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 = '747475' 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 = '747475' 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 CA031020005Odor · detected(CAN) AFTER T/O THRU 8,000 FT HAD A STRONG ODOR OF SMOKE IN C/P CABIN. THE ODOR WAS SULPHERUS AND NOT ELECTRICAL. TURNED OFF RECERC AND GASPER FANS AND ODOR DISSAPPEARED. FLT CONTINUED TO DESTINATION AND NO FURTHER FAULT.SDR CA021121002Fairing · damaged(CAN) PANELS 462EL AND 462FL FOUND MISSING OFF NR 2 ENGINE PYLON AND NR 1 TRAILING EDGE FLAP AND CANOE FAIRING FOUND DAMAGED ON WALK AROUND. AIRCRAFT WAS ON A DELIVERY FLIGHT AFTER HAVING UNDER GONE A HEAVY MAINTENANCE VISIT IN SINGAPORE. AIRCRAFT RELEASED FROSDR CA020315007Tube · cracked(CAN) ON CLIMB, EICAS ENGINE OVERHEAT NR 2 NAC. FLIGHT CREW FOLLOWED THE CHECK LIST, BLEED OFF, MESSAGE REMAINED. REDUCED THRUST TO APPROX 75 PERCENT POWER, MESSAGE DISAPPEARED. AIRCRAFT RETURNED TO HAWAII. FOUND CRACK AT UPPER BEND OF NR 2 HP TURBINE COOLINSDR CA020228002Bearing · cracked(CAN) RT BODY GEAR RETRACT ACTUATOR,, LOWER BEARING FAILED.FOUND SPHERICAL BEARING INNER RACE CRACKED THROUGH. LARGE PIECE OF INNER RACE BROKEN OUT. ROLLERS CORRODED AND MISSING. WATER INGRESSION TO BEARING EVIDENT UPON DISASSEMBLY. HIGH LEVEL OF CORROSION SDR CA010905008Sleeve · shorted(CAN) A/C 381 M FOUND DURING UNRELATED ROUTINE MAINT IN AREA. EVIDENCE OF FIRE DAMAGE CAUSED BY SHORTED LEAD AT WASTER TANK DUMP VALVE HEATER SLEEVE. FIRE TRACK WAS FOLLOWED FROM SOURCE FWD THROUGH LIGHTNING HOLE OF ADJACENT STRUCTURE, & UPWARD ALONG FRAME TO SDR CA000518004Engine · failed(CAN) NR 2 ENGINE SHUT DOWN DUE TO HIGH VIBRATIONS NO OTHER DETAILS SUBMITTED.SDR CA000209007Fire Loop · chafed(CAN) APU FIRE WARNING CAME ON DURING CLIMB FIRE BOTTLE DISCHARGED AND STILLWARNING ON A/C RETURNED. FOUND WIRING CHAFFED AND SHORTED BENEATH SUPPORT CLAMP. REPAIRED.SDR CA000118018Blade · seized(CAN) ENGINE WAS SHUTDOWN DUE TO VIBRATION. INSPECTION REVEALED LPT BLADES DAMAGED AND ENGINE SEIZED. SECONDARY DAMAGE TO OUTBRD AILERON WAS EXPERIENCED. REPORT TO FOLLOW.SDR CA000110019Blade · seized(CAN) ENGINE WAS SHUTDOWN DUE TO VIBRATION. INSPECTION REVEALED LPT BLADES DAMAGED AND ENGINE SEIZED. SECONDARY DAMAGE TO OUTBRD AILERON WAS EXPERIENCED. REPORT TO FOLLOW.SDR CA991208053Oxygen Masks · failed(CAN) DURING INSPECTION, OXYGEN MASKS DID NOT DEPLOY PROPERLY FROM PASSENGER CONTROL UNITS. MASKS INCORRECTLY PACKED. ALL MASKS PACKED PER MM.SDR CA990728021Coupling · disconnected(CAN) UNABLE TO TRANSFER FUEL FROM 4 MAIN TANK TO 3 MAIN FUEL TANK. FUEL DUMPED AND AC DIVERTED. FOUND RIGID COUPLING FOR 3 RESERVE TRANSFER FUEL LINE TO 3 MAIN TANK ADRIFT. LINE RECONNECTED WITH NEW O-RING, LEAK CHECK SERVICED.SDR CA990719006Case · deformed(CAN) SEAT TELEPHONE BOXES 7 WIRE CORD REELS EXCESSIVELY HOT AND CASE DEFORMED. REFER TO ASB 6600-23-04.SDR CA990310041Valve · failed(CAN) PRIOR TO PUSHBACK, FUEL SPILL OCCURRED FROM SURGE TANK VENT HOLE. NR 3 FUEL TANK OVERFILL