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 = '182R' 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 = '182R' 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 2026FA0000672Cylinder · separatedCYLINDER NR 3 HEAD SEPARATED FROM BARREL. THE OPERATOR HAD PREVIOUSLY INSPECTED AN OIL LEAK ON OR AROUND CYLINDER NR 3. PRESENTATION OF OIL LEAK AND SEPARATION OF HEAD FROM BARREL IS THE SAME AS DESCRIBED IN AD 86-13-04 R3. THIS CYLINDER PN STAMPED ON THE FLANSDR 2023FA0000376Camshaft · distressedDURING ROUTINE MAINTENANCE SEVERE DISTRESS OF CAMSHAFT LOBE AND LIFTERS WAS IDENTIFIED. THE MAINTENANCE WAS CARRIED OUT DURING INTERNATIONAL TRAVEL, IN AUSTRALIA. PLEASE CONTACT ME FOR PHOTOGRAPHS/ENGINE INSPECTION REPORT.SDR 2021FA0000365None · noneELECTRIC TRIM ACTIVATION WAS KEYING RADIO AND PRESSING PTT SWITCH WAS DISCONNECTING AUTOPILOT. THE YOKE COIL CORD INSULATION WAS FALLING OFF OF 2 ADJACENT WIRES ALLOWING THE 2 CONDUCTORS TO TOUCH AND SHORT CIRCUIT. THE COIL CORD IS A CYGNET CA3934-24 INSTALLEDSDR 2021FA0000256Wire · arcedDURING INITIAL TAKEOFF ROLL AFTER APPLICATION OF FULL POWER. PILOT NOTICED SPARKS COMING FROM BELOW PILOT'S INSTRUMENT PANEL. POWER WAS REDUCED TO IDLE AND TAKEOFF ROLL WAS ABORTED. SPARKS STOPPED ONCE POWER WAS PULLED TO IDLE. AFTER TAXI TO RAMP AND ENGINE SHSDR Q532018F00001Gear · chippedCRANKSHAFT GEAR CHIPPED ONE TOOTH OFF. PROB DUE TO STARTER KICKBACK (ENERGIZER STARTER). AROUND 05/20/2018 AT TACK 3175 OWNER REPORTED TICKING NOSE ON GROUND. SOUND WENT AWAY WITH INCREASE RPM. ABOUT 1500. EVENTUALLY FOUND ONE TOOTH MISSING FROM CRANKSHAFSDR 2018FA0000015Cylinder Head · separatedENGINE VIBRATION. DISCOVERED NR 3 CYLINDER LOW PRESSURE, AT 20 PSI DURING TEST. FOUND THE CYLINDER HEAD AND BARREL SEPARATING AFTER REMOVAL.SDR 2017FA0000549Cylinder · crackedCRACKED CYLINDER INSTALLED. THE ENGINE HAS APPROXIMATELY 850 HOURS ON IT SINCE OVERHAUL. DURING OVERHAUL, SIX NEW CYLINDERS WERE INSTALLED. THE ACFT RECENTLY CAME IN FOR A 50 HOUR INSPECTION AT WHICH TIME A COMPRESSION TEST WAS CONDUCTED. DURING THE COMPRESDR 2016FA0000231Heat Exchanger · failedHEAT EXCHANGER FAILED IN FLIGHT, CAUSED MELTING OF PLASTIC, RUBBER COMPONENTS IN ENGINE COMPARTMENT. RESULTING IN SMOKE IN THE COCKPIT AND A INFLIGHT EMERGENCY DECLARED. LANDED WITHOUT INCIDENT.SDR 6NAR2015FA0000566Gasket · leakingALL VALVE COVERS FOUND LEAKING. REMOVED ALL VALVE COVERS AND FOUND