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 = '182P' 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 = '182P' 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 2026FA0000813Arm · backed outNOTED UNUSUAL FEEL IN ELEVATOR CONTROL DURING INSP. PROBLEM DETERMINED TO BE A HEAVY RUB OF THE TORQUE TUBE USED BY THE PITCH SERVO AND THE LOWER ELEVATOR PRIMARY CONTROL CABLE. THE PITCH SERVO CONTROL ARM WAS FOUND TO HAVE ALL FOUR SCREWS THAT SECURE IT TO THSDR 9WQR202609170736Bolt · unsecureDURING AN ANNUAL INSPECTION THE ALTERNATOR WAS FOUND TO BE LOOSE BUT STILL WEDGED IN THE MOUNT, AND THE FAN BLADES RUBBING ON THE ENGINE/ALTERNATOR MOUNT. THE ALTERNATOR MOUNTING BOLT WAS FOUND IN THE LOWER COWLING, THE NUT AND WASHER WERE NOT FOUND. IT IS BSDR 2025FA0000360Rivet · failedCARB AIRBOX BUTTERFLY VALVE ATTACHMENT TO ACTUATING SHAFT FAILED BY POORLY SHOT RIVET PULLING THROUGH THE BRACKET HOLE ON RIGHT SIDE. LEFT SIDE RIVET IS LOOSE AS WELL BUT HAD NOT FAILED AT THE TIME OF DISCOVERY. VALVE WAS HANGING DOWN AWAY FROM THE SHAFT. OWNESDR 2023FA0000673Rocker Boss · brokenPILOT REPORTED THAT APPROX. AN HOUR INTO FLIGHT AT 3500 FEET AND 30 DEGREES AND ON AUTOPILOT, EXPERIENCED SEVERE ENGINE VIBRATION AND REDUCED POWER. PILOT REDUCED POWER TO AROUND 1700-1800 RPM IN EFFORT TO DECREASE VIBRATION. ULTIMATELY MADE EMERGENCY LANDINSDR 2026FA0000428Fuel Cell · leakingNEW FFC BLADDER INSTALLED SEPT 2023 .. LEAKED .. UNABLE TO RESOLVE LEAKING, BLADDER RETURNED TO FFC FOR INSPECTION AND REPAIR FEB 2024 .. REPAIRED BLADDER INSTALLED MAR 2024 .. LEAKING CONTINUED .. AGAIN RETURNED TO FFC .. BLADDER REPLACED WITH ANOTHER NEW BLASDR 2022FA0000518Seat Track · deformedCONDUCT OF AD 2011-10-9, THE AD STATES:"INSPECT THE DIAMETER OF EACH SEAT LOCKING PIN ENGAGEMENT HOLE.. .THE MOST USED HOLES DO NOT HAVE A "DIAMETER", BUT INSTEAD HAVE A HOLE THAT IS ELLIPTICAL IN SHAPE. THUS, MEASUREMENTS FORE AND AFT AND PORT TO STARBOARD MUSDR 2023FA0000233Flap · unknownSMALL CRACK ON EXTERNAL TOP OF THE RH FLAP, THE CRACK IS NOT LONGER THAN 2 INCHES AND THE INTERNAL RIBS AND AC STRUCTURE WERE UNDAMMAHED. THE CRACK DID NOT PROTRUDE TO ANY FASTENERS AND WAS RELATED TO PREVIOUS FLAP DAMAGE. CESSNA WAS CONTACTED AND VIA PHONE SDR 2021FA0000153Seal · unsecureAIRCRAFT WAS IN CRUISE FLIGHT AND SUDDENLY LOST ENGINE POWER WITH NO PRIOR WARNING. AIRCRAFT PERFORMED EMERGENCY LANDING TO AIRSTRIP WITH NO DAMAGE. UPON INSPECTION IT WAS DETERMINED THAT THE SEAL THAT SURROUNDS THE CONNECTION BETWEEN THE AIR INTAKE AND THE CASDR 2020FA0000415Fitting · fracturedDURING INSPECTION FOUND FITTING SEPARATED ON RIGHT SIDE AND