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 = '172N' 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 = '172N' 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 96ZZZX5345Gauge · failedOUT OF BOX FAILURE OF LT FUEL GAUGE. NEED SOME QUALITY CONTROL. ROCHESTER, P/N 6247-00133.SDR 97ZZZX828Discharge Tube · detachedCARBURETOR PUMP DISCHARGE TUBE ASSY CAME ADRIFT INGESTING IN ENGINE, KNOCKING LOOSE THE SOLID COMBUSTION PARTICLES IN THE COMBUSTION CHAMBER WHICH FOULED A NUMBER OF THE SPARK PLUGS SIMULTANEOUSLY LOSING 50 PERCENT OR MORE OF THE POWER. BEING NEXT TO THE AIRSSDR 96ZZZX5312Magneto · excess wearAFTER INSTALLING A FACTORY REBUILT 3000 SERIES, MAGNETO AIRCRAFT WAS PLACED BACK ON RENTAL STATUS ON 9-27-96, A FLIGHT INSTRUCTOR NOTICED TAKEOFF POWER WAS DOWN BY APPROXIMATELY 200 RPM AT FULL THROTTLE. MAINTENANCE INVESTIGATION REVEALED BOTH SETS OF MAGNETOSDR 96ZZZX5226Valve · stem failedPRECAUTIONARY LANDING MADE DUE TO POWER LOSS AND FLUCTUATING OIL PRESSURE. ENGINE WOULD MAINTAIN 1,800 RPM, AT FULL THROTTLE. NR 3 CYLINDER EXHAUST VALVE FAILED JUST ABOVE HEAD/STEM RADIUS. SECONDARY CYLINDER AND PISTON DAMAGE REMNENTS OF VALVE FOUND IN MUFSDR 96ZZZX5311Magneto · failedDURING CRUISE FLIGHT, ENGINE STOPPED PRODUCING POWER. AN OFF-AIRPORT LANDING MADE WITHOUT INCIDENT. MAINTENANCE INSPECTION REVEALED BOTH SETS OF POINTS IN THE DUAL 2000 SERIES MAGNETO HAD CLOSED CAUSING ENG TO STOP. POINTS WERE RESET AND ENG RAN AND PRODUCESDR 96ZZZX5015Mount · defectiveAFTER ORDERING LORD MOUNTS J-9613-49 FOR REPLACMENT OF CESSNA 172N ENGINE, BARRY MOUNTS WERE AUTOMATICALLY SUBSTITUTED BY THE SUPPLIER. SUBMITTER STATED ALTHOUGH THESE ARE APPROVED BY FAA, THEY DO LACK THE CENTER (DAMPER BAG) AND CESSNA RECOMMENDS NOT DOING WSDR CA961003002Alternator · failed(CAN) THE AIRCRAFT RETURNED WITH A DEAD BATTERY. THE ALTERNATOR WAS FOUND TO HAVE NO OUTPUT. ALTERNATOR REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR 96ZZZX4148Bearing · failedMAGNETO POINTS WERE NOT OPENING DUE TO EXCESSIVE WEAR ON THE POINTS' CAM FOLLOWER. THIS WEAR WAS ACCELERATED BY A HEAT BUILD-UP ON THE MAGNETO SHAFT GENERATED BY A FAILED REAR BEARING.SDR CA960826092Spar · cracked(CAN) DURING INSPECTION A CRACK WAS DETECTED IN THE CENTRE OF THE SPAR. SPAR WAS REPLACED. CRACKED DETECTED WAS APPROXIMATELY 1 INCH LONG.SDR AU961106Engine · rough running(AUS) ENGINE RAN ROUGH FOR SEVERAL SECONDS - SUSPECT FUEL PROBLEM - INVESTIGATION COULD FIND NO CAUSE AND THERE WAS NO REPETITION OF THE PROBLEMSDR CA960826097Stud · broken(CAN) DURING FLIGHT ENGINE STARTED TO RUN ROUGH. ENGINE POWER REDUCED AND AIRCRAFT LANDED ON HIGHWAY. GROUND INSPECTION FOUND #4 CYLINDER EXHAUST ROCKER STUD BROKE ALLOWING THE ROCKER ARM AND STUD TO FALL INTO THE BOTTOM OF THE ROCKER COVER. THIS RESTRICTED THSDR 96ZZZX3884Starter · screws