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 = '58' 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 = '58' 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 Q5QA20180501303Spar Web · crackedDURING A ROUTINE INSPECTION, THE FORWARD CARRY-THRU SPAR AFT WEB WAS FOUND TO HAVE A SMALL CRACK IN THE UPPER RH CORNER. BEECHCRAFT FRONT SPAR CARRY THRU STRUCTURE REINFORCEMENT DOUBLER KIT 58-4008 HAD BEEN PREVIOUSLY INSTALLED. REPAIRS REQUIRED INSTALLATIONSDR Q5QA201805010202Spar · crackedDURING A ROUTINE INSPECTION, THE FORWARD CARRY-THRU SPAR AFT WEB WAS FOUND TO HAVE A SMALL CRACK IN THE UPPER RH CORNER. BEECHCRAFT FRONT SPAR CARRY THRU STRUCTURE REINFORCEMENT DOUBLER KIT 58-4008 HAD BEEN PREVIOUSLY INSTALLED. REPAIRS REQUIRED INSTALLATIONSDR Q5QA20170412009Spar Web · crackedDURING A PHASE INSPECTION, CRACKS WERE DISCOVERED ON THE WING CARRY-THRU FORWARD SPAR WEB .SDR Q5QA20170412008Circuit Breaker · failedSTALL WARNING VANE DE-ICE SYSTEM WAS FOUND TO BE INOPERATIVE. DISCOVERED CIRCUIT BREAKER TO HAVE FAILED INTERNALLY.SDR Q5QA20170412007Circuit Breaker · failedFUEL VENT DE-ICE SYSTEM WAS FOUND TO BE INOPERATIVE. DISCOVERED CIRCUIT BREAKER TO HAVE FAILED INTERNALLY.SDR 2017FA0000146Starter · damagedENGINE WOULD NOT START. FOUND THE STARTER DRIVE SHAFT TO SPIN FREELY INSIDE OF THE STARTER MOTOR ARMATURE.SDR Q5QA20161115005Channel · crackedWHILE PERFORMING A ROUTINE INSPECTION, CRACKS WERE NOTED ON A LATERAL CHANNEL IN THE TAIL SECTION OF THE FUSELAGE. CRACKS WERE APPEARING ON THE UPPER LT AND RT CORNERS AT THE CUTOUT RELIEFS. THIS AREA IS DIFFICULT TO VIEW AND ANY DEFECTS EASILY OVERLOOKED.SDR Q5QA20161108003Channel · crackedWHILE PERFORMING A ROUTINE INSPECTION, CRACKS WERE NOTED ON A LATERAL CHANNEL IN THE TAIL SECTION OF THE FUSELAGE. CRACKS WERE APPEARING ON THE UPPER LT AND RT CORNERS AT THE CUTOUT RELIEFS.SDR Q5QA2016110704Channel · crackedWHILE PERFORMING A ROUTINE INSPECTION, CRACKS WERE NOTED ON A LATERAL CHANNEL IN THE TAIL SECTION OF THE FUSELAGE. CRACKS WERE APPEARING ON THE UPPER LT AND RT CORNERS AT THE CUTOUT RELIEFS.SDR 2016FA0000499Cylinder · corrodedTHE CYLINDER BARREL HAD RUST AT THE INSIDE TOP OF THE CYLINDER AND A SPOT OF RUST 1/4 TO 1/2 DOWN INSIDE OF THE CYLINDER.SDR 2016FA0000488Wire Harness · chafedDURING AVIONICS MODIFICATIONS ON THIS AIRCRAFT, THE TECHNICIAN NOTED A BLACKENED STRINGER (LOCATED ON THE RIGHT SIDE OF THE FUSELAGE, ADJACENT TO THE INSTRUMENT PANEL GLOVE BOX) WITH A WIRE BUNDLE LAYING HARD AGAINST IT. FURTHER INVESTIGATION DISCLOSED A 4 AWSDR PE2A2016070100001Drag Link · brokenTHE AFT NLG RETRACT LINK BROKE JUST FORWARD OF THE