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 = '152' 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 = '152' 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 CA130726005Tube · split(CAN) RIGHT TIRE WENT SUDDENLY FLAT. UPON DISASSEMBLY OF WHEEL, TUBE WAS FOUND TO HAVE A SMALL SPLIT IN IT. NOTE: FAILED TUBE IS A 6:00 X 6 SIZE TUBE AND IN THE LAST FEW YEARS MANY OF THESE TUBES HAVE FAILED IN THE SAME MANNER. THEY MAKE THESE TUBES MUCH SMSDR CA130531009Riser · cracked(CAN) FOUND RISER CRACKED WERE IT ENTERS MUFFLER, 3" CRACK.SDR BQVR20130325001Spar · crackedDURING COMPLIANCE OF CESSNA SEB03-6 VERTICAL TAIL ATTACH BRACKET & AFT HORIZONTAL STABILIZER SPAR INSPECTION, CRACKS WERE FOUND IN THE UPPER RADIUS AREA OF BOTH AFT HORIZONTAL STABILIZER SPARS (PART NO. 0432001-56) AND REINFORCEMENT (P/N 0432001-15). CRACKS WSDR 2013FA0000209Caliper · crackedWHILE TAXING OFF RUNWAY, LOST LT BRAKE AND ACFT ENTERED IN THE GRASS AREA. THERE WERE NO MAJOR DAMAGE TO THE ACFT OR INJURIES. DISCOVERED THAT THE LT WHEEL BRAKE CALIPER WAS CRACKED AND LEAKING. BRAKE CALIPER WAS REPLACED, BRAKES TESTED AND PASSED. THE ACSDR 2013FA0000124Magneto · contaminatedPILOT REPORTS ROUGH RUNNING RT MAGNETO IN FLIGHT. INSPECTION FINDS MAGNETO HAS OIL INTERNALLY. MAGNETO WAS REMOVED FOR OVERHAUL AND SERVICEABLE MAGNETO INSTALLED.SDR CA130213002Spar · cracked(CAN) RUDDER SPAR CRACKED THROUGH THE UPPER LIGHTENING HOLE AT UPPER RUDDER MOUNTING HINGE. IT WAS NOTED AS CRACKED WHILE CARRYING OUT SID NR 22.SDR CA121206013Strobe · wrong part(CAN) ACFT HAD JOURNEY LOG REPORTED DEFECT FOR, LANDING LIGHT SWITCH UNSERVICEABLE, SWITCH RED HOT. DURING TROUBLESHOOTING AND SWITCH REPLACEMENT THE MAINTENANCE TECH NOTICED THAT THE INCORRECT PN, SWITCH WAS INSTALLED. THE ACFT HAD A DOUBLE POLE SWITCH, PN SDR CA121130008Plug · worn(CAN) DURING ROUTINE CPC NR 2 INSPECTION, THE ACFT OIL FILTER WAS OPENED TO CHECK FOR CONTAMINATION AND ALUMINUM WAS FOUND IN THE FILTER ELEMENT. WE PROCEEDED TO REMOVE ENGINE CYLINDERS AND FOUND NR 1 CYLINDER PISTON PIN PLUG WORN, FURTHER INSPECTION OF CYLISDR BQVR20111129Exhaust Valve · wornPREMATURE EXHAUST VALVE WEAR DETECTED BY LOW COMPRESSION/ EXHAUST VALVE LEAKAGE. EXCESSIVE WEAR STEP FOUND ON THE FACES OF THE LOW TIME EXHAUST VALVES. THE EXHAUST VALVES FROM ALL 4 CYLINDERS ARE AFFECTED. FURTHER ENGINE EVALUATION IN PROGRESS.SDR BR82013F00000Main Bearing · spunWE BELIEVE THAT THE FAILURE OF