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 CA131008013Controller · failed(CAN) CARBURETOR HEAT CONTROL FAILED DURING GROUND RUN UP.SDR CA131003003Control Cable · frayed(CAN) 2 STRANDS BROKEN ON AFT ELEVATOR CABLE AT AFT PULLEY LOCATION.SDR CA130923007Wire · loose(CAN) PTT SWITCH WIRING CRIMP FOUND TO BE LOOSE. CONNECTION RECRIMPED.SDR FAA2014022000093Screw · looseDURING ROUTINE INSPECTION, DISCOVERED LEFT MAGNETO TIMING TO BE ADVANCED 6 DEGREES BEYOND SPECIFICATION. REMOVED MAGNETO TO RESET INTERNAL TIMING AND DISCOVERED HOLD DOWN SCREW LOOSE. THIS WAS THE FIRST MAGNETO TIMING INSPECTION PERFORMED SINCE THE INITIAL SDR 2013FA0000510Lifter · spalledINSPECTED FILTER DURING ROUTINE OIL CHANGE, FOUND EXCESSIVE FERROUS METAL. DISCUSSION WITH O/H FACILITY CAUSED US TO REMOVE LIFTERS FOR INSPECTION. FOUND 7 OF 8 LIFTERS WITH DAMAGE. SUBSEQUENT DISASSEMBLY OF THE ENGINE REVEALED THE CAMSHAFT WAS ALSO DAMAGEDSDR CA130918014Oil System · overpressured(CAN) ENGINE FOUND TO HAVE EXTREME LOW OIL PRESSURE WITH EXTREME HIGH OIL TEMP ON INTIAL POST ENGINE INSTALLATION. ENGINE RUN-UP WITH A NEW REFURBISHED O-320-H2AD.SDR CA130822008Switch · stuck(CAN) FLAP UP-LIMIT MICROSWITCH FOUND STUCK CLOSED DUE TO ACCUMULATION OF GREASE ON SWITCH. SWITCH CLEANED AND FUNCTION CHECKED SERVICEABLE.SDR CA130702012O-Ring · damaged(CAN) ACFT HAS EXPERIENCED 2 FLAT NOSE OLEOS. IN BOTH CASES, THE O-RINGS WERE ROLLED AND EXPERIENCED A FAILURE IN A SPIRAL PLANE. THE O-RINGS WERE PROCURED AS PART OF SEAL KIT SK172-1F. IT IS UNUSUAL IN OUR FLEET TO SEE A FAILURE IN THIS MANNER, PARTICULARLYSDR 2013FA0000352Retainer · failedAFTER DESCENDING TO 2,500 FT, EXPERIENCED A VIBRATION FOLLOWED BY PARTIAL POWER LOSS. DECLARED AN EMERGENCY. LANDED . MX DETERMINED THAT THE ENGINE EXPERIENCED A NR 2 CYLINDER FAILURE. CYLINDER EXHAUST VALVE SPRING RETAINER FAILED.SDR CA130509007Control Cable · broken(CAN) UPON ENGINE SHUTDOWN THE PILOT PULLED THE MIXTURE CONTROL CABLE TO IDLE CUT OFF. THE HANDLE OF THE CONTROL CABLE CONTINUED TO COME OUT FARTHER THAN EXPECTED. ACFT WAS SNAGGED. UPON INSPECTION THE INNER CABLE WAS FOUND TO BE BROKEN INSIDE THE PROTECTIVESDR CA130304010Seat Belt · malfunctioned(CAN) ON ROUTINE INSPECTION IT WAS FOUND THAT THE PILOT SIDE SECONDARY SEAT RESTRAINT, PN 505590-403 REEL ASSY OF SERVICE KIT SK210-174B WAS NOT LOCKING WHEN ENGAGED. ADJUSTMENT OF THE CABLE WAS CARRIED OUT