strippedTHREE OF FOUR FORWARD CAP SCREWS HOLDING STARTER MOTOR TO GEARBOX HOUSING THE BENDIX - STRIPPED.SDR 96ZZZX3694Case · crackedLEFT CASE CRACKED BELOW NR 2 CYLINDER BASE. CRACK WAS ABOUT 2.5 INCHES LONG.SDR 96ZZZX3763Crankcase · crackedRIGHT CRANKCASE CRACKED BELOW NR 1 CYLINDER BASE. CRACK WAS APPROXIMATELY 6 INCHES LONG. CASE WAS NOT REPAIRABLE.SDR AU960935Spar · cracked(AUS) TAILPLANE FORWARD SPAR AND CENTRE SKIN CRACKED - FOUND DURING INSPECTION IAW AD/C170/59SDR AU960971Switch · burnt(AUS) ENGINE IGNITION SWITCH CONTACT CUPS (3OFF) PNO A-1196-A AND TERMINAL BOARD PNO A-546-A WORN AND BURNT - FOUND DURING INSPECTION IAW AD/ELEC/59 AMDT1SDR AU960858Connecting Rod · failed(AUS) NO3 CYLINDER CONNECTING ROD FAILED IN AREA APPROXIMATELY HALF WAY BETWEEN THE BIG END AND THE GUDGEON PIN BUSHING - FAILURE INVESTIGATION FOUND EVIDENCE OF A PRE-EXISTING FLAW IN THE PISTON PIN BEARING HOUSING WHICH WAS HEAVILY OXIDISEDSDR 96ZZZX3077Cylinder · defectiveROCKER STUD BACKED OUT CAUSING EXCESSIVE VALVE CLEARANCE WHICH CAUSED THE PUSHROD TO GET JAMMED AND BENT. CYLINDER WAS IN C/W SB 412B (AD 77-20-07) WHICH REQUIRES STUDS TO BE LOCKTITE INTO POSITION. CYLINDER WAS MARKED IAW THIS PROCEDURE. SUBMITTER SUGGESTSSDR 96ZZZX4750Starter · armature openSTARTER REMOVED DUE TO OPEN IN ARMATURE. FOUND WIRE WINDINGS OF ARMATURE ON DRIVE END WERE POTTED WITH MATERIAL RESEMBLING BODY PUTTY TO INSULATE THE WIRES. ALSO, A PIECE OF A CARDBOARD BOX WAS INSERTED BETWEEN THE COPPER FIELD LEAD AND THE CASE FOR INSULATISDR 96ZZZX3358Venturi · fracturedDURING INSPECTION FOR OVERHAUL, VENTURI WAS FOUND BROKEN AT 3 SUPPORT LEGS AT CENTER OF THE VENTURI.SDR AU960504Distributor · damaged(AUS) MAGNETO RH SIDE DISTRIBUTOR GEAR BUSHING LOOSE CAUSING DAMAGE TO THE GEAR SHAFT - MAGNETO CAPACITOR OPEN CIRCUITEDSDR AU960469Clamp · faulty(AUS) DUAL MAGNETO RETAINING CLAMP ALLOWED MAGNETO TO ROTATE ON THE MOUNTINGSDR CA960418015Breaker Points · worn(CAN)ON THE 100 HOUR INSPECTION, BOTH MAGNETOS HAD BEEN CHECKED FOR CONDITION AND TIMING AS CALLED FOR IN THE CESSNA INSPECTION PROGRAM AND A POST INSPECTION RUN-UP DONE WITH ALL ENGINE PARAMETERS FOUND NORMAL. ON THE FIRST FLIGHT AFTER INSPECTION, A POWER LOSSDR AU960434Carburettor · faulty(AUS) CARBURETTOR FAULTY - SUSPECT TEMPORARY CONTAMINATION OR INTERMITTENT FAILURE COMBINED WITH NON FIRING OF NO4 CYLINDERCAUSED ROUGH RUNNING ENGINE - CARBURETTOR ICING WAS DISMISSED AS THE CAUSESDR CA960412002Gear · sheared teeth(CAN)IN CRUISE, ENGINE SUDDENLY RAN ROUGH AND RPM DROPPED. MAG CHECK INDICATED LEFT MAG DEAD. MAGNETO REMOVED FOR TEST. PLASTIC GEAR HAD 12 TEETH SHEARED OFF. THIS MAG HAD BEEN OVERHAULED BY REPAIR STATIONUT2R226L.SDR 96ZZZX2064Contact Assy · looseENGINE FAILED TO MAKE FULL STATIC RPM ON GROUND. UPON FURTHER INSPECTION, IT WAS DETERMINED TO BE A MAGNETO