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 = '172K' 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 = '172K' 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 2026FA0000176Bulkhead · crackedFOUND FORWARD PROPELLER BULKHEAD P/N 0550321-4 CRACKED AT ONE BOLT HOLE LOCATION.SDR 2019FA0000115Attach Bolt · shearedA/C WAS INVOLVED IN AN ACCIDENT AT VAY. UPON LANDING, THE PILOT'S SEAT BACK DISCONNECTED AT THE LEFT HAND SIDE OF THE SEAT BACK ASSEMBLY ATTACH POINT ATTACHING BOLT SHEARED. UPON INSPECTION OF THE AIRCRAFT, THE BOLT HEAD HAD SHEARED OFF FROM THE SEAT BACK ASSDR CA150415008Pulley · worn(CAN) MAX RT RUDDER PRESSURE NEEDED TO MAINTAIN STRAIGHT LEVEL FLIGHT. INSPECTION OF RUDDER CONTROL SYSTEM CARRIED OUT, FOUND RT RUDDER CABLE OUT OF FWD PULLEY. CABLE INSPECTED AND NO DAMAGE FOUND. PULLEY, PN MCS378-4 REPLACED AND RUDDER CONTROL SYSTEM FUNCSDR CA140626008Ball · corroded(CAN) PILOT COMPLAINED FUEL SELECTOR WAS VERY STIFF. CYCLED IT A COUPLE TIMES AND IT SEIZED IN THE LT TANK POSITION. FUEL WAS DRAINED AND SELECTOR REMOVED. THE DETENT BALL WAS FOUND TO BE ROUGH, CHROME PEELING SLIGHTLY, SMALL AMOUNT OF CORROSION. DETENT BALL SDR CA130531010Contact · burned(CAN) HARD STARTING ENGINE. TROUBLESHOT TO NO SPARK AT LOW RPM. SLICK SB1-12, MAG SN. THE MAGNETO WAS NEW WITH ONLY 300.2 HRS ON IT. POINTS WERE BURNED.SDR CA101125004Bellcrank · misinstalledBELL-CRANK FOUND INSTALLED UPSIDE DOWN. JOGGLE CAUSES INTERFERENCE WHEN INSTALLED UPSIDE DOWN. LOWER CLEVIS RUBS AFT BULKHEAD CLEARANCE OPENING. PARTS CATALOGUE DOES NOT SHOW ORIENTATION OF JOGGLE ON THE BELL-CRANK.SDR 2010FA0000584Mount · damagedUPON ROUTINE INSP, CRACK WAS FOUND ON LOWER LT ENGINE MOUNT BRACE. THERE IS NO DAMAGE HISTORY ON THE ACFT. THE MOUNT DOES NOT HAVE RELIEF HOLES FOR WELDING, AND THUS CAN`T ACHIEVE FULL PENETRATION ON THE WELDS THERE. COMBINED WITH FATIGUE AND VIBRATION, THISDR CA090805004Cylinder · pressure lossREPORTED HIGH OIL CONSUMPTION, FOUND NR 2 CYL LOW COMPRESSION 20/80 PAST RINGS.SDR CA090629001Cylinder Head · cracked(CAN) INITIALLY FOUND ALUMINUM SHAVINGS IN OIL SCREEN, CYL NR 3 FOUND AT LOW COMPRESSION 20/80. CYLINDER ASSY REMOVED AND FOUND PISTON BROKEN BETWEEN THE TOP 2 RINGS, CREATING THE SHAVINGS. ALSO, FOUND CYLINDER HEAD CRACK STARTING NEAR SPARK PLUG HOLE.SDR CA090710002Ignition Switch · worn(CAN) REF AD 93-05-06. THIS ACFT HAS AFFECTED SWITCH INSTALLED. ACFT IS OUTSIDE OF S/N RANGE. DUE TO AGING ACFT ISSUES, PARTS FROM OUTSIDE THE S/N RANGE ARE GETTING INTO OTHER ACFT. THE LOGS INDICATE THAT, IN THE CLASSIC MANNER, THE AD IN QUESTION HAS "C/W"SDR CA081201002Switch · overheated(CAN) LANDING LIGHT SWITCH MAY BE ORIGINAL (8865 HRS) DETENTS BECAME "STICKY" AND NOT AS POSITIVE AS NORMAL. SWITCH FUNCTION DID NOT FAIL. INSP