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 CA000614017Hub · cracked(CAN) FIELD MAINTENANCE FOUND SUSPECTED CRACK, N.D.T. CONFIRMED CRACK. HUB REPLACED, PROPELLER RETURNED TO SERVICE.SDR 20000602SH002Crankshaft · unserviceablePER TCM MSB 00-5, CRANKSHAFT WAS REJECTED BY TELEDYNE CONTINENTAL MOTORS. (X)SDR 20000712SH020Spar · crackedDURING ROUTINE INSP, NOTED THE RT WING AFT SPAR WEB CRACKED IN 5 PLACES AND THE ROLL SERVO ATTACH BRACKET 60931 CRACKED AT THE OTBD SERVO ATTACH HOLE. ALL CRACKS ARE IN VICINITY OF S-TEC ROLL SERVO BRACKET ATTACHMENT BOLTS. S-TEC TWO AXIS AUTOMATIC FLIGHT GUSDR AU000242Spark Plug · faulty(AUS) NR 3 CYLINDER SPARK PLUGS (2 OFF) BRIDGED ACROSS ELECTRODES.SDR AU000176Control Panel · burned(AUS) ALTERNATOR CONTROL UNIT INTERNAL FAULT.SDR 2000ZZZX645Hose · leakingDURING ANNUAL INSPECTION, FOUND ABOVE MENTIONED HOSE LEAKING PROFUSELY. THE HOSE APPEARED TO BE SUPPORTED PROPERLY. WHEN FUEL PRESSURE WAS APPLIED WITH AIRCRAFT ELECTRIC BOOST PUMP, FUEL BEGAN COMING OUT OF BRAIDED, CRIMPED AREA NEAR THE END OF THE HOSE. ADSDR 99ZZZX4699Magneto · failedPILOT REPORTED MINOR ENGINE ROUGHNESS IN-FLIGHT AT HIGH ALTITUDES. IN-FLIGHT MAGNETO CHECK SHOWED MAGNETO ON LEFT SIDE TO BE COMPLETELY DEAD. POINTS AND ROTOR AND CONDENSER ARE OK.SDR CA991229016Bolt · broken(CAN) DURING 100 HOUR INSPECTION, MAINTENANCE PERSONNEL CHECKED THE BOLT AT THE AFT END OF THE NOSE GEAR DRAG STRUT, WITH A WRENCH. LIGHT PRESSURE FRACTURED THE BOLT HEAD FROM THE SHANK. THE SUBMITTER HAS FOUND A NUMBER OF THESE BOLT HEADS BROKEN OFF IN VARIOUSDR 99ZZZX4217Engine · failedIN-FLIGHT FAILURE OF ENGINE. APPARENT BROKEN CRANKSHAFT. NOTE: AD 99-09-17 C/W BY FACTORY. INSTALLATION OF NEW CRANKSHAFT 5-26-99. NO DAMAGE TO AIRCRAFT DUE TO SUCCESSFUL EMERGENCY LANDING.SDR CA991027040Crankshaft · failed(CAN) CRANKSHAFT FAILED - THERE ARE MAINTENANCE LOG ENTRIES OF PREVIOUS PROP STRIKE.SDR CA991027039Bolt · sheared(CAN) DURING MAINTENANCE, NOSE GEAR DRAG LINK, AFT ATTACH BOLT FOUND WITH BOLT HEAD SHEARED OFF.SDR AU991027Actuator · worn(AUS) ELEVATOR TAB ACTUATOR SPROCKET LOCATING PINS MIGRATED PREVENTING THE TAB FROM MOVING. INVESTIGATION FOUND WEAR IN THE GROOVE PIN HOLES.SDR AU991080Piston Pin · failed(AUS) NR 2 CYLINDER PISTON PIN END CAP SHEARED OFF. ENGINE OIL SYSTEM CONTAMINATED WITH METAL.SDR 99ZZZX3475Hinge Assy · crackedBOTH