ACTUATOR ATTACH AREA, CAUSING THE NLG TO COLLAPSE DURING LANDING. THE DRAG LINK BROKE AT THE FORWARD MOST AREA OF WELD WHERE THE CAST ACTUATOR ATTACH STRUCTURE IS WELDED TO THE TUBE STRUCTURE. IT WAS ALSO NOSDR PE2A2016F00153Drag Link · brokenNLG UPPER DRAG LINK BROKE DURING THE LANDING GEAR EXTENSION CYCLE, CAUSING COLLAPSE OF THE NLG DURING LANDING. THE BREAK OCCURRED AT THE AFT SECTION OF THE RT SIDE OF THE DRAG LINK, JUST BELOW THE ACTUATOR ROD ATTACH AREA. TO BE MORE SPECIFIC, THE BREAK WAS SDR 2016FA0000216Brace · crackedLEFT LANDING GEAR A FRAME CRACKED AT FORWARD ATTACH POINT.SDR 2016FA0000048Pump · burnedCABIN HEATER CIRCUIT BREAKER POPPED DURING HEATER OPERATION WHILE AIRCRAFT WAS IN FLIGHT. UPON LANDING MAINTENANCE PERFORMED INSPECTION/TROUBLESHOOTING OF HEATER SYSTEM MALFUNCTION AND FOUND HEATER FUEL PUMP HOUSING BURNED THROUGH DUE TO POSSIBLE INTERNAL DEFSDR 2015FA0000455Magneto · bindingROUGH RT ENGINE, LT MAGNETO OPERATION DURING RUN-UP CHECK. REMOVED MAGNETO, PN BL-349350-4, SN F11EA076R, MODEL S6RN-1225 AND FOUND MAGNETO GEAR BUSHING AND RETAINER BROKEN. CONSULTED WITH MFG FOR ADDITIONAL INSTRUCTIONS. REMOVED OIL PAN AND RECOVERED MISSISDR Q5Q2015F00002Bushing · worn100 HOURS AGO, NOTED THA THE INBD GEAR DOOR ACTUATOR ROD BOLTS AT THE GEAR ACTUATOR CROSSARM HAD BECOME LOOSE. WE HAD REPLACED THE 130909B84 BOLT, 58-8100151, BUSHING AND THE AN960-416 WASHERS WITH NEW PARTS. WE MARKED THE HEAD OF THE BOLT TO THE ABLE TO TELSDR Q5Q2015F00001Bushing · deformedFOUND NUT MISSING, RT SIDE INBD LANDING GEAR ACTUATOR ROD ATTACH POINT WHERE IT ATTACHES TO THE GEAR ACTUATOR CROSS ARM. DISCOVERED NUT AND COTTER PIN REMNANTS UNDER GEAR ACTUATOR. UPON CLOSER EXAMINATION, NOTED THAT THE ACTUATOR ROD BUSHING (56-810015-1) HASDR Q5Q2015F00000Bushing · deformedFOUND NUT MISSING, RT SIDE INBD LANDING GEAR ACTUATOR ROD ATTACH POINT WHERE IT ATTACHES TO THE GEAR ACTUATOR CROSS ARM. DISCOVERED NUT AND COTTER PIN REMNANTS UNDER GEAR ACTUATOR. UPON CLOSER EXAMINATION, NOTED THAT THE ACTUATOR ROD BUSHING (56-810015-1) HASDR CXIA2015F00000Connecting Rod · failedRIGHT ENGINE WAS SHUTDOWN IN FLIGHT, ENROUTE TO TOP DUE TO OIL LEAKING FROM COWLING. AIRCRAFT LANDED WITHOUT INCIDENT. ENGINE WAS FOUND TO HAVE HOLES IN THE TOP OF THE CRANKCASE AND A BROKEN CONNECTING ROD. UNABLE TO DETERMINE IF ANY SPECIFIC PART OR COMPONSDR CA150121006Shaft · failed(CAN) DURING A STUDENT IFR FLIGHT IN VFR CONDITIONS THE INSTRUCTOR NOTED THAT THERE WASN`T ANY INSTRUMENT PRESSURE FROM EITHER ENGINE. UPON INSPECTION WE NOTICED THAT BOTH PRESSURE PUMPS HAD SHEARED THEIR SHAFTS. WE COULD NOT FINE ANY OBSTRUCTIONS. ALL