REVEALED PWR SUPPLY WIRE END AND LUG ON SWITCH OVERHEATED. DISASSY SHOWED LUG CONTACT RIVET DETERIORATED AS WELL ASSDR CA080826008Cylinder · corroded(CAN) CYLINDER CASTING COMPOSED OF ALUM STEEL ANCHOR BOLTS MOUNTED IN CASTING CAUSED CORROSSION OF ALUM BOSS BORES WHICH OVER TIME CAUSED THE BOSS CASTING TO CRACK DUE TO THE (SWELLING) ACTION OF THE CORROSION NEXT TO THE STEEL PINS. DUE TO THE NORMAL DIRT CRESDR CA071019002Nut Plate · misrepaired(CAN) UPON INSPECTING THE FUEL TANKS, FOUND SEVERAL NUTPLATES PREVIOUSLY DAMAGED. UPON FURTHER INSPECTION FOUND THAT AT A PREVIOUS TIME, SOME SCREWS BROKE OFF IN THE NUTPLATES AND RATHER REPAIR/REPLACE THE NUTPLATES, IT APPEARS THE DAMAGED NUTPLATES WERE DRILLSDR CA070814009Seat Belt · failed(CAN) SEAT BELT LOOPS THAT SECURE THE FRONT SEAT LAP BELTS TO THE SEAT FAILED. THIS ALLOWED THE SEAT BELT, WHILE BEING SECURED, TO LOOP OVER THE SEAT BACK ADJUSTMENT LEVER. WHEN THE PILOT ADJUSTED HIS SEAT PRIOR TO TAXI, THE SEAT BACK ADJUST LEVER WAS ACTIVASDR CA070727006Web · cracked(CAN) CRACK FOUND AT LOWER WELD WEB LT SIDE. (TC NR 20070727006)SDR CA070507013Rotor · failed(CAN) PILOT OF AC ON FLOATS DETECTED A DEAD MAGNETO ON HIS PRE-TAKEOFF INSPECTION, AND RETURNED TO THE DOCK. (TC NR 20070507013)SDR CA070726005Gear · failed(CAN) ENGINE WOULD NOT START, STARTER REMOVED, BENDIX FOUND SHATTERED. (TC NR 20070726005)SDR CA061124008Support · cracked(CAN) AIRCRAFT BEING SERVICED FOR MFG CARE NR 4 (200-HOUR) INSPECTION AND CHANGED OVER TO SKIS. LT OB SUPPORT FOR LANDING GEAR WAS FOUND TO HAVE SEVERAL CRACKS. PART WAS REPLACED WITH NEW. AIRCRAFT IS OPERATED AS FLOATPLANE AND SKIPLANE FOR FLIGHT TRAININGSDR 2006FA0000747Fuel Line · chafedDURING AN ANNUAL INSPECTION, BOTH ENGINE FUEL SUPPLY LINES WERE FOUND TO BE CHAFFING THE FWD BULKHEAD OF THE LANDING GEAR BOX STRUCTURE AT BS 56.70. MDG HAS INSTALLED A THIN PLASTIC SLEEVE OVER THE LINES IN THE AREA OF THE CHAFE BUT, AFTER 2564 HOURS, THE SLESDR CA060621003Cylinder Head · crackedENGINE RUNNING ROUGH FOUND NR 1 CYLINDER HEAD CRACKED.SDR CA060825003Spar · cracked(CAN) P/N 0532001-97 SPAR REINFORCEMENT AND P/N 0532001-98 FRONT SPAR ASSEMBLY WAS REPALCED DUE TO CRACKED CENTER SECTION OF MAIN SPAR. PARTS WERE INSTALLED USING EXISTING RIVET SIZE AND PATTERN ACCORDING TO SPECIFIED APPROVED METHODS IN MFG SRM. (TC NR 20060SDR CA050803008Mount · cracked(CAN) 2 CRACKS FOUND AT LOWER CROSS TUBE SAME CRACKS FOUND ON PREVIOUS MOUNT. BOTH MOUNTS OVERHAULED, WELDING CRACKS LOCATED BESIDE WELD AREA SHOULD HAVE GUSSET PLATE WELDED AT THIS AREA TO RE-INFORCE.SDR CA040827003Rail · cracked(CAN) THE LT UPPER ENGINE RAIL WAS FOUND TO BE CRACKED DURING SCHEDULED MAINTENANCE. PN 0513132-3 WAS REPLACED WITH NEW PART. NEW HARDWARE WAS INSTALLED.SDR CA040511002Support