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 = '208' 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 = '208' 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 MT9A00000021Housing · wornRT BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THIS IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATASTROPHIC DAMAGE TO THSDR MT9A00000013Bellcrank · damagedTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K)SDR MT9A00000012Bellcrank · damagedTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K)SDR MT9A00000011Bellcrank · damagedTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K)SDR MT9A00000010Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)SDR CA080320013Tube · failedON TAXI PILOT FELT AIRCRAFT PULLING TO ONE SIDE AND DISCOVERED FLAT TIRE. TIRE WAS CHANGED AND FLOWN BACK TO BASE. TIRE ASSY WAS DISASSEMBLED AND TUBE WAS FOUND BLOWN WITH ABOUT A FOUR INCH SPLIT IN IT. THE TUBE WAS ALSO FUSED TO THE INSIDE OF THE TIRE IN TSDR MAC070705Unknown · smokeSMELLED SMOKE FROM RADIO, COCKPIT, RADIO HOT TO TOUCH.SDR 2007FA0000884Plate · crackedFOUND TORQUE PLATE CRACKED DURING ROUTINE INSPECTION. (K)SDR 2007FA0000443Rod · failedRECEIVED PROPELLER FOR OVERHAUL. DURING PREFUNCTION TEST FOUND BLADE NR 1 WAS NOT LINKED TO THE PITCH CHANGE ROD. AFTER DISASSEMBLY OF PROPELLER FOUND NR 1 BLADE ACTUATING PIN PN B5072-1 DISCONNECTED FROM BLADE. ACTUATING PIN ATTACHMENT SCREWS WERE SAFETIED ANSDR CA070515001Relay · inoperative(CAN) A/C ABORTED TAKEOFF AUX PUMP LIGHT ON AT HIGH POWER. RELAY REPLACED, A/C GROUND RUN AT HIGH POWER NO FAULT FOUND (TC NR 20070515001)SDR CA070516002Exhaust Duct · cracked(CAN) SECONDARY EXHAUST DUCT CRACKED ALONG THE SEAM ON THE OUTER SIDE FROM ABOUT .2500 THE LENGTH DOWN TO .7500 THE LENGTH, CAUSING SEVERAL SMALLER CRACKS TO FORM ALONG INITIAL CRACK 90 DEGREES FROM THE ORIGINAL BOTH ON THE UPPER AND LOWER SIDES. OTHER OPERATSDR CA070523006Gusset · mismanufactured(CAN) AS THE RESULT OF BUMPING A DOCK, THE FWD BULKHEAD HAD TO BE REPLACED ON THE LT FLOAT ASSY ON THE ACFT. AFTER GAINING ACCESS, IT WAS FOUND THAT THE AREA WHICH IS NOT NORMALLY ACCESSED HAD SEVERAL PARTS RIVETED AS PART OF THE STRUCTURE HAD NO PROPER EDGE SDR CA070321006Latch · loose(CAN) LT ENGINE UPPER COWL OPENED IN FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS FLYING THROUGH TURBULENCE WHEN THE COWL OPENED. DURING THE INSPECTION OF THE COWL, IT WAS FOUND THAT ALL 3 LATCHES WERE LOOSE. THE LATCHES WERE RE-ADJUSTED. (TC NR 20SDR CA060704018Adapter · fractured(CAN) AT TOP OF CLIMB, ENGINE TORQUE WAS SEEN TO FLUCTUATE FOLLOWED BY AN ENGINE LOW OIL PRESSURE WARNING. THE ENGINE WAS SHUT DOWN IN FLIGHT AND