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 = '441' 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 = '441' 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 SAI050601Cap · crackedDURING THE ROUTINE CQB 03-1 400 HR EDDY CURRENT INSPECTION A CRACK IN THE UPPER LEFT CANTED RIB NEAR THE AFT SIDE OF THE FORWARD MAIN SPAR BEHIND THE HYDRAULIC COMPONENTS AT APPROX FS 179.6. THE CRACK WAS APPOX 1-1.5 INCHES LONG. THE CAP WAS REPLACED PER CESSDR SAI050602Cap · crackedCRACK FOUND DURING ROUTINE CQB 03-1 EDDY CURRENT INSPECTION OF RIGHT UPPER CANTED RIB CAP APPROX 1.5 INCHES FS 179.6. THE UPPER CANTED RIB CAP WAS REPLACED PER CQB 03-1 AND SK441-110B WITH IMPROVED PART 5790066-11. DURING REINSTALLATION OF HI-LOKS AND RIVETSSDR CA060313010Brushes · brokenSCHEDULED MX CHECK OF BRUSHES, OPERATOR FOUND 1 BRUSH HAMMERPLATE BROKEN OFF DURING INSPECTION OF BRUSHES. RETURNED UNIT TO OVERHAUL AMO FOR REPAIRS. UNIT HAS ONLY 90 HOURS TSO. AMO FOUND ALL BRUSHES CHIPPED AT T/E AND WORN FROM OSCILLATION MOTION IN BRUSH SDR CA060207001Axle · cracked(CAN) THE FORK, AXLE ASSY WAS SENT TO SHOP FOR BUSHING REPLACEMENT, INPECTION AND PAINTING. THEY FOUND THE AXLE BACK PLATE CRACKED. NEW AXLE FITTED.SDR 2006FA0000041Connector · mismarkedWE PURCHASED A REPLACEMENT CONNECTOR FOR THE RT ENGINE FUEL FLOW TRANSDUCER. INSTALLED NEW CONNECTOR AND UPON CHECKOUT FOUND THAT FUEL FLOW INDICATOR NOW OPERATES BACKWARDS. FURTHER INVESTIGATION REVEALS THAT NEWLY INSTALLED CONNECTOR PIN HOLES ARE NOT PROPESDR 2006FA0000034Connector · mismarkedREPLACEMENT CONNECTOR FOR RT ENGINE FUEL FLOW TRANSDUCER. INSTALLED NEW CONNECTOR AND UPON CHECKOUT FOUND THAT FUEL FLOW INDICATOR NOW OPERATES BACKWARDS. FURTHER INVESTIGATION REVEALS THAT NEWLY INSTALLED CONNECTOR PIN HOLES ARE NOT PROPERLY MARKED. IN FACSDR 2006FA0000037Connector · mismarkedPURCHASED A REPLACEMENT CONNECTOR FOR THE RT ENGINE FUEL FLOW TRANSDUCER. INSTALLED NEW CONNECTOR AND UPON CHECKOUT FOUND THAT FUEL FLOW INDICATOR NOW OPERATES BACKWARDS. FURTHER INVESTIGATION REVEALS THAT NEWLY INSTALLED CONNECTOR PIN HOLES ARE NOT PROPERLYSDR AU510002181Acm · failedAIR CYCLE MACHINE (ACM) FAILED AND EMERGENCY PRESSURISATION VALVE AUTOMATICALLY OPENED.SDR AU510002173Outflow Valve · faulty(AUS) CABIN EMERGENCY PRESSURIZATION VALVE HAD UNCOMMANDED ACTUATION. (CASA NR 510002173)SDR AU510002156Door · separatedLT FORWARD NOSE LOCKER SEPARATED FROM AIRCRAFT SEVERING BOTH HINGES. ONE BAG LOST OVERBOARD. DOOR STRUCK PROPELLER CAUSING A TORQUE SHIFT IN THE ENGINE. LT ENGINE, PROPELLER AND LT WING INBOARD LEADING EDGE DAMAGED. INVESTIGATION CONTINUING.SDR AU510002108Switch · shortedNOSE LANDING GEAR ACTUATOR DOWNLOCK SWITCH SHORT CIRCUIT.SDR AU510002093Encoder · failedALTIMETER ENCODER OUTPUT FAILED GIVING FALSE READINGS.SDR AU510002026Engine · seizedRT ENGINE SEIZED. INVESTIGATION CONTINUING.SDR AU510001993Altimeter · failedENCODING ALTIMETER FAILED.SDR AU510001944Governor · faulty(AUS) RT ENGINE PROPELLER GOVERNOR FAULTY. INVESTIGATION CONTINUING. (CASA NR 510001944)SDR AU510001886Rib · crackedRT CANTED RIB CAP FORWARD PN 5720001-4S AND AFT PN 5720001-6S ANGLES CRACKED, FOUND DURING EDDY CURRENT INSPECTION.SDR