THE CRANK WAS CAUSED BY A CENTER MAIN BEARING THAT SPUN. THE SPUN BEARING PUT UNDO STRESS AND POSSIBLE DAMAGE TO THE CRANK ASSY THAT WAS INSTALLED IN THE ENGINE. BECAUSE OF THE WEAR OF THE SPUN BEARING, WE BELIEVE THAT THE CRANSDR CA121109010Plug · worn(CAN) DURING ROUTINE OIL CHANGE, ALUMINIUM WAS FOUND IN ENGINE OIL FILTER. SUSPECTED TO BE PISTON PIN PLUG. CYLINDERS REMOVED AND NR 1 CYLINDER PISTON PIN PLUG FOUND WORN. CYLINDER CHECKED AND FOUND INPERFECTION INSIDE CYLINDER BARREL 1-2" FROM BASE, SUSPECTSDR CA121109012Spring · broken(CAN) PILOT REPORTED RUDDER PEDAL LOOSE, INSPECTED RUDDER CABLE RETURN SPRING BROKEN, NEW SPRING INSTALLED. ACFT RETURNED TO SERVICE.SDR EY2R2012080106221Hub · crackedREMOVED FOR AD 2010-04-05, FOUND HUB CRACK IN THE PROCESS OF COMPLYING WITH AD. FLIGHT SCHOOL, PROPELLER WAS INSTALLED ON MULTIPLE AIRCRAFT, TOTAL TIME UNKNOWN.SDR CA120726001Seat · cracked(CAN) THE SEAT POST WAS CRACKED AT THE SEAT LOCKING PIN MECHANISM. THE WELD BROKE WHERE IT ATTACHES TO THE SEAT FRAME, NO INDICATIONS WERE GIVEN TO MAINTENANCE REGARDING PROBLEMS WITH THE SEAT PRIOR TO INSPECTION. IF NOT DETECTED THIS COULD CAUSE THE SEAT TO SDR CA120529008Starter · inoperative(CAN) THE ACFT WOULDN`T START. MAINTENANCE DISCOVERED THAT THE FRONT OF THE STARTER CASE HAD SNAPPED A CHUNK OFF.SDR CA120327002Bolt · sheared(CAN) DURING LANDING, THE NOSE GEAR FOLDED UNDER THE ACFT AND CAUSED DAMAGE TO PROPELLER, ENGINE, ENGINE MOUNT AND FIREWALL. IT WAS NOTED THAT THE UPPER TORQUE LINK BOLT WAS NOT ATTACHED TO THE GEAR ASSY. THUS CAUSING THE NOSE OLEO TO BE EXTENDED BEYOND ITS SDR 2012FA0000175Bolt · brokenIN CRUISE FLIGHT PILOT REPORTED LOSS OF ENGINE OIL PRESSURE. ACFT LANDED IN A FIELD. VISUAL EXTERNAL EXAMINATION OF THE ENGINE REVEALED AN 8" SQUARE AREA OF THE BOTTOM OF THE CRANKCASE MISSING BY THE NR 1 AND NR 2 CYLINDERS. THE CONNECTING ROD FOR THE NR 1 SDR CA120131013Line · chafed(CAN) DURING INSPECTION, FUEL LINES FROM LT AND RT TANKS WERE FOUND WEEPING DUE TO CHAFING. PARTS REPLACED.SDR CA120120004Carburetor · sticking(CAN) THROTTLE WAS STICKING AT IDLE POSITION.SDR CA120106002Crankcase · cracked(CAN) WHILE DOING 100HR INSPECTION OIL LEAK NOTICED AT FRONT OF ENGINE CRANKCASE. AME REMOVED BAFFLING AND OIL COOLER. CLEANED PAINT FROM CRANKCASE CRACK FOUND BETWEEN FRONT TWO THRU STUDS. CRACK WAS ALSO HEADING TO TOP OF CASE. ENGINE REMOVED AND SENT OUT FORSDR 2012FA0000012Rotor · looseFOUND