SEPARATION GAP OPEN APPROXIMATELY .75". NO DAMAGE TO FIREWALL FOUND. NO DAMAGE TO CENTER TUNNEL FOUND. NO LOOSE HARDWARE WAS FOUND. METAL IN SEPARATION SHOWS CRACK WAS APPROXIMATELY 1/2 THROUGH MESDR 2017FA0000081Capacitor · looseDURING RUN UP, MAGETO FAILED TEST. LESS THAN 1 HR OPERATION AFTER OVERHAULED MAGETOS INSTALLED. DURING INSPECTION FOUND THE CAPACITOR LOOSE IN HOUSING AND COIL WIRE LOOSE AND MAGETO SET IN E GAP. REMOVED OTHER MAG AS A PRECAUTION AND FOUND ITS COIL WIRE LSDR 2016FA0000039Elt · false activationOCCURED WHILE ACFT WAS IN HANGER. EMERGENCY LOCATION TRANSMITTER: AK451, 121.5/406 HZ ACTIVATED GIVING FALSE ACCIDENT SIGNAL. COAST GUARD CALLED REGISTERED OWNER AND UNIT WAS TURNED OFF. 70 PERCENT OF THESE UNITS HAVE FAILED IN THIS WAY. CONTACTED FSDO SW SDR LC1R201512225723Vent Line · out of positionREPORTED FUEL WOULD DRAW FROM LT FUEL TANK EVEN WITH THE SELECTOR VALVE POSITIONED IN THE RT TANK POSITION. DISCOVERED THAT SATISFACTORY RESULTS COULD NOT BE OBTAINED FROM THE VENT SYSTEM CHECKS DESCRIBED IN MM SECTION 12-22. FOUND THE LONG RANGE TANK INTERNSDR CA150617019Support · damaged(CAN) DURING ELEVATOR CONTROL MOVEMENT, THE CLEVIS PIN AN21-10, ATTACHED TO THE ARM ASSEMBLY, IS CONTACTING THE SUPPORT ASSEMBLY WEARING A .025 DEEP GROOVE IN THE SUPPORT ASSEMBLY. THIS IS APPROX 50% OF THE MATERIAL THICKNESS. THIS GROOVE EXTENDS DIRECTLY TSDR CA150617013Support · damaged(CAN) AT FULL UP ELEVATOR, WITH THE ELEVATOR RIGGED WITHIN LIMITS, THE ARM ASSEMBLY IS CONTACTING THE SUPPORT ASSEMBLY CAUSING DAMAGE TO THE SUPPORT ASSEMBLY.SDR CA150617014Support · damaged(CAN) DURING ELEVATOR CONTROL MOVEMENT, THE CLEVIS PIN AN21-10, ATTACHED TO THE ARM ASSEMBLY, IS CONTACTING THE SUPPORT ASSEMBLY WEARING A GROOVE IN THE SUPPORT ASSEMBLY. THIS GROOVE EXTENDS DIRECTLY THROUGH A HOLE IN THE SUPPORT ASSEMBLY CREATING THE POTENTISDR CA150616026Support · damaged(CAN) AT FULL UP ELEVATOR, WITH THE ELEVATOR RIGGED WITHIN LIMITS, THE ARM ASSEMBLY IS CONTACTING THE SUPPORT ASSEMBLY CAUSING DAMAGE TO THE SUPPORT ASSEMBLY.SDR CA150616024Support · damaged(CAN) AT FULL UP ELEVATOR, WITH THE ELEVATOR RIGGED WITHIN LIMITS, THE ARM ASSEMBLY IS CONTACTING THE SUPPORT ASSEMBLY CAUSING DAMAGE TO THE SUPPORT ASSEMBLY.SDR CA150616023Support · damaged(CAN) AT FULL UP ELEVATOR, WITH THE ELEVATOR RIGGED WITHIN LIMITS, THE ARM ASSEMBLY IS CONTACTING THE SUPPORT ASSEMBLY CAUSING DAMAGE TO THE SUPPORT ASSEMBLY.SDR CA150616009Support · damaged(CAN) AT FULL UP ELEVATOR, WITH THE ELEVATOR RIGGED WITHIN LIMITS, THE ARM ASSEMBLY IS CONTACTING THE SUPPORT ASSEMBLY CAUSING DAMAGE TO THE SUPPORT ASSEMBLY.SDR 