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 = '172E' 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 = '172E' 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 2025FA0000733Filter Adapter · backed outOIL FILTER ADAPTER BECAME LOOSE FROM ACCESSORY CASE CAUSING LOSS OF ENGINE OIL AND SUBSEQUENT ENGINE FAILURE. ADAPTER IS SUBJECT TO AD 96-12-22 AND WAS RECENTLY INSPECTED WITH NO DEFECTS NOTED, HOWEVER AN ENTRY WAS MADE IN THE AIRCRAFT RECORDS THAT THERE WAS ASDR 2022FA0000007Yoke · brokenDURING AN INSTRUCTIONAL FLIGHT, WHILE PRACTICING STEEP TURNS, IT WAS NOTICED BY STUDENT AND INSTRUCTOR THAT THEY HAD NO UP ELEVATOR CONTROL BUT DID HAVE DOWN ELEVATOR CONTROL. THE AIRCRAFT RETURNED TO THE FIELD, KAZC AND THE INSTRUCTOR WAS ABLE TO MAKE AN UNEVSDR 2020FA0000102Cylinder · crackedPILOT REPORTED A LOUD POP/BANG. THEN RPM DROPPED TO 1200 AND LOSS OF POWER. APPROXIMATELY 30 SECONDS, RPM DROPPED TO 400, THEN ENGINE STOPPED, ACFT LANDED SAFELY IN FIELD. INSPECTION, ONCE COWLING WAS REMOVED (DAMAGE NEAR NR 3 CYLINDER). CYLINDER HAD SEPARSDR 2013FA0000175Control Wheel · brokenTHE RT PLASTIC CONTROL WHEEL BROKEN AT THE UPPER LEFT AND LOWER RIGHT CORNERS.SDR 2013FA0000120Counterweight · looseWHILE PERFORMING ELECTRICAL TROUBLESHOOTING FOR THE RUDDER WIRING, RUDDER COUNTERWEIGHT ATTACH RIVETS WERE EITHER WORN THROUGH THE MOUNTING BRACKET OR MISSING. ONLY 1 OF THE 8 ATTACH RIVETS WAS ENGAGED IN THE COUNTERWEIGHT. SEIZURE OF THE RUDDER ASSY COULD OSDR CA110817005Control Wheel · broken(CAN) DURING STALL PRACTICE, VERY LITTLE AFT PRESSURE APPLIED TO CO-PILOT YOKE (AS PILOT WAS ALREADY APPLYING MOST OF THE PRESSURE), AND IT SNAPPED OFF. UPON RETURN FROM FLIGHT, TECH ON GROUND WAS ABLE TO SNAP BROKEN PIECE AGAIN WITH LITTLE FORCE. COPILOT CSDR 2011FA0000505Hinge · crackedNOTICED THAT UPPER LT DOOR HINGE HAD A CRACK IN IT WHERE IT ATTACHES TO THE FUSELAGE. THIS WAS THE SECOND PLANE SEEN WITH THIS PROBLEM.SDR 2011FA0000004Link · crackedTHE NOSE GEAR UPPER STRUT TORQUE LINK HAD 2 CRACKS (1CRACK ON EACH SIDE) OF THE LOWER SIDE NEAR TO THE UPPER ATTACH POINT. IN TRYING TO FIND THE OWNER AN AIRWORTHY SERVICEABLE 1, CONTACTED 7 MAJOR SALVAGE DEALERS IN THE USA. THESE DEALERS FOUND THE SAME TYPE SDR 2010FA0000196Solenoid · sticksBURNED ODOR OF ELECTRICAL COMPONENTS AFTER ENGINE START UP. SELECTED ACFT MASTER SWITCH OFF AND SHUTDOWN ENGINE. INSP REVEALED STARTER MOTOR HAD OVERHEATED. FURTHER EXAMINATION REVEALED STARTER SOLENOID HAD STUCK IN THE CLOSED POSITION DURING ENGINE START ASDR CA090813006Yoke · corrodedYOKE BROKE DURING WIND STORM. YOKE FOUND BORKEN AT THE BOTTOM PART DUE TO CORROSION (INSIDE TUBE).SDR 2007FA0001075Adapter · wornLT ELEVATOR TORQUE TUBE ARM ADAPTER RIVET HOLES WERE WORN POSSIBLY DUE TO UNSECURED CONTROLS IN GUSTY WINDS.SDR 2007FA0000592Cylinder · separatedCYLINDER BARREL SEPARATED APPROXIMATELY 2 NR ABOVE THE CYLINDER BASE FLANGE.SDR CA070216004Spacer · sheared(CAN) A RATTLE NOISE WAS HEARD AT ENGINE START. CLOSE INSP OF THE ENGINE MOUNT ASSY REVEALED ALL 4 MOUNT SPACERS, P/N 829, HAD SHEARED THEIR ATTACHMENT RIVET HEADS. THIS AC WAS MODIFIED IN THE PAST WITH 180HP CONVERSION. DISASSEMBLY REVEALED THE USE OF VERY SOSDR CA051221007Spar · crackedTHE STABILIZER FORWARD SPAR WAS CRACKED AND BUCKLED AT THE CENTER LIGHTENING HOLE. THERE WERE 2 SMALL CRACKS RADIATING OUTWARD. STABILIZER WAS REPAIRED AS PER CESSNA SEB94-8.SDR AUS20030983Exhaust Valve · sticking(AUS) ENGINE EXHAUST VALVE STUCK OPEN. TWO OTHER VALVES ALSO STICKING.DURING