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 = 'E90' 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 = 'E90' 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 2024FA0000739Gps · defectiveWHILE ENROUTE TO KLVS FROM KGUY, THE GARMIN GNS530W SCREEN SHUT OFF. WHILE TROUBLESHOOTING, A STRONG ELECTRICAL SMELL FILLED THE CABIN. THE AIRCRAFT DIVERTED TO KTDW FOR FURTHER EVALUATION BY THE MAINTENANCE TEAM. UPON FURTHER EVALUATION, IT HAS BEEN DETERMINESDR T4OR2022071400002Brake Assy · brokenDURING LANDING ROLL-OUT BRAKING, THE LEFT BRAKE PEDAL WENT MOST OF ITS TRAVEL WITH LITTLE BRAKING EFFECT. IT WAS DISCOVERED THE LEFT BRAKE TORQUE PLATE WAS CRACKED AND OPENED UP SO CALIPER THE GUIDE PIN WAS NOT RETAINED IN THE TORQUE PLATE. TORQUE PLATE P/N SDR 9LMR032222N600ACTest Switch · crew errorLANDING GEAR INDICATOR GREEN LIGHT PRESS-TO-TEST, REMOVED, INSPECTED AND RE-INSTALLED . NO DISCREPANCIES NOTED AT THIS TIME. LANDING GEAR RETRACTION SYSTEM INSPECTION COMPLIED WITH, FOR PROPER OPERATION, WARNING HORN AND LIGHT, BY TWO COMPLETE CYCLES, OPERSDR HAEA20190614001Axle · missingON DEPARTURE FROM KGVT THE CREW HEARD A NOISE FROM THE RH WING AREA, NOT SURE WHAT IT WAS THEY LEFT THE GEAR DOWN AND LOCKED AND PERFORMED A FLY BY THE TOWER AND DETERMINUED THE RH M/L/G PISTON/AXLE ASSEMBLY WAS MISSING. THE AIRCRAFT WAS FLOWN TO KAFW WHERE THSDR 2019F00061Boot · detached08-11-2018 THE AIRCRAFT HAD A PROPELLER DE-ICE BOOT REPLACED THAT HAD FALLEN OFF. 08-12-2018 ON A FLIGHT, THE BOOT DETACHED FROM THE PROPELLER AND WAS REPAIRED. 08/15/2018 AT APPROXIMATELY 17:10, AT ABOUT 1000' AGL, THE PILOT HEARD A POP IN THE COCKPIT, CSDR 2018FA0000290Bolt · looseDURING FLIGHT FROM KVNY TO KJAC THE CAPTAIN NOTICED FUEL LEAKING FROM THE FILL CAP AREA OF THE LEFT HAND NACELLE FUEL TANK. THE AIRCRAFT WAS DIVERTED TO KLAS FOR INSPECTION. UPON INSPECTION BY A MAINTENANCE TECHNICIAN IT WAS DETERMINED THAT THE LEAK WAS DUE SDR 2018FA0000081Skin · chafedON REMOVAL OF THE HORIZONTAL STABILIZERS FROM THE FUSELAGE, SIGNIFICANT FUSELAGE SKIN CHAFFING WAS FOUND ON BOTH SIDES OF THE AIRCRAFT FROM THE RUBBER SEAL THAT FITS BETWEEN THE FUSELAGE AND HORIZONTAL STABILIZERS. IT WOULD BE ASSUMED TIME, VIBRATION, AND ATMSDR 2018FA0000057Clamp · brokenFOUND BOTH OXYGEN BOTTLE HOLD-DOWN CLAMP BASES BROKEN IN TWO.SDR CA180117004Bracket · cracked(CAN) DURING ROUTINE MAINTENANCE DISCOVERED FLAP TRACK BRACKET CRACKED AT REAR OF SLOT. (TC NR 20180117004).SDR 2016F00123Wire · chafedEXPERIENCED A MASTER WARNING & FIRE INDICATION ON