Bracket · cracked(CAN) RT MAIN LANDING GEAR OB SUPPORT BRACKET CRACKED AT U BOLT FORWARD HOLE.SDR 2004FA0000366Bolt · corrodedWHILE REMOVING WING BOLTS, FOUND BOLTS RUSTED AND CORRODED. RECOMMENDED BOLTS BE INSPECTED AND COATED WITH EPOXY PRIMER, INSTALLING NEW BOLTS.SDR CA040220006Line · chafed(CAN) FUEL LINE WAS FOUND CHAFED DURING 200 HR INSPECTION.SDR CA040506003Torque Link · cracked(CAN) DURING INSPECTION, IT WAS DISCOVERED THE UPPER TORQUE LINK PART NUMBER 0442506-1WAS CRACKED. NEW PART WAS INSTALLED.SDR ISO11030019Exhaust Valve · brokenAIRCRAFT IN CRUISE AT 5000 FT., EXPERIENCED LOSS OF POWER, PILOT LANDED IN WHEAT FIELD, 2 POB, NO INJURIES, MINOR DAMAGE.SDR 2003FA0000269Roller · damagedRT FLAP, INBOARD AFT FLAP ROLLER, FAILED AND BOUND DURING FLAP RETARCTION. THE RT OUTBOARD FLAP END CONTINUED TO RETRACT DEFORMING THE FLAP TO SOME EXTENT.SDR AUS20030011Cable · worn(AUS) ENGINE MIXTURE CONTROL INNER CABLE WORN.SDR AUS20020945Strap · broken(AUS) LH FUEL TANK REAR STRAP ASSEMBLY LOOSE. RH FUEL TANK REAR STRAP ASSEMBLY BROKEN NEAR THE SCREW END. FOUND DURING INSPECTION IAW CESSNA CONTINUED AIRWORTHINESS PROGRAM 28-30-01.SDR CA020610003Line · worn(CAN) - FUEL LINE FROM UNION TO FIREWALL (STRAINER) FOUND RUBBING ON CO-PILOT STEERING TORQUE TUBE AND STEERING ARM. FUEL LINE HAD A SMALL PIN HOLE AND A SMALL AMOUNT OF FUEL WAS LEAKING. - NEW LINE WAS MANUFACTURED AND ROUTED AWAY FROM STEERING ARM.SDR 2001FA0000363Shaft · shearedPILOT REPORTED 700 RPM DROP ON LEFT MAGNETO. MAGNETO REMOVED AND INSPECTED. FOUND DRIVE SHAFT/ MAGNETO/ ROTOR SHEARED IN HALF. MAGNETO REPLACED.SDR CA010907010Stringer · cracked(CAN) DURING ROUTINE MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE RIGHT HAND ENGINE RAIL WAS CRACKED. P/N 0513132-4 STRINGER ASSEMBLY IN FUSELAGE FRONT SECTION STRUCTURE ASSEMBLY WAS REPLACED.SDR 20001207SH013Rib · damagedDURING A HIDDEN DAMAGE INSP, LT WING ASSY PN 0523005-83 FOUND LIGHT DAMAGE TO MID L/E SKIN AND 1 NOSE RIB, UNAPPROVED REPAIR FOUND TO AFT INBD SPAR ASSY. ALMOST ALL NOSE RIBS IN WING FOUND DAMGED, 10 IN ALL. A T/E RIB WAS CUT BY A FLAP CONTROL CABLE. 4 SKINSDR 20010326CW008Spar · damagedDURING HIDDEN DAMAGE INSPECTION SOME LIGHT DABAGE TO MID LEADING EDGE SKIN AND ONE NOSE RIB WAS FOUND. UNAPPROVED REPAIR FOUND TO AFT INBD SPAR ASSY. DAMAGE WAS FOUND ON ALMOST ALL NOSE RIBS IN WING. RECORDS CHECK BY OWNER FOUND WING WAS REPAIRED AND RETURNESDR CA000530047Gyro · wrong part(CAN) SUSPECTED UNAPPROVED PART DETECTED DURING IMPORTATION INSPECTION. UNIT INSTALLED: SEPT 10 1999 INVESTIGATION IN PROGRESS BY NEW OWNER. INVESTIGATION INTO DISCREPANCIES BETWEEN THE INSTALL AND PURCHASE DATES. FOLLOW UP BY PAH-HAM IN PROGRESSSDR CA000222007Cam · broken(CAN) CAM ASSY FOUND BROKEN. REPLACED WITH NEW PART.SDR