THE UPPER SECTION OF THE VALVE COVER GASKET NEAR THE EXHAUST VALVE HAD SHRUNK, PULLING IN TOWARD EXHAUST VALVE SPRING. WE HAVE FOUND THIS ISSUE ON NUMEROUS ENGINES WITH THE SUPERIOR VALVE COVSDR 2011FA0000591Cylinder Head · separatedCYLINDER HEAD SEPARATION.SDR 2009FA0000367Cable · frayedUPON APPLYING FULL THROTTLE FOR TAKEOFF, THE PILOT NOTED THAT THE ENGINE ONLY REACHED 2000 RPM. TAKEOFF WAS ABORTED AND A VISUAL CHECK OF THE PROPELLER GOVERNOR WAS MADE. THE MX RATED PILOT DETERMINED THAT THE CONTROL WAS STICKING BEFORE REACHING THE HIGH RPM SDR 2009FA0000467Tube · separatedA SIGNIFICANT PROBLEM OCCURRED IN THE FUEL INDUCTION SYSTEM, WHERE A RUBBER INTAKE TUBE CONNECTS THE INTAKE MANIFOLD TO THE FUEL INDUCTION RAIL. SHORTLY AFTER A FLIGHT WHERE ENTIRELY NORMAL OPERATION WAS EXPERIENCED, ENGINE RESTART COULD NOT BE ACCOMPLISHED. SDR 2009FA0000480Piston · failedCYLINDER NR 2 PISTON SKIRT BROKE FROM THE PISTON AND CREATED A METAL CONTAMINATION IN THE ENGINE. (K)SDR 2007FA0000728Alternator · shortedALTERNATOR SHORTED, THIS UNIT IS (1) OF (3) REPLACED IN THE LAST MONTHS. (K)SDR 2007FA0000664Spring Assy · crackedDURING NDI OF MAIN LANDING GEAR SPRING ASSY, THE RT FITTING WAS FOUND CRACKED. DURING WFPT FOR ASTM E1417. PART WAS REPLACED WITH A SERVICEABLE UNIT. SUSPECT CRACK WAS DUE TO CORROSION BETWEEN THE SPRING AND ALUMINUM FITTING. (K)SDR 2006FA0000783Seat · brokenINSPECTED SEATS IAW AD. FOUND PILOTS SEAT BOTTOM ASSY BROKEN AT LT FWD ATTACH POINT AND RT FWD CRACKED. (K)SDR LAT2006F00000Elt · inoperativeG-SWITCH INOPERATIVE, TOGGLE SWITCH BENT, PART NO LONGER AVAILABLE. INSTALL NEW UNIT. (K)SDR 2004FA0000379Control Cable · frayedWHILE INSTALLING THE BATTERY AFTER SERVING, IT WAS NOTICED THAT THE FORWARD RT RUDDER CABLE WAS FRAYED IN TWO SPOTS. IT WAS DETERMINED THAT, AT SOMETIME, DURING BATTERY REMOVAL OR REINSTALLATION THE RUDDER CABLE ARCED ON BOTH POSITIVE AND NEGATIVE POSTS. THESDR N736ZXTorque Tube · detachedLT RUDDER BAR TORQUE TUBE ASSEMBLY, PN 2260114-5 FAILURE. FAILURE OCCURRED IN FLIGHT RESULTING IN LT SIDE PILOT'S TOTAL LOSS OF LT RUDDER AND STEERING CONTROL. NATURE OF FAILURE; LT OB RUDDER PEDAL SOCKET ON TORQUE TUBE BROKE AWAY FROM THE TORQUE TUBE. THERE ISDR 2004FA0000002Pushrod · wornON ROUTINE FLIGHT PILOT HEARD A BANG AND ENGINE LOST POWER BUT CONTINUED TO RUN. UNABLE TO MAINTAIN ALTITUDE, PILOT MADE AN OFF AIRPORT LANDING. FOUND NR 1 EXHAUST PUSHROD