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 = '172L' 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 = '172L' 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 CA000519008Circuit Breaker · burned(CAN) VOLTAGE REGULATOR A WIRE SHORTED TO GROUND. THE 60 AMP ALTERNATOR CIRCUIT BREAKER SMOKED BUT DID NOT TRIP. THE MANUFACTURING DATE ON THE CIRCUIT BREAKER WAS FEB, 1972. THE CIRCUIT BREAKER WAS REPLACED WITH ONE SUPPLIED IN A CESSNA SERVICE KIT. INTERNASDR CA000516005Mount · cracked(CAN) DURING SCHEDULED MAINTENANCE, THE ENGINE MOUNT LOWER HORIZONTAL BRACE WAS FOUND CRACKED AT BOTH ENDS.SDR CA000621014Mount · broken(CAN) ON ROUTINE 100 HOUR INSPECTION LT VERTICAL TUBE ON ENGINE MOUNT WAS FOUND BROKEN.FURTHER INVESTIGATION FOUND THAT THIS AIRCRAFT HAD HAD A LONG HISTORY OF NOSE WHEEL SHIMMY. OVERHAULED ENGINE MOUNT AND SERVICING OF SHIMMY DAMPER, FIXED THE PROBLEMS.SDR CA000621015Static Line · kinked(CAN) THE AIRSPEED INDICATOR HAD BEEN REMOVED FOR MAINTENACE, AND RE-INSTALLED. SUPPOSEDLY A PITOT/STATIC TEST WAS CARRIED OUT, AND SIGNED FOR. AIRCRAFT WHEN ON INITIAL FLIGHT AND AIRSPEED & ALTIMETER DID NOT FUNCTION.THE CAUSE OF THE PROBLEM WAS THAT, THE STASDR CA000301047Screw · loose(CAN) EVIDENCE OF A CARBURETOR FIRE WAS NOTED DURING INSPECTION. UPPER HALF AND LOWER BOWL WERE FOUND LOOSE, THROTTLE BODY ATTACHMENT SCREWS WERE FOUND LOOSE WITH LOCKING TABS IN PLACE. SCREWS TORQUED AND TABS BENT.SDR CA991229069Fillercap · cracked(CAN) DURING INSPECTION, MAINTENANCE NOTICED THE FUEL TANK FILLER NECK SEEMED TO FLEX MORE THAN NORMAL. AFTER TANK REMOVAL THE FILLER NECK WAS FOUND TO BE SEALED TO THE TANK WITH AN UNSPECIFIED SEALING COMPOUND. THE SEALER WAS REMOVED, REVEALING THE NECK TO BSDR CA991229055Strap · broken(CAN) UPON FUEL TANK REMOVAL, THE REAR FUEL TANK STRAP WAS FOUND BROKEN.SDR CA991210018Disc · incorrect part(CAN) UPON REMOVAL FROM THE WHEEL ASSY, THE BRAKE DISC WAS DETERMINED TO BE AN INCORRECT PART FOR THE WHEEL ASSY TO WHICH IT WAS INSTALLED. THE SUBMITTER STATED THAT THE CORRECT BRAKE DISC PART NUMBER IS 164-40 AND THAT THE ONLY PERCEPTIBLE DIFFERENCE IS THE DSDR 99ZZZX1976Selector Valve · malfunctionedFUEL SELECTOR VALVE INSTALLED. APPROX 8 GALLONS OF FUEL WERE ADDED TO EACH TANK AND FUEL SELECTOR AND FUEL LINES WERE CHECKED FOR LEAKS WITH SELECTOR IN ALL DETENTS. DURING OPS CHECK, ENG WAS RUN APPROX 5 MINUTES WITH EACH LEFT, RIGHT, AND BOTH DETENTS SELESDR CA981130020Shroud · cracked(CAN) CARBURETOR HEAT SHROUD FOUND SLIPPED DOWN ON EXHAUST STACK. PART OF UPPER CLAMP P/N AN7377W56 WAS MISSING. SHROUD CRACKED IN FOUR PLACES. SCREEN IN SHROUD PARTLY BURNED, LOOSE OR DISINTEGRATING.SDR CA981013003Muffler · cracked(CAN) DURING OIL CHANGE, THE OVERBOARD PIPE ON THE MUFFLER WAS FOUND LOOSE. A CRACK WAS FOUND IN THE EXHAUST PIPE BRACE AND COLLECTOR CAN JOINT RUNNING HALF WAY ROUND THE CIRCUMFERENCE, TOTALLING ABOUT 4 INCHES IN LENGTH. SUBMITTER SAYS THESE UNITS LAST