2013FA0000444Gasket · deformedENGINE WAS RUNNING ROUGH AND SHOWING SIGNS OF RUNNING LEAN. FOUND ALL INTAKE GASKETS SHRUNK AND DEFORMED CAUSING INTAKE LEAKS AT ALL CYLINDERS.SDR 2013FA0000224Spark Plug · brokenWHILE COMPLETING A 1000 HOUR INSPECTION AND CLEANING THE SPARK PLUGS (XL URHB32S LOT 1269) 1 OF THE PLUGS WAS FOUND TO HAVE THE WIRE ELECTRODE LOOSE AT ITS ATTACHMENT TO THE END OF THE SPARK PLUG. THE WIRE COULD BE ROTATED UP OUT OF ALIGNAMENT WITH THE CENTER SDR 2013FA0000085Switch · failedMFG SWITCHES S-1579-2 COMMONLY USED FOR AUX LIGHTING AND MISC ACCESSORIES COMMONLY FAIL TO OPERATE. FOUND TWO ON SAME AIRCRAFT FOR PITO HEATER AND NAV LIGHTS.SDR CA120827011Gear · failed(CAN) WHILE TURNING THE PROPELLER BY HAND, THE OWNER/PILOT FOUND THAT THE ENGINE LOCKED UP. THE AME WORKING ON THE ACFT REMOVED AN ENGINE ACCY TO GAIN ACCESS TO THE INTERNAL GEARS AND FOUND THAT THERE WERE 2 TEETH MISSING FROM THE CRANKSHAFT GEAR. THE ENGINESDR CA120507021Bellcrank · cracked(CAN) BELLCRANKS FOUND CRACKED. PINS THAT SECURED THE BELLCRANK ON THE LT SIDE HAD PARTIALLY SHEARED PLACING THE LOAD ON 2 OF THE 4 HOLES AND APPEARED TO CAUSE CRACKS TO SPREAD OPEN. DAMAGE TO THE RT BELLCRANK WAS LESS SEVERE AND PINS WERE INTACT. COMPLETE SDR EVGR20120326001Skin · corrodedCORROSION WAS FOUND UNDER THE BLACK SOUND DEADENING PATCHES ON THE INSIDE OF THE ACFT SKIN, AND WAS NOT DETECTED UNTIL THE PATCHES WERE REMOVED.SDR CA120103015Nut · failed(CAN) UPON INSPECTION IT WAS NOTED THAT THE NUT LOCATED ON THE NR 6 CYLINDER TOP FWD THRU STUD WAS CRACKED. REQUIRED INSPECTION WERE CARRIED OUT WITH NO DEFECT FOUND, NUT WAS REPLACED & A COMPLETE ENGINE TORQUE SEQUENCE WAS CARRIED OUT. NO OTHER NUTS WERE FOSDR HYIA20110607001Strap · corrodedDURING HEAVY CHECK INSPECTION, CORROSION WAS FOUND ON THE UPPER SURFACE OF THE RT WING STRIP STRAP OF RIB 20 AT WS 7900. THE CORROSION WAS REMOVED IAW SRM 51-21-58 AND EXCEEDED THE LIMITS OF THE SRM. REPAIRED IAW WITH EA 12-2011-014.SDR 2010FA0001255Cylinder Head · brokenIN CRUISE FLIGHT, ENGINE STARTED TO LOSE POWER AND BACKFIRE. PILOT MADE AN EMERGENCY LANDING IN FIELD WITH NO DAMAGE TO ACFT. VISUAL INSP OF THE ENGINE WAS ACCOMPLISHED. THE NR 6 CYLINDER WAS FOUND TO HAVE FAILURE OF EXHAUST ROCKER ARM BOSS RESULTING IN THE SDR 2010FA0001216Bulkhead · crackedDURING ANNUAL INSPECTION AD 72-07-09 WAS DUE FOR RE-INSPECTION, DURING INSPECTION FOUND THAT THE AFT BULKHEAD WAS CRACKED ON THE LEFT AND RIGHT SIDE FROM THE RUDDER CUT OUT TO THE BULKHEAD FLANGE.AS SHOWN IN CESSNA SERVICE LETTER SE72-3 FIG 1. THE CRACKS WERE SDR CA111117003Strut · damaged(CAN) FLOAT STRUT LOWER BOLT HOLE ELONGATED