INBOARD AND OUTBOARD AILERON HINGE BRACKET ASSYS ON THE RIGHT WING WERE CRACKED ON THE BOTTOM AND HAD LOOSE OF SHEARED RIVETS WHERE THEY ATTACH TO THE REAR SPAR. THIS DAMAGE CANNOT BE SEEN WITHOUT REMOVING THE FALSE SPAR, BUT CAN BE DETECTED BY LOOSENESSSDR 99ZZZX3491Hub · crackedET INDICATIONS IN BLADE SOCKETS 2 AND 3 IN EXCESS OF 350 MICRORAMPS.SDR 99ZZZX3139Engine · failedPILOT REPORTED ENGINE VIBRATING BADLY AND LOSING POWER ON CLIMB-OUT. AIRCRAFT MADE A SAFE LANDING AT DEPARTURE AIRPORT. OIL WAS ALL ALONG THE RIGHT SIDE OF THE AIRCRAFT. ON REMOVING THE COWL, A HOLE APPROXIMATELY 2 INCHES BY 3 INCHES WAS IN THE CASE AND A CSDR 99ZZZX2544Rod End · brokenROD END BROKE WHERE IT EXITS SPACER ASSY, PN 1260632-3, WHICH IS THE RUDDER TRIM SPROCKET AT THE END OF THE STEERING BUNGEE. SUBMITTER STATED THIS IS THE THIRD ONE KNOWN TO BREAK IN 10 YEARS. NO NOSE WHEEL STEERING, BUT STILL RUDDER STEERING.SDR AU990679Blade · misrigged(AUS) PROPELLER BLADE SETTINGS INCORRECT. FINE PITCH SET AT 12.5 DEGREES INSTEAD OF AT 11.2 DEGREES.SDR 99ZZZX1638Head · crackedHEAD CRACKED, STARTING FROM THE EXHAUST VALVE SEAT AND TRAVELING UP ABOVE THE SPARK PLUG BOSS AND BACK DOWN APPROXIMATELY ONE INCH FROM THE INTAKE VALVE SEAT. THE ENTIRE LENGTH OF THE CRACK WAS APPROXIMATELY FOUR INCHES. A .1250 INCH BY ONE INCH HOLE HAD OPESDR 99ZZZX953Bracket · corrodedANNUAL INSPECTION OF AIRCRAFT USED EXTENSIVELY IN SALT WATER/FLOAT OPERATION, REVEALED BOTH OTBD ELEVATOR ATTACH BRACKETS CORRODED AND LIGHT DAMAGE TO STABILIZER REAR SPARS.SDR 99ZZZX1429Valve · wornAT ENGINE TT 378.8 HOURS, REMOVED ALL CYLINDERS AND HONED DUE TO 'GLAZING'. AT ENGINE TT 380.0 HRS, PILOT REPORTED ENGINE RUNNING ROUGH. REPLACED NR 6 CYLINDER ASSY DUE TO 'LOW' COMPRESSION 20/80 PSI. FURTHER INSPECTION OF CYLINDER REVEALED EXCESSIVELY WORN ISDR CA990223002Bolt · broken(CAN) AFT DRAG LINK BOLT FOUND WITH THE BOLT HEAD SHEARED OFF. SUBMITTER STATED THIS IS THE SECOND ONE FOUND IN 200 HOURS ON THE SAME AIRCRAFT.SDR AU990087Bracket · broken(AUS) ENGINE THROTTLE/MIXTURE CONTROL CABLE SUPPORT BRACKET BROKEN. BRACKET IS MOUNTED ON THE INDUCTION MANIFOLD.SDR CA990318027Bolt · sheared(CAN) ON INSPECTION OF THE MLG, THE FRONT RIGHT HAND BOLT ATTACHING THE GEAR LEG WAS FOUND TO BE SHEARED. OTHER BOLTS WERE INVESTIGATED WITH NO FAILURES.SDR 99ZZZX949Line · chafed100 HOUR INSPECTION FOUND RT