LINES WSDR MZER2015FA0000009Pin · shearedACFT INCURRED A LANDING GEAR MALFUNCTION. DURING GEAR RETRACTION, IN-FLIGHT THE SHEAR PIN, 60-810082-3, FAILED IN THE RETRACT CONTROL ROD ASSEMBLY. THE GEAR RETRACTED AN ESTIMATED .7500 UP WHEN THE LEFT 60-810082-3 ALUMINUM SHEAR PIN SHEARED WHICH CAUSED THESDR RIQA2015011600001Control Cable · brokenTHROTTLE CABLE SNAPPED IN CRUISE FLIGHT ENROUTE TO A DESTINATION AIRPORT. NO POWER CHANGES WERE BEING MADE AT THE TIME OF FAILURE, PROBABLE CAUSE OF FAILURE SUSPECTED TO BE FATIGUE FROM NORMAL USAGE AND SLIGHT CORROSION FROM EXPOSURE TO THE ELEMENTS. RECOMMESDR 2014FA0000698Bearing · failedLEFT ENGINE, RT MAGNETO FAILED. MAGNETO WAS REMOVED AND SENT FOR REPAIR. MAGNETO WAS DISASSEMBLED, FOUND BEARING WELDED TO ROTOR SHAFT AND INTERNAL COMPONENTS DAMAGED BEYOND REPAIR. PREMATURE FAILURE OF BEARING DUE TO LACK OF LUBRICATION OR DEFECT. MAGNETOSDR KC2R2014FA0000705Impulse Coupling · crackedDURING A 500 HR INSPECTION OF MAGNETO, IT WAS DISCOVERED THAT IMPULSE COUPLING BASE PLATE WAS CRACKED AT BOTH ADVANCE STOP LOCATION. CRACKS WERE VISIBLE USING FLUORESCENT MAGNETIC PARTICLE INSPECTION NDT. CRACKS RADIATE FROM SHARP CORNERED FEATURE OF BASE PLSDR KC2R2014FA0000704Impulse Coupling · crackedDURING A 500 HR INSPECTION OF MAGNETO, IT WAS DISCOVERED THAT IMPULSE COUPLING BASE PLATE WAS CRACKED AT BOTH ADVANCE STOP LOCATION. CRACKS WERE VISIBLE USING FLUORESCENT MAGNETIC PARTICLE INSPECTION NDT. CRACKS RADIATE FROM SHARP CORNERED FEATURE OF BASE PLSDR KC2R2014FA0000703Impulse Coupling · crackedDURING A 500 HR INSPECTION OF MAGNETO, IT WAS DISCOVERED THAT IMPULSE COUPLING BASE PLATE WAS CRACKED AT BOTH ADVANCE STOP LOCATION. CRACKS WERE VISIBLE USING FLUORESCENT MAGNETIC PARTICLE INSPECTION NDT. CRACKS RADIATE FROM SHARP CORNERED FEATURE OF BASE PLSDR KC2R2014FA0000702Impulse Coupling · crackedDURING A 500 HR INSPECTION OF MAGNETO, IT WAS DISCOVERED THAT IMPULSE COUPLING BASE PLATE WAS CRACKED AT BOTH ADVANCE STOP LOCATION. CRACKS WERE VISIBLE USING FLUORESCENT MAGNETIC PARTICLE INSPECTION NDT. CRACKS RADIATE FROM SHARP CORNERED FEATURE OF BASE PLSDR A6YA2014052831822Lifter · spalledAFTER REMOVAL OF ALL CYLINDERS DUE TO TOP PISTON RING PLATING FLAKING, SDR A6YA2010052738221, ALL LIFTERS WERE REMOVED & INSPECTED IAW SID 05-1A. NR 2 & NR 5 EXHAUST VLV LIFTERS WERE FOUND TO HAVE FULL FACE SPALLING AS PICTURED IN SID 05-1A FIG 6 AND FIG 8. SDR A6YA2010052738221Piston Ring · flakingDURING AN OIL CHANGE FLAKES OF METAL WERE FOUND IN THE OIL FILTER. THE TOP SPARK PLUGS WERE REMOVED & CYLINDER NR 3 HAD OIL ON THE TOP SPARK PLUG. THE CYLINDER WAS