THE NR 2 ENG, SHORTLY AFTER GETTING INTO SOME HEAVY PRECIPITATION. THE PILOT RESET THE MASTER WARNING, BOTH THE MASTER WARNING & ENG FIRE INDICATION WENT OUT. ALL OTHER ENG PARAMETERS WERE NORMAL. HE ASKED TSDR NBFA201508030001Unknown · smokeDURING CRUISE, THE CREW SMELLED AND SAW LIGHT SMOKE COMING FROM BEHIND THE GLARE SHIELD. USING CREW PROCEDURES, UNNECESSARY ELECTRICAL SYSTEM WERE SHUTDOWN. SOURCE OF SMELL AND SMOKE STOPPED. THE ACFT LANDED SAFELY.SDR HAEA2015040500231Rudder Mast · damagedDURING PHASE 1 ACFT INSPECTION, DISCOVERED THE RUDDER TO BELL CRANK RT ATTACH BOLT MISSING. FURTHER INVESTIGATION REVEALED THE BOLT HAD FAILED. AN INSPECTION OF THE RUDDER TORQUE TUBE WAS CONDUCT & IT WAS NOTED THAT THE ATTACH HOLES OF THE BELL CRANK & RUDDESDR CA130524003Gyro · failed(CAN) AFTER REPLACEMENT OF DISPLACEMENT GYRO, FLIGHT CREW NOTIFIED MAINTENANCE THAT THE ATTITUDE INDICATOR INFORMATION WAS BACKWARDS. MAINTENANCE FOUND THE FORWARD POINTING ARROW ON THE COVER OF THE UNIT WAS INSTALLED BACKWARDS. THIS ARROW IS TO GUIDE THE INSDR GNL2013F00000Attach Fitting · crackedLEFT LOWER FORWARD WING ATTACH FITTING CRACKED. CRACK WAS FOUND DURING SIRM WING ATTACH FITTING INSPECTION. EDDY CURRENT WAS THE INSPECTION METHOD. MFG SUPPORT WAS CONTACTED IAW SIRM INSTRUCTIONS. THE FITTING WAS REPLACED BY MFG SERVICES TECH USING WING FISDR 2013FA0000150G Switch · misinstalledWHILE PERFORMING THE ANNUAL ELT INSPECTION, THE ELT WOULD NOT SIGNAL DURING THE "SHAKE" TEST. THE COVER WAS REMOVED FOR A VISUAL INSPECTION. THE G-SWITCH WAS INSTALLED BACKWARD. ALL INDICATIONS WITH A MAGNIFYING GLASS APPEAR THIS TO BE A FACTORY INSTALL, NOSDR CA121004006Support Bracket · cracked(CAN) DURING SCHEDULED INSPECTION, THE BEARING INSIDE THE LANDING GEAR TORQUE TUBE SUPPORT BRACKET HAD MOVED OUT OF PLACE. FURTHER INVESTIGATION REVEALED A CRACK THROUGH THE GREASE FITTING HOLE ON THE SUPPORT BRACKET.SDR CA120719002Gasket · split(CAN) NACELLE GASKETS SPLIT AT BOLT HOLES AND CAUSED FUEL LEAK. GASKETS REPLACED IAW SB 28-4059.SDR CA110802009Rib · crackedDURING INSP, FRETTING (SMOKING) WAS FOUND TO BE COMING FROM BETWEEN THE ELEVATOR TORQUE TUBE AND THE INBD RIB THAT THE TUBE ATTACHES TO. AFTER DISASSEMBLY, CRACKS WERE FOUND IN THE RIB AND DOUBLER. BOTH ELEVATORS HAVE SIMILAR DAMAGE.SDR GNL2011F00001Resistor · shortedACFT IN CRUISE FLIGHT. ELECTRIC SMOKE FILLED THE CABIN AND COCKPIT. NON-ESSENTIAL EQUIPMENT WAS TURNED OFF AND THE SMOKE CLEARED. THERE WERE NO TRIPPED CIRCUIT BREAKERS AND THE PILOT NOTICED THE "PILOT INSTRUMENT