CA991004052Rod · broken(CAN) DURING FLIGHT, A STUDENT PILOT EXPERIENCED LOSS OF CONTROL OF THE AIRCRAFT. TAKING CONTROL, THE INSTRUCTOR NOTICED THAT THE LEFT AILERON FAILED TO RESPOND TO CONTROL WHEEL INPUT. THE INSTRUCTOR LANDED THE AIRCRAFT SAFELY. MAINTENANCE DETERMINED THAT TSDR 99ZZZX3817Sleeve · brokenREMOVED SUCTION SCREEN DURING OIL CHANGE AND FOUND TWO CHUNKS OF ALUMINUM TRAPPED BY SCREEN. INVESTIGATION FOUND THE PIECES HAD BROKEN OFF THE OIL RELIEF VALVE SLEEVE. REASON FOR FAILURE NOT DETERMINED. THERE IS NOT MUCH STRESS ON THIS PART.SDR 99ZZZX2194Tube · looseACCELERATING PUMP DISCHARGE TUBE CAME OUT AND STRUCK THROTTLE OPEN, STOPPING ENGINE, THEN PART FELL DOWN INTO THE AIRBOX. (THIS OCCURRED IN-FLIGHT AT EFT).SDR CA980811006Blade · corroded(CAN) PROPELLER CORRODED.SDR CA980811008Bearing · broken(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER BLADE BEARING WAS FOUND BROKEN.SDR 98ZZZX2695Engine · fireENGINE WAS WARM. WHEN STARTING AIRCRAFT ACCORDING TO WARM ENGINE START-UP PROCEDURE, IT CAUGHT FIRE BEFORE IT STARTED. RECOMMENDATION: LET ENGINE COOL OFF LONGER OR MODIFY STARTING PROCEDURE.SDR 98ZZZX2044Spring Seat · failedENGINE SUCTION SCREEN REMOVED DURING ANNUAL INSP AND SEVERAL LARGE PIECES OF FERROUS METAL WERE FOUND. RECORDS INDICATED THE ENG HAD NEW CYLINDERS INSTALLED DURING OVERHAUL 272.7 HOURS PREVIOUSLY. THE PIECES OF METAL WERE FROM THE LOWER INTAKE VALVE SPRING SSDR CA980325032Spar · cracked(CAN) RUDDER SKIN WRINKLED ON RIGHT SIDE APPROX 1.5 INCHES ABOVE LOWER HINGE POINT. 0.5 INCH CRACK IN RIGHT SIDE OF FORWARD SPAR. REPLACED.SDR CA970709010Rail · cracked(CAN) DURING MAINTENANCE, IT WAS DISCOVERED THAT THE LEFT HAND ENGINE RAIL WAS CRACKED. P/N 0513132-3 STRINGER ASSY IN THE FUSELAGE FRONT SECTION WAS REPLACED. THE ENGINE RAIL WAS CRACKED AROUND THE ENGINE MOUNT BOLT HOLE.SDR 97ZZZX2815Handle · brokenHANDLE BROKE AT PIVOT POINT. ALLOWED THE ARM TO FALL FROM PIVOT POINT CAUSING THE SEAT LATCH DROP PIN TO NOT ENGAGE THE SEAT RAIL ALLOWING THE PASSENGER SEAT TO SLIDE BACK WHEN POWER TO THE AIRCRAFT IS APPLIED. INDIVIDUALS SHOULD LOOK AT THIS AREA ON 100 HOUSDR 97ZZZX2900Throttle Valve · out of adjustOVERHAULED CARBURETOR FURNISHED WITH LYCOMING OVERHAULED ENGINE WOULD NOT IDLE BELOW 1,000 RPM AFTER BUILD-UP AND INSTALLATION. CARUBURETOR WAS NEWLY OVERHAULED. REMOVAL AND INSPECTION REVEALED THE THROTTLE PLATE WAS NOT ALIGNED CORRECTLY AND WAS BINDING ON SDR 97ZZZX1146Spring · brokenRECEIVING INSPECTION OF A NEWLY OVERHAULED ENGINE FOUND PUSH ROD HOUSING COULD BE POPPED OUT OF SEAT. REMOVED ROCKER COVER AND FOUND HOLD-DOWN SPRING BROKEN. FURTHER INVESTIGATION FOUND 3 OF 4 PUSH ROD SPRINGS BROKEN. SUBMITTER SUSPECTS SPRINGS MISMANUFACTU
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