFIED BY THE OWNER THAT HE HAD EXPERIENCED AND FLAT NOSE LANDING GEAR TIRE AFTER LANDING. HE REPORTED TO ME THE TIRE WAS FLAT WHILE WHEN WE WAS TAXIING HE AIRCRAFT BACK TO THE HANGAR. I REMOVED THE NOSE LANDING GEAR WHEEL ASSEMBLY AND INSPESDR 2019FA0000107Tailpipe · crackedOWNER STATED TAIL PIPE CLAMP WAS REPLACED AT ANNUAL INSPECTION 5-25-18 AS WELL AS 3 OTHER CLAMPS ON THE WASTE GATE AND EXHAUST. OWNER FOUND ON PREFLIGHT THAT THE TAIL PIPE WAS LOOSE. UPON FURTHER INSPECTION AT THE MAINTENANCE SHOP FOUND TAIL PIPE CLAMP TO BE ISDR 2018FA0000337Cylinder Head · bypassingPILOT REPORTED NO START CONDITION AFTER 2 HOUR FLIGHT. COMPRESSION CHECK COMPLETED AND FOUND CYLINDER NR 1, 72, ALL OTHER CYLINDERS BELOW 16 PSI, WITH CYLINDERS 4 & 5 AT 0. BORESCOPE FOUND EXHAUST VALVES STUCK OPEN ON CYLINDERS 4 & 5. ALL OTHER PERIMETERS NORSDR BQVD2018081300001Flex Hose · disintegratedON RAMP, AFTER FLIGHT, PILOT NOTICED A PUDDLE OF FUEL UNDER THE ENGINE COWL. FOUND THE ENGINE DRIVEN FUEL PUMP SEAL WAS LEAKING. THE LEAKING FUEL PUMP PROBLEM WAS COMPOUNDING WITH ANOTHER SERIOUS PROBLEM. MAINTENANCE DISCOVERED THE DRAIN HOSE MATERIAL IS NOT SDR 2018FA0000417Cylinder Head · bypassingENGINE EXTREMELY HARD TO START AND KEEP RUNNING SMOOTHLY. FLEW TO KPNE WITHOUT INCIDENT. ENGINE PERFORMED WITHIN PARAMETERS. DELIVERED AIRPLANE TO MAINTENANCE AND STARTING PROBLEM DIAGNOSIS. MECHANIC DETERMINED 5 OUT OF THE 6 CYLINDERS HAD VERY LOW COMPRESSIONSDR 2018FA0000416Cylinder Head · bypassingENGINE EXTREMELY HARD TO START AND KEEP RUNNING SMOOTHLY. FLEW TO KPNE WITHOUT INCIDENT. ENGINE PERFORMED WITHIN PARAMETERS. DELIVERED AIRPLANE TO MAINTENANCE AND STARTING PROBLEM DIAGNOSIS. MECHANIC DETERMINED 5 OUT OF THE 6 CYLINDERS HAD VERY LOW COMPRESSIONSDR 2018FA0000415Cylinder Head · bypassingENGINE EXTREMELY HARD TO START AND KEEP RUNNING SMOOTHLY. FLEW TO KPNE WITHOUT INCIDENT. ENGINE PERFORMED WITHIN PARAMETERS. DELIVERED AIRPLANE TO MAINTENANCE AND STARTING PROBLEM DIAGNOSIS. MECHANIC DETERMINED 5 OUT OF THE 6 CYLINDERS HAD VERY LOW COMPRESSIONSDR CA180510005Bearing · out of adjust(CAN) BEARING ALIGNMENT HOLES INCORRECTLY INDEXED RESULTING IN MISALIGNED BEARING HALVES. (TC# 20180510005)SDR 2017FA0000360Exhaust Pipe · crackedDURING ANNUAL INSPECTION, OVERBOARD EXHAUST PIPE WAS DISCOVERED CRACKED AND LEAKING AT THE WASTE GATE ATTACH FLANGE.SDR 2016FA0000591Pushrod · scoredPUSHRODS INSPECTED PER SA-167A AND 6 PUSHRODS SHOW SIGNS OF SCORING.SDR 2016FA0000268Spline · shearedSHAFT SHEARED ON TAKEOFF. PUMP SEIZED. DRIVE SHAFT SPLINE SHEARED.SDR 2015FA0000264Exhaust Stack · crackedDURING AN OIL CHANGE THE TECH WAS DOING A VISUAL INSPECTION OF THE ENGINE AND NOTICED SOME