LIGHTS" RHEOSTAT WAS ONLY PARTIALLY FUNCTIONSDR GNL2011F00000Controller · intermittentACFT CLIMBING THROUGH 12,000 FT, CREW NOTICED A HAZE IN THE CABIN FOLLOWING INCREASE IN CABIN TEMP. A DESCENT TO 11,000 FT WAS MADE. ATTEMPTS WERE MADE TO STOP BOTH THE HEAT AND SMOKE. CABIN PRESSURIZATION "DUMP" SWITCH WAS SELECTED AND THE ACFT WAS LANDEDSDR YUUR101220105690Connector · separated(YUUR) DURING PRE-INSP GROUND RUNS THE PROPELLER DE-ICE AMPERAGE WAS NOTED LOW. INSP REVEALED THE BLADE DE-ICE BOOT LEAD IS A 2 PIECE ASSY WITH A MOLEX TYPE CONNECTOR SECURED TO THE BLADE. INSIDE THE CONNECTOR THERE IS AN ORANGE PIECE OF FOAM FOR SEALING THE SDR DGCA10851Windshield · crackedCO-PILOTS WINDSHIELD CRACKED.SDR 2010FA0001089Fire Warning · false activationFIRE WARNING ON RT ENGINE WITH NO SUPPORTING EVEDENCE OF ACTUAL FIRE. CHECK LIST COMPLIED WITH AND PRECAUTIONARY LANDING ACCOMPLISHED. INSPECTED AND TROUBLESHOT FIRE DETECTION SYS IAW MM 26-10-00 CHART 101, PROBLEM NR4. NO DEFECT NOTED CLEANED AND DRIED ELECTSDR 2010FA0001085Fire Warning · false activationFIRE WARNING ON RT ENGINE WITH NO SUPPORTING EVIDENCE OF ACTUAL FIRE. CHECKLIST COMPLIED WITH AND PRECAUTIONARY LANDING ACCOMPLISHED.SDR CA100922002Control Cable · damagedELEVATOR TRIM CABLE WAS FOUND UNSPOOLED OFF BOTH FWD AND AFT TRIM DRUMS.SDR CA100531006Blower Motor · overheatedCABIN VENTILATION BLOWER MOTOR OVERHEATED AND CREATED SMOKE IN THE COCKPIT. PILOT WAS FORCED TO DO AN EMERGENCY LANDING. UPON INVESTIGATION THE BLOWER MOTOR CIRCUIT BREAKER WAS FOUND TRIPPED. THE BLOWER MOTOR WAS REPLACED WITH A O/H UNIT AND THE CIRCUIT BRESDR VIB4 1536Circuit Breaker · intermittent(VIB4) DURING TAKEOFF THE ACFT ATTEMPTED A NORMAL GEAR RETRACTION. THE LANDING GEAR STARTED A NORMAL RETRACTION WHEN IT STOPPED EARLY IN THE RETRACTION CYCLE. WHEN IT STOPPED THE ACFT DID NOT HAVE ANY DOWN AND LOCK LIGHTS NOR DID IT HAVE AN UNSAFE LIGHT IN THESDR CA100218013Skin · cracked(CAN) FUSELAGE PRESSURE SKINS P/N 50-420011-1051 AND 1052 CRACKED AND WORN BY CHAFING ACTION BETWEEN THEM AND FILLETS PN 50-420023-31 AND 32 DUE TO NORMAL WING MOVEMENT. (TC 20100218013)SDR CA100218012Skin · cracked(CAN) FUSELAGE PRESSURE SKINS PN 50-120156-81 AND 82 CRACKED AT LOWER SPAR CAP PENETRATIONS. (TC 20100218012)SDR DGCA09331Fuel Control · hung upON LANDING THE ENG POWER HUNG AT APP 800 LBS OF TORQUE. FOUND FUEL CONTROL UNIT FAULTY.SDR CA091020001Splice · missing(CAN) DURING INSP OF FUSELAGE BELLY SKINS JUST AFT OF FWD WING SPAR, AN UNUSUAL SKIN BUTT SPLICE WAS FOUND. SPLICE