DURING A 500HR MAG AND IMPULSE COUPLING INSPECTION, A DEFECTIVE DISTRIBUTOR GEAR FINGER. THIS FINGER HAD WORKED LOOSE FROM ITS PLASTIC SEAT ALLOWING SOME MOVEMENT BOTH SIDE TO SIDE AS WELL AS UP AND DOWN THE SHAFT. PARTS WERE STILL FUNCTIONING WHEN DISSDR CA120103023Bracket · cracked(CAN) THE BOTTOM HINGE TOP BRACKET WAS FOUND CRACKED AFTER THE RUDDER WAS REMOVED FOR BEARING REPLACEMENTS.SDR CA111103013Fork · cracked(CAN) DURING A ROUTINE 100 HR INSPECTION, SUBJECT NOSE FORK, PN 0442503-497 (LATER STYLE) WAS FOUND TO BE CRACKED ON BOTH SIDES OF THE UPPER AREA APPROX 2" BELOW THE TOP. AFTER EXAMINING THE FORK, IT DOES NOT APPEAR TO HAVE BEEN CAUSED BY A SINGLE INCIDENT ASSDR CA111021010Skin · cracked(CAN) A 1" CRACK WAS FOUND IN BETWEEN THE 2 RIBS OF THE STAB AT THE T/E WHERE THE REAR SPAR IS LOCATED ON THE RT SIDE LOWER SKIN. THE CRACK WAS FOUND ON A ROUTINE INSPECTION AND THE STAB WAS R & R WITH A SERVICEABLE UNIT.SDR 2011FA0000688Tachometer · inoperativeACFT IN SHOP FOR ANNUAL INSPECTION. REPLACED MALFUNCTIONING TACHOMETER WITH A NEW TACHOMETER, PN D1-112-5025, SN 25479. FAA-PMA. RAN THE ENGINE--TACHOMETER READINGS WERE VERY SLUGGISH AND WITH SEVERE LAG. TACHOMETER REMOVED FROM THE ACFT AND RETURNED TO THE DISDR CA111017007Switch · stuck(CAN) LANDING LIGHT SWITCH STUCK IN THE "ON" POSITION. THE LANDING LIGHT SUBSEQUENTLY DID NOT ILLUMINATE. SUBJECT SWITCH IS ON A 5 YEAR REPLACEMENT CYLE IAW SPECIAL INSPECTION ITEM NR 26 ON THE INSPECTION CHECKLIST OF D2064-1-13. THIS SWITCH FAILED AFTER ONLSDR CA111013004Switch · stiff(CAN) LANDING LIGHT SWITCH, STIFF TO OPERATE.SDR CA111012010Air Box · separated(CAN) DURING A ROUTINE INSPECTION IT WAS DISCOVERED THAT THE SCOOP FOR THE HEATED AIR INLET WAS SEPARATED FROM THE AIRBOX STRUCTURE. THE SCOOP IS NORMALLY SWAGED OR WELDED IN PLACE AND THE SCAT DUCT IS CLAMPED TO THIS SCOOP TO DIRECT INCOMING WARM AIR FROM THSDR CA111012007Piston · burned(CAN) ACFT DEPARTED ON A REGULAR TRAINING FLIGHT AFTER A NORMAL PRE-FLIGHT CHECK. SOON AFTER CLIMBOUT, THE CREW NOTICED ENGINE VIBRATION AND IT WAS NOT DEVELOPING FULL POWER. THE PILOT DECIDED TO RETURN TO THE AIRPORT AND LANDED WITHOUT INCIDENT. A POST-FLIGHSDR CA111006002Plug · worn(CAN) UPON 100 HR INSPECTION, FOUND METAL CONTAMINATION IN OIL FILTER AND INLET SCREEN. NON-FERROUS (ALUMINUM) SHINY SHAVINGS. DISCUSSION WITH LOCAL ENGINE O/H FACILITY LEADED TO INVESTIGATION OF CYLINDER REMOVAL AND CONFIRMATION