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 = 'U206G' 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 = 'U206G' 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 AU981183Fitting · corroded(AUS) FUSELAGE TO RIGHT WING REAR ATTACHMENT FITTING CONTAINED INTERGRANNULAR CORROSION BETWEEN THE FITTING AND THE CARRY-THROUGH SPAR. PART TC: 11,194.SDR AU981182Fitting · corroded(AUS) FUSELAGE TO LEFT WING REAR ATTACHMENT FITTING CONTAINED INTERGRANNULAR CORROSION BETWEEN THE FITTING AND THE CARRY-THROUGH SPAR. PART TC: 11,194.SDR 98ZZZX1670Crankcase · crackedTHE CRANKCASE SPLIT FROM NR 6 CYLINDER HOLE TO OIL FILLER HOLE ON TOWARD TO THE FRONT OF THE CASE. THIS OCCURRED IN CONJUNCTION WITH THE CYLINDER MOUNTING STUD IN THIS IMMEIDATE AREA FAILING. THE CIRCUMSTANCES UNDER WHICH IT OCCURED WERE 'NORMAL OPERATION'. SDR AU980485Guide · worn(AUS) ENGINE CYLINDER REMOVED DUE TO LOW COMPRESSION. EXHAUST VALVE P/N 636242 FOUND WORN 0.178 MM (0.007 INCH). EXHAUST VALVE GUIDE P/N 652956 WORN 0.0432 MM (0.017 INCH).SDR AU980333Hub · cracked(AUS) PROPELLER HUB CRACKED ON FLANGE AREA. INVESTIGATION ALSO FOUND THAT ALL THREE BLADE SOCKETS WERE FILLED WITH `SILASTIC' SEALANT. PERSONNEL/MAINTENANCE ERROR.SDR 98ZZZX1342Reinforcement · crackedDURING AN ANNUAL INSPECTION ON THE HORIZONTAL STABILIZER, THE LEFT REAR REINFORCEMENT, PN 1232623-1, WAS FOUND CRACKED. THIS PART IS RIVETED TO THE REAR SPAR. A NEW P/N 1232624-1 WAS INSTALLED ON BOTH SIDES. THE NEW PART IS RE-DESIGNED AND MADE OF STEEL INSSDR 97ZZZX5111Rod End · failedDURING PRE-FLIGHT INSPECTION, EXCESSIVE FREE MOVEMENT IN RUDDER WAS NOTED. FURTHER INVESTIGATION REVEALED THE ROD END BETWEEN THE RUDDER BAR AND BUNGEE HAD CRACKED OFF. THE PART SHOWED EVIDENCE OF HAVING BEEN CRACKED FOR A WHILE. THIS PART SEEMS TO BE VERY SDR 97ZZZX4882Relay · shortedGENERATOR WOULD NOT STAY ON LINE, FOUND REVERSE CURRENT RELAY FULL OF WATER WHICH SHORTED RELAY. AIRCRAFT SAT OUTSIDE IN HEAVY RAIN. SUGGEST SEALING ELECTRICAL BOX WITH NEOPHRENE GASKET AND WIRE BUNDLE WITH SILICON. THIS AIRCRAFT IS A SOLOY CONVERSION.SDR 97ZZZX4582Torque Plate · crackedDURING A PRE-FLIGHT INSPECTION, NOTED RUB MARKS ON INSIDE OF BRAKE DISC. FURTHER INVESTIGATION FOUND THE TORQUE PLATE CRACKED AT THE BUSHING FOR THE SLIDE PINS OF THE CALIPER. SUBMITTER STATED THIS IS THE SECOND CRACKED TORQUE PLATE ON LT SIDE OF A 206 SUBMISDR 97ZZZX4391Crankshaft · brokeWHILE IN CRUISE FLIGHT, CRANKSHAFT BROKE WHERE NR 1 ROD THROW COMES OFF REAR OF NR 2 MAIN. AIRCRAFT ON FLOATS, MADE EMERGENCY LANDING ON DRY LAKE BED. FLOATS SHEARED OFF, PLANE WENT UPSIDE DOWN, AND PLANE IS DESTROYED.SDR 97ZZZX3978Crankshaft · failedCRANKSHAFT SEPARATED BETWEEN NR 2 ROD BEARING AND NR 2 MAIN BEARING JOURNALS. FRETTING NOTED ON CASE MATING HALVES. NR 1 CYLINDER WAS PREVIOUSLY REMOVED AND