PROBLEM. UPON OPENING MAG COVER, BOTH SETS OF CONTACTS WERE FOUND TO BE LOOSE. THE CONTACT ASSY SCREW (NOT MOUNTING SCREWS) WERE DETERMINED TO BE LOOSDR 96ZZZX1778Bulkhead · crackedDURING AN ANNUAL INSPECTION, THE LOWER REAR CABIN DOORPOST BULKHEAD WAS FOUND CRACKED ON THE LEFT AND RIGHT SIDES AT THE POINT WHERE THE CABIN FLOOR AND BULKHEAD MEET. THE CRACK BEGINS AT A RADIUS RELIEF POINT AND PROPAGATES TO THE UPPER MOUNTING HOLE OF THE SDR AU960348Line · separated(AUS) PITOT SYSTEM PRESSURE LINE SEPARATED FROM CONNECTION TO HOURMETER AIRSPEED SWITCH - SUSPECT LINE DISCONNECTED DURING REFITMENT OF TACH INDICATOR DURING AD/INST/9 CALIBRATION CHECK WHICH WAS CARRIED OUT FOLLOWING PITOT/STATIC CALIBRATION CHECKSDR AU960266Hub · corroded(AUS) WHEEL HUB CORRODED - THREADS STRIPPED ALLOWING WHEEL FLANGE AND TYRE TO SEPARATE FROM HUBSDR CA960429003Valve Cover · worn(CAN) AIRCRAFT LOST POWER ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED. WHEN THE FUEL SELECTOR WAS MOVED THE POWER WAS RESTORED. INSPECTION OF THE VALVE SHOWED WEAR TRACKS BETWEEN THE DETENT LOCKING HOLES SO THAT POSITIONING OF THE SELECTOR HANDLE WAS NOT IN THE PSDR CA960429004Exhaust Valve · sticking(CAN)PERFORMING CESSNA SEB92-21 (LYC SB388B), #4 CYLINDER EXHAUST VALVE TO GUIDE CLEARANCE BELOW SPECIFIED. REWORKED IN ACCORDANCE WITH LYCOMING SI 1425. SB WAS NOT DUE FOR ANOTHER 170 HOURS.SDR 96ZZZX1772Vent Line · deterioratedFUEL VENT LINE CONNECTING HOSES DETERIORATED TO THE POINT OF LEAKAGE OF FUEL IN THE WING ROOT AREA. ALL 3 HOSES ON BOTH SIDES NEEDED REPLACING DUE TO AGE.SDR 96ZZZX1710Geartooth · brokenREMOVED MAGNETO DUE TO ROUGH ENGINE. FOUND A TOOTH BROKEN OFF OF LEFT DISTRIBUTOR GEAR. MAGNETO WAS ON A LYCOMING FACTORY OVERHAUL. MAGNETO WAS OVERHAULED BY ELECTRO SYSTEMS, INC.SDR 96ZZZX853Clamp Nut · missingRIGHT MAGNETO TOP ATTACHMENT MISSING. CLAMP, 66M21195. WASHER, STD-475. WASHER, STD-1727. NUT, STD-1410. RIGHT MAGNETO INSTALLED 10-12-95. TOTAL TIME 168 HOURS. ACFT TT 4,328.5 HOURS.SDR AU960389Door Post · cracked(AUS) LH AND RH DOOR POST CRACKED FROM RELIEF RADIUS AT FLOOR LEVEL TO HIGH SHEAR FASTENER HOLE ON LH POST AND EXTENDING APPROXIMATELY7.937MM (0.3125IN) PAST HIGH SHEAR FASTENER HOLE ON RH POST - MAXIMUM CRACK LENGTH OF 31.75MM (1.25IN) EXTENDING OUTBOARD FROSDR AU960039Door Post · cracked(AUS) AFT DOOR POST ASSEMBLY CRACKED IN AREA OF INNER RELIEF AT FS 65.3 TOWARDS OUTBOARD LANDING GEAR HOUSING FASTENERSSDR AU960038Brush · worn(AUS) ALTERNATOR BRUSHES WORN EXCESSIVELY - PIGTAIL JUNCTION WORN INTO SLIP RINGSDR CA960122021Spar · cracked(CAN)DURING THE PERFORMANCE OF SEB 94-8 THE FRONT SPAR OF THE HORIZONTAL STABILIZER WAS FOUND CRACKED AT THE LIGHTENING HOLE.SDR 96ZZZX371Line · loosePILOT REPORTED SMOKE IN COCKPIT AFTER APPLYING CABIN HEAT. REMOVED COWLING AND INSPECTED MUFFLER ASSEMBLY. SMALL