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 = '180A' 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 = '180A' 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 2026FA0000351Tail Wheel · faultyPILOT REPORTED PROGRESSIVELY SEVERE TAILWHEEL SHIMMY DURING LANDING ROLLOUT, LEADING TO LOSS OF CONTROL AND GROUND LOOP WITH SIGNIFICANT DAMAGE TO AIRCRAFT. POST ACCIDENT INSP FOUND THE TAILWHEEL SPRING HAD AN EXISTING CRACK FROM THE TAILWHEEL HEAD MOUNTING BOSDR 2016FA0000147Rocker · brokenWHILE ON A FLIGHT, ACFT AT CRUISE, 4500 VMC, PILOT FELT A SUDDEN POWER LOSS AND A VIBRATION. PILOT LANDED AND PERFORMED AN INSPECTION WITH A MECHANIC. ONCE IN THE ENGINE, THEY FOUND A BROKEN ROCKER ARM. REPLACED SAME AND RETURNED THE ACFT TO SERVICE.SDR CA150317002Cylinder · delaminated(CAN) DURING A ROUTINE INSPECTION, HIGH METAL CONTENT FOUND IN ENGINE OIL SCREEN. CONTINUED INSPECTION OF THE ENGINE FOUND CYLINDER NR 4 NOT ABLE TO OBTAIN HIGHER THAN 10 PSI ON A COMPRESSION TEST. PRIMARY LOSS OF COMPRESSION OBSERVED FROM CRANKCASE BREATHER,SDR CA120301014Cup · split(CAN) FUEL POURING OUT OF CARBURETOR THROAT, ACCELLERATOR PUMP NOZZLE, WHEN ENGINE OFF AND CARBURETOR AT IDLE CUTOFF. CARBURETOR DISSASSEMBLED AND FOUND ACCELLERATOR PUMP PLUNGER CUP SPLIT.SDR CA110112013Latch · failedWHILE STILL ON WATER, DURING TAKEOFF, LT DOOR WINDOW LATCH OPENED. WINDOW POPPED OPEN AT TOP FRONT THEN OPENED COMPLETELY. FRONT HINGE BROKE. REAR WINDOW HINGE STAYED INTACT. REAR HINGE AND RETAINER ARM HELD WINDOW SO THAT IT DID NOT DETACH FROM DOOR. PILSDR CA071011009Rocker Shaft · damaged(CAN) POOR DIFF ON INSPECTION, EXH VALVE ROCKER SHAFT FOUND DAMAGED DUE TO LACK OF OIL, CAUSING OVERHEATING AND FAILURE OF ROCKER BUSHING. VALVE DAMAGED DUE TO LACK OF COOLING OIL ALSO. CAUSE OF OIL LOSS TO ROCKER UNKNOWN, MAY POSSIBLY HAVE BEEN A BLOCKED GALSDR 2007FA0000332Snap Ring · mismanufacturedSNAP RING USED TO RETAIN PLATE PN 643629 AND COUNTERWEIGHT PIN 643626-101 WAS BEING INSTALLED IN COUNTERWEIGHT. UPON INSTALLING, THE LAST SNAP RING, IT WAS NOTICED THAT THE SNAP RING DID NOT HAVE ANY RETAINING PROPERTIES. IT LACKED TEMPER TO SPRING BACK AND SDR 2006FA0000688Seat · misinstalledA BOLT WAS INSTALLED ON THE FORWARD MOST HOLE ON THE SEAT TRACK FOR USE AS A FORWARD STOP. THE SEAT COULD BE POSITIONED OVER THE HOLE AND THE SEAT LOCKING PIN WOULD ENGAGE, BUT NOT FULLY DUE TO THE BOLT PASSING THROUGH THE HOLE. THE MFG DESIGN DOES NOT ALLOWSDR 2006FA0000687Seat Track · damagedA BOLT WAS INSTALLED ON THE FORWARD MOST HOLE ON THE SEAT TRACK FOR USE AS A FORWARD STOP. THE SEAT COULD BE POSITIONED OVER THE HOLE AND THE SEAT LOCKING PIN WOULD ENGAGE, BUT NOT FULLY DUE TO THE BOLT PASSING THROUGH THE HOLE. THE MFG DESIGN DOES NOT ALLOWSDR DHL2006750520Stringer · corrodedFOUND CORROSION ON STR 28 R BS 1166 AFT PIT. CORROSION OUT OF LIMITS, CUT OUT DAMAGED STRINGER SECTION 9". FABBED FILLER