REPLACED APPROXIMATELY 555 HOURS BEFORE FAILURE OF CRANK. NR 2 MAIN BEARING HAD SHOWED SIGNS OF SPINSDR CA971027012Fuel Transducer · rusted(CAN) THE LEFT FUEL TRANSDUCER FOUND RUSTED, REPLACED BY NEW PLASTIC TYPE. THIS AIRCRAFT HAS THE FLINT AUXILIARY SYSTEM STC SA4366WE INSTALLED WHICH CONTAINS STEEL PARTS AND ACCORDING TO SUBMITTER IS CAUSING THE CORROSION AND CAN CLOG FUEL SYSTEM.SDR AU971274Regulator · failed(AUS) REGULATOR (2OFF) FAILED DUE TO SHORT CIRCUIT. SUSPECT CAUSED BY FAULTY ALTERNATOR.SDR AU970783Hinge · cracked(AUS) LH OUTBOARD ELEVATOR HINGE ASSEMBLY CRACKED ALONG WELD - CRACK LENGTH APPROXIMATELY 8MM (0.314IN)SDR 97ZZZX2343Cylinder · head separatedCYLINDER HEAD SEPARATED FROM BARREL IN FLIGHT. PILOT NOTICED ROUGH ENGINE AND MADE PRECAUTIONARY LANDING. FAILED CYLINDER WAS 'LIGHT' CASTING WHILE OTHER FIVE WERE 'HEAVY' CASTING. HEAD SEPARATION ALSO CAUSED FUEL LINE SEPARATION AND EXHAUST Y-PIPE DAMAGE. SDR CA971027011Fuel Pump · rusted(CAN) LEFT AUXILIARY FUEL PUMP CORRODED AND BOTH THE LEFT AND RIGHT CHECK VALVES P/N FACKV-4-100-6 FUND CLOGGED. THIS AIRCRAFT HAS FLINT STC SYSTEM STEEL PARTS WHICH ACCORDING TO SUBMITTER ARE CAUSING THE CORROSION AND CAN CLOG FUEL SYSTEM. STC SA4368WE.SDR 97ZZZX1959Hub · crackedDURING EDDY CURRENT INSPECTION, TWO CRACKS FOUND IN NR 2 HOLE, 3RD AND 4TH THREADS IN AT 6 O'CLOCK.SDR 97ZZZX1872Adapter · damagedDURING ENGINE CHANGE, THE OIL FILTER ADAPTER WAS REMOVED AND THE THREADS WERE FOUND DAMAGED AS DEPICTED IN AD 96-12-22. THERE WERE NO SIGNS OF LEAKAGE, BUT THE BREAKAWAY TORQUE APPEARED TO BE LOW. SUBMITTER STATED THIS IS THE THIRD ADAPTER OF THIS TYPE FOUNDSDR CA971027013Fuel Pump · rusted(CAN) LEFT AUXILIARY FUEL PUMP FOUND RUSTED. THIS AIRCRAFT CONTAINS FLINT AUXILIARY SYSTEM AS PER STC SA4368WE WHICH CONTAINS STEEL PARTS AND ACCORDING TO SUBMITTER CAUSES THE RUSTING AND COULD CLOG THE FUEL SYSTEM. THE AIRCRAFT REGISTRATION IS NOW C-FJSTSDR AU970389Hinge · cracked(AUS) RH AILERON HINGE ATTACHMENT ANGLE CRACKED FROM BOTTOM RELIEF NOTCH - CRACK LENGTH APPROXIMATELY 6.35MM (0.25IN)SDR AU970158Connecting Rod · broken(AUS) ENGINE NO5 CYLINDER CONNECTING ROD BIG END BEARING FAILED DUE TO LACK OF LUBRICATION/COOLING CAUSED BY LOSS OF OIL OVERBOARD - LOSS OF OIL WAS THROUGH A WORN AND HOLED EXHAUST PUSHROD TUBE CAUSED BY A BENT PUSHROD, DUE TO STICKING VALVE - CONNECTING RODSDR CA970206005Propeller · high vibration(CAN) HARTZELL PROPELLER INSTALLED AS PER STC #SA685AL. TROUBLESHOT VIBRATION SINCE INSTALLATION. INSTALLED SECOND PROP AND DID DYNAMIC BALANCE, THIS CHANGED THE POSITION OF VIBRATION. REMOVED PROP AND INSTALLED ZERO TIME MCCAULEY PROP. VIBRATION GONE.SDR 96ZZZX5840Chain Assy · lock missingPILOT REPORTED RUDDER TRIM INOPERATIVE, BUT WOULD TURN WHEEL. MASTER LINK LOCK MISSING, INSTALLED NEW MASTER LINK ASSY. (ADJUSTED