IAW ICA AND STILL THE REEL WOULD NOT LOCK INTO PLACESDR CA130218005Door Frame · cracked(CAN) CRACK PROPAGATING FROM LOWER DOOR HINGE ATTACH SCREW. FOUND WHILE CARRYING OUT IAW 03-5 CABIN FORWARD DOOR POST INSPECTION.SDR CA130218004Arm · cracked(CAN) FOUND DURING A ROUTINE 200HR INSPECTION CRACKED ARM ASSY EXTENDING OUT FROM GREASE FITTING.SDR CA130115017Cable · broken(CAN) PILOT WAS ON APPROACH WHEN HE PULLED CARB HEAT. THE CONTROL CAME OUT TO A POINT WHERE HE COULD SEE IT WAS NOT ATTACHED AND BROKEN. IT WAS THEN PLACED BACK INTO THE HOLE. IT WAS REPORTED THAT HE DID NOT PULL EXCESSIVELY HARD ON IT AND WAS NOT BINDING BESDR CA130111003Bracket · damaged(CAN) THE CONTROL YOKE MAIN ATTACH BRACKETS PN 0513310-1 AND 0513310-2 IN THE CENTER CONSOLE STRUCTURE WERE FOUND TO HAVE THE MAIN PIVOT BOLT HOLES ELONGATED AND WORN CAUSING A FAIR BIT OF PLAY IN THE CONTROL YOKE ASSY.SDR 2013FA0000024Seal · leakingFRONT CRANKSHAFT OIL SEAL DETERMINED TO BE LEAKING, AND ALLOWING OIL TO DRIP INTO CABIN HEAT EXCHANGER ON MUFFLER, WHICH WAS THE SOURCE OF A SMOKE ODOR. SEAL REPLACED AND ACFT WAS GROUND RUN AND TEST FLOWN WITHOUT DISCREPANCIES.SDR CA121130006Bushing · worn(CAN) THE TWO BUSHINGS THAT SUPPORT THE UPPER SECTION OF THE FUEL SELECTOR SHAFT WERE FOUND WORN AND STARTING TO BREAK APART.SDR CA121130007Exhaust Valve · stuck(CAN) DURING ROUTINE ACFT INSPECTION THE NR 3 CYLINDER HAD A READING OF "0" ON A COMPRESSION LEAK DOWN CHECK. UPON FURTHER INSPECTION THE EXHAUST VALVE WAS STUCK IN THE OPEN POSITION. THE CYLINDER HAD APPROXIMATELY 700 HRS ON IT SINCE IT WAS LAST O/H WO 10-1SDR CA121126016Limit Switch · failed(CAN) UPON DAILY INSPECTION BY DISPATCH, FLAPS WOULD NOT EXTEND. NO MOVEMOVEMENT NOTED WHEN SELECTING FLAPS DOWN. ACFT TAKEN OUT OF SERVICE. MAINTENANCE PERSONAL DISCOVERED FAULTY LIMIT SWITCH DURING INSPECTION. REPLACED SWITCH WITH NEW PN S1906-1. FUNCTSDR CA121121006Cylinder · damaged(CAN) PILOT REPORTED ROUGH RUNNING ENGINE. RETURNED FOR LANDING. ACFT RUN UP AND INSPECTED ON NOV 19, 2012. ENGINE RAN ROUGH ON RUN UP BY MAINTENANCE PERSONAL. UPON INSPECTION -NR 3 PUSHROD TUBE WAS BENT. NR 3 EXHAUST VALVE STUCK OPEN. CYLINDER REMOVED FOR SDR CA121018003Bearing · cracked(CAN) RUDDER PEDALS BEARING HALF FOUND CRACKED, PROABLE CAUSE FROM EXCESSIVE BRAKING OR RUDDER TRAVEL. REPLACED WITH NEW, NO OTHER DAMAGE FOUND UPON INSPECTION.SDR CA121016005Flange · broken(CAN) EXHAUST