AILERON CABLE RUBBED THROUGH FORWARD FUEL LINE INSIDE CABIN (UPPER RT SIDE WHERE FUEL LINE ENTERS CABIN BY WINDSHIELD.) INSTALLED NEW PART, ADJUSTED AWAY FROM CABLE WHEN CONNECTED TO TANK.SDR 99ZZZX1078Frame · crackedRIGHT DOOR POST JAMB HAD A CRACK IN OUTBOARD EDGE OF JAMB THROUGH A SCREW HOLE AND EXTENDING 1 INCH FROM EDGE.SDR CA990318026Handle · broken(CAN) OUTSIDE LEVER ON CARGO DOOR BROKEN.SDR AU990001Nut · missing(AUS) DURING PERIODIC ENGINE INSPECTION, IT WAS DISCOVERED THAT THE BOLT (PN AN7-46A) SECURING THE ALTERNATOR TO THE ALTERNATOR MOUNT (PN 643935) WAS LOOSE AND HAD ELONGATED THE MOUNTING HOLES IN THE MOUNT AND ALTERNATOR. FURTHER INVESTIGATION REVEALED THAT TSDR CA990318021Jackscrew · worn(CAN) EXCESSIVE PLAY FOUND IN ELEVATOR TRIM JACK WORM GEAR.SDR AU981678Switch · corroded(AUS) ON SELECTION, FLAPS FAILED TO EXTEND. INVESTIGATION FOUND CORRODED TERMINALS ON THE SELECTOR SWITCH MICROSWITCHES.SDR AU981679Connector · loose(AUS) MAIN LANDING GEAR 'UP' PRESSURE LINE CONNECTION TO SELECTOR FOUND NOT CORRECTLY TIGHTENED - RESULTING IN COMPLETE LOSS OF RESERVOIR OIL.SDR AU981664Wing Tip · damaged(AUS) AFTER LANDING, THE AIRCRAFT DEPARTED RUNWAY AND RAN INTO SOFT SOIL SLIGHTLY DAMAGING BOTH DROP WING TIPS AND ONE PROPELLER BLADE.SDR 98ZZZX4330Bushing · damagedDEFECT MAY HAVE BEEN CAUSED BY OVERCENTER NOT GOING TO FULL TRAVEL.SDR 98ZZZX4329Bushing · damagedDEFECT MAY HAVE BEEN CAUSED BY OVERCENTER NOT GOING TO FULL TRAVEL.SDR CA981109001Bolt · missing(CAN) DURING OPS 4 INSPECTION, THE PILOTS CONTROL COLUMN WAS FOUND LOOSE. FURTHER INVESTIGATION FOUND ONE BOLT MISSING AND TWO OTHER BOLTS LOOSE. PART TC: 7,577.SDR 98ZZZX4260Strut Fitting · crackedDURING ANNUAL INSPECTION, FOUND THE AFT LEFT UPPER DIAGONAL STRUT FITTING CRACKED IN FIVE SEPARATE AREAS ON BOTH THE UPPER AND LOWER SURFACES ALONG THE LONGITUDINAL GRAIN. IT WAS ALSO NOTED THAT TWO CRACKS WERE LOCATED ALONG AN ORIGINAL MACHINING MARK. THE MSDR 98ZZZX4580Strut Fitting · corrodedDURING THE RECEIVING INSPECTION OF A WIPLINE 3730 FRONT STRUT JOINING FITTING, PITTING CORROSION WAS FOUND ON THE FRONT FACE SURFACE. THE PART WAS RED TAGGED AND RETURNED TO WIPAIRE, INC.SDR 98ZZZX4579Fitting · corrodedDURING RECEIVING INSPECTION OF A WIPLINE 3730 NOSE LANDING GEAR PIVOT BLOCK, CORROSION/CASTING FLAWS WERE FOUND ON THE LOWER FACE SURFACE. THE PART WAS RED TAGGED