CHAIN TENSION).SDR 96ZZZX5134Muffler · cone missingON AN ANNUAL INSPECTION, FOUND CONE BAFFLE 'INTERNAL PART MISSING' ON LT MUFFLER. THIS UNIT WAS OVERHAULED AT 230 HOURS PREVIOUSLY AND WAS INSTALLATED 2 YEARS PREV ANNUAL.SDR AU961149Exhaust Pipe · wrong part(AUS) RH EXHAUST COLLECTOR NO5 RISER PIPE RUBBING ON NO3 INLET MANIFOLD CAUSING WEAR DAMAGE TO BOTH ITEMS - COLLECTOR ASSEMBLY WAS NOT A GENUINE CESSNA PART AND APPEARS TO HAVE BEEN INCORRECTLY MANUFACTURED - A GENUINE CESSNA PART FITTED CORRECTLY -PERSONNEL/MSDR CA960807011Valve · broken(CAN) DURING INSPECTION THE EXHAUST VALVE ON #1 CYLINDER WAS FOUND BROKEN. COMPRESSION TEST INDICATED "0" COMPRESSION.SDR CA960807010Piston Ring · broken(CAN) INSPECTION FOUND THE TOP RING ON THE #3 CYLINDER BROKEN INTO SEVEN PIECES. THE COMPRESSION CHECK FOUND COMPRESSION AT 12 PSI.SDR AU961018Bearing · incorrect fit(AUS) NOSE LANDING GEAR OLEO UPPER BEARING PNO 1243021-1 AND RETAINER PNO 841200-19 SEPARATED - INVESTIGATION FOUND THAT THE BEARING HAD BEEN INSTALLED UPSIDE DOWN PREVENTING CORRECT SEATING OF THE RETAINER - PERSONNEL/MAINTENANCE ERRORSDR AU960928Cylinder · cracked(AUS) ENGINE NO2 ENGINE CYLINDER CRACKED IN THE INLET PORT - CRACK LENGTH APPROXIMATELY 40MM (1.5IN) - THE CRACK WAS DIFFICULT TO SEE DUE TO THE ENGINE BAFFLINGSDR 96ZZZX5119Alternator · malfunctionPILOT ATTEMPTED START, START SOLENOID CLICKING. LOW BATTERY OUTPUT TO LOW TO CLOSE SOLENOID. ALTERNATOR CHECKED FOR CHARGING. ALTERNATOR OUTPUT APPROXIMATELY 19.3 VDC FOR 24 VDC SYSTEM. ALTERNATOR REPLACED WITH OVERHAULED UNIT.SDR 96ZZZX2973Rod End · brokenPILOT HEARD A LOUD NOISE WHILE TAXIING AFTER LANDING. HE ALSO NOTICED LOSS OF NOSE WHEEL STEERING AND VERY FREE MOVEMENT OF RUDDER CONTROL. INVESTIGATION FOUND THE ROD END ON AFT STEERING BUNGEE HAD BROKEN OFF AND TRIM CHAIN WAS OFF OF SPROCKET. THIS IS THESDR AU960584Piston · damaged(AUS) NO2 CYLINDER PISTON SEVERELY ERODED AND HOLED IN THE AREA OF THE OIL RING GROOVE - METAL CONTAMINATION OF OIL SYSTEM - NO4CRANKSHAFT BEARING ALSO TURNEDSDR 96ZZZX2785O-Ring · defectiveOWNER COMPLAINT FOR FUEL CAP O-RINGS BEING TOO LARGE. INVESTIGATION REVEALED RINGS .25 INCH IN DIAMETER TOO LARGE. O-RINGS HAD BEEN INSTALLED ABOUT 30 DAYS, 1.5 HOURS TT. INSTALLED NEW O-RINGS. INSPECTED ACFT 3 WEEKS LATER AND FOUND SAME CONDITION. INSPECSDR 96ZZZX2427Torque Link · crackedCRACKED UPPER TORQUE LINK ON NOSE GEAR. DEFECT FOUND DURING 100-HOUR INSPECTION AND LUBRICATION OF NOSE GEAR. SUSPECT CAUSE MAY BE WORN STOP LUG ON SCISSORS. THE TWO CRACKS LOCATED APPROXIMATELY 2 INCHES FROM END OF SCISSORS BOTTOM SIDE.SDR AU960492Fitting · loose(AUS) HORIZONTAL STABILISER WAS REMOVED DUE TO EXCESSIVE MOVEMENT - INVESTIGATION FOUND THAT EACH OF THE TWO FORWARD ATTACHMENT FITTINGS HAD FOUR OF THE FIVE RIVETS SHEARED - SUSPECT INCORRECT