EXHAUST SOOT/STAINING ON THE HEAT SHIELD FOR THE J BOX. DISCOVERED THE SOURCE TO BE THE CRACKED EXHAUST ELBOW.SDR CA141117005Breather · cracked(CAN) THE OIL BREATHER/SEPARATOR TAKES BLOWBY GASES FROM THE ENGINE CRANKCASE AND CENTRIFUGALLY SEPARATES OIL MISTS FROM THEM BEFORE DUMPING THE GASES OVERBOARD THROUGH THE BREATHER TUBE. OIL IS RETURNED TO THE ENGINE SUMP. OIL WAS NOTED SEEPING FROM A CRACKSDR LC1R20140613001Wastegate Valve · erodedTROUBLE SHOT A LOW MANIFOLD PRESS PROBLEM, FOUND WASTE GATE BUTTERFLY OVER 80% ERODED AWAY. THERE WAS NO OTHER DAMAGE TO THE INDUCTION SYS OR TO THE TURBOCHARGER.SDR CA140516002Bolt · interference(CAN) BALANCE CABLE TO LT AILERON BELLCRANK ATTACH BOLT FOUND TO BE INTERFERING WITH AILERON PUSHROD AT FULL TRAVEL.SDR 2014FA0000111Screw · looseCOMPLIED WITH SB SEB-27-01. SEVERAL DAYS LATER, ACFT WAS FLOWN AND THE ELEVATOR CONTROL BECAME INCREASINGLY STIFF DURING THE FLIGHT TO THE POINT OF LOCKING UP. THE ACFT RETURNED AIRPORT AND MADE AN UNEVENTFUL LANDING. DURING INSPECTION, TENSION WAS RESET ONSDR YWYR201209159368Master Switch · damagedPILOT REPORTED THAT ACFT MASTER SWITCH WOULD NOT ACTUATE ACFT POWER ON SEVERAL OCCASIONS. IF THE MASTER SWITCH WAS CYCLED ON AND OFF SEVERAL TIMES IT WOULD EVENTUALLY TURN ACFT POWER ON. NEW MASTER SWITCH INSTALLED AND OPERATION WAS NORMAL.SDR 2012FA0000542Bracket · missingDURING A SCHEDULED INSPECTION, IT WAS NOTED THAT THE RIVETS ATTACHING HORIZONTAL STABILIZER LT AND RT ATTACH BRACKETS TO THE TAILCONE BULKHEAD WERE NOT INSTALLED. FURTHER INSPECTION REVEALED THAT THE BRACKET CLIPS HAD PILOT HOLES BUT WERE NOT DRILLED TO MATCSDR CA120509009Bulkhead · dented(CAN) ACFT WAS OPEN FOR INSPECTION. NOTICED THAT BULKHEAD WAS DENTED. ALSO FOUND OUT THAT DEALER HAS NOTED THAT THIS IS A COMMON PROBLEM IN MANY OF THE NEWER MODEL. THIS DAMAGE IS NOT NEGLIGABLE IAW SRM. SUGGEST THAT MFR IS CONTACTED TO MODIFY THE SRM TO ALLOSDR YN8R2012041013834Hose · leakingON COMPLIANCE WITH SB 599, FUEL PUMP REPLACEMENT, IT WAS DISCOVERED THAT THE ENGINE DRIVEN FUEL PUMP INLET HOSE HAD INDICATIONS OF OUTER FIRESLEEVE DETERIORATION AND BULGING INDICATIVE OF THE FUEL HOSE LEAKING FUEL FROM CRIMPED AREA OF FITTING/HOSE. REPLACED SDR CA120316003Bulkhead · dented(CAN) DURING IMPORT INTO CANADA NOTICED FS 207 BULKHEAD DAMAGE. LOWER PORTION OF BULKHEAD HAS 3 SMALL DENTS. DAMAGE APPEARS TO HAVE OCCURRED DURING THE MFG PROCESS. THERE IS EVIDENCE OF RUB MARKS ON THE PEAKS OF THE DENTS PRESUMABLY CAUSED BY A BUCKING BAR.SDR ESMR2012022801Pump · leakingACFT WAS INBOUND WHEN THE ENGINE BEGAN TO LOOSE POWER. THE PILOT USED THE FUEL BOOST PUMP TO KEEP THE ENGINE RUNNING AND LANDED WITHOUT INCIDENT. THE