ABOUSDR CA981027022Seal · failed(CAN) STC SA71GL WAS INCORPORATED ON THE ENGINE. FAA AD 96-09-06, WHICH SUPERSEDES FAA AD 95-03-02, CALL FOR THE INSPECTION OF THE CARBURETOR AIR INTAKE FILTER GASKET AT 100 HOUR INTERVALS. REQUIREMENTS FOR TERMINATING ACTION OF THIS AD IS THE REPLACEMENT OFSDR 98ZZZX3024Bushing · missingWHILE PERFORMING AN ANNUAL INSPECTION, FOUND AFT ELEV TRIM CABLE SEVERELY FRAYED DOWN TO THE CENTER STRAND AT THE 90 DEGREE PULLEY IN THE TAIL SECTION. FURTHER INSPECTION DISCLOSED THE CABLE WAS TWISTED AROUND THE OTHER CABLE INSIDE THE HORIZONTAL STABILIZER.SDR 98ZZZX3023Control Cable · frayedWHILE PERFORMING AN ANNUAL INSPECTION, FOUND AFT ELEV TRIM CABLE SEVERELY FRAYED DOWN TO THE CENTER STRAND AT THE 90 DEGREE PULLEY IN THE TAIL SECTION. FURTHER INSPECTION DISCLOSED THE CABLE WAS TWISTED AROUND THE OTHER CABLE INSIDE THE HORIZONTAL STABILIZER.SDR CA980629006Seat Track · misinstalled(CAN) PILOTS SEAT RAILS HAD BEEN RE-INSTALLED USING WRONG RIVETS. PROPER RIVETS INSTALLED.SDR CA980507003Muffler · cracked(CAN) TOP INBOARD SEAM CRACKED. THIS SEAM IS VERY HARD TO SEE SINCE IT IS HIDDEN BY THE OVERBOARD EXHAUST STACK AND THE OVERLAPPING PLATE. ONLY TWO .250 INCH HOLES TO INSPECT THIS PORTION OF THE SEAM. REPLACED.SDR 98ZZZX1678Solenoid · failedWHEN AIRCRAFT MASTER SWITCH WAS TURNED ON THE STARTER ENGAGED CAUSING THE PROPELLER TO TURN. THE SOLENOID P/N S-199-1 WAS REMOVED AND OPENED UP. WATER, RUST, AND CORROSION WERE FOUND. THIS CAUSED THE SOLENOID TO REMAIN IN THE CLOSED POSITION. THIS CONDITIOSDR 98ZZZX1655Carburetor · wornFUEL INLET FITTING HAD STRIPED THREADS OUT OF CARBURETOR HOUSING AND LEAKING FUEL. INSTALLED REBUILT PART.SDR 98ZZZX1654Actuator · wornHAD EXCESSIVE PLAY. MAXIMUM PLAY .131 - HAS .330 PLAY. INSTALLED NEW PART.SDR 98ZZZX1653Dampener · wornSHIMMY DAMPENER HAD NO FLUID AND SHAFT WOULD NOT COME OUT FOR OVERHAUL. INSTALLED NEW PART.SDR CA960223013Oil Pump · cracked(CAN) AFTER 2.5 HOUR FLIGHT, PILOT REPORTED OIL PRESSURE CREEPING DOWN DURING DESCENT. GROUND RUN CARRIED OUT AND PRESSURE MAINTAINED AT 70 TO 75 PSI. WHILE COMPASS SWING CARRIED OUT, PRESSURE DROPPED OFF AGAIN. ENGINE REMOVED FOR OVERHAUL. REPORT FROM O/SDR 98ZZZX1593Magneto · failedMAGNETO WAS INSTALLED AS A NEW UNIT WITH STC SE419CH ON THIS AIRCRAFT ON 4-28-97. THE STC IS THE UNISON ELECTRONIC IGNITION SYSTEM. DURING THE MAG CHECK WITH THE ENGINE RUNNING AND THE MAG SWITCH IN THE LEFT POSITION, THE ENGINE QUIT. OPERATION WAS NORMAL ISDR CA970722016Bulkhead · worn(CAN) DURING THE INSPECTION ON REMOVAL OF THE FLOOR INSPECTION COVERS, IT WAS DISCOVERED THAT THE RUDDER AND ELEVATOR CABLES HAD BEEN RIDING ON AND CUTTING THE BULKHEADS BELOW THE FLOOR FROM STA 8.12 TO STA 124.00. CABLES REMOVED AND INSPECTED AND FOUND TO BESDR CA970722015Magneto · cracked(CAN) DURING ANNUAL INSPECTION THE MAGNETO COIL WAS FOUND CRACKED ACROSS ITS CASE. FAA AD 81-16-05 WHICH PERTAINS TO THIS SUBJECT WAS SIGNED OFF IN THE