THAT PISTON PIN PLUGS ON CYLISDR CA110811009Plunger · brokenDURING ROUTINE CPC INSP OF CUSTOMERS COMMERCIALLY REGISTERED ACFT, PROCEDED TO CARRY OUT AD 2011-10-09 (SEAT SLIPPAGE CAUSED BY LOCKING PIN NOT ENGAGING). NOTICED THE SPRING FOR THE PLUNGER BROKEN. SPRING WAS SUBSEQUENTLY REPLACED AND NO FURTHER ACTION TAKENSDR CA110811006Control Cable · separated(CAN) THE ACFT WAS ON APPROACH AFTER A ROUTINE PIPELINE PATROL WHEN THE PILOT PULLED THE CARBURETOR HEAT CONTROL TOWARDS THE "ON" POSITION. THE PILOT REALIZED THAT THE CONTROL FELT LOOSE AS HE CONTINUED TO PULL IT OUT OF THE PANEL. THE INNER CONTROL CABLE HADSDR CA110804001Distributor Gear · looseAT ROUTINE 500 HR MAGNETO INSP, THE DISTRIBUTOR FINGER OF THE DISTRIBUTOR GEAR WAS FOUND TO BE LOOSE - DISTRIBUTOR GEAR REPLACED.SDR CA110630003Cylinder · scoredOIL FILTER INSPECTION SHOWED CONTAMINATION. PISTON PIN FWD PLUG WEARING/SCORING BOTTOM OF 2 FRONT CYLINDERS. TIME IS FROM REPLACEMENT DUE SAME ISSUE.SDR 2011FA0000418Nut · looseROCKER ADJUSTMENT JAM NUT LOOSENED; ALLOWED ADJUSTER TO BACK OUT; CAUSED EXCESSIVE VALVE CLEARANCE; PARTIAL LOSS OF POWER AND FORCED OFF-FIELD LANDING.SDR CA110621010Camshaft · wornINTAKE LOBE NR 1 IS ALMOST COMPLETELY WORN DOWN.SDR CA110407005Bolt · sheared(CAN) VERTICAL FIN AFT ATTACH BOLT, 1 OF 4, WAS FOUND SHEARED DURING 100 HOUR INSPECTION. VERTICAL FIN ATTACH BRACKET INSPECTION COMPLETED & VERTICAL FIN ATTACH BOLTS REPLACED WITH NEW.SDR CA110315006Carburetor · malfunctioned(CAN) IMH 13082.3 TTSN AIRCRAFT SNAGGED POWER LOSS DURING FINAL APPROACH. AIRCRAFT INSPECTED FOR WATER CONTAMINATION IN ALL FUEL SYSTEM DRAIN LOCATIONS. SMALL AMOUNT (NORMAL) FOUND AND FLUSHED OUT. ENGINE INSPECTED FOR DEFECTS, NO FOUND. ALL SPARK PLUGS RSDR CA110307007Breather Tube · clogged(CAN) THE PILOT NOTICED SMOKE IN THE CABIN DURING FLIGHT AND DECLARED AND EMERGENCY LANDING. UPON INSPECTION IT WAS NOTED THAT THE ENGINE BREATHER TUBE HAD BEEN PLUGGED SOLID WITH ICE WHICH PRESSURIZED THE ENGINE CRANKCASE CAUSING THE FRONT CRANKSHAFT OIL SEASDR CA110223003Distributor Gear · loose(CAN) WHILE PERFORMING A ROUTINE 500 HR INTERNAL MAGNETO INSPECTION THE DISTRIBUTOR FINGER WAS FOUND TO BE LOOSE IN THE DISTRIBUTOR GEAR, PN M3008. THIS IS A PROBLEM THAT WAS COMMON TO THE EARLIER SERIES MAGNETOS OF 20 YEARS AGO. A DISTRIBUTOR GEAR FINGER THASDR 2011FA0000135Spark Plug · fracturedA LOSS OF ENGINE POWER DURING FLIGHT. EXAMINATION OF