ENGINE RAN FINE AT IDLE ON THE GROUND. WITH THE ENGINE OFF AND THE FUEL SELECTOR TURNED ON, FUEL WAS RUNNINGSDR TRBA2012013001Switch · faultyTHE CREW REPORTED TE EMERGENCY LIGHTS ABOVE THE F/A JUMP SEATS ON AT ALL TIMES. THE ACFT WAS REMOVED FROM SERVICE. REPLACED 2 MIN LIGHT PUSH BUTTON SWITCH NEAR PASSENGER ENTRANCE DOOR, PERFORMED OPS CHECK AND FOUND WORKING PROPERLY IAW MM 20-27-17. THE OPS CSDR CA100805004Antenna · failedWAAS/GPS/COMM COMBINATION ANTENNA NO LONGER ABLE TO RECEIVE GPS SATELLITE INFORMATION. COMM FUNCTIONALITY UNAFFECTED.SDR 2010FA0000232Circuit Breaker · defectiveON GROUND ROLL AFTER LANDING FLAPS STOPPED RETRACTING AT 10 DEGREES. FLUSH TYPE CIRCUT BREAKER DID NOT POP OUT BUT WAS TRIED NUMEROUS TIMES. ALL SWITCHES AND MOTOR CHECKED GOOD. REINVESTIGATING CIRCUT BREAKER, CAUSED CIRCUT BREAKER TO CLICK AND SYSTEM TO RUNSDR 2008FA0000291Unknown · malfunctionedWHEN TURNING THE (CRS) COURSE KNOB, THE INNER KNOB (BARO) BAROMETRIC PRESSURE KNOB WOULD TURN ALSO. CHANGING THE ALTITUDE INDICATED.SDR O7TR200800001Turbocharger · failedMAJOR TURBO FAILURE DUE TO SEPARATION OF TURBINE WHEEL HEAD FROM SHAFT.SDR 2007FA0000562Line · cracked30 DEGREE FITTING HAS CRACK ON WRENCH FLAT. (K)SDR 2007FA0000233Spring · brokenNEW POINTS (PN M3081) WERE INSTALLED IN BOTH MAGNETOS AT THE ANNUAL INSPECTION ON 2/22/07, TT 649.2. ON 3/10/07, TT 658.2, PART TT - 9.0 HOURS, THE PILOT/OWNER PERFORMED MAG CHECK AND THE ENGINE QUIT. A MECHANIC REMOVED THE RT MAG AND FOUND THAT THE SPRING TSDR FAA1012001Fuel · leakingAFTER AN APPROXIMATELY 30 MILE UNEVENTFUL FLIGHT WITH A LANDING AND TAXIBACK FOR DEPARTURE AT HVN THE AIRCRAFT WAS CLEARED FOR TAKEOFF BY THE TOWER. THERE WAS A FEW MINUTES OF HOLDING PRIOR TO BEING RELEASED. ON TAKEOFF FROM HVN RWY 2, THE AIRCRAFT FUNCTIONESDR 2006FA0000944Relief Valve · failedPILOT REPORTED, ON TAKEOFF ROLL, THE MANIFOLD PRESSURE WENT TO GREATER THAN 40 MP FOR 3 TO 4 SECONDS. THE PILOT WENT BACK TO RUNUP AREA AND CONFIRMED THAT MP COULD GO ABOUT 40 MP, PILOT TAXIED BACK TO RAMP AND GROUNDED AIRCRAFT. TROUBLESHOT TURBO CHARGER SYSSDR 2006FA0000727Guard · out of rigPROTECTIVE GUARDS ARE CALLED OUT BY IPL ORIGINALLY, IPL REV 7 DOES, REV 8 DOES NOT. CURRENT REVISION 12, CALLS FOR THE GUARDS TO BE INSTALLED REV 13 IS IN TRANSIT BUT SHOULD INCLUDE THE CALL OUT. THIS AIRCRAFT HAS INDICATIONS THAT ELEVATOR CONTROL LINES HAVESDR 2006FA0000089Fuel Line · wornFOUND FUEL INJECTION LINE RUBBING CYLINDER COOLING FINS. CAUSING WEAR TO THE LINE. IF WORN CAN CAUSE FUEL LEAK ON TO THE TURBO CHARGER. AD WAS IN COMPLIANCE BUT THE CLAMP WAS LOOSE ALLOWING FUEL LINE TO ROTATE. (SW01200603311) (K)SDR 2005FA0000309Switch · inoperativeSTALL