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 = 'A185F' 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 = 'A185F' 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 CA961007012Rudder Bar · broken(CAN) WHILE WATER TAXIING, RUDDER BAR BROKE AT OUTBOARD PEDAL ATTACH AT REINFORCEMENT. REFERENCE AD CF-73-05. THIS UNIT HAS WELDED TAB WHICH BROKE THROUGH ALSO.SDR CA961002006Starter · shorted(CAN) STARTER FIELD COILS LOOSE ON POLE SHOES RUBBED ON THE THROUGH BOLTS CREATING A DEAD HIGH AMPERAGE SHORT RESULTING IN BOTH MASTER SOLENOID AND STARTER SOLENOID CONTACT PLATES WELDING TO TERMINALS - A VERY DANGEROUS AND FIRE CONDITION - SUSPECT INSUFFICIENSDR 96ZZZX4793Rib · crackedWHILE DOING THE CESSNA CONTINUAL AIRWORTHINESS PROGRAM, FOUND LEADING EDGE RIB BROKEN. THIS IS A PUBLIC AIRCRAFT AND IS SUBJECTED TO MANY HOURS OF LOW LEVEL FLYING.SDR 96ZZZX4792Rib · crackedWHILE DOING THE CESSNA CONTINUAL AIRWORTHINESS PROGRAM, FOUND LEADING EDGE RIB BROKEN. THIS IS A PUBLIC AIRCRAFT AND IS SUBJECTED TO MANY HOURS OF LOW LEVEL FLYING.SDR 96ZZZX4791Rib · crackedWHILE DOING THE CESSNA CONTINUAL AIRWORTHINESS PROGRAM, FOUND LEADING EDGE RIB BROKEN. THIS IS A PUBLIC AIRCRAFT AND IS SUBJECTED TO MANY HOURS OF LOW LEVEL FLYING.SDR 96ZZZX4790Rib · crackedWHILE DOING THE CESSNA CONTINUAL AIRWORTHINESS PROGRAM, FOUND LEADING EDGE RIB BROKEN. THIS AIRCRAFT IS SUBJECTED TO MANY HOURS OF LOW LEVEL FLYING.SDR 96ZZZX4789Rib · crackedWHILE DOING THE CESSNA CONTINUAL AIRWORTHINESS PROGRAM, FOUND LEADING EDGE RIB BROKEN. THIS IS A PUBLIC AIRCRAFT AND IS SUBJECTED TO MANY HOURS OF LOW LEVEL FLYING.SDR 96ZZZX4141Bracket · crackedFREE-PLAY WAS OBSERVED IN TAIL WHEEL STINGER DURING SERVICING OF TAIL WHEEL. TAIL CONE WAS REMOVED AND BRACKET FOUND CRACKED AROUND BOLT HOLE UNDER NUT. PART WAS REPLACED WITH NEW FROM FACTORY.SDR 98ZZZX3578Bolt · brokenWHEN ATEMPTING TO LOCATE AN OIL LEAK, NOTICED THE ENGINE MOVED FAIRLY EASY ON THE MOUNTS. FURTHER INSPECTION OF THE 'LOOSE ENGINE' PROBLEM REVEALED THE RIGHT REAR BOLT SECURING THE ENGINE TO THE AIRCRAFT MOTOR MOUNT HAD BROKEN AT THE BEGINNING OF THE THREADS.SDR 97ZZZX2592Crankshaft · failureIN-FLIGHT FAILURE OF CRANKSHAFT RESULTED IN FORCED LANDING. AIRCRAFT WAS DESTROYED. PILOT HAD REPORTED INCREASE IN OIL TEMPERATURE (NOT ABOVE RED LINE, BUT HIGHER THAN NORMAL). NO OTHER SYMPTOMS REPORTED, AND MAINTENANCE COULD NOT IDENTIFY A PROBLEM. ENGINSDR 96ZZZX3551Spark Plug · electrode looseNEW SPARK PLUG HAS DEFECT, SIDE ELECTRODE LOOSE.SDR 96ZZZX3220Fuel Cap · defectiveDESIGN OF THESE FUEL CAPS ALLOWS WATER TO COLLECT IN FILL AREA AFTER RAINS. NEXT REMOVAL OF CAP ALLOWS WATER TO ENTER FUEL TANK.SDR 96ZZZX3380Bolt · failedTHIS THROUGH-BOLT HOLDS CYLINDERS NR 3 AND NR 2 TOGETHER AT TOP OF CLYLINDER, ALSO, BOLT CLAMPS THE CASE TOGETHER. THE