FROM BAC 1498-145 9" PO 422371 AND SPLICE FROM BAC 1498-131; 12" PO 5070593 IAW B727 SRM 53-10-3 FIG 1. TREATED AND PRIMED REPAIRED PARTSDR CA040401005Reinforcement · cracked(CAN) REPAIRED HORIZONTAL STABILIZER. AFT ATTACHMENT POINT REINFORCEMENT BRACKET PN 07321014 REPLACED WITH NEW. ADJACENT RIVETS REPLACED. TAIL REASSEMBLED. INDEPENDENT CONTROL CHECK CARRIED OUT.SDR FCPR200300011Separator · leakingFOUND 1 BALL BEARING MISSING FROM BLADE NR 3, PN A1634-9, SEPARATOR PN B5223.SDR CA020830016Mount · cracked(CAN) ENGINE MOUNT HAD BROKEN TUBE JUST ABOVE FISHMOUTH WELD 11 INCHES BELOW UPPER RT FUSELAGE ATTACH.SDR CA020725010Pin · broken(CAN) PILOT NOTICED INCREASING VAGUENESS IN ELEVATOR CONTROL AND LANDED ASAP. UPON CLOSE EXAMINATION TURN BARREL AND PIN EYE HAD SEPARATED CAUSING VAGUENESS IN CONTROL SAFETY WIRE WAS HOLDING PARTS TOGETHER, TURN BARREL HAD FRACTURED AT BARREL END. THE ABOVE SDR CA010628030Engine · contaminated(CAN) ENGINE LOST OIL PRESS AT NORMAL OPERATING RPM. FURTHER INSPECTION REVEALED CONTAMINATION IN OIL SCREENS, LOOSE RODS, PROBABLE MAIN BEARING SHOT. ENGINE REPLACED IN A/C WITH FACTORYSDR CA010625026Mount · cracked(CAN) ENG MOUNT FOUND CRACKED ON UPPER LT STRUT.SDR CA000828007Gasket · leaking(CAN) CARBON MONOXIDE IN CABIN DUE TO LEAKING EXHAUST GASKETSSDR 20000719SH015Crankshaft · failedPER TCM MSB 00-5, CRANKSHAFT WAS REJECTED BY TELEDYNE CONTINENTAL MOTORS. (X)SDR 20000602SH003Crankshaft · unserviceablePER TCM MSB 00-5, CRANKSHAFT WAS REJECTED BY TELEDYNE CONTINENTAL MOTORS. (X)SDR 2000ZZZX220Hose · deterioratedDURING AN ANNUAL INSPECTION BOTH MASTER CYLINDER FLEXIBLE HOSES WERE FOUND SEVERELY DETERIORATED.SDR CA990927051Bellcrank · broken(CAN) WHILE TAXIING FOR TAKEOFF ON FLOATS, THE RIGHT RUDDER BELLCRANK ARM BROKE AT THE CABLE ATTACHMENT HOLE, CAUSING A LOSS OF DIRECTIONAL CONTROL. AIRCRAFT RETURNED TO DOCK AND THE LEFT AND RIGHT BELLCRANKS WERE REPLACED.SDR CA981207014Bracket · cracked(CAN) BOTH RUDDER BELLCRANK BRACKETS REPLACED AT STA 209 ON THE REAR BULKHEAD. PARTS WERE CRACKED THROUGH THE UPPER BOLT HOLES WHERE THEY ARE BOLTED ONTO BULKHEAD.SDR CA980330006Strut · fractured(CAN) ON LANDING, THE LEFT STRUT FRACTURED 4 INCHES ABOVE THE AXLE, AIRCRAFT ON SKIS. UPPER LEG FELL ON SKI AND COMPLETED THE ROLL OUT. NO SUBSEQUENT DAMAGE TO AIRCRAFT. REPLACED.SDR CA970609024Bearings · worn rusty(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. BALANCE WEIGHTS AND BALLS AND SCREWS RUSTY AND WORN. PARTS REPLACED.SDR EY2R9600131Hub · crackedHUB CRACKED IN MOUNTING FLANGESDR EY2R9600797Retain Bearing · corrodedRETAIN BEARING CORRODED.SDR CA960227010Lifter · galled(CAN) #3 CYLINDER EXHAUST HYDRAULIC LIFTER GALLED (DISINTEGRATED).SDR 95ZZZX819Hinge · corrodedUPON ANNUAL INSPECTION, FOUND SEVERE EXFOLIATION CORROSION ON RT HORIZONTAL STABILIZER HINGE. NOTE: ACFT USED ON FLOATS.
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