BENT, WORN AND BROKEN. REMOVED ALL CYLINDERS AND FOUND NR 1 CYLINDER INTAKE PUSHROD BSDR 2003FA0001267Pushrod · failedON ROUTINE FLT PILOT HEARD A BANG AND ENGINE LOST POWER BUT CONTINUED TO RUN. UNABLE TO MAINTAIN ALTITUDE PILOT MADE AN OFF AIRPORT LANDING. FOUND EXHAUST PUSHROD BENT, WORN AND BROKEN. REMOVED ALL CYLINDERS AND FOUND NR 1 CYLINDER INTAKE PUSHROD BENT SLIGHSDR 2004FA0000091Piston · failedTHE PISTON WAS INSTALLED NEW AT TIME OF MAJOR OVERHAUL. ONE SIDE OF PISTON SKIRT, AT LOWER SCRAPER RING BROKE AWAY AND BECAME SMALL CHUNKS OF ALUMINUM, AND RING PIECES IN THE OIL PAN. THE PROBLEM WAS DETECTED BY APPROX 5 EACH. .020 X .040 PIECES OF CAST ALUSDR 2002FA0001363Skin · crackedDURING A 100 HOUR INSPECTION, A CRACK WAS FOUND IN THE FUSELAGE SKIN JUST BEHIND THE STEP THAT IS ATTACHED TO THE FUSELAGE TO AID THE PILOT FOR FUEL CAP INSPECTION OR REFUELING. THIS STEP IS LOCATED ON BOTH SIDES OF THE AIRCRAFT AT STATION 17.0 AND IS ATTACHESDR 2001FA0000229Detector · inoperativeUPON INSTALLING NEW LIFT DETECTION, NOTED THAT WHEN WIRED AS ORIGINALLY REMOVED FROM AIRCRAFT, WITH HEAT TURNED ON, DETECTION WAS INOPERATIVE. GROUND FOR HEATER WAS INSTALLED ON COMMON FOR DETECTION; CAUSING A NO POTENTIAL WHEN HEATER TURNED ON.SDR 2001F00248Detector · inoperativeUPON INSTALLING NEW LIFT DETECTION NOTED THAT WHEN WIRED AS ORIGINALLY REMOVED FROM AIRCRAFT, WITH HEAT TURNED ON, DETECTION WAS INOPERATIVE. GROUND FOR HEATER WAS INSTALLED ON COMMON FOR DETECTION; CAUSING A NO POTENTIAL WHEN HEATER TURNED ON.SDR 2001FA0000108Hose · disintegratedCUSTOMER REPORTED LOW VACUUM INDICATION BUT GYROS RUNNING OK. INITIAL INVESTIGATION ALL HOSES LOOKED OK, HOWEVER WHEN HOSES WERE TOUCHED, FELL APART. THE ABOVE REFERENCED PN IS FOR ONE OF THE VACUUM GAUGE HOSES, HOWEVER ALL INSTRUMENT HOSE WERE OF THE SAME TSDR 20010206CW003Indicator · reads lowWHILE COMPLYING WITH AD, 3.5 MINIMUM VACUUM COULD NOT BE OBTAINED, EVEN AT SEA LEVEL. TROUBLESHOOTING REVEALED VACUUM INDICATOR WAS 2-2 1/2 IN HG LOW AND REGULATOR HAD BEEN MIS-ADJUSTED. INSTALLED NEW GAGE, WHICH WAS CALIBRATED, AND RESET REGULATOR DOWN. STSDR 20000925SH008Line · deterioratedWHILE CERTIFYING THE STATIC SYSTEM, DISCOVERED THE VACUUM LINES WERE DETERIORATING. AFTER FURTHER INVESTIGATION, FOUND THE VACUUM LINES WERE THE LINES THAT HAD AD ISSUED AGAINST THEM. REMOVED ALL VACUUM LINES AND REPLACED WITH NEW HOSES. POSSIBLE CAUSE FOR SDR 