AND RETURNED TO WIPAIRE, INC.SDR AU981519Cylinder · cracked(AUS) NR 4 CYLINDER HEAD CRACKED. CRACK LENGTH APPROXIMATELY 25.4 MM (1 INCH). PART TC: 1,865.SDR AU981114Support · cracked(AUS) HORIZONTAL STABILIZER REINFORCEMENT CRACKED.SDR CA980928006Collar · broken(CAN) ON TAKEOFF, THE STEERING COLLAR BROKE. AIRCRAFT LANDED OK. NEW PART APPEARS TO BE OF A HEAVIER MATERIAL.SDR 99ZZZX301Nut · crackedDURING INSPECTION OF ENGINE FOR OIL LEAK, THE LOWER FORWARD CYLINDER FLANGE ATTACH NUT (AT THRU-BOLT) WAS FOUND CRACKED AND LOOSE ON BOLT. UNABLE TO DETERMINE CAUSE OF FAILURE.SDR 98ZZZX3478Skin · corrodedCORROSION UNDER THE VIBRATION ABSORBING PADS DUE TO WATER BEING TRAPPED WHERE THE BONDING OF THE PAD TO THE SKIN HAS FAILED. SUBMITTER STATES THIS IS A COMMON PROBLEM WITH CESSNA AIRCRAFT.SDR 98ZZZX3141Bearing · failedBEARING SHOULD HAVE 519.9 HOURS IF CHANGED AT OVERHAUL. ENGINE OVERHAULED BY T.W. SMITH ON 6-25-93. MAY HAVE ALSO BEEN CAUSED BY OVERTIGHTENING OF ALTERNATOR BELT. BEARING FAILURE RESULTED IN METAL CONTAMINATION OF THE OIL AND OIL FILTER.SDR 98ZZZX2984Bungee · weakON TWO NON-CONSECUTIVE LANDINGS WITH THE SAME PILOT, THE A/C VEERED OFF THE RUNWAY TO THE RIGHT. PILOT EXPRESSED A LOSS OF DIRECTIONAL CONTROL OF THE A/C DUE TO AN UNSTEERABLE NOSE GEAR AND POSSIBLY A NOSE GEAR THAT MAY HAVE NOT BEEN FULLY CENTERED ON INITIALSDR 98ZZZX3570Fitting · crackedFITTINGS CRACKED, BUSH OPERATIONS.SDR 98ZZZX3569Fitting · crackedLT MLG FITTINGS CRACKED, BUSH OPERATIONS.SDR 98ZZZX2357Spinner · crackedDURING A 100-HOUR INSPECTION, THE PROP SPINNER WAS FOUND CRACKED IN THREE PLACES. THE CRACKS WERE IN THE CENTER OF EACH BLADE CUT-OUT. NO OTHER DAMAGE WAS FOUND. THE PROBLEM MAY HAVE BEEN CAUSED FROM PUSHING ON THE SPINNER DURING GROUND HANDLING.SDR 98ZZZX3174Fitting · crackedDURING A 200-HOUR INPSECTION, BOTH MAIN GEAR OUTBOARD ATTACHMENT FITTINGS WERE FOUND CRACKED. THIS AIRCRAFT HAD AN INCIDENT SEVERAL HUNDRED HOURS AGO, BUT NO RECENT REPORT OF A HARD LANDING. THIS ACFT IS SUBJECTED TO MANY LANDINGS ON GRAVEL STRIPS WHICH MAY SDR 98ZZZX3173Fitting · crackedDURING A 200-HOUR INSPECTION, BOTH MAIN GEAR OUTBOARD ATTACHMENT FITTINGS WERE FOUND CRACKED. THIS AIRCRAFT HAD AN INCIDENT SEVERAL HUNDRED HOURS AGO, BUT NO RECENT REPORT OF A HARD LANDING. THIS ACFT IS SUBJECTED TO MANY LANDINGS ON GRAVEL STRIPS WHICH MAY
Back to Cessna U206G