WARNING INOP FOUND STALL WARNING SWITCH TERMINAL SCREW LAYING INSIDE WING, SCREW BACKED OUT IN FLIGHT.SDR 2005FA0000303Terminal · looseSTALL WARNING INOP, FOUND STALL WARNING SWITCH TERMINAL SCREW LAYING INSIDE WING, SCREW BACKED OUT IN FLIGHT.SDR 2006FA0000181Connector · disconnectedPLASTIC CONNECTOR THAT CONNECTS TO TACHOMETER TRANSDUCER HAS NO LOCKING DEVICE, THIS TYPE OF CONNECTOR SHOULD HAVE A SNAP LOCK AT THE END OF IT THREAD TRAVEL. FOUND THIS SAME SIMILAR PROBLEM ON 2 OTHER SINGLE ENGINE AIRCRAFT WITH THE SAME TRANSDUCERE. ALSO HSDR CA041216010Wastegate Valve · seized(CAN) WASTEGATE BUTTERFLY VALVE FOUND SEIZED ON INSPECTION. THIS IS THE SECOND VALVE FOUND SEIZED ON TWO DIFFERENT AIRCRAFT WITH LOW TTSN.SDR 2004FA0000859Circuit Breaker · misinstalledGPS CIRCUIT BREAKER IS PROVIDING POWER TO MULTIPLE UNITS WHICH IS CONTRARY TO AC20-138A. AC20-138 STATES THAT GPS CIRCUIT BREAKER CAN ONLY POWER GPS. REFERENCE ATTACHED DRAWINGS FROM MFG WIRING DIAGRAM MANUAL. PAGES 34-20-00-01 AND 34-52-03-01.SDR CA031217008Restraint · inoperative(CAN) DURING INSPECTION IT WAS NOTICED THAT BOTH REAR SEAT RESTRAINT SYSTEM INERTIA REELS WOULD INTERMITTENTLY LOCK AND NOT ALLOW BELT TO EXTEND. IT WAS DECIDED THAT IF RESTRAINTS WERE RELEASED IN FLIGHT IT MAY NOT BE POSSIBLE TO REFASTEN THEM SO BOTH UNITS WESDR 2003FA0001028Cylinder · wrong partDURING A ANNUAL INSPECTION, FOUND THE NR 1 CYLINDER TO BE INCORRECT FOR THIS INSTALLATION, INCORRECT CYLINDER INSTALLED BY CESSNA OR LYCOMING PRIOR TO INSTALLATION ON AIRCRAFT. CYLINDER WAS FOR SHORT REACH PLUGS, ENGINE USES LONG REACH. CYLINDER FOUND ON 2ND ASDR 2003FA0001027Cylinder · wrong partDURING A ANNUAL INSPECTION, FOUND THE NR 1 CYLINDER TO BE INCORRECT FOR THIS INSTALLATION, INCORRECT CYLINDER INSTALLED BY MFG PRIOR TO INSTALLATION ON AIRCRAFT. CYLINDER WAS FOR SHORT REACH PLUGS, ENGINE USES LONG REACH. CYLINDER FOUND ON 2ND ANNUAL INSPECTIOSDR 2003FA0001026Cylinder · wrong partDURING A ANNUAL INSPECTION, FOUND THE NR 1 CYLINDER TO BE INCORRECT FOR THIS INSTALLATION, INCORRECT CYLINDER INSTALLED MFG PRIOR TO INSTALLATION ON AIRCRAFT. CYLINDER WAS FOR SHORT REACH PLUGS, ENGINE USES LONG REACH. CYLINDER FOUND ON 2 ND ANNUAL INSPECTION SDR 2003FA0000598Connector · improperTHE CONNECTOR FROM AIRCRAFT HARNESS THAT MATS TO THE TURN COORDINATOR HAS IMPROPERLY CRIMPED PINS. THIS FAULTY CONNECTION CAUSES AUTOPILOT WING ROCKING AND CAN CAUSE UNDESIRABLE ROLL RATES DURING CLIMBS.SDR 2002FA0001028Magneto · damagedOWNER COMPAINED WHEN RT MAGNETO WAS SELECTED ENGINE WOULD QUIT. AFTER REMOVING MAGNETO FOUND MANY INTERNAL PARTS BURNED. REPLACED WITH NEW MAGNETO.
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