FLANGE BROKEN IN HALF.SDR CA121004002Tube · detached(CAN) POWER COULD NOT BE REDUCED BELOW 2000 RPM IN FLIGHT. WORKED OK AFTER LANDING. ACCELERATOR PUMP TUBE WAS FOUND LAYING IN THE AIRBOX. THROTTLE CABLE AND CARBURETOR REPLACED.SDR 2012FA0000602Circuit Breaker · inoperativeNOTED A CLICKING ACCOMPANIED BY AMMETER INDICATING A HEAVY DISCHARGE. PROBLEM ISOLATED TO A CIRCUIT BREAKER THAT WASN`T TRIPPING THE INDICATOR BUTTON AND WAS WORKING AS AN AUTO RESET BREAKER. A SHORT WAS LOCATED WITHIN THE ALREADY PLACARDED " INOP" ADF. THESDR 2012FA0000573Sending Unit · misinstalledFUEL SENDERS, SERVICED, LEAK FUEL THROUGH THE MOUNTING FLANGE, WHICH IS BOLTED, OUTSIDE OF TANK, TO THE TOP OF THE FUEL TANK.SDR CA120607001Spar · cracked(CAN) CRACK FOUND THROUGH THE FRONT SPAR AND CENTER SKIN WHERE THE HORIZONTAL SPAR ATTACHES TO THE FUSELAGE. THE SPAR HAD THE SPAR REINFORCING KIT INSTALLED AND IT STILL CRACKED THROUGH.SDR CA120322003Tube · punctured(CAN) NOSEWHEEL TIRE WENT FLAT DURING LANDING ROLLOUT. TUBE FOUND TO HAVE .5" CUT. TIRE INSPECTED AND NO OUTSIDE PUNCTURE OR INTERIOR OBJECT OR DEFECTS FOUND TO CAUSE PROBLEM.SDR 2012FA0000211Pawl · looseTRIED TO START ACFT, PROP WOULD TURN BUT IMPULSE COUPLING COULD NOT BE HEARD SNAPPING. REMOVED LEFT MAGNETO AND FOUND THAT THE RIVET HOLDING ONE OF THE PAWLS HAD BROKEN OFF AND THE PAWL WAS BEATING THE EDGE OF THE MAGNETO, DESTROYING THE LIP. THERE WAS ALSDR 2012FA0000212Sleeve · mismanufacturedFUEL LEAK OCCURED AT RIGHT AFT FUEL TANK OUTLET FITTING FUEL LINE FLARED FITTING JOINT. FUEL LINE WAS MANUFACTURED WITH A DEFECTIVE SLEEVE WITH A SHOULDER OF .045" AS OPPOSED TO THE STANDARD DIMMENSION OF .170. FOUND BACK OF FLARE CUT INTO AND NO LONGER ABLESDR CA120120007Unknown · odor(CAN) PILOTS DEFECT: AFTER LANDING ROLL OUT AND THE TAXI WAY. THE SMELL OF ELECTRICAL SMOKE WAS DETECTED. NOTHING WAS OBSERVED. INSPECTION C/O IN ENGINE COMPARTMENT, ALL ELECTRICAL WIRES, ALTERNATOR, STAERTER, BATTERY AND COMPNOENTS, ELECTRICAL WIRES AND COMPOSDR CA120105010Indicator · inoperative(CAN) WARNING FLAG NOT IN VIEW - GYRO NOT SPINNING. NO INDICATION OF TURN.SDR CA111223006Stud · broken(CAN) ENGINE HAD A SUDDEN LOSS OF POWER. ACFT DIVERTED & LANDED SAFELY. UPON INSPECTION THE ENGINE NR 2 CYLINDER INTAKE VALVE RETAINING STUD WAS FOUND BROKEN. CYLINDER INTERIOR INSPECTED W/BOROSCOPE & NO FAULTS FOUND. CYLINDER VALVE DRIVE TRAIN INSPECTED & NOSDR CA111208009Skin · damaged(CAN) ON PREFIGHT WALKAROUND, PILOT DISCOVERED THE RT FLAP TOP CENTER SKIN TO BE TORN WHERE THE CONTROL ROD ATTACHES TO THE FLAP BRACKET.SDR CA111201008Tube · split(CAN) AS ACFT TAXIED OUT FOR A TRAINING FLIGHT THE RT TIRE WENT FLAT. UPON REMOVAL OF TIRE AND TUBE IT WAS FOUND THAT THE TUBE HAD A .5" LONG SPLIT IN IT. NO FOREIGN OBJECTS FOUND IN TIRE. THIS HAS BEEN AN ONGOING PROBLEM IN THE LAST FEW YEARS AS THE TUBES SDR CA111118017Skin · damaged(CAN) DURING A PRE-FLIGHT INSPECTION, PILOT NOTICED ELEVATOR BINDING WHEN ELEVATOR FULL NOSE DOWN. CONSIDERABLE FORCE WAS NECESSARY TO FREE THE ELEVATOR. FLIGHT CANCELLED, ACFT SENT FOR INVESTIGATION. AMO REPORTED TWO TEMP RIVETS BINDING ON HS SKIN WHEN ELESDR IQJ2012F00000Cylinder Head · crackedCYLINDER HEAD CRACKED, CAUSED AN ENGINE POWER REDUCTION ON TAKEOFF: A SUCCESSFUL RETURN TO AIRPORT AND LANDING WAS ACCOMPLISHED. VISIBLE IN COMBUSTION CHAMBER FROM .3750: BELOW INTAKE VALVE, CLOCKWISE THROUGH LOWER SPARK PLUG, AROUND OUTSIDE OF EXHAUST VALVE SDR CA111117005Bulkhead · cracked(CAN) CRACKS FOUND AT PROPELLER BOLT HOLES.SDR CA110928012Ignition Switch · shorted(CAN) ACFT WAS SHUTDOWN IAW CHECKLIST. ON RESTART, THE MASTER SWITCH WAS TURNED ON AND THE ACFT ENGINE STARTED TO TURN OVER WITHOUT TURNING THE THE IGNITION KEY TO START POSITION. MASTER WAS IMMEDIATELY TURNED OFF AND STARTER DISENGAGED. INTERNAL PARTS OF SSDR CA110920011Engine · making metal(CAN) ON 100HR SCHEDULED INSPECTION, METAL DEBRIS FOUND IN OIL FILTER. ON FURTHER INSPECTION, SCORING FOUND ON CAMSHAFT AND LIFTER "MISSING A CHUNK (OF METAL)". ACFT REMOVED FROM SERVICE, ENGINE REMOVED FROM AIRFRAME AND SENT FOR MAJOR O/H.SDR CA110823003Control Cable · separated(CAN) THE ACFT WAS BEING GROUND RUN BEFORE A FLIGHT AND WHEN CHECKING CARBURETOR HEAT OPERATION, THE PILOT PULLED THE CONTROL TO THE "ON" POSITION. AT THIS POINT THE CONTROL FELT VERY LOOSE AND THE PILOT THEN REALIZED THAT THE CABLE HAD FAILED AS THE SEPARATEDSDR CA110810007Switch · failedTHE LANDING LIGHT SWITCH WAS REPORTED TO BE STUCK IN THE "ON" POSITION DURING A PRE-FLIGHT INSPECTION OF THE ACFT. THE SWITCH WAS REPLACED AND THE ASSOCIATED WIRING CHECKED FOR CONDITION. GROUND TEST CHECKED SERVICEABLE. THIS TYPE OF SWITCH IS SUBJECT TO A SDR 2011FA0000429Pushrod · brokenCYLINDER NR3 EXHAUST VALVE PUSH ROD BROKEN, DUE TO A STUCK VALVE IN THE CLOSED POSITION. THE VALVE WAS NOT STUCK AT THE TIME OF THE