20000925SH012Transponder · inoperativeTRANSPONDER REPORTED INOPERATIVE. BENCH TEST REVEALED CAVITY TRANSMITTING AT 2,012 MEGAHERTZ AND IT COULD NOT BE ADJUSTED INTO TOLERANCE. FOUND TUBE INSTALLED WAS PC2080A, DATE CODE 99-13. INSTALLED BY FAA CRS AJVR135C, PRESENT MANUFACTURER (SIGMA-TEK) DOESSDR 20000920SH016Support Bracket · crackedON INSPECTION OF AIRCRAFT, FOUND LEFT AND RIGHT BATTERY BOX SUPPORTS CRACKED IN BEND RADIUS, P/N 0712059-1. 24V BATTERY LOCATED IN TAIL SECTION OF AIRCRAFT. NOTE: THIS PROBLEM HAS BEEN FOUND IN OTHER 182R''S. (X)SDR 20000920SH015Hose · deterioratedFOUND HOSE MADE BY IMPERIAL EASTMAN HYTYON YP006 250 PSI W.P. FOUND OUTSIDE OF HOSE CRACKED AND COMING APART. FOUND INSIDE OF HOSE RED IN COLOR VERY BRITTLE, CRACKING. HOSE USED FOR INSTRUMENT VACUUM SERVICE. HOSE ROUTED FROM INSTRUMENT AIR FILTER TO ARTIFSDR CA000606033Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. BLADES TRIMMED, ALODINED, PAINTED.SDR AU991070Exhaust Valve · worn(AUS) NR 1 CYLINDER EXHAUST VALVE P/N 652956 AND EXHAUST VALVE GUIDE P/N 643767 WORN BEYOND LIMITS.SDR 99ZZZX3655Hose · crackingAIRCRAFT BEGAN TO LOSE VACUUM ON INSTRUMENT AIR SYSTEM. FOUND A POSSIBLE LINE CRACK ON THE OUTSIDE FROM AGE. AFTER REMOVING THAT LINE AND OTHER LINES ALSO CONNECTED TO THE INSTRUMENTS, FOUND THAT NOT ONLY THE OUTSIDE OF THE LINE WAS CRACKED, BUT THE INSIDE LSDR 99ZZZX3593Support · crackedBATTERY BOX SUPPORT ANGLES WERE FOUND CRACKED DURING ANNUAL INSPECTION. IF UNDETECTED, BATTERY CAN BECOME LOOSE IN TAIL. IT IS VERY COMMON IN THIS TYPE OF DESIGN, USING THESE ANGLES. SUBMITTER STATED SHOULD HAVE A STRONGER RE-DESIGN FOX.SDR 99ZZZX2594Hose · deterioratedALL VACUUM HOSES INSTALLED IN THIS AIRCRAFT HAVE HEAVY DETERIORATION BOTH INSIDE AND OUTSIDE OF THE HOSE. THE ONLY INDICATION OF A PROBLEM WAS A DROP IN THE VACUUM GAUGE PRESSURE WITH THE AIRCRAFT IN-FLIGHT. THIS AIRCRAFT HAS HAD TWO PREVIOUS VACUUM PUMPS INSSDR 99ZZZX2037Impulse Coupling · corrodedIMPULSE COUPLING CORRODED ON MAGNETO.SDR 99ZZZX1080Prop Governor · failedGOVERNOR WAS REMOVED DUE TO FAILURE TO CONTROL THE PROPELLER. WHEN IT WAS RECEIVED FOR OVERHAUL, DISASSEMBLED FOR INSPECTION, AND FOUND THE FLYWEIGHT ASSY COMPLETELY DESTROYED DUE TO CATASTROPHIC FAILURE. THERE WERE SHAVINGS OF METAL IN THE PUMP BODY. OWNERSDR 99ZZZX651Bolt · failedNR 2 MAIN JOURNAL THROUGH-BOLT WAS BROKEN AT TOP OF NR 2 CYLINDER. NO OTHER DEFECT NOTED. PILOT