DUE TO UNCOMMANDED FUEL TRANSFER. AIRCRAFT HAD JUST COMPLETED MAINT AND NR 3 JETTISON OVERRIDE PUMP HOUSING AND CHECK VALVE REPLACED. SEALS RUPTURED DUE TO OVERTSDR CA980602021Slide · deployed(CAN) UPPER DECK R/H SLIDE ASSY ACCIDENTLY DEPLOYED DUE FLIGHT CREW L/H AND R/H UPPER DECK DOORS ARMED UPON ARRIVAL. SLIDE DEPLOYED CAUSING DAMAGE TO PACK BOARD. DAMAGE CAUSED BY LANYARD PIN INSTALLED INCORRECTLY ALLOWING BOTTLES TO INITIATE INFLATION PRIORSDR CA971216029Impeller · worn(CAN) OVERRIDE JETTISON PUMP IMPELLER SHROUD WORN FROM CONTACT WITH THEIR RESPECTIVE INLET CHECK VALVES. SHROUD HAD BEEN WORN DOWN ENOUGH TO CAUSE IMPELLER DAMAGE. ALSO, THE DISCHARGE CHECK VALVE WAS WORN INTO THE ATTACHED FUEL PIPES. ALL REPLACED.SDR CA971113015O-Ring · missing(CAN) ON DISASSEMBLY OF BRAKE PISTON, FOUND "O" RING MISSING. REPLACED.SDR CA970731005Valve · worn(CAN) FOUND WHEN INVESTIGATING FUEL IMBALANCE. WEAR CAUSED BY INLET CHECK VALVE TO IMPELLER AND IMPELLER HOUSING, DEBRIS FROM WEAR CAUSING DAMAGE TO MAIN ROTOR. REPLACED.SDR CA970626002Clamp · worn(CAN) ECIAS MESSAGE "DETECT FIRE/OHT 2". AIRCRAFT RETURNED. LOWER AFT LPB ELEMENT OPEN, REPLACED. FIVE CLAMPS WORN ON LOOP A WEARING INTO WIRE REPAIRED.SDR CA970508007Input Rod · worn(CAN) DURING BRAKE SYSTEM FUNCTIONAL CHECK GRATING NOISE HEARD WHEN BRAKE PEDALS MOVED. FOUND WEAR ON #3 AND #4 BRAKE CONTROL INPUT RODS, ONE ROD WORN .040". WEARING ON TEFLON WEAR BLOCKS ATTACHED TO FUSELAGE STRUCTURE. RODS REPLACED AND CLEARANCE PROVIDED.SDR CA970731004Valve · worn(CAN) DURING TORUBLE SHOOTING FOR FUEL IMBALANCE DISCREPANCIES FOUND INLET CHECK VALVE WEARING INTO PUMP INLET IMPELLER, DEBRIS CAUSING DAMAGE TO MAIN PUMP ROTOR. REPLACED.SDR CA970109005Switch · failed(CAN) EICAS STATUS MESSAGE, GEAR MONITOR. CMC CORROLATED MESSAGE, LH BODY GEAR TRUCK TILT ALT. PROXIMITY SENSOR WIRE FAIL. S612 SENSOR REPLACED.SDR CA960711007Transformer · burnt(CAN) LH ANGLE OF ATTACK SENSOR FAILED. ON INSTALL ANGLE OF ATTACK SENSOR TRANSFORMER OVERHEATED AND CAUSED BURNING SMELL IN COCKPIT. TRANSFORMER SELF DESTRUCTED. REPLACED.SDR CA960524007Regulator · out of tolerance(CAN)DURING A SAMPLE DEPLOYMENT OF A SLIDE/RAFT FROM A 747 PASSENGER DOOR, THE SLIDE/RAFT FAILED TO DEPLOY. THE INFLATION CYLINDER REGULATOR WAS SENT TO THE MANUFACTURER FOR EXAMINATION. THE EXAMINATION SH OWED THAT THE INFLATION CYLINDER REGULATOR AND TEMPERASDR CA951219103Bolt · sheared(CAN)DURING ROUTINE INSPECITON AND RETORQUE OF THE MAIN FLAP CARRIAGE SPINDLE RETAINING NUTS, THE #1 T.E. FLAP SPINDLE NUT RETAINER HAD FALLEN OUT OF POSITION AND DAMAGED THE STRUCTURE. INSPECTION REVEALED THAT THE RETAINER NUT LOCK BOLT HAD SHEARED DUE TO HSDR CA951219101Bracket · worn(CAN)DURING "D" CHECK FOUND THE PRIMARY ELEVATOR CABLE E1A NOT FITTED TO ITS PULLEY AT STN 1310. CABLE HAS CUT ITS WAY THROUGH THE PULLEY FRAME ASSEMBLY BOTH FORWARD AND AFT OF THE PULLEY. BOTH PULLEY AXLEBOLT AND CABLE GUIDE BOLT FITTED AND STILL SEALED WITH
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