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 = 'G36' 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 = 'G36' 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 2024FA0000857Elt · abnormalTHE ELT NEEDED TO BE REPROGRAMMED TO REFLECT "N" NUMBER CHANGE. LOCATION OF ELT WAS NOT PLACARDED AND THERE IS NO ACCESS PANEL FOR THE ELT. I WAS BARELY ABLE TO ACCESS THE ELT FOR REMOVAL AND INSTALLATION FROM AN AFT PANEL.SDR 2024FA0000957Alternator · faultedALTERNATOR WOULD INTERMITTENTLY GO OFF-LINE. ULTIMATELY HIGH FIELD RESISTANCE WAS DETERMINED TO BE A FACTOR....VOLTAGE REGULATOR AND ALTERNATOR WERE REPLACED. CONTINENTAL SB23-4 WAS COMPLIED WITH IN CONJUNCTIONSDR 2022FA0000467None · noneFOR AIRCRAFT N745SL MODEL G36 SN: E-3804
HOBBS: 789.7 IN MARCH 2022 THE STARTER ADAPTER WAS SENT OUT FOR OVERHAUL TO
AN APPROVED VENDOR, WESTERN SKYWAYS, INC CRS NO. WS9R575J.
THE OWNER OF N745SL E-3804 HAS RECENTLY REQUESTED TO HAVE THE ENGINE
OVERHAULED SDR YN82020F00000Exhaust Stack · crackedDURING OIL CHANGE, WITH THE RIGHT HAND LOWER COWL PANEL REMOVED, NOTICED THE AERODUCT HAVING EXHAUST RESIDUE ON IT. INSPECTED THE EXHAUST STACK AND FOUND THE LOWER FORWARD SEAM OF THE STACK TO BE SPLIT ABOUT 5 INCHES ABOVE THE MUFFLER ASSEMBLY. THE AREA OF TSDR 2018FA0000430Motor · failedAIR CONDITIONING RELAY MODULE FAILS AND LATCHES THE COMPRESSOR ON AS SOON AS BATTERY POWER IS ON. ALSO THE CONDENSER FAN IS FAILED AND WILL NOT COOL THE CONDENSER WHICH CREATES A OVER PRESSURE PROBLEM IN THE AC SYSTEM. WHEN THIS OCCURS THE COMPRESSOR CAN FAIL SDR 2018FA0000145Spring · brokenWHILE PERFORMING AN OIL CHANGE, OBSERVED BROKEN THROTTLE SPRING. THE SPRING GOES ON THE THROTTLE BODY SENDING ENGINE TO FULL THROTTLE IN THE EVENT THE THROTTLE CABLE WERE TO BREAK.SDR Z08R201803210001Tab · bentTHE RUDDER TRIM TAB WAS BENT TO THE RIGHT AT NEARLY 90 DEGREES. REPLACED.SDR PAIR20170713A3219Compressor · separatedTHE AIR CONDITIONER COMPRESSOR CLUTCH CAME OFF THE COMPRESSOR AND IMPACTED THE AVIONICS CURRENT LIMITER AND OTHER ELECTRICAL BUSS TERMINALS WHICH ARE LOCATED ON THE FIREWALL DIRECTLY BEHIND THE COMPRESSOR CLUTCH, THE PULLEY REMAINED INSTALLED TO THE COMPRESSSDR 14XR20160412001Pump · intermittentAFTER 1 HOUR WE WERE INSTRUCTED BY THE MAINTENANCE SHEET TO REDUCE POWER TO 65 PERCENT THEN ALTERNATE BACK TO 75 PERCENT. WE DECIDED WE WOULD DO THIS EVERY 15 MINUTES, AS THERE WAS NO TIME LISTED ON THE MAINTENANCE SHEET. WE REDUCED THE POWER TO 23" MANIFOLDSDR NF2R201812200001Lifter · galledINSPECTION FOUND #1 CYLINDER EXHAUST LIFTER IN EARLY STAGES OF SPALLING AS REFERENCED IN TCM SID05-1.SDR KC2R2014FA0000394Impulse Coupling · crackedIMPULSE COUPLING HUB BASE PLATE FOUND TO BE CRACKED AT ADVANCE STOP NOTCH. CRACK DISCOVERED USING NDT, MAGNETIC PARTICLE INSPECTION OF IMPULSE COUPLING DURING "500 HR INSPECTION" OF MAGNETO.SDR KC2R2014FA0000393Impulse Coupling · crackedIMPULSE COUPLING HUB BASE PLATE FOUND TO BE CRACKED AT ADVANCE STOP NOTCH. CRACK DISCOVERED USING NDT, MAGNETIC PARTICLE INSPECTION OF IMPULSE COUPLING DURING "500 HR INSPECTION" OF MAGNETO.SDR PAI5201401161393Mixing Valve · failedPILOT COMPLAINED OF NO CABIN HEAT. INSPECTION FOUND HEATER MIXING VALVE ON FIREWALL WITH BROKEN FLANGE, ALLOWING FLEX DUCT FROM HEAT MUFF TO COMPLETELY DISCONNECT FROM THE MIXING VALVE. FLANGE SHOWED VERY LITTLE WELD PENETRATION.SDR 2012FA0000827Cylinder Head · crackedNR 1 CYLINDER HEAD CRACKED FROM THE SPARK PLUG HOLE TO THE INTAKE VALVE SEAT AND LEAKING EXHAUST EXTERNALLY.SDR X0NR20120619001Contact · looseENGINE RAN VERY ROUGH & RPM DROPPED OFF ON LT MAGNETO DURING MAG CHECK. REMOVED LT MAGNETO. FOUND CONTACT POINT ON MOVEABLE ARM LOOSE & MOVING AROUND DURING POINT OPEN DWELL TIME. ON REMOVING POINTS & OPENING MANUALLY, CONTACT POINT FELL OUT OF ARM. CAPACSDR 2011FA0000630Autopilot Sys · failedAUTOPILOT FAILED TO DISENGAGE ON COUPLED APPROACH.SDR E81R20110830001Pin · missingINVESTIGATED PILOT COMPLAINT OF NOT BEING ABLE TO MOVE COPILOT'S SEAT FORWARD OR AFT. FOUND CENTER TRACK LOCKING PIN NOT LIFTING HIGH ENOUGH TO DISENGAGE FROM TRACK LOCK HOLES. AFTER REMOVING SEAT AND PARTIALLY DISASSEMBLING TRACK LOCKING MECHANISM, FOUND .0SDR 2011F00118Cylinder · cracked04/26/2011, OWNER FLYING AIRCRAFT, RECEIVED WARNING INDICATION/OVER TEMP ON 3RD CYLINDER. MADE UNSCHEDULED LANDING. UPON INSP, FOUND HOLE IN TOP OF CYLINDER ADJACENT TO SPARK PLUG. REMOVED AND REPLACED CYLINDER. VISUALLY INSPECTED OTHER CYLINDERS- NO DISCRSDR PIYR S261101160Strut · misalignedDURING LANDING GEAR RETRACTION TEST, IT WAS NOTED THAT THE NOSE WHEEL ASSY WOULD CONTACT