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 = '172M' 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 = '172M' 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 YAA2012F00000Crankshaft · brokenCRANKSHAFT BROKE IN FLIGHT AND PROPELLER DEPARTED ENGINE.SDR CA130115013Seat · cracked(CAN) UPON INSPECTION OF PILOT SEAT, FOUND THAT INBD SEAT BASE SIDE HAS A CRACKED 1.25" LONG RADIATING FROM FORWARD SEAT ROLLER HOUSING ASSY UPPER AFT ATTACH SCREW HOLE. THE CRACK WAS HIDDEN BEHIND BY FORWARD SEAT ROLLER HOUSING ASSY WHICH WERE BEING REMOVED FSDR CA121023004Tube · worn(CAN) BALLJOINT, REF: SERVICE MANUAL, FIG 5-6 ITEMS 18 AND 19, ON LT STEERING TUBE SEPARATED WITH NUT AND COTTER PIN STILL IN PLACE RESULTING IN DIFFICULT TO NO NOSEWHEEL STEERING POSSIBLE.SDR CA121017009Nut · cracked(CAN) UPON INSPECTION, I NOTICED THE FWD VERTICAL FIN ATTACH HARDWARE, THAT THE NUT WAS CRACKED IN HALF ON ONE OF THE BOLTS. THE HARDWARE APPEARED TO BE THE ORIGINAL EQUIPMENT.SDR CA130301005Tappet · failed(CAN) O/H ON O-320-E2D WITH NEW CAM AND TAPPET BODIES. SMOKE IN EXHAUST AT TAXI WHEN ENGINE WARM. OIL IN INDUCTION. CYLINDERS HONED AND CROSS HATCHED, ASSUMED TO BE THE PROBLEM) SMOKE AND OIL PROBLEM. NEW CYLINDERS INSTALLED. SMOKE AND OIL PERSISTS. ENGINE RESDR CA121211011Bushing · loose(CAN) ELEVATOR BELLCRANK UPON INSPECTION FWD CENTER BEARING RETAINING BUSHING FOUND TO HAVE COME LOOSE IN ITS CRIMP WITH BLACK FRETTING PRESENT AROUND THE BUSHING. WITH SLIGHT FOR AND AFT MOTION OF THE CONTROL YOKE WITH ONE HAND WILL CAUSE 1 TO SEE THE LOOSESDR CA121212002Bushing · worn(CAN) UPON INSPECTION CONTROL TEE LOWER PIVOT POINT RETAINING BUSHING FOR PIVOT BEARING FOUND TO HAVE COME LOOSE IN ITS CRIMP WITH BLACK FRETTING PRESENT AROUND THE BUSHING. WITH SLIGHT FOR AND AFT MOTION OF THE CONTROL YOKE WITH 1 HAND WILL CAUSE ONE TO SEE TSDR CA120529012Exhaust Pipe · failed(CAN) WHILE ON LEVEL FLIGHT, THE PILOT OBSERVED A SUDDEN CHANGE IN THE SOUND WITH THE ENGINE`S EXHAUST. IT WAS LOUD, THEN BECAME LOUDER WITHIN A FEW SECONDS. AS A PRECAUTIONARY MEASURE, THE PILOT ELECTED TO CLIMB. THE INDIVIDUAL DETERMINED THAT THE ENGINE WAS SDR 2012FA0000305Brake Assy · crackedPART HAS A CRACK AT 1 OF THE BLEEDER PORTS. IT MAY HAVE BEEN FROM COMPONENT FAILURE, BUT IT MAY WELL HAVE BEEN CAUSED BY OVER-TIGHTENING.SDR CA120820001Seal · failed(CAN) THE CARBURETOR HEAT SEAL WAS PARTIALLY BROKEN CLOGGED THE VENTURI CARBURETOR RESULTING IN A RICHER MIXTURE AND A PARTIAL POWER LOSS.SDR CA120403008Tube · failed(CAN) UPON LANDING AND SETTING THE NOSE WHEEL DOWN, THE PILOT EXPERIENCED A VIBRATION IN THE RUDDER PEDALS/CONTROL COLUMN AND COULD NOT CONTROL THE DIRECTION OF THE ACFT. HE MANAGED TO STOP THE ACFT AT THE FAR LT OF THE RUNWAY CENTERLINE. HE INFORMED THE TOWSDR CA121212001Bushing · worn(CAN) UPON INSPECTION, CONTROL TEE LOWER PIVOT POINT RETAINING BUSHING FOR PIVOT BEARING FOUND TO HAVE COME LOOSE IN ITS CRIMP WITH BLACK FRETTING PRESENT