THREADS ON THE STUD AND NUT FAILED CAUSING OIL TO LEAK.SDR 96ZZZX3217Lever · worn'AN' BOLT/CASTLE NUT RETAINING HARDWARE FOR THROTTLE CABLE ROD END TO LEVER, LOOSENED AND WORE ITSELF THROUGH LEVER. FAILURE OCCURRED AT LIFT-OFF, SUCCESSFUL ON-FIELD LANDING WAS MADE. ASSY WAS 85 HOURS OUT OF 100 HOUR INSPECTION. SUBMITTER SUGGESTS IMPROVISDR AU960725Cylinder · cracked(AUS) ENGINE CYLINDER CRACKED FROM SPARK PLUG HOLESDR CA960529003Ico Valve · incorrect assy(CAN)MIXTURE CONTROL AND IDLE CUT-OFF INOPERATIVE. UNIT ASSEMBLED INCORRECTLY WITH MIXTURE CONTROL AND I C O VALVE OUT OF THE VALVE BORESDR 97ZZZX2657Rib · corrodedDURING ANNUAL INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIB AT BASE OF VERTICAL STABILIZER. FORWARD 6 INCHES OF RIB WAS COMPLETELY DELAMINATED. AIRCRAFT HAD BEEN ON FLOATS IN SALT WATER ENVIRONMENT. REST OF AIRCRAFT IN GOOD CONDITION.SDR 96ZZZX2512Lifter · galledWHILE DOING TOP OVERHAUL, FOUND 3 HYDRAULIC LIFTERS PITTED AND GALLED. SUBMITTER RECOMMENDS CLOSER INSPECTION OF LIFTERS AT OVERHAUL.SDR 96ZZZX2052Actuator · stuckTHE OWNER COMPLAINED HE COULD NOT TRIM PLANE FOR NOSE DOWN. UPON INSPECTION, TRIM SYSTEM WOULD BECOME STUCK REQUIRING EXTREME FORCE TO FREE SYSTEM. UPON STABILIZER REMOVAL, FOUND ACTUATOR WOULD BIND IN APPROXIMATELY NEUTRAL POSITION. AFTER SOAKING PARTS IN SDR 96ZZZX2051Actuator · stuckTHE OWNER COMPLAINED HE COULD NOT TRIM PLANE FOR NOSE DOWN. UPON INSPECTION, TRIM SYSTEM WOULD BECOME STUCK REQUIRING EXTREME FORCE TO FREE SYSTEM. UPON STABILIZER REMOVAL, FOUND ACTUATOR WOULD BIND IN APPROXIMATELY NEUTRAL POSITION. AFTER SOAKING PARTS IN SDR CA960507014Gear Leg · broke(CAN) ON SLOWING DOWN AFTER LANDING ON SKIS, LEFT GEAR BROKE AT THE UPPER AXLE ATTACHMENT BOLT HOLES. THIS AIRCRAFT HAS HAD PREVIOUS REPAIRS DUE TO A HARD LANDING ON SKIS.SDR 96ZZZX2396Shaft · wornSTABILIZER TRIM CONTROL WHEEL/SHAFT HAD EXCESSIVE PLAY. UPON INSPECTION, FOUND ROLL PINS, P/N NAS561-3-8, BOTH SHEARED AND ONLY RETAINED BY THE SAFETY WIRE PASSED THROUGH THE ROLL PIN PER CESSNA MM FOR ROLL PIN RETENTION. TRIM WHEEL SHAFT HAD THE HOLES OR THSDR 96ZZZX2395Roll Pin · shearedSTABILIZER TRIM CONTROL WHEEL/SHAFT HAD EXCESSIVE PLAY. UPON INSPECTION, FOUND ROLL PINS, P/N NAS561-3-8, BOTH SHEARED AND ONLY RETAINED BY THE SAFETY WIRE PASSED THROUGH THE ROLL PIN PER CESSNA MM FOR ROLL PIN RETENTION. TRIM WHEEL SHAFT HAD THE HOLES OR THSDR CA960423106Shaft Pivot · broken(CAN) WHILE TAXI TURNING, THE HYDRAULIC WHEEL SKI RIGHT HAND SHAFT PIVOT FRACTURED. THE FRACTURED OCCURRED AT THE STEP TRANSITION TO THE KEYWAYS. THIS ALLOWED THE SKI TO DEPART THE AIRCRAFT. THE SUBMITTER STATES THAT THE SHAFT DESIGN HAS LEFT SHARP EDGES AND SSDR CA960327012Bracket Stab · cracked(CAN)AT INSPECTION THE STABILIZER WAS REMOVED AND THE LEFT BRACKET STABILIZER