A DEAD-STICK LANDING ACCOMPLISHED. SUBSEQUENT INSPECTION REVEALED EXTERNAL OIL LEAKAGE ASSOCIATED WITH A FRACTURSDR CA060606010Pressure Switch · failed(CAN) UPON APPROACH FOR LANDING, WHEELGEAR WOULD NOT EXTEND (AMPHIBIAN AIRCRAFT) ABORTED APPROACH , AICRAFT LANDED ON FLOATS AT WATER BASE. AIRCRAFT PLACARDED (FLOATPLANE OPERATION ONLY). (TC# 20060606010)SDR CA060227010Compressor · seizedTHE ENGINE ACCESSORY GEARBOX CHIP DETECTOR WARNING ANNUNCIATED IN FLIGHT AND AN UNSCHEDULED LANDING WAS CARRIED OUT. SUBSEQUENT INSPECTION REVEALED SEIZURE OF THE COMPRESSOR SECTION. P&WC WILL INVESTIGATE THE INCIDENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABSDR AU510001936Blade · crackedPROPELLER BLADE CRACKED AT 40` STATION. FURTHER INVESTIGATION OPENED UP THE CRACK AND FOUND A LARGE AREA OF CORROSION.SDR CA051124002Spar · corroded(CAN) SEVERE CORROSION ON FACE OF SPAR UNDER BALANCE WEIGHT. AIRCRAFT IS A FLOAT PLANE.SDR BSYA200500020Gyro · failedAFTER TAKEOFF, DIRECTIONAL GYRO QUIT, AIRCRAFT RETURNED TO DEPARTURE. REMOVED AND REPLACED GYRO, CHECKS GOOD.SDR AU510001487Blade · corroded(AUS) PROPELLER BLADE CRACKED SPANWISE ON THE LEADING EDGE APPROXIMATELY 140MM (5.5IN) FROM BLADE TIP. FURTHER INVESTIGATION FOUND SEVERE INTERNAL EXFOLITAION CORROSION. THE SAME PROPELLER HAD A SIMILAR DEFECT APPROXIMATELY 50 HOURS PREVIOUS. (CASA# 510001487SDR PNSA050701Fairing · failedDEPARTED AKN EN ROUTE FOR DLG ON V453, JUST AFTER LEVELING OFF AT 4000 FEET THE AIRCRAFT STARTED SHAKING. CREW DECLARED AN EMERGENCY AND RETURNED TO AKN WITHOUT INCIDENT. MAINTENANCE FOUND LT WING FAIRING P/N 2620014-23 HAD FAILED.SDR LU4R12482Spring · stretchedSPRING ASSY STRETCHED TOO LARGE. (K)SDR 2005FA0000638Spring · stretchedSPRING ASSY STRETCHED TOO LARGE. (K)SDR AU510001737Support · corroded(AUS) LT HORIZONTAL STABILIZER OUTER HINGE FITTING CONTAINED SEVERE EXFOLIATION CORROSION. AIRCRAFT OPERATES AS A SEAPLANE IN A SALTWATER ENVIRONMENT. SEE ATTACHMENTS FOR PHOTOGRAPHS OF DEFECT.(OTHER CAUSE: ENVIRONMENT ) (CASA NR 510001737)SDR CA041108006Mount · loose(CAN) MOUNTING STUD NUTS ON FLAP MOTOR BACKED OFF TO THE POINT WHERE THE DRIVE COUPLING DISENGAGED BETWEEN THE FLAP MOTOR AND THE ACTUATOR.SDR 761187Support · damagedNLG SUPPORT DAMAGED. (K)SDR PNSA040601Roll Pin · shearedDURING TAXI LT RUDDER ROLL PIN PN NAS561C3-18 SHEARED CAUSING RUDDER PEDAL TO DISCONNECT AND CAUSE LOSS OF STEERING AND BRAKING ACTION ON LT SIDE.SDR CA040421003Card · broken(CAN) THE CO-PILOT'S DIRECTIONAL GYRO WAS RECENTLY REPLACED WITH THE ABOVE MENTIONED OVERHAULED INSTRUMENT. UPON COMPLAINT FROM PILOT, THE INSTRUMENT WAS HARD TO SET, A FUNCTIONAL TEST WAS COMPLETED. IT WAS FOUND