AU510001885Rib · crackedRT CANTED RIB CAP CRACKED BENEATH REPAIR.SDR AU510001814Spring · broken(AUS) PROPELLER FEATHERING AND UNREVERSING SPRING FAILED. (CASA# 510001814)SDR AU510001776Rib · crackedLT WING ROOT CANTED RIB UPPER CAP LOCATED AT CWS 26.85 CRACKED.SDR AU510001769Bulb · burned out(AUS) RT MAIN LANDING GEAR POSITION INDICATOR LIGHT BULB BLOWN. (CASA NR 510001769)SDR AU510001768Bracket · cracked(AUS) LT ELEVATOR OB HINGE ASSY IB ATTACHMENT BRACKET CRACKED IN LOWER FORWARD RADIUS. FOUND DURING INSPECTION IAW AD/C400/102 AMDT 3 PART 3. BOTH LT AND RT ELEVATOR OB BRGS STIFF IN OPERATION. (AD/SB DESC: AD/C400/102 AMDT 3 PART 3 ) (CASA NR 510001768)SDR AU510001767Cap · cracked(AUS) RT WING CANTED RIB CAP CRACKED. CRACK LENGTH APPROXIMATELY 40MM (1.574IN). CRACK WAS LOCATED IN THE RADIUS OF THE UPPER CAP AND TRAVELLED REARWARDS FROM THE AUXILIARY SPAR. FOUND DURING NDI IAW SB CQB03-01 PART B REV 1. (AD/SB DESC: SB CQB03-01 PART B RESDR AU510001724Rivet · crackedELEVATOR LT OUTBOARD HINGE BRACKET ATTACHMENT RIVET HEAD CRACKED. FOUND DURING INSPECTION IAW AD/C400/102 AMDT3.SDR AU510001559Actuator · faultyRT MAIN LANDING GEAR NIL DOWN INDICATION.SDR AU510001538Tensioner · shearedHF ANTENNA SUPPORT AND TENSION UNIT SNAPPED AT ANTENNA CONNECTION TO VERTICAL STABILIZER.SDR AU510002089Skin · crackedUPPER AFT RT NACELLE SKIN CRACKED AND CORRODED.SDR 2005FA0001400Rib · crackedWHILE ACCOMPLISHING MFG CQB 03-1 EDDY CURRENT INSPECTION THE CANTED RIB CAPS WERE FOUND CRACKED ON THE LT AND RT WINGS. THE AIRCRAFT WILL REQUIRE SERVICE KIT SK441-110-1 REPAIR KIT IAW CQB 03-1 BEFORE FURTHER FLIGHT. (K)SDR JKWS1205Hose · leakingTHE ENGINE OIL LINE SUPPLYING OIL TO THE OIL COOLER BEGAN TO LEAK RAPIDLY IN-FLIGHT. OIL PRESSURE WAS LOST, THE ENGINE WAS SHUTDOWN AND AN UNSCHEDULED LANDING WAS ACCOMPLISHED WITHOUT DAMAGE. INSPECTION REVEALED THAT THE LOSS WAS FROM THE P/N AE7013002H0194 SDR JK1205Line · leakingTHE ENGINE OIL LINE SUPPLYING OIL TO THE OIL COOLER BEGAN TO LEAK RAPIDLY INFLIGHT. OIL PRESSURE WAS LOST, THE ENGINE WAS SHUTDOWN AND AN UNSCHEDULED LANDING WAS ACCOMPLISHED WITHOUT DAMAGE. INSPECTION REVEALED THAT THE LOSS WAS FROM THE P/N AE7013002H0194 OSDR AU510001966Governor · faultyLT ENGINE PROPELLER GOVERNOR FAULTY.SDR 2005FA0000846Fire Bottle · dischargedTHIS FIRE BOTTLE HAS 1 YEAR ON IT AND THE PRESSURE HAS DROPED TO 20 PSI. THIS IS THE SECOND FIRE BOTTLE THAT DID NOT MAKE IT TO 5 YEARS. OVERHAULED BY KELLY AEROSPACE. (QUALITY OF WORKMANSHIP AND OR PARTS)? THIS NEVER HAS BEEN A PROBLEM.SDR CA050712011Wire Harness · shorted(CAN) ENGINE START PROBLEM INTERMITTENT. EXPERT TROUBLESHOOTING FOUND 2 WIRES THAT CROSSED AND HAD CHAFED TOGETHER. ONLY A FAINT BLACK DUST AT THE CONNECTION REVEALED POTENTIAL SHORTING OF WIRES. CORRECTED AND ENGINE START CORRECTED.SDR AU510002204Uplock Hook · cracked(AUS) RT MAIN LANDING GEAR UPLOCK HOOK CRACKED. (CASA NR 510002204)SDR AU510001809Rib · crackedLT WING UPPER FORWARD PN 572001-3S AND AFT PN 572001-5S DRAG ANGLES CRACKED. FOUND DURING EDDY CURRENT INSPECTION IAW CQB03-1 REV 1. EDDY CURRENT INSPECTION REVEALED A TOTAL OF NINE CRACKS ALL AROUND 5MM (0.196IN) IN LENGTH.SDR LQY2005F00000Control Cable · frayedRT AFT ELEVATOR CABLE WAS FRAYED THROUGH 4 OF THE 7 STRANDS - FAILURE WAS IMMINENT. THIS CABLE SHOWED NO SIGNS OF WEAR ON THE PREVIOUS INSPECTION 500 HOURS BEFORE AND IT ONLY TAKES A 20 DEGREE BEND AT THIS PULLEY. PROBABLY SHOULD BE INSPECTED EVERY 300 HOURSSDR CA050125006Link · wrong part(CAN) MLG WAS REMOVED FOR MODIFICATION IAW STC. NR SA00487SE. ON RE-INSTALLATION THE MLG TRAILING LINK P/N 5741140-5 - LT WAS INSTALLED ON THE RT MLG, AND P/N 5741140-6 RT WAS INSTALLED ON THE LT MLG. THIS ERROR WAS NOT OBVIOUS DURING LANDING GEAR FUNCTIONAL RSDR CA050118004Bypass Valve · failed(CAN) AFTER DEPARTURE THE DUCT OVERHEAT WARNING CAME ON.EMERGENCY CHECKLIST CARRIED OUT. SMOKE BEGAN TO EMIT FROM FLOOR INTO CABIN AND COCKPIT. AIRCRAFT RETURNED AND SHUTDOWN AS PER FIRE CHECKLIST. AIRCRAFT EVACUATED.UPON INVESTIGATION THE AIR CONDITIONING BSDR CA041110019Support Bracket · cracked(CAN) AILERON BELLCRANK SUPPORT BRACKET WAS DISCOVERED TO BE CRACKED. PART WAS REPLACED WITH A NEW BRACKET AND THE AIRCRAFT RETURNED TO SERVICE.SDR LATA02010501Engine · power lossUPON DEPARTURE AT APPROX 1000 FEET AGL, WHILE STILL IN THE TRAFFIC PATTERN, THE RIGHT SIDE ENGINE TORQUE ROLLED BACK TO LESS THAN 200LBS. THE PILOT ELECTED NOT TO TROUBLESHOOT THE LOSS OF TORQUE AND SECURED THE ENGINE AND RETURNED TO THE AIRPORT. SUBSEQUENT ISDR 6346753Frame · brokenCO-PILOTS BOTTOM WAS BROKEN IN THE REAR AT BOTH .2500 INCH AND .5000 INCH TUBES ON THE RT AND LT SIDE WHERE THE SIDE TUBES ATTACH TO THE REAR CROSS PIECE AT THE GUSSETS. FORWARD CROSS PIECE TUBING WAS BROKEN AT THE LT SEAT ADJUSTMENT BRACKETS AND CRACKED HALF SDR CA040609018Fuel Control · failed(CAN) DESCENDING THROUGH 7000 FEET ON APPROACH THE RT ENGINE SPOOLED DOWN. WHEN AUTO IGNITION WOULD NOT RELIGHT IT, THE CAPTAIN SECURED THE ENGINE AND LANDED WITHOUT FURTHER INCIDENT. THE ENGINE WOULD NOT RESTART ON THE GROUND. MAINTENANCE TROUBLESHOT THE PROBSDR AUS20040448Selector Valve · faulty(AUS) LANDING GEAR SELECTOR VALVE SOLENOID FAILED.SDR AUS20040447O-Ring · damaged(AUS) NOSE LANDING GEAR UPLOCK ACTUATOR O-RING DAMAGED. HYDRAULIC FLUID LEAKING FROM ACTUATOR BODY.SDR AUS20040368Boot · failed(AUS) RT WING OUTER DE-ICE BOOT BURST AT THE UPPER SEAM AND SPLIT FOR THE ENTIRE LENGTH FROM THE OB RT NACELLE TO THE WINGTIP.SDR AUS20040324Wire · worn(AUS) RT FUEL TANK QUANTITY WIRE CHAFED ON STRINGERS LOCATED AT STATION PWS 61.80.SDR AUS20040327Pump · cracked(AUS) ENGINE OIL PUMP HOUSING CRACKED.SDR AUS20040333Valve · leaking(AUS) START FUEL VALVE LEAKING BETWEEN VALVE BODY AND SOLENOID.SDR AUS20040325Spacer · worn(AUS) MAIN LANDING GEAR UPLOCK HOOK ROLLER SPACER WORN.SDR CA040601008Bolt · brokenGROUND HANDLING PERSONAL ATTEMPTED TO TOW THE AIRCRAFT INTO THE HANGAR FOR A MAINTENANCE FUNCTION. THE TOW BAR BECAME DETATCHED FOLLOWING HOOK UP. THERE WAS NO DAMAGE TO THE AIRCRAFT OTHER THAN THE BROKEN LOWER TORQUE LINK BOLT ON THE NOSE GEAR.SDR 2004FA0000359Regulator Valve · defectiveWINDSHIELD BLEED AIR TEMP SENSOR/REGULATOR WHICH ARE REQUIRED TO BE FUNCTIONALLY TESTED AND REPLACED IF NECESSARY EVERY PHASE 13 (3 YRS) ARE NO LONGER AVAILABLE FROM MANUFACTURE.
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