ENGINE LOG BOOKS, BUT WAS NOT COMPLIED WITH.SDR 97ZZZX3099Throttle Arm · jammedMISALIGNMENT OF THE RIGGING OF THE THROTTLE ARM TO THE CARBURETOR (IN 1994) CAUSED THE THROTTLE ARM TO JAM PREVENTING THE ENGINE FROM ACCELERATING.SDR AU970536Bulkhead · cracked(AUS) LOWER AFT DOOR POST BULKHEAD CRACKED - FOUND DURING INSPECTION IAW CESSNA SEB 97-1SDR 97ZZZX1918Casting · creepTHE END-SHAKES, (BACK AND FORTH MOVEMENT) OF THE THREE CRITICAL ROTATING SHAFTS OF THE MECHANISM OF THIS ALTIMETER WERE CHECKED. THE OH MANUAL CALLS OUT .0020 INCH MINIMUM END-SHAKE. ONE END-SHAKE MEASURED .00020 INCH. THIS IS TEN TIMES SMALLER THAN THE SPESDR 97ZZZX1979Carburetor Screw · looseIDLE ADJUSTMENT SCREW BACKED OUT OF CARBURETOR IN-FLIGHT. ENGINE FAILED TO RUN WITH POWER SETTING BELOW 2300 RPM'S. INSTALLED NEW SPRING AND SCREW. CARBURETOR THREADS APPEAR TO BE LOOSE.SDR 96ZZZX6162Spring · brokenOPERATOR COMPLAINED OF HEAVY RUDDER AND OUT OF TRIM. UPON INSPECTION, FOUND RT RUDDER CENTERING SPRING BROKEN AT AFT ATTACHMENT. AIRCRAFT 4.6 HOURS SINCE 'OWNER ASSISTED ANNUAL INSPECTION' WAS COMPLETED. AREA IS AWKWARD TO INSPECT UNLESS AREA PANELS ARE REMSDR 96ZZZX6161Discharge Tube · brokenTHROTTLE JAMMED IN-FLIGHT. SAFE LANDING MADE. FOUND CARB DISCHARGE TUBE BENT AND BROKEN IN CARB HEAT BOX. FOUND THROTTLE SHAFT BUSHINGS EXCESSIVELY WORN AND LEAKING. AIRCRAFT 4.6 HOURS SINCE 'OWNER ASISTED ANNUAL' WAS COMPLETED. THESE ITEMS ARE PART OF ASDR 96ZZZX5959Spring · weakINSTALLED OVERHAULED CARBURETOR AND RIGGED. WITHIN 10 HOURS, OWNER REPORTED ENGINE VERY ROUGH AT LOW POWER SETTINGS OR WOULD NOT EVEN IDLE. FOUND IDLE MIXTURE ADJUST SCREW GONE. NOTIFIED OVERHAULER WHO SENT NEW CARB. UPON INSTALLATION OF NEW UNIT, SPRING TSDR CA960123022Valve · jammed(CAN) NON FERROUS METAL IN THE MAIN AND SUCTION OIL SCREENS. ZERO COMPRESSION ON #4 CYLINDER, SUSPECT A JAMMED VALVE. #4 CYLINDER REMOVED AND SENT FOR REPAIR.SDR 95ZZZX4209Adapter · loose rivetsLOOSE/WORKING RIVETS WERE FOUND AT AN ANNUAL INSPECTION ON THE LEFT ELEVATOR TORQUE TUBE ADAPTER (6 AN-4 RIVETS). THE REMOVED RIVETS WERE CLINCHED AND INCOMPLETELY BUCKED (UPSET HEADS NOT OF PROPER DIMENSION). THE RIVETS WERE REPLACED AND AIRCRAFT RETURNED SDR 95ZZZX3651Bracket · brokenUPON ROUTINE INSPECTION, FOUND BRACKET BROKEN COMPLETELY THROUGH ACROSS AFT BOLT HOLE. SUBMITTER SUGGESTS LYC MANUFACTURE BRACKET WITH GUSSETS ACROSS CORNERS. LYC NEW P/N 07A21443 STILL SAME AS OLD P/N 76906 DIMENSIONALLY.SDR 95ZZZX2713Bendix Drive · failedTHE STARTER MOTOR TURNS, BUT THE BENDIX WILL NOT ENGAGE. POSSIBLE FAULTS: 1. WORN. 2. WRONG LUBRICANT - NOT SILICONE AS RECOMMENDED. 3. DIRT/OIL PREVENTING 'SLIDING' AS REQUIRED.SDR 95ZZZX1634Strainer · plunger failedPRIOR TO A FLIGHT, PILOT ATTEMPTED TO DRAIN FUEL STRAINER. IT WOULD NOT DRAIN. UPON DISASSEMBLY, FOUND RUBBER TIP OF PLUNGER HAD DISBONDED FROM ASSY AND WAS PREVENTING FUEL FROM DRAINING.
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