UPON VISUAL INSPECTION.SDR CA100218008Cylinder · damaged(CAN) DURING A 100 HOUR INSP, A ROUTINE COMPRESSION TEST WAS CARRIED OUT AS PART OF ENGINE ON CONDITION PROGRAM IAW AN B041. A LEAK WAS NOTED ASSOCIATED WITH LOW COMPRESSION ON THE NR 5 CYL ASSY AT TOP DEAD CTR. THE PISTON WAS THEN PLACED AT BOTTOM DEAD CTR ANSDR 2010FA0000098Nut · brokenONE OF THE 4 BOLTS HOLDING THE REAR ATTACHMENT BRACKET ON VERTICAL STABILIZER, HAD A BROKEN/ SPLIT NUT. PROBABLE CAUSE COULD HAVE BEEN FROM CORROSION FOUND BETWEEN THE NUT AND WASHER CAUSING STRUCTURAL LOSS OF THE NUT. INSPECTED NUTS FOR CORROSION AND REPALCSDR 2010FA0000188Impulse Coupling · looseDISCOVERED DURING FINAL TORQUING OF THE MAGNETO HOLD DOWN NUTS, THE IMPULSE COUPLING WOULD BOTTOM OUT IN THE ENGINE GEAR HSG. THIS WOULD LOCK THE COUPLING, CAUSING IT TO NOT WORK. IF THE COUPLING WAS PARTIALLY ENGAGED, IT WOULD HOLD THE DISPLACED TIMING BETWSDR CA090915006Cylinder · wrong part(CAN) DURING ROUTINE MAINTENANCE THE NR 1 AND 3 CYLINDERS WERE FOUND TO HAVE LOW COMPRESSION. THE CYLINDERS AND PISTONS WERE REMOVED AND SENT IN FOR REPAIR. AFTER RECEIVING THE CYLINDERS AND PISTONS, DISCOVERED THAT THE PISTONS PART NUMBERS WERE THAT OF A "U"SDR 2009FA0000452Tube · splitSPLIT IN SIDE OF NOSE WHEEL TUBE CAUSING FLAT TIRE. THIS SEEMS TO BE A PROBLEM WITH SYNTHETIC TUBES. (K)SDR 2009FA0000073Connector · burnedPILOT REPORTED SMOKE IN COCKPIT AFTER TAKEOFF AND RETURNED TO THE AIRPORT MAKING AN UNEVENTFUL LANDING. MX INSPECTED THE ACFT AND FOUND A LOOSE CONNECTION AT THE LANDING LIGHT SWITCH WITH BURNED WIRING INSULATION. INSTALLED NEW WIRING AND CONNECTOR AS NEEDEDSDR C2X2008F00049Rotor · erodedTHE CREW REPORTED ENGINE NR 1 HP INDICATION IN YELLOW RANGE AFTER TAKEOFF, THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD. SUPPLEMENT TO FOLLOW: CONDITION REPORT FROMSDR 2008FA0000231Line · leakingFUEL LEAKING FROM GAS COLATOR BOWL, TIGHTENED AT FACTORY DURING ACCEPTANCE FLIGHT (5.0 HOURS). FUEL LEAKING FROM GAS COLATOR INLET LINE (10 HOURS SINCE NEW) RESULTED IN OFF-AIRPORT LANDING DUE TO FUEL QUANTITY. (K)SDR EA25070193Landing Gear · departedAIRCRAFT ALTERED IAW STC SA02031NY INSTALLATION OF 3400 AMPHIBIOUS FLOATS APPROXIMATELY 36 HOURS PRIOR TO OCCURRENCE. ON TAKEOFF FROM HARD SURFACE RUNWAY, RT FORWARD WHEEL AND SUPPORT ASSY DEPARTED LANDING GEAR STRUT. WHEEL AND SUPPORT ASSY LT GEAR STRUT CLEANSDR 2007FA0000797Fuel Cap · ventingFUEL CAPS WERE INSTALLED ON AIRCRAFT IAW STC SA2376CE AND HAD BEEN IN SERVICE FOR ABOUT 40 HOURS IN A 4 MONTH PERIOD. THEY BEGAN VENTING FUEL FROM BOTH TANKS RESULTING IN A FORCED EMERGENCY LANDING DUE TO FUEL