DID NOT STATE ABOUT ANYTHING TO CAUSE THIS, ALL OTHER ASSOCIATED ATTACH POINTS INSPECTED OK. ENGINE ONLY HAS 146.6 TSMOH AT FACTORY. PER SB 97-6, THROUGH-BOLTS SDR 98ZZZX2180Support · failedBOTH BATTERY SUPPORT BRACKETS WERE FOUND BROKEN DURING AN ANNUAL INSPECTION. THESE SUPPORT BRACKETS ARE ONLY INSTALLED WITH THE MANIFOLD BATTERY INSTALLATION. ITEM 12 OF PART'S LIST.SDR 98ZZZX999Line · failedLEFT BRAKE FAILED ON TAKEOFF ROLL AND TAKEOFF ABORTED. FOUND SMALL HOLE WORN THROUGH ALUMINUM BRAKE LINE WHERE LINE CHAFED ON AFT SIDE OF ENTRY STEP CASTING. INSTALLED NEW 0700099-93 BRAKE LINE. SUGGEST REMOVING LANDING GEAR STRUT FAIRINGS FOR INSPECTION ATSDR 98ZZZX803Fuel Cap · mismarkedC/W CESSNA SI TO REMOVE FLUSH-TYPE LARGE OPENING FUEL CAPS AND INSTALLING ABOVE WING CAPS WITH SMALL FILL OPENINGS SUPPLIED IN KIT SK182-86C. INSPECTED FILL ADAPTER PLATES PRIOR TO INSTALLATION AND FOUND FUEL CAPS OPEN IN A REVERSE/NON-STANDARD DIRECTION. ORSDR 98ZZZX1558Skin · crackedTHE (FUEL CHECK) STEPS ARE MOUNTED WITH AN3 BOLTS ATTACHED TO THE ACFT'S SKIN, P/N 0713334-3, AND P/N 0713334-4, LEFT AND RIGHT FORWARD SKINS. THE UPPER BACK BOLT WAS THROUGH THE SKIN AND THE BULKHEAD AT STA 1700. THE USE OF THE STEP CAUSED THE BOLT TO BREAKSDR 98ZZZX1557Skin · crackedTHE (FUEL CHECK) STEPS ARE MOUNTED WITH AN3 BOLTS ATTACHED TO THE ACFT'S SKIN, P/N 0713334-3, AND P/N 0713334-4, LEFT AND RIGHT FORWARD SKINS. THE UPPER BACK BOLT WAS THROUGH THE SKIN AND THE BULKHEAD AT STA 1700. THE USE OF THE STEP CAUSED THE BOLT TO BREAKSDR 97ZZZX3671Nut · brokenNUT WAS BROKEN THROUGH COMPLETELY. ALL TORQUE WAS RELEASED. THIS NUT WAS INSTALLED AT ENGINE OVERHAUL IAW CONT SB M92-9.SDR 97ZZZX3327Bulkhead · failedSPINNER BULKHEAD CRACKED BEWEEN BOLT HOLES AND SEPARATED CAUSING SPINNER TO WOBBLE. ACTION OF SPINNER CAUSED DAMAGE TO BOTH PROPELLER BLADES AT THE ROOTS, AND DAMAGE TO PROPELLER HUB, SPINNER AND BULKHEAD. SUBMITTER STATED CLOSE INSPECTION OF SPINNER BULKHEASDR 97ZZZX464Control Arm · misdrilledWASTEGATE CONTROL ARM (NEW PART) WAS MIS-DRILLED. SUBMITTER HAD TO ORDER 4 UNITS BEFORE RECEIVING A USEABLE PART.SDR 97ZZZX6215Bulkhead · crackedINSPECTION FOUND PROPELLER SPINNER BULKHEAD CRACKED.SDR 97ZZZX6214Piston Rod · corrodedPROPELLER INSPECTION FOUND PISTON ROD CORRODED.SDR 97ZZZX152Dowel Pin · corrodedINSPECTION FOUND PROPELLER ASSY DOWEL PIN CORRODED.
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