GROUND HANDLING TECHNIQUESDR 96ZZZX2078Wheel Assy · crackedAIRCRAFT WAS MODIFIED BY INSTALLING GAR-AERO WHEEL ADAPTERS AND 8:50X10 TIRES PER STC SA4305WE WITH THE EXCEPTION - INSTALLED ON MCCAULEY WHEELS INSTEAD OF CLEVELAND WHEELS WITH A FIELD APPROVAL, 60.5 HRS AGO. THIS AIRCRAFT HAD A LIGHT DUTY WHEEL, PN C163006-SDR AU960347Bracket · broken(AUS) THROTTLE CONTROL CABLE ATTACHMENT BRACKET BROKEN ALLOWING INNER AND OUTER CABLES TO MOVE TOGETHER - BRACKET WAS MANUFACTURED FROM0.8128MM (0.032IN) ALCLADSDR AU960283Torque Tube · loose rivets(AUS) RH ELEVATOR ASSEMBLY TORQUE TUBE PNO 1234650-6 TO ELEVATOR ATTACHMENT RIVETS LOOSE AND WORKING - AIRCRAFT IS OPERATED AS AFLOAT PLANESDR AU960281Bulkhead · cracked(AUS) FIREWALL AND LH BULKHEAD CRACKED AT EXHAUST MOUNT ATTACHMENT - AIRCRAFT IS USED AS A FLOAT PLANESDR AU960280Bulkhead · cracked(AUS) FIREWALL AND RH BULKHEAD CRACKED IN AREA OF EXHAUST MOUNT ATTACHMENT - AIRCRAFT IS USED AS A FLOAT PLANESDR AU960274Doubler · cracked(AUS) REAR BULKHEAD RH TAILPLANE ATTACHMENT BRACKET DOUBLER CRACKED THROUGH - FURTHER INSPECTION FOUND REAR BULKHEAD CRACKED IN THESAME AREASDR AU960393Trim Tab · incorrect rigged(AUS) ELEVATOR TRIM TAB INCORRECTLY RIGGED - DURING INVESTIGATION IT WAS FOUND THAT THE ELEVATOR TRIM TAB WAS SET AT 5 DEGREES 'UP' AND 25 DEGREES 'DOWN' - THE CORRECT TRAVEL SHOULD HAVE BEEN 25 DEGREES 'UP' AND 5 DEGREES 'DOWN' - AIRCRAFT HAS DONEAPPROXIMATELSDR CA960327008Wing Tank · leaking(CAN)INSP FOUND WING TANK LEAKINGSDR CA960327006Torque Plate · cracked(CAN)ON INSPECTION THE TORQUE PLATE OF THE LEFT BRAKE WAS FOUND CRACKED.SDR CA960327001Bracket · cracked(CAN)DURING INSPECTION THE AILERON BRACKET WAS FOUND CRACKED WHERE IT ATTACHES TO THE WING TRAILING EDGE STRUCTURE.SDR AU960382Bulkhead · cracked(AUS) RH FORWARD DOOR POST BULKHEAD CRACKED IN AREA OF BEND RELIEF NOTCH - AD/CESSNA206/48 AMDT1 CARRIED OUT APPROXIMATELY 200 HOURSPREVIOUSSDR 96ZZZX2393Arm · corrodedWHEN REMOVING LT RUDDER PEDAL AND ARM ASSYS TO ACCESS FIREWALL INSIDE OF RUDDER ARM, TUBE WAS FOUND BADLY CORRODED. THERE WAS NO EVIDENCE OF CORROSION ON OUTSIDE OF TUBE. THE TUBE IS MOUNTED VERTICALLY AND IS OPEN ON TOP AND SEALED ON BOTTOM. ANY WATER THATSDR 96ZZZX2391Engine · chip lightRECEIVED OIL CHIP LIGHT INDICATION. PERFORMED REQUIRED MAINTENANCE PER ALLISON 250-C20S AND SOLOY/CESSNA MAINTENANCE AND OVERHAUL MANUALS. RECEIVED SECOND CHIP LIGHT INDICATION 3.9 HRS TIS LATER. ENGINE REMOVED AND SENT OUT FOR INSPECTION/REPAIR PER ALLISONSDR AU960079Bolt · sheared(AUS) NOSE LANDING GEAR DRAG LINK BOLT SHEARED AT NUT END ADJACENT TO THE LAST THREADED PORTION PRIOR TO THE BOLT SHANKSDR AU960016Duct · cracked(AUS) AIRBOX DUCT ASSEMBLY CRACKED BEYOND REPAIR - DUCT ASSEMBLY HAS BEEN PREVIOUSLY REPAIRED
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