HAS ONLY A SINGLE ROW OF RIVETS IN A PRESSURIZED VESSEL, WHERE THERE IS NORMALLY A DOUBLE ROW. FURTHER INVESTIGATION OF THE INSTALLATIOIN DWG FORSDR CA090617003Hinge · cracked(CAN) LT HORIZ STAB CTR HINGE LWR OTBD CORNER CRACKED. INITIALLY APPEARED TO BE CRACK IN THE PAINT UNTIL CLOSER EXAMINATION.SDR 2009F00036Bolt · crackedPOSSIBLE CRACK IN AFT WING BOLTS UPPER (POSSIBLY WAS CAD PLATING ON BOLTS) SHOWING IN THREADS OF BOLTS.SDR T4OR 4995 70Roller · wornRT OTBD FLAP ATTACH POINT BRACKETS (RIBS) ARE WORN WHERE AFT FLAP TRACK ROLLERS ARE ATTACHED. BRACKETS ARE WORN APPROXIMATELY .015 INCH TO .020 INCH DEEP IN THE BRACKET SIDES FROM THE ROLLER IN THE SHAPE OF THE ROTATING ROLLER ENDS. SUSPECT CAUSE TO BE WORN SDR VQMAF010510Circuit Board · burned outA CABIN ALTITUDE WARNING PRESSURE SWITCH TEST WAS PERFORMED BY METHOD 2, AS REFERENCED IN MM 21-30-00, PAGE 214, ITEMS A-F. DETERMINED THAT THE TEST FAILED ITEM C OF THE TEST, BECAUSE THERE WAS NO VISUAL AMBER "CABIN ALTITUDE HIGH" WARNING ANNUNCIATION AVAILABSDR CIEA200800009Windshield · crackedDURING CRUISE AT FL240 APPROX 80 TO 90 MILES FROM KCPR, THE RT SIDE FRONT WINDSHIELD CRACKED. AT THE TIME, THE TEMPERATURE OUTSIDE WAS -38 DEGREES CELSIUS AND THE WINDSHIELD HEAT WAS OFF WITH CLEAR SKIES OBSERVED. THE PILOT CONTACTED ATC AND LET THEM KNOW THSDR 2008FA0000670Fuel Line · crackedWHILE PERFORMING ENGINE RUNS FOR RIGHT ENGINE FLOW PACK CHANGE FOUND FUEL LEAK FROM FUEL LINE FROM FCU TO TOP OF START CONTROL UNIT. FITTING CRACKED ABOVE SCU. REMOVED CRACKED FUEL LINE FROM FCU TO TOP OF START CONTROL UNIT. INSTALLED OVERHAULED LINE P/N 30SDR 2008FA0000321Spar Cap · crackedTHE CRACK EMANATES FROM THE 5TH RIVET OUTBOARD OF THE LOWER FORWARD WING BOLT FITTING, (4TH RIVET FROM END OF SPAR CAP)IN THE REAR ROW OF RIVETS, & EXTENDS TO THE TRAILING EDGE OF CAP. THE A/C PASSED 2-400 HR WING SIRM INSPECTIONS. THE CRACK WAS DETECTED AT THSDR 2008FA0000326Spar Cap · crackedTHE CRACK EMANATES FROM THE 5TH RIVET OUTBOARD OF THE LOWER FORWARD WING BOLT FITTING, 4TH RIVET FROM END OF SPAR CAP, IN THE FRONT ROW OF RIVETS, AND EXTENDS TO THE LEADING EDGE OF CAP. THE A/C PASSED 2-400 HOUR WING SIRM INSPECTIONS. 