REMOVED & PLATING WAS FOUND TO BE FLAKING OFF THE TOP PISTON RING. ALL 6 CYLINDERS WERE REMOVSDR FQ5R2015032700001Ahrs · unknownWHILE AT CRUISE ALTITUDE OF 14,000FT, ON A VERY COLD DAY THE G500 PANEL FLAGGED THE AIRSPEED, ALTITUDE, AIS, OAT, HEADING AND HORIZON ALL "X" OUT WITH BIG RED X'S. LOSS OF ALL DATA FROM THE AHARS. PILOT USED THE BACK UP INSTRUMENTS TO COMPLETE THE FLIGHT. WSDR XGN2013F00002Fitting · crackedTHIS MOUNT IS RIVETED ONTO THE REAR SPAR, IT IS WHERE THE LG MOUNTS INSIDE THE LT WING AFT SIDE. THE BOLT THAT GOES THRU THE LG MOUNT GOES INTO THIS FITTING ON THE SPAR. THE FITTING IS CRACKED HORIZONTALLY JUST ABOVE THE BOLT PASS THROUGH ON THE VERTICAL LEGSDR 2014FA0000148Clamp · looseON ENTERING PATTERN AND MOVING THE LANDING GEAR HANDLE DOWN TO THE EXTENDED POSITION, PILOT NOTICED SMOKE IN THE COCKPIT. PULLED THE LANDING GEAR AND LANDING GEAR RELAY CIRCUIT BREAKERS AND EXTENDED LANDING GEAR UTILIZING THE ALTERNATE EXTENSION HANDLE. OBSSDR 2013FA0000593Stud · missingDURING CLIMBOUT, PILOT NOTICED SMOKE TRAILING FROM THE LT ENGINE. IMMEDIATELY LANDED AT DEPARTURE AIRPORT AND AT SHUTDOWN, SAW A GREAT DEAL OF OIL DRIPPING FROM LOWER COWLING AND COWL FLAP. DURING AN INSPECTION RUN-UP, OIL WAS SEEN PUMPING FROM AREA OF TACHSDR BSYR201309252062Engine · surgesAFTER TAKEOFF, LT ENGINE STARTED TO SURGE. PILOT NOTICED FUEL PRESSURE WAS FOLLOWING THE SURGE. SHUTDOWN LT ENGINE AND RETURNED AND LANDED SAFELY WITHOUT INCIDENT. OPENSDR 2013FA0000554Bladder · deterioratedRIGHT ENGINE SURGED DURING CLIMB POWER SETTINGS, DURING TROUBLESHOOTING FOUND FUEL NOZZLES PARTIALLY PLUGGED WITH A BLACK MATERIAL, SCREEN ALSO HEAVILY CONTAMINATED WITH SMALL BLACK PARTICLES. CHECK OF THE OTHER ENGINE, SHOWED CONTAMINATED PARTICLES LOCATED ISDR BSYR20130916061Door · unsecureAFTER TAKEOFF, EMERGENCY EXIT POPPED OPEN. PILOT TURNED BACK AND LANDED SAFELY WITHOUT INCIDENT. MX IS INSPECTING.SDR BSYR201307222052Unknown · unknownENROUTE, PILOT FELT A JOLT AND RPM FLUCTUATION. DIVERTED AND LANDED WITHOUT INCIDENT. OPENSDR YWBR2013061725111Thru Bolt · undertorquedRECEIVED NEW IO-550-C ENGINE SN 1008500. REMOVED ENGINE FROM SHIPPING CRATE AND PLACED IN ENGINE STAND. UPON INSPECTION OF THE NEW ENGINE IT WAS NOTICED THE FRONT THRUST BEARING UPPER AND LOWER THROUGH BOLTS WERE NOT TORQUED. THE NUTS WERE ONLY FINGER TIGHTSDR BSYR20130531050Unknown · malfunctionedON APPROACH INTO PSM, LANDING GEAR WOULD NOT EXTEND. PILOT WAS ABLE TO EXTEND THE GEAR DOWN BY HOLDING THE GEAR CIRCUIT BREAKER IN. PILOT NOTIFIED ATC AND LANDED SAFELY AT PSM WITHOUT INCIDENT.SDR E81R2013052970025Tube · disconnectedINVESTIGATED