HINGE WAS FOUND CRACKED FROM THE CENTRE DOWNWARDS. THE RIGHT STABILIZER HINGE WAS GROOVED TO THE POINT OF PART REJECTION AS WEL L AS THE RIGHT ANGLE REINFORCEMENT.SDR CA960327011Nose Ribs · cracked(CAN)DURING INSPECTION THE FIRST TWO RIBS ON THE STABILIZER WERE FOUND CRACKED AND PUSHED IN.SDR CA960327010Rear Spar · cracked(CAN)DURING AN INSPECTION THE RUDDER SPAR AND ONE DOUBLER WAS FOUND STARTING TO CRACK BETWEEN THE FIRST AND SECOND BOLTS LOCATED AT THE BOTTOM OF THE SPAR.SDR CA960327009Mount · cracked(CAN)CRACK FOUND ON THE ENGINE MOUNT BY THE GUSSET PLATE. THE MOUNT WAS REMOVED AND INSPECTED WITH LIQUID PENETRANT AND THE CRACK WAS CONFIRMED.SDR CA960327003Engine Mount · cracks(CAN)DURING INSPECTION TWO CRACKS WERE FOUND. ONE ON EACH SIDE UNDER THE LORD MOUNT. SUBMITTER SPECULATES THAT WINTER SKI OPERATION MAY HAVE SOMETHING TO DO WITH THE CRACKS.SDR 96ZZZX2563Control Cable · frayedELEVATOR CABLE WORN. SUBMITTER STATED PROBLEM IS TYPICAL OF ALL 185'S. CABLE CHAFES ON RIB AND IS JUST A MATTER OF TIME UNTIL STRANDS IN CABLE BREAK. SUBMITTER SUGGESTS INSTALLING PULLEY AT THIS LOCATION (FS 140.0).SDR AU960276Collar · wrong part(AUS) CRANKSHAFT FITTED WITH INORRECT OIL TRANSFER COLLAR - STANDARD COLLAR PNO 626739 FITTED TO M10 CRANKSHAFT RESULTING IN EXCESSIVECLEARANCE - LOG BOOK ENTRY ALSO DETAILED FITMENT OF STANDARD SIZEBEARINGS FITTED ALTHOUGH THE ACTUAL BEARINGS WERE M010 SIZE -SDR 96ZZZX857Bracket · brokenFLAP PULLEY BRACKET FOUND BROKEN ON RIGHT FORWARD SIDE OF FUSELAGE AT STATION 65.33. TANGS WERE BROKEN OFF OF BRACKET. AIRCRAFT HOURS, 7,000.SDR 96ZZZX1105Crnakshaft · failedCRANKSHAFT BROKE AFT OF NR 2 MAIN JOURNAL AT OIL TRANSFER TUBE. PARTS SET TO TCM FOR DETERMINATION OF FAILURE. CAUSE WAS DETERMINED TO BE LOW THROUGH-BOLT TORQUE WHICH, IN TURN, CAUSED BEARING TO SHIFT AND CRANKSHAFT TO VIBRATE. AIRCRAFT HAD DEPARTED NORMALSDR AU960073Trim Jack · worn(AUS) ELEVATOR TRIM JACK SCREWS LOOSE AND WORN - SPROCKET ROLL PIN LOOSE - SUSPECT LUBRICANT ON SCREW JACK DRIED OUT RESULTING IN PREMATURE WEAR OF SCREW AND NUT ASSEMBLIES - AIRCRAFT OPERATES INA DUSTY ENVIRONMENTSDR CA960515003Static Sensor · leaking(CAN) PIEZO STATIC SENSOR HOUSING ASSEMBLY LEAKING IN EXCESS OF LIMITSSDR 96ZZZX482Bracket · brokenCESSNA 185 WITH ROBERTSON STOL KIT INSTALLED WAS AIRBORNE WHEN PILOT APPLIED FLAPS AND THE AIRCRAFT STARTED TO ROLL TO THE RIGHT. A PASSENGER REPORTED HEARING A SOUND COMING FROM THE FLOOR OF THE AIRCRAFT. PILOT PUT FLAPS BACK UP AND LANDED AT NEAREST AIRPORSDR 96ZZZX1528Pin · missingDURING TAKEOFF, ENGINE STARTED TO RUN ROUGH AND SHAKE. THE TAKEOFF WAS ABORTED AND ACFT RETURNED TO RAMP. ENGINE AND PROP WERE THEN INSPECTED FOR ABNORMALTIES. WHILE INSPECTING THE PROP, A MECHANIC DISCOVERD THE NR 2 PROP BLADE COULD BE ROTATED INDEPENDENTLSDR 