181 HRS INTO NEXT INTESDR R025878Clamp · cracked838-67 CLAMP ASSY SN EF3099. CRACK FOUND INTERSECTING THE THREADED LINK SCREW HOLE.SDR CA080423013Fuel Control · malfunctioned(CAN) DURING APPROACH, UPON RETARDING THE POWER LEVER TO IDLE, THE ENGINE ACCELERATED TO 90 PERCENT NG WITH AN ASSOCIATED TEMPERATURE OF 800 DEGREES. THE PILOT ELECTED TO SHUTDOWN THE ENGINE AND FEATHER THE PROP. THE FUEL CONTROL WAS SUBSEQUENTLY REPLACED AND SDR 2008FA0000082Capacitor · burnedAT CRUISE FL 150, CREW NOTICED SMOKE AND ELECTRICAL ODOR COMING FROM SIDEWALL UNDERNEATH EMERGENCY EXIT. PIC DECLARED EMERGENCY AND LANDED AC WITHOUT FURTHER INCIDENT. UPON INSP OF SIDEWALL UNDER EMERGENCY EXIT, IT WAS NOTICED THAT A SMALL HOLE WHICH APPEARSDR O7Z2008F00000Spar Cap · crackedFWD OB LOWER WING SPAR CAPS ARE CRACKED. LT AND RT ASSY CRACKS RADIATE FROM THE (4) HUCK RIVET FWD THROUGH WING ATTACH HINGE. THE AIRCRAFT WAS INSPECTED 15 MONTHS AND 404.2 HOURS AGO BY EDDY CURRENT AND NO CRACKS WERE FOUND AT THAT TIME. (K)SDR LW29212112007Unknown · odorDEPARTED, UPON REACHING 7500 FEET SMELLED BURNING OIL FUMES IN CABIN. CLOSED BLEED AIR'S, TURNED OFF ENVIRONMENTAL SYSTEMS AND DUMPED CABIN. SAFELY RETURNED TO DEPARTURE. MAINTENANCE CHECKED AIRCRAFT AND ENGINE PNEUMATIC LINES, INSPECTED THE PRESSURIZATION SYSDR 2007FA0000853Flange · cracked(2) NEW ENGINES WERE INSTALLED IAW MFG MODIFICATIONS, WITH 938.0 HRS SINCE NEW. AIRCRAFT WAS IN FOR A PHASE INSPECTION AND FOUND 3 OUT OF L1 EXHAUST FLANGES ON THE ENGINE CRACKED. ACCORDING TO THE MFG PARTS MANUAL, EXHAUST STIFFENERS ARE NOT USED ON THIS SN SDR 2007FA0000752Engine · failedAIRCRAFT IN CRUISE AT 22,000 WITH ALL ENGINE INDICATIONS NORMAL. A LOUD NOISE FOLLOWED BY POWER LOSS AND REDLINE ITT ON THE LT ENGINE. THE CT BLADES, ITT PROBES, PT VANE AND PT BLADES ALL MELTED AND WENT THROUGH THE EXHAUST STACKS. COMPRESSOR STATOR AND SPASDR CIEA200700003Cowling · bentDURING TAKEOFF ROLL OF THE AC, AT THE POINT OF LIFTOFF, THE PILOT NOTICED THE LT ENGINE UPPER AFT COWLING HAD COME OPEN. THE TAKEOFF WAS ABORTED AND THE AC CAME TO A SAFE STOP ON THE RUNWAY. THE PILOT SHUTDOWN THE LT ENGINE AND TAXIED BACK TO THE HANGAR ON TSDR LE72008F00000Relay · failedLANDING GEAR FAILED TO EXTEND, GEAR LOWERED MANUALLY. (K)SDR CA060822006Frame · cracked(CAN) LT SIDE OF FUSELAGE, DISCOVERED 4 LOOSE RIVETS AT FS 176.5. MAINTENANCE DEPT REMOVED INTERIOR TO INVESTIGATE DEFECT. IT WAS DISCOVERED THAT FRAME MEMBER P/N 50-420028-57 WAS CRACKED IN SEVEN SPOTS. MAINTENANCE DECIDED TO INVESTIGATE THE RIGHT HAND OF SDR 2006FA0000090Plate · crackedDURING A PHASE I AND II INSPECTION A CRACK WAS FOUND IN THIS PART ATTACHED TO THE RT GEAR ASSY. THE CRACK IS ON THE TORQUE PLATE UPPER FORWARD BRAKE CYLINDER PIN ATTACH HOLE. A BUSHING INSTALLED IN THIS HOLE HAS NO SIGN OF DAMAGE. PROBABLE CAUSE OF CRACKING
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