STARVATION.SDR 2006FA0000441Oil Filter · mismanufacturedMOUNTING STUD TOO LONG, APPROX .200 LONGER. INSTALLED OIL FILTER AFTER OIL CHANGE, RAN ENGINE TO LEAK CHECK AND LOST ALMOST 2 QTS OF OIL. INVESTIGATION FOUND THAT THE OIL FILTER STUD WAS TOO LONG CAUSING THE FILTER TO TORQUE BEFORE SEAL TOUCHED FLANGE, LEAVISDR AU510001572Exhaust Valve · wornNR 3 CYLINDER EXHAUST VALVE STEM WORN EXCESSIVELY. WEAR WAS APPROXIMATELY 3.175MM (0.125IN). SUSPECT INCORRECT VALVE GUIDE/VALVE COMBINATION.SDR CA051220005Rod · brokenDURING TAXI (AFTER HARDWIND DURING THE DAY WITH THE AIRCRAFT PARKED WITH TAIL TO THE WIND), AT THE END OF THE DAY THE PILOT HAD NO CONTROL ON PEDALS FOR TAXIING. THE PILOT SIDE RT PEDAL WAS JAMMED IN PLACE. AFTER EVALUATION OF PROBLEM, FOUND A BROKEN ROD ENDSDR 2005FA0001477Support Bracket · crackedWING T/E SKIN SUPPT BRKT CRACKED CAUSED FLAP INTERFERENCE AND FAILURE. BRKT IS ATTACHED TO EACH FLAP TRACK RIB INSIDE T/E OF WING, SUPPT T/E WING SKIN IN FLAP BAY. PART CRACKED, ALLOWED FLAP SUPPT TO GET CAUGHT DURING FLAP RETRACTION, BINDING FLAP. FLAP STRSDR 2005FA0000976Magneto · crackedFOUND AN OIL LEAK COMING FROM THE BASE OF THE LEFT MAGNETO. REMOVED MAG TO REPLACE GASKET. FELT SOMETHING ON THE MOUNTING FLANGE OF THE MAG. FOUND A SECTION OF THE FLANGE ABOUT 1 1/4 INCH CRACKED WHERE THE HOLD DOWN CLIP CLAMPS THE MAG TO THE ENGINE CASE. A LISDR 2005FA0000975Magneto · crackedFOUND AN OIL LEAK COMING FROM THE BASE OF THE LEFT MAGNETO. REMOVED MAG TO REPLACE GASKET. FELT SOMETHING ON THE MOUNTING FLANGE OF THE MAG. FOUND A SECTION OF THE FLANGE ABOUT 1 1/4 INCH CRACKED WHERE THE HOLD DOWN CLIP CLAMPS THE MAG TO THE ENGINE CASE. A LISDR 2005FA0000974Magneto · crackedFOUND AN OIL LEAK COMING FROM THE BASE OF THE LEFT MAGNETO. REMOVED MAG TO REPLACE GASKET. FELT SOMETHING ON THE MOUNTING FLANGE OF THE MAG. FOUND A SECTION OF THE FLANGE ABOUT 1 1/4 INCH CRACKED WHERE THE HOLD DOWN CLIP CLAMPS THE MAG TO THE ENGINE CASE. A LISDR 2005FA0001109Control Cable · wornCABLES WORN BEYOND LIMITS AT A CABLE RUB STRIP IN RT WING BY AUTOPILOT SERVO AT STA RBL 102. (K)SDR CA041019005Hub · corroded(CAN) PROP RECEIVED FOR 10 YR. CALENDAR O/H. AFTER PAINT REMOVAL FROM HUB CORROSION WAS FOUND ON THE EXTERNAL SURFACES. THIS CORROSION CANNOT BE REMOVED WITHIN THE MANF.'S MINIMUM SPEC'S. THIS PROPELLERHAS EXCEDED THE MANF'S RECOMMENDED CALENDAR TBO BY 60 MONTSDR 2004FA0000787Valve Guide · wornON DOING A COMPRESSION CHECK, 3 OUT OF 6 CYLINDERS HAD VALVES LEAKING. WHEN REMOVED FOR REPAIR, DISCOVERED GUIDES WORN BEYOND MAX SERVICE LIMIT. (NM09200412745)
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