ENGINE FOUND THAT THERE WAS A CATASTROPHIC FRACTURE AT THE FLANGE OF THE SPARK PLUG LEAVING THE COPPER GASKET WASHER STILL HELD IN PLACE ALONG WITH THE THREAD FROM THE SPARK PLUG BUT THE PLUG WAS COMPLETELYSDR CA110211003Breather Tube · icedSHORTLY AFTER TAKEOFF, PILOT NOTICED SMOKE COMING IN THE COCKPIT AND REQUESTED AN IMMEDIATE LANDING. AFTER LANDING, MX CAME AND SAW THAT THE FRONT OF THE ENGINE WAS COVERED IN OIL AND DETERMINED THAT CRANKSHAFT SEAL HAD DISLODGED ALLOWING OIL TO LEAK OUT AND SDR CA110209020Line · puncturedAFTER REPLACING A NAVIGATION LIGHT BULB, MX WENT INTO THE COCKPIT TO TURN ON THE SWITCH TO TEST IT AND SMELLED A FAIRLY STRONG FUEL SMELL. AFTER FURTHER EXAMINATION, THE RT FUEL LINE FROM THE RT AFT TANK OUTLET TO THE "T" UNDER THE FLOOR HAD A PINHOLE IN THESDR CA110208021Fuel Line · corroded(CAN) FUEL LINE CORRODED THROUGH ENTIRE WALL THICKNESS. FUEL LINE IS DIRECTLY OFF THE RT FUEL TANK AND RUNS DOWN THE AFT DOOR POST AND ALONG THE DOOR FRAME. LEAK WAS FOUND ALONG THE DOOR FRAME PART OF THE FUEL LINE. ALSO NEED TO MENTION THAT THE FUEL LINE CSDR CA110125026Rib · cracked(CAN) DURING ANNUAL INSPECTION, THE AME IDENTIFIED A CRACK IN THE RIB AT THE 90 DEGREE BEND. WHERE THE RIB ATTACHES TO THE SPAR OF THE HORIZONTAL STABILIZER. NEW RIB INSTALLED . THE END (TC# 20110125026)SDR V56R20110204001Encoder · defectiveALTITUDE REPORTING SYS DISPLAYED ALTITUDES IN EXCESS OF 20,000 FT AT AN ACTUAL ACFT ALTITUDE OF 1,000 FEET ASL. THE PROBLEM WAS CAUSED BY AN INTERNAL FAILURE IN THE ALTITUDE ENCODER. THE PROBLEM WAS WAS SUBSEQUENTLY DUPLICATED ON THE GROUND. THE DEFECTIVE ESDR 2011FA0000114Line · leakingSMALL AMOUNT OF CORROSION ON UNDERSIDE OF FUEL LINE, RESULTED IN PIN-HOLE LEAK.SDR CA110104006Switch · failedSWITCH FAILED IN ON POSITION SWITCH INSTALLED IN OCT 2009 IAW SEB09-6 TTIS 462.1 HRS/14 MONTHS.SDR CA110106006Armature · burnedTHE BATTERY WAS THE INITIAL SNAG FROM THE PILOT. THE PLANES ELECTRONICS WEREN`T COMING ON. FUMES WERE COMING FROM THE OIL DOOR ON THE COWLING WHICH WAS THE BATTERY BEING BOILED OVER. FOUND BATTERY HAD PUKED ITS GUTS OUT. TLOOKED FOR CAUSE AND FOUND WHEN SDR ZB0R201000007Case Half · crackedDURING ENGINE TEAR DOWN INSP FOR PROPELLER STRIKE, TECH FOUND LT CASE HALF CRACKED IN 2 PLACES AT THE NR2 CYL OPENING. THE DAMAGE CAN BE TOTALLY ATTRIBUTED TO THE PROP STRIKE. CASE WAS REPLACED WITH AN O/H UNIT.
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