SOURCE OF FUEL STAINS NOTED ON RT WING INBD L/E INBD RT NACELLE AREA. FOUND RT ENGINE FUEL RETURN LINE TUBE ASSY. DISCONNECTED FROM FUEL RETURN LINE NACELLE FIREWALL BULKHEAD FITTING ON AFT (NACELLE) SIDE.SDR BSYR20120524049Unknown · malfunctionedON APPROACH TO PHL, LANDING GEAR WOULD NOT EXTEND. PILOT PROCEEDED TO MANUALLY CRANK LANDING GEAR DOWN AND LANDED SAFELY AT PHL WITHOUT INCIDENT.SDR 2013FA0000233Bearing · seizedDURING ENGINE START PROCEDURE, RT ENGINE WOULD NOT START. INSPECTION OF RT ENGINE MAGNETOS, THE LT MAGNETO WAS FOUND TO BE HARD TO ROTATE DUE TO DRIVE END BEARING FAILURE. NO OTHER DAMAGE WAS FOUND WITH MAGNETO. STIFF / FROZEN BEARING WAS CAUSING IMPULSE COUSDR 2013FA0000212Servo · defectiveTHE PITCH SERVO OVERHEATED CAUSING SMOKE IN THE COCKPIT. THE CURRENT LIMITING RESISTOR HAD MELTED. THE PILOT REPORTED THAT THE AIRCRAFT HAD EXPERIENCED SOME MINOR PORPOISING PRIOR TO THE SMOKE. THIS IS THE THIRD TIME THIS ACFT HAS EXPERIENCED THIS PROBLEM ASDR PAI5201302261142Exhaust Stack · brokenPILOT NOTED RT ENGINE EGT INDICATOR INOPERATIVE IN CRUISE FLIGHT. MX FOUND EXHAUST STACK BROKEN IN 2 JUST FORWARD OF EGT PROBE. NO DAMAGE TO COWLING NOTED.SDR 2013FA0000153Gear · wornUPON REMOVAL FROM ENGINES, IT WAS DISCOVERED THAT BOTH CAM GEARS SHOWED EXCESSIVE WEAR ON 2-3 TEETH. THE CAUSE FOR THIS WEAR CANNOT
BE DETERMINED. A SUGGESTION FOR PREVENTION WOULD NOT BE POSSIBLE.SDR EA39201303010001Landing Gear · collapsedLT MLG COLLAPSED ON LANDING. GEAR INDICATOR SHOW ALL 3 GEARS DOWN & LOCKED BEFORE TOUCHDOWN. THE LT GEAR FOLDED IMMEDIATELY UPON TOUCHDOWN. INSPECTION OF MAIN GEAR SYS REVEALED HEAVY DAMAGE TO THE SYS THEREFORE IT IS UNABLE TO KNOW EXACTLY THE RIGGING POSITSDR 2013FA0000059Bearing · seizedDURING ENGINE RUN-UP, BEFORE TAKEOFF WHEN THE RT ENGINE, RT MAGNETO WAS CHECKED IT WAS FOUND TO BE INOPERATIVE. ACFT RETURNED TO BLOCK. RT ENGINE, RT MAGNETO WAS REMOVED AND FOUND HARD TO ROTATE BY HAND. OPENED MAGNETO AND FOUND TO BE SCORCHED AND MELTED DUSDR 2013FA0000058Bearing · seizedDURING ENGINE RUN-UP BEFORE TAKE OFF WHEN THE RIGHT ENGINE RIGHT MAGNETO WAS CHECKED THERE WAS EXCESSIVE RPM DROP. AIRCRAFT RETRUNED TO BLOCK. RIGHT ENGINE, RIGHT MAGNETO WAS REMOVED AND FOUND VERY HARD TO ROTATE BY HAND. OPENED MAGNETO AND FOUND NO VISUAL INDSDR 2013FA0000025Coil · shortedDURING RUN-UP BEFORE TAKEOFF, THERE WAS EXCESSIVE RPM DROP ON RT ENGINE, RT MAGNETO. REMOVED RT MAGNETO. REMOVED BACK COVER AND MAG HAD A BURNED ELECTRICAL ODOR. REMOVED COIL AND FOUND TO BE ARCING TO CASE. LOOKS LIKE THERE WAS A SMALL CRACK IN COIL HOUSIN
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