INVESTIGATION. NO MARKS WERE SEEN ON THE TOP OF THE PISTON AS VIEWED THROUGH A BORESCOPE. THE SPARK PLUGS HAD ONLY SLIGHT BLASDR 2011FA0000428Pushrod · brokenCYLINDER NR 3 EXHAUST VALVE PUSH ROD BROKE, DUE TO A STUCK VALVE IN THE CLOSED POSITION. THE VALVE WAS NOT STUCK AT THE TIME OF THE INVESTIGATION. NO MARKS WERE SEEN ON THE TOP OF THE PISTON AS VIEWED THROUGH A BORESCOPE. THE SPARK PLUGS HAD ONLY SLIGHT BLASDR CA110609005Tube · splitACFT WAS PARKED ON RAMP AFTER FLIGHT AND A COUPLE HOURS LATER A PASSING PILOT NOTICED THE NOSE TIRE COMPLETELY FLAT. MX REMOVED THE TIRE AND DISCOVERED THAT THE TUBE HAD A 1" LONG SPLIT IN IT. THIS HAS BEEN A COMMON OCCURRENCE ON THIS SIZE OF TUBE OVER THE LASDR CA110531009Retainer · failedDURING A WALKAROUND THE PILOT NOTICED AN ODD NOSEWHEEL WOBBLE. UPON INSP BY THE AMO, IT WAS DISCOVERED THAT THE INNER BEARING RACE RETAINER ON 1 OF THE WHEEL HALVES HAD CRACKED FREE, ALLOWING THE RACE, BEARING, SEALS AND RINGS TO FALL INTO THE INTERIOR OF THE SDR CA110329008Radio · inoperative(CAN) AFTER ENGINE START PILOT WENT TO TURN ON AVIONICS MASTER THE MASTER WOULD NOT WORK, RADIO WOULD NOT COME ALIVE. ENGINE SHUTDOWN FLIGHT WAS CANCELED.SDR CA110322006Rotor · broken(CAN) MAG WAS RECEIVED FOR WARRANTY PURPOSES AS IT FAILED IN SERVICE. MAG WAS OPENED UP & THE NYLON ROTOR GEAR, CAM & 2 TANGS OF THE ROTOR WERE FOUND ASSEMBLED BUT BROKEN AWAY FROM THE ROTOR SHAFT. WHILE INSPECTING THE DISTRIBUTOR BLOCK & GEAR ASSEMBLY IT WASDR CA110321011Magneto · failed(CAN) THE PILOT ELECTED TO CARRY OUT A MAGNETO CHECK IN CRUISE FLIGHT. A 200 RPM DROP WAS THE RESULT. THE PILOT ELECTED TO RETURN TO BASE. MAINTENANCE REMOVED THE MAGNETO AND RETURNED IT TO THE MFG FOR WARRANTY. A STRIP REPORT HAS BEEN REQUESTED AND WILL BSDR CA110323005Magneto · failed(CAN) PILOT EXPERIENCED ENG VIBRATION DURING CLIMB OUT & ELECTED TO CARRY OUT A MAGNETO CHECK. THE NR 2 RT MAGNETO FAILED COMPLETELY. THE PILOT ELECTED TO RETURN TO BASE. MX CONFIRMED THE FAILURE & REMOVED THE MAGNETO FOR RETURN TO THE MFG FOR WARRANTY. A SDR CA110216006Rotor · broken(CAN) CUSTOMER REPORTED MAG DEAD. WHEN INSPECTED FOR WARRANTY RETURN THE DISTRIBUTOR GEAR DID NOT TURN WHEN THE MAGNETO ROTOR WAS TURNED. THIS INDICATES THE ROTOR IS PROBABLY BROKEN AT THE CAM SLOT LOCATION. SEE SDR 20110209025 FOR SIMILAR PROBLEM WITH ANOTHER
Back to Cessna 172N