OIL STAIN ON MUFFLER SHROWD. FOUND OIL RETURN LINES WERE SLIGHTLY 'WET' WITH OIL. TIGHTENED OIL RETURN LINE CLAMPS. WASHED DOWN ENGINE AND MUFSDR 97ZZZX3333Magneto · teeth shearedTEETH ON DISTRIBUTOR GEAR WERE SHEARED CAUSING A SEVERE MAG DROP ON LEFT MAGNETO SIDE. CAUSE UNKNOWN. A MAGNETO LOCKING TOOL WAS NOT USED DURING INSTALLATIONS AFTER AD COMPLIANCES. THIS IS A SINGLE POINT DUAL MAGNETO.SDR 97ZZZX3328Magneto · teeth strippedTEETH ON DISTRIBUTOR GEAR WERE SHEARED CAUSING A VERY SEVERE MAG DROP ON RIGHT MAGNETO SIDE. A MAGNETO LOCKING TOOL WAS NOT USED DURING INSTALLATIONS AFTER AD CHECKS. THIS IS A SINGLE POINT DUAL MAGNETO.SDR 96ZZZX84Regulator · wire detachedFIELD WIRE SEPARATED FROM CONNECTOR PLUG ON THE ALTERNATOR CONTROL UNIT. SUSPECT CAUSE - VIBRATION AND FATIGUE ON WIRE.SDR CA951221030Collar · broken(CAN)DURING ROUTINE MAINTENANCE FOUND CRACKED COLLAR ON THE NOSE GEAR. REMOVED STEERING COLLAR AND FOUND BROKEN BEARING. REPLACED PARTS AND RETURNED AIRCRAFT TO SERVICE.SDR 96ZZZX81Plate · corrodedSPAR CAP ANGLE EXHIBITED INTERGRANULAR CORROSION IN SEVERAL LOCATIONS ALONG ITS LENGTH AND AFFECTED THE DOUBLER PLATE AT THE POINTS WHERE THE CORROSION CONTACTED. SUBMITTER STATED THIS INTERGRANULAR CORROSION IS DISPLAYING SIGNS OF PRESENCE IN THE LT SPAR CAPSDR 96ZZZX80Angle · corrodedSPAR CAP ANGLE EXHIBITED INTERGRANULAR CORROSION IN SEVERAL LOCATIONS ALONG ITS LENGTH AND AFFECTED THE DOUBLER PLATE AT THE POINTS WHERE THE CORROSION CONTACTED. SUBMITTER STATED THIS INTERGRANULAR CORROSION IS DISPLAYING SIGNS OF PRESENCE IN THE LT SPAR CAPSDR 96ZZZX79Angle · corrodedSPAR CAP ANGLE EXHIBITED SEVERE INNER CORROSION IN 2 LOCATIONS AND MODERATE INTERGRANULAR CORROSION IN SEVEREAL OTHER LOCATIONS. CORROSION AFFECTED THE DOUBLER PLATE WHERE THE POINT OF CORROSION CONTACTED.SDR 95ZZZX6573Valve · stuckSOME POWER LOSS WAS NOTED AFTER TAKEOFF WHEN EXHAUST VALVE STUCK. SUBMITTER SUGGESTS LYCOMING SERVICE BULLETINS BE COMPLIED WITH.SDR CA951120013Valve Guide · cracked(CAN) DURING DIFFERENTIAL COMPRESSION CHECK IT WAS FOUND THAT NR 3 CYLINDER HAD A SEVERE EXHAUST LEAK (20/80). AFTER REMOVAL AND INSPECTION OF THE NR 3 CYLINDER IT WAS REVEALED THAT THE EXHAUST VALVE GUIDE WAS CRACKED AND BADLY WORN AS A RESULT OF THE LONGITUSDR 95ZZZX6176Stabilizer · corrodedDURING THE ANNUAL INSPECTION, THE HORIZONTAL STABILIZER ASSEMBLY WAS FOUND CORRODED BEYOND ECONOMICAL REPAIR LIMITS. INTERNAL PORTION OF STABILIZER ASSY IS VERY DIFFICULT TO INSPECT WITH THE ELEVATOR ASSY INSTALLED. SUBMITTER RECOMMENDS EXTRA EFFORT TO THOROSDR 95ZZZX6441Spar · crackedFOUND 3 CRACKS AT LIGHTENING HOLE IN FRONT SPAR OF HORIZONTAL STABILIZER (CENTER SECTION), APPROXIMATELY .75 INCH EACH. SUSPECT CAUSE - IMPROPER GROUND HANDLING. RECOMMENDATION - USE TOW BAR.
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