97ZZZX791Torque Plate · crackedINSP FOUND PLATE CRACKED AT TOP CALIPER BUSHING. THIS AREA IS THE WEAKEST OF THE ENTIRE PLATE, YET TAKES A HIGH PERCENTAGE OF THE TORQUE.SDR CA951215013Magneto · gear failure(CAN)THE MAGNETO INTERNAL DRIVE GEAR FAILED. THERE WAS NO APPARENT REASON.SDR 96ZZZX256Disc · brokenRIGHT BRAKE DISC SEPARATED FROM WHEEL AFTER LANDING, AND SUBSEQUENT BRAKE APPLICATION. SUBMITTER STATED IT APPEARS AS IF THE BRAKE DISC MATERIAL FAILED AND PULLED AWAY FROM WHEEL BOLTS. THICKER MATERIAL WOULD HELP SOLVE PROBLEM. ADDING ANOTHER BOLT TO THE WSDR 96ZZZX198Fuel Control · bushing wornSTEEL BUSHING HAS WORN AWAY ABOUT 90 PERCENT OF THE THROTTLE ARM. THE BOLT WAS CORRECTLY INSTALLED AND PROPERLY TORQUED. THIS AREA HAS BEEN SUBJECT TO CLOSE INSPECTION AT EACH 100-HOUR INSPECTION SINCE EARLIER REPORTS OF SIMILAR PROBLEMS (CESSNA SEB 95-15), SDR CA951122015Actuator Screw · worn(CAN)LEFT AND RIGHT HAND TRIM ACTUATOR SCEWS WORN WHERE THEY SIT IN THE BEARING. SUBMITTER SUGGESTS INSTALLING KIT P/N SK 185-27 WHICH INCLUDES AN INSPECITON PANEL AND LUBRICATION PROVISIONS.SDR CA951122014Horizontal Stab · cracked(CAN) LEFT HAND ATTACH POINT FOR HORIZONTAL STABILIZER FOUND CRACKED. REINFORCEMENT P/N 0712048-7 IS PART OF THE STABILIZER ATTACHMENT. SUBMITTER STATES THAT SUSPECT CAUSE IS USING THE HORIZONTAL STABILIZER TO PUSH THE AIRCRAFT.SDR CA951122013Fitting · cracked(CAN)MIDDLE FITTING FOR THE VERTICAL SABILIZER FOUND CRACKED ON REMOVAL.SDR CA951116008Tank · fod(CAN) WHILE INSTALLING A NEW FUEL FILLER CAP FILLER KIT THE PRO SEALED INSPECTION PLATES WERE REMOVED AND WHAT LOOKED LIKE A FACTORY PRC CLEANING TOOL WAS FOUND INSIDE THE FUEL TANK. TOOL REMOVED AND FOD CHECK COMPLETED.SDR 95ZZZX6387Crankshaft · failedIN-FLIGHT, CRUISE SETTING, ENGINE RPM DROPPED TO ZERO, PROPELLER ROTATED 2-3 TIMES AFTER RPM GAUGE READ ZERO. PILOT EXECUTED EMERGENCY LANDING. UPON ENGINE TEAR-DOWN, FOUND CRANKSHAFT BROKEN AT FORWARD CHEEK OF NR 2 MAIN BEARING JOURNAL. SUSPECT DEFECT (SCRSDR CA951018027Doubler · cracked(CAN)CRACK FOUND DURING INSPECTION ON THE LEFT HAND SIDE OF THE RECESS FOR THE TORQUE TUBE. REFERENCE SB 95-2.SDR CA951010024Stabilizer · cracked(CAN)THE RIGHT HAND REINFORCEMENT BRACKET WAS FOUND TO BE CRACKED. REPLACED.SDR CA951010023Spar · cracked(CAN)THE LEFT HAND STABILIZER REINFORCEMENT BRACKET P/N 6732101-4 WAS FOUND TO BE CRACKED. IT WAS REMOVED AND REPLACED. UPON REMOVAL THE AFT SPAR WAS ALSO FOUND TO BE CRACKED.SDR 95ZZZX4526Roto Coil · making metalWHEN REPLACING ROCKER COVER GASKETS BECAUSE OF OIL LEAKS, FOUND STEEL SLIVERS IN BOTTOM OF COVERS ON NR 3 AND NR 5 CYLINDERS. SENT SLIVERS TO CONTINENTAL TO BE ANALYZED. WAS INSTRUCTED BY CONTINENTAL TO REPLACE ALL ROTO COILS IN BOTH CYLINDERS. NO METAL FOU
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