AROUND THE BUSHING. WITH SLIGHT FOR AND AFT MOTION OF THE CONTROL YOKE WITH 1 HAND WILL CAUSE ONE TO SEESDR CA120228015Magneto · failed(CAN) AIRCRAFT RETURNED TO BASE AFTER RIGHT MAGNETO FAILED DURING PRETAKE OFF RUN UP. TROUBLESHOOTING WAS CONDUCTED AND FOUND THE MAGNETO TO HAVE COMPLETE FAILURE. MAGNETO RETURNED.SDR CA120215004Bracket · broken(CAN) ALTERNATOR BRACKET FOUND BROKEN ON ENGINE UNSCHEDULED INSPECTION. NEW REPLACEMENT BRACKET NR 07A-21443 INSTALLED. REPLACEMENT PART SUPPLIED BY MFG DISTRIBUTOR AS REPLACEMENT FOR NR 76906.SDR LHO2012F00000Gear · failedSTARTER MOTOR TURNS WITH NO BENDIX OUTPUT.SDR CA120127005Tube · failed(CAN) TUBE WENT FLAT DURING TAXI, INSPECTION OF TUBE SHOWS PIN HOLE IN RUBBER.SDR FK8R201110240001Bulkhead · crackedAFT SPINNER BULKHEAD CRACKED.SDR CA111025010Valve · stuck(CAN) THE ACFT HAD TO LAND BECAUSE OF LOSS OF ENGINE POWER AND HIGH VIBRATION. A STUCK VALVE AND BENT PUSH ROD WERE FOUND ON LT REAR CYLINDER (ENGINE WAS ON-CONDITION). CUSTOMER DECIDED TO REPLACED THE ENGINE, WITH AND O/H ONE. NO DAMAGE TO AIRCRAFT.SDR CA111003003Flap Track · sheared(CAN) THE FWD LOWEST HORIZONTAL RIVET ATTACHING THE RT WING INBD FLAP RAIL (PN 0523231-13) WAS FOUND TO BE SHEARED DURING INSPECTION. WITH SLIGHT UPWARDS PRESSURE ON THE FLAP, WITNESSED THE RIVET HEAD FLEX IN AN ABNORMAL WAY WITH SLIGHT MOVEMENT AND SHOWINGSDR CA110914005Switch · unserviceable(CAN) PILOT REPORTED ELECTRICAL FIRE SMOKE DETECTED WITH TRANSPONDER INOPERATIVE AND ELECTRICAL FIRE SMOKE DETECTED WHEN TRANSMITTING ON COMM 1. FURTHER DISCUSSION WITH PILOT DETERMINED THAT NO ACTUAL SMOKE WAS SEEN AND ONLY AN ELECTRICAL BURN ODOUR WAS DETECSDR CA110819004Cable · frayed(CAN) THE RT RUDDER CABLE WORN.SDR 2011FA0000516Exhaust Valve · brokenNR 3 ENGINE CYLINDER EXHAUST VALVE HEAD BROKE OFF INSIDE THE CYLINDER COMBUSTION CHAMBER. THIS HAPPEND AFTER TAKEOFF AND UPON REACHING 500 FEET. STC 2375SW AND SE3692SW WERE COMPLIED WITH ON THE ENGINE.SDR CA110729010Tube · failedACFT NOSE TIRE WENT FLAT TAXIING TO TAKEOFF POSITION, ACFT UNABLE TO MOVE, TOWED CLEAR OF RUNWAY. MX FOUND THE TUBE HAD LARGE CRACKS AND DETERIORATED RUBBER ON THE INSIDE CIRCUMFERENCE. THESE DETERIORATED SECTIONS APPEARED TO LINE UP WITH THE WHEEL SEAMS OF SDR FK8R201107190004Support Bracket · crackedAIRBOX FRONT SUPPORT BRACKET WAS FOUND CRACKED AT THE STARTER. THIS PART WAS REPLACED AT THE ANNUAL INSPECTION IN 2010.SDR CA110719012Muffler · leakingWHILE CARRYING OUT AD CF90-03-R2 PART 2- PRESSURE TEST- LARGE LEAKS WERE FOUND IN THE AREA SURROUNDING THE MUFFLER TAIL PIPE AREA UNDER THE STRUCTURE FOR SUPPORTING THE HEAT MUFF SHROUD. THE LEAKS WERE COMING FROM UNDER THIS SUPPORT STUCTURE AND NO DEFECTS WESDR CA110608007Bolt · brokenPILOT REPORTED RT BRAKE INOPERATIVE. INSPECTED BRAKE AND FOUND LOWER BACKING PLATE BOLT BROKEN AT THREADS ALLOWING BACKING PLATE TO PIVOT. SUSPECT CALIPER PINS HAD FOULED, CAUSING CALIPER TO SEIZE AND EXCESSIVE LOAD ON BOLTS. REMOVED