THAT PUSHING THE KNOB IN AND TURNING IT DID NSDR 2003FA0001294Jackscrew · backed outFLAP ACTUATOR JACKSCREW SEPARATED FROM THE ACTUATOR ASSEMBLY CAUSING FAILURE OF THE FLAP SYSTEM DURING TAKE OFF. TEAR DOWN REVEALED THAT THE JACKSCREW RETAINING NUT HAD LOOSENED AND SEPARATED FROM THE JACKSCREW ALLOWING IT TO BE PULLED FROM THE ACTUATOR ASSEMBSDR 2003FA0001295Jackscrew · backed outFLAP ACTUATOR JACKSCREW SEPARATED FROM THE ACTUATOR ASSEMBLY CAUSING FAILURE OF THE FLAP SYSTEM DURING TAKE OFF. TEAR DOWN REVEALED THAT THE JACKSCREW RETAINING NUT HAD LOOSENED AND SEPARATED FROM THE JACKSCREW ALLOWING IT TO BE PULLED FROM THE ACTUATOR ASSEMBSDR AUS20031229Firewall · distorted(AUS) RT FIREWALL BUCKLED DUE TO ASSYMETRIC WASTER CONTACT DURING TAKEOFF IN GUSTY CONDITIONS. AIRCRAFT IS CONFIGURED AS AN AMPHIBIAN.SDR WIW2004F00000Pin · separatedNOSE LANDING GEAR STRUT WAS RESEALED 5/1/01 SO FAILURE OCCURED AFTER THAT TIME. AIRCRAFT WAS HAVING RECURING SHIMMY PROBLEMS WHICH LED TO THE STRUT DISASSEMBLY FOR INSPECTION. DURING INSPECTION THE LOWER PLUG WAS FOUND SEPARATED FROM METERING PIN ASSEMBLY CASDR 2003FA0000909Control Cable · misinstalledDURING A SCHEDULED INSPECTION FOUND THE LEFT WATER RUDDER CABLE IN EMPENNAGE WAS OFF ITS PULLEY AND CUTTING INTO THE PULLEY BRACKET. THE PULLEY SAFETY PIN HAD BEEN INSTALLED IN THE BRACKETT WHILE THE CABLE WAS NOT ON THE PULLEY AT THE TIME OF THE FLOAT INSTALSDR 2003FA0000692Bearing · corrodedROD ASSY PN 2613440-1 LOCATED CENTER FLOOR FORWARD BY PEDESTAL FORWARD BEARING NOTED, CORRODED AND WORN TO HAVE EXCESSIVE PLAY. BEARING HAS GREASE FITTING BUT HARD TO GAIN ACCESS TO, ALSO NOTED, EXCESSIVE WATER ACCUMULATING IN THIS AREAS AND NO DRAIN HOLES NOSDR JUL2003F00000Adapter · defectiveUPON REMOVAL OF FUEL NOZZLES FOR CLEANING, FOUND ROLL PIN IN SECONDARY HOLE. NOTIFIED MFG OF CONDITION.SDR 0065077Hub · corrodedCORROSION ON PROPELLER HUB.SDR 0065202Counterweight · corrodedCORRISON ON PROPELLER COUNTERWEIGHT.SDR AUS20020958Chip Detector · contaminated(AUS) PROPELLER REDUCTION GEARBOX CHIP DETECTOR CONTAINED A SMALL AMOUNT OF METAL PARTICLES.SDR CA020806004Tube · deformed(CAN) OPERATOR PURCHASED A/C FROM COMMERCIAL OPERATOR & INHERITED PERSISTENT & ELUSIVE HYD LEAK. AFTER TROUBLESHOOTING, SOURCE ISOLATED TO TWO B-NUTS NOT TIGHT. FITTINGS WERE NOT ACCESSIBLE. 