RECTIFICATION FOR THE STICKING VALVES IT WAS NOTICED THAT THE CARBURETTOR BUTTERFLY SHAFT TO BUSHING FITTING SEEMED EXCESSIVE (EXCESSIVE END FLOAT AND AXIAL WEAR).SDR 20010503CW005Door Frame · misinstalledFUEL LINES RUBBING AND STRESSED DUE TO UPPER OUTBOARD DOOR FRAME PARTIALLY COVERING HOLE AND NOT ALLOWING CLEARANCE FOR FUEL LINE. CAUSED BY THE HOLE IN DOOR FRAMES NOT BEING CUT OUT TO ORIGINAL SIZE FOR CLEARANCE BY MFG. RECOMMENDATION IS TO ROUND OUT HOLESSDR 20010503CW004Door Frame · misinstalledFUEL LINES RUBBING AND STRESSED DUE TO UPPER OUTBOARD DOOR FRAME PARTIALLY COVERING HOLE AND NOT ALLOWING CLEARANCE FOR FUEL LINE. CAUSE BY HOLE IN UPPER OB DOOR FRAMES NOT BEING CUT OUT TO ORIGINAL SIZE FOR CLEARANCE BY MFG. RECOMMENDATION IS TO ROUND OUT HSDR 99ZZZX961Bolt · brokenDURING ANNUAL INSPECTION DISCOVERD RT MAIN GEAR LEG LOOSE AND REAR NUT MISSING FROM U-BOLT AT GEAR ATTACH. REMOVED U-BOLT AND REPLACED WITH NEW BOLT, NUTS, AND WASHERS. APPEARED TO HAVE BROKEN JUST BEHIND NUT AS IF OVERTORQUED. RUST COVERED BREAK AREA. BOLSDR 98ZZZX1651Tank · broken weldWHILE MOVING AIRCRAFT A CLICKING SOUND WAS HEARD. AFTER LOOKING IN THE GAS CAP, A LARGE PART WAS FOUND SLIDING AROUND IN FUEL TANK. AFTER A CLOSER LOOK, FOUND BROKEN WELDS ON INTERNAL RIB OR BAFFLE. CAUSE WAS FUEL MOVEMENT IN TANK, AND RIB WAS ONLY WELDED OSDR 98ZZZX1650Tank · brokenWHILE MOVING AIRCRAFT A CLICKING SOUND WAS HEARD. AFTER LOOKING IN THE GAS CAP, A LARGE PART WAS FOUND SLIDING AROUND IN FUEL TANK. AFTER A CLOSER LOOK, FOUND BROKEN WELDS ON INTERNAL RIB OR BAFFLE. CAUSE WAS FUEL MOVEMENT IN TANK, AND RIB WAS ONLY WELDED OSDR AU980380Rocker Arm · broken(AUS) NR 4 CYLINDER INLET VALVE ROCKER ARM BROKEN AND PUSHROD BENT. PART TC: 3,090.SDR 98ZZZX992Actuator · corrodedDURING ROUTINE ANNUAL, TRIM ACTUATOR WAS FOUND ALMOST COMPLETELY STRIPPED. DUE TO CORROSION VERY FEW THREADS REMAINED INSIDE ACTUATOR. AIRCRAFT HAD BEEN ON F LOATS MOST OF ITS LIFE.SDR 97ZZZX4033Wheel · brokeCOPILOT'S CONTROL WHEEL BROKE APPROXIMATELY IN HALF WITH THE OUTBOARD HALF SEPARATING FROM THE INBOARD. THE INBOARD HALF REMAINED ATTACHED TO THE TUBE. THIS HAPPENED WHEN THE INSTRUCTOR WAS CORRECTING THE PILOT'S CROSS-WIND LANDING TECHNIQUE. THE LAST ANNUASDR 96ZZZX3678Piston · crackedDURING SCHEDULED OIL CHANGE, OWNER REQUESTED A COMPRESSION CHECK BE DONE. NR 1 CYLINDER WAS LOW AT 28/80. FURTHER INVESTIGATION REVEALED THE FOLLOWING: PISTON CRACKED FROM SKIRT TO FACE AT 6:00 O'CLOCK POSITION. TOP COMPRESSION RING BROKEN AND CYLINDER WALSDR CA960131201Line · abraided(CAN)UPPER ELEVATOR CABLE ABRAIDED THE ALUMINUM BRAKE LINE. REPAIRED AND AIRCRAFT RETURNED TO SERVICE.SDR CA960311009Torque Tube · corroded saddle(CAN)DURING A 100 HOUR INSPECTION WHITE RESIDUE WAS NOTED ON THE RIGHT HAND RUDDER BAR SADDLE. UPON REMOVAL THE SADDLE HALVES WERE FOUND TO BE CORRODED. THE SUPPORTING STRUCTURE, FIG. 31 #34 CESSNA 172 PAR TS MANUAL, WAS ALSO FOUND CORRODED.SDR 95ZZZX6013Guide · defectivePILOT REPORTED ENGINE RUNNING ROUGH. COMPRESSION CHECK CYLINDERS, ALL 70/80 OR BETTER. SPARK PLUG INSPECTION SHOWED NR 2 CYLINDER NOT FIRING PROPERLY. FOUND NR 2 EXHAUST VALVE STICKING. REAMED GUIDE AND RETURNED TO SERVICE.SDR 95ZZZX2639Support Assy · crackedSUPPORT ASSY IS A 'Y' SHAPED SUPPORT THAT TRANSFERS LOADS FROM THE CONTROL LOCK COLLAR TO THE FIREWALL. THESE LOADS ARE IMPOSED WHEN THE CONTROL LOCK IS INSTALLED AND THE AIRCRAFT IS PARKED DOWNWIND IN STRONG WINDS. A CLUE IS CRACKS IN THE FIREWALL FORWARD
Back to Cessna 172E