CALIPER AND INSPECTED FSDR 2011FA0000322Spring · brokenUPON INVESTIGATING AN OIL LEAK ON NR 3 CYLINDER, REMOVED VALVE COVER AND FOUND BROKEN PUSH ROD TUBE SPRING, ALLOWING PUSH ROD TO BACK OUT OF SEALING POSITION. REMOVED ALL VALVE COVERS AND FOUND ALL PUSH ROD TUBE SPRINGS BROKEN. THIS REALLLY NEEDS TO BE ADDRESDR CA130116003Bulkhead · cracked(CAN) UPON ROUTINE INSPECTION OF THE PROPELLER AND SPINNER. IT WAS NOTICED UPON REMOVAL OF THE SPINNER THAT THE FORWARD SPINNER BULKHEAD HAD 2 CRACKS IN THE AREA AROUND THE CIRCUMFERENCE OF 2 SEPARATE PROPELLER MOUNTING BOLT HOLES. FORWARD SPINNER BULKHEAD RSDR CA110419001Bolt · cracked(CAN) UPON INSPECTION, THE MLG LEGS SEEMED TO MAKE A CREAKING SOUND WHEN MOVED FORWARD AND AFT. THE ACFT WAS JACKED UP AND THE LANDING GEAR ATTACH BOLTS WERE REMOVED AND INSPECTED. BOTH BOLTS WERE FOUND CRACKED AT THE POINT WERE THEY GO THROUGH THE GEAR ATTASDR CA110414010Grounding Strap · cracked(CAN) AIRCRAFT EXPERIENCED INTERMITTENT ELECTRICAL FAILURE DURING FLIGHT. ALTERNATOR INSPECTED AND GROUNDING STRAP, PN 10-1025 ON REAR CASE FROM THE F2 TERMINAL TO CASE GROUND WAS FOUND TO BE CRACKED THROUGH. THE GROUND STRAP WAS STILL IN CONTACT WITH THE CASSDR CA110322007Rotor · 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 CA110321009Magneto · failed(CAN) PILOT DETECTED A VIBRATION IN CRUISE FLIGHT & ELECTED TO CARRY OUT A MAGNETO CHECK. THE RT MAGNETO FAILED COMPLETELY. THE PILOT ELECTED TO CLIMB FOR ALTITUDE & RETURNED TO BASE. REMOVED THE MAGNETO & RETURNED IT TO THE MFG FOR WARRANTY. A STRIP REPORSDR 2011FA0000171Carburetor · damagedCARB WAS INSPECTED DUE TO ROUGH ENGINE OPERATION. UPON INSP IT WAS FOUND THAT 2 BOLTS THAT AFFIX THE 2 HALVES OF THE CARB TOGETHER WERE LOOSE ALLOWING A GAP OF APPROX .0265 INCH BETWEEN THE 2 HALVES OF THE CARB. THE BOLTS WERE STILL HELD IN PLACE BY THE TAB SDR CA110201005Oil Filter · damaged(CAN) THE FILTER WOULD NOT SCREW INTO THE ENGINE`S RECEPTACLE. EXAMINATION REVEALED SEVERAL DAMAGED THREADS ON THE MOUNTING SPUD. THE FILTER HAD COME DIRECTLY FROM A SEALED BAG WITHIN THE FACTORY SIX-PACK.SDR CA110418007Terminal · burned(CAN) WIRE END TERMINALS AND SWITCH TERMINALS FOUND TO BE BURNED BLACK ON SCHEDULED INSPECTION. CHECKED TO ENSURE SEB09-6 WAS COMPLIED WITH IT WAS ENTERED IN LOG BOOK ON MARCH 25, 2010. AFTER READING TP 185 E ISSUE 4/2010. ARTICLE TITLED "SMOKE IN CABIN" LASDR CA101217001Fuel Tank · cracked(CAN) ANTI CHAFE RUBBER STRIPS UNBONDED FROM STRAPS LOOSENING TENSION ON TANK. TANK MOVEMENT IN WING CAVITY CAUSED A FATIGUE CRACK WHERE FILLER NECK WAS WELDED TO TANK SINCE FILLER IS SCREWED TO STRUCTURAL PANEL (UPPER WING SKIN). FUEL LEAK WHEN TANK WAS FILLESDR CA101207002Leg Assy · cracked(CAN) PILOT FRONT SEAT ASSEMBLY INFINITE ADJUST, FRONT LEFT SUPPORT LEG CRACKED AND NO LONGER ATTACHED TO FRAME. (TC# 20101207002)SDR ZB0R201000008Case · leaking(ZB0R) DURING OIL CHANGE, TECH FOUND NR3 CASE SEAM BOLT ON TOP HAD OIL ON IT. RUN-UP