5 CYCLES LATER NR 13 HYDRAULIC LINE FAILED ON GEAR RETRACTION EMPSDR CA020612005Fitting · elongated(CAN) DURING REINSTALLATION OF FLOATS, BOTH LT FORWARD STRUT ATTACH FITTINGS WERE NOTED TO HAVE ELONGATED BOLT HOLES. AT CLOSER EXAMINATION YOU COULD SEE THAT THE HOLES WERE NOT WORN ELONGATED BUT THE POUNDING FORCE OF LANDING HAD ACTUALLY DISTORTED THE METALSDR 2002FA0000881Fuel Control · failedPILOT REPORTED LOSS OF ENGINE CONTROL. INVESTIGATION REVEALED A THRUST BEARING (PN 2523973) FAILURE INSIDE THE FUEL CONTROL.SDR 2002FA0000198Washer · wrong partDURING A ROUTINE INSPECTION, FOUND THE ENGINE MOUNT BOLTS HAD AN960616L WASHERS INSTALLED UNDER BOLT HEADS (12 BOLTS ) TOTAL. THIS TYPE BOLT MUST HAVE MS20002C6 WASHERS.SDR 2003F00017Brake Assy · contaminatedMOS - FLT 8706 - LEFT BRAKE SPONGY. AIR ENTRAPMENT IN THE LEFT BRAKE SYSTEM. REQUIRES BLEEDING SERVICE, INSPECTION, AND OPS CHECK. BLEED LEFT BRAKE SEVERAL TIMES. BRAKE PEDAL PRESSURE IS GOOD. NO LEAKAGE EVIDENT AT THIS TIME. (M)SDR 2001FA0000689Line · crackedAIRCRAFT WOULD NOT MAKE TAKEOFF POWER, RESULTED IN RTO. CRACKED PY LINE BETWEEN FUEL CONTROL AND PROP GOV. REMOVED AND REPLACED PY RIGHT LINE GOING TO PROP AND PERFORMED A SUCCESSFUL OPERATIONAL AND LEAK CHECK. (M)SDR 2001F00683Door · unsecureBOI - FLT 7861 - ON TAKEOFF ROLL, DOOR WARNING ANNUNCIATOR ILLUMINATED. CARGO NOT SECURED PROPERLY. AIRCRAFT RETURNED TO RAMP WHERE CARGO DOOR WAS CYCLED AND RESECURED. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. (M)SDR CA011001002Connector · burned(CAN) DURING AN INSPECTION OF THE AREA BEHIND THE ELECTRICAL PANEL BY THE PILOTS LEFT FOOT. A WIRE CONNECTOR WAS FOUND BURNED. THE WIRE CONNECTOR BETWEEN THE PROP ANTI-ICE WIRE HA-20 EXITING FROM THE CIRCUIT BREAKER PANEL AND THE WIRE HA-21 GOING TO THE PROP SDR CA011029010Spar Cap · corroded(CAN) DURING AN ANNUAL INSPECTION OF THIS AIRCRAFT, SEVERE CORROSION WAS NOTED ON THE AFT UPPER TRAILING EDGE SPAR CAP ON THE HORIZONTAL STABILIZER AT APPROXIMATELY SS 80.60 LEFT HAND AND ARIGHT HAND SIDES. THE CORROSION HAS GONE THROUGH THE SPAR CAP BUT HAD NSDR CA011029009Bulkhead · corroded(CAN) DURING AN ANNUAL INSPECTION ON THIS AIRCRAFT AN AREA OF CORROSION WAS FOUND ON THE AFT CANTED BULKHEAD AT STATION 427.88 AFT LEFT WL 1 OR 2 INCHES OFF CENTRE. THE CORRORION WAS REMOVED AND THE DAMAGE WAS FOUND TO BE THROUGH 50 PERCENT OF THE MATERIAL. THSDR CA011029008Hinge · corroded(CAN) WHILE PERFORMING AN ANNUAL INSPECTION ON THIS AIRCRAFT, EXCESSIVE MOVEMENT WAS NOTED FROM THE OUTBOARD AND CENTRE HINGE BEARINGS FOR THE R/H ELEVATOR. WHEN THE HINGE SUPPORTS WERE DISMANTLED TO REPLACE THE BEARINGS, CORROSION WAS FOUND ON BOTH HALVES OF SDR CA011029007Seat Track · corroded(CAN) WHILE PERFORMING AN ANNUAL INSPECTION THE AREA AT THE AFT END OF NR 2 / 3 / 4 SEAT RAIL UNDER THE FLOOR AT FS 283.85 WAS NOTED TO HAVE SEVERE CORROSION ON THE STIFFENER P/N 2611131-3 AND THE DOUBLERS P/N 2611192-4 AS WELL AS THE SEAT RAIL. THE CORROSION
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