REVEALED CASE SEAM LEAKING 1" FWD OF BOLT. ENGINE REMOVED FOR OVERHAUL.SDR CA101103005Screw · failed(CAN) FUEL CAP RETAINING SCREW LOOSENED AND CAP SEPARATED PERMITTING INTERNAL PARTS OF THE FUEL CAP TO FALL INTO THE FUEL TANK. THE FUEL CAP AND SCREW WAS FOUND ON THE RUNWAY. THE AIRCRAFT WAS CONDUCTING NIGHT CIRCUITS AT THE TIME OF THE OCCURRENCE.SDR CA100930010Cable · frayedTHIS REEL IS PART OF A SECONDARY SEAT STOP KIT (SK210-174A) THAT WAS MARKETED IAW SEB 07-5 TO ALLEVIATE THE DANGER OF THE PILOT`S SEAT SLIDING BACK AND CAUSING ACFT CONTROL PROBLEMS. A MORE RECENT REVISION TO THE SB DEMANDED A CHANGE TO THE REEL ASSY TO ADDRSDR CA100910003Bracket · crackedDURING 100 HR INSP, BOTTOM HINGE ASSY ON RUDDER WAS FOUND CRACKED. TOP AND BOTTOM HINGE PN 0531018-1 AND 0531018-2 OF RUDDER WERE REPLACED.SDR CA100901003Magneto · failedGOVERNOR WAS NOT MAINTAINING RPM ON RUN UP, MAGNETO FOUND UNSERVICEABLE.SDR 2010FA0000844Contactor · stuckSTART CONTACTOR STUCK IN CLOSED POSITION. TURNED MASTER ON AND STARTER MOTOR WOULD ENGAGE, HAVE TO TURN MASTER OFF TO STOP STARTER. THIS CONTACTOR WAS CHANGED 8 MONTHS AGO FOR SAME PROBLEM. HAVE HAD SAME PROBLEM ON OTHER MAKES OF ACFT IN THE PAST. SEEMS TOSDR RTE2010F00000Tube · dislodgedTHE ACCELERATOR PUMP DISCHARGE TUBE DISLODGED FROM ITS MOUNTING IN THE FLOAT BOWL ASSY AND BECAME LODGE IN THE THROTTLE UPON LANDING. THE PILOT WAS ABLE TO MAKE A SAFE LANDING WHEN THE ENGINE WAS SHUTDOWN. THE DISCHARGE TUBE FELL OUT OF THE THROTTLE VALVE ASDR 2010FA0000667Mount · crackedDURING ROUTINE MX, A CRACK WAS FOUND ON LOWER LT ENGINE MOUNT BRACE. THERE IS NO DAMAGE HISTORY ON THE ACFT. THE MOUNT DOES NOT HAVE RELIEF HOLES FOR WELDING, AND THUS CAN`T ACHIEVE FULL PENETRATION ON THE WELDS THERE. COMBINED WITH FATIGUE AND VIBRATION, TSDR CA100806008Carburetor · malfunctionedON START UP, IDLE JUMPED TO 900 RPM FROM STANDARD 625 RPM FOR NO REASON, TURNED IDLE DOWN TO 700 RPM ENGINE RAN ROUGH. REPEATED CARBURETOR WITH O/H UNIT, PROBLEM WENT AWAY.SDR CA100621013Switch · overheatedUNKNOWN CYCLES, TSN AND PART TSO -AT PRESENT- HOWEVER WE CHANGED OUT COUPLE OF YEARS AGO DUE AMENDED LIFE LIMIT PARTS. THE SWITCH APPEARS TO HAVE OVERHEATED AND WELDED ACROSS CONTACTS, CONNECTIONS SHOWING BURNING, SWITCH TOGGLE CANNOT BE SWITCHED. APPEARS SWSDR CA100806004Case Half · crackedDURING SCHEDULED INSP, OIL LEAK WAS FOUND ON LT ENGINE CASE. FURTHER INSPECTION REVEALED A 1-INCH CRACK BELOW THE FWD OIL PRESSURE FITTING. ENGINE WAS REMOVED AND SENT OUT FOR SERVICING OR REPAIR.SDR CA100617012Rotor · unserviceableONE OF THE SHAFT TANG SHEARED THUS ALLOWING SLIPPAGE OF THE TIMING TO OUT OF RANGE.SDR CA101103004Door · damaged(CAN) FASTENERS HOLDING THE LUGGAGE COMPARTMENT LOWER ACCESS PANEL FAILED, THUS, PERMITTING OBJECTS STORED IN THE LUGGAGE BAY TO MIGRATE AFT INTO THE AIRCRAFT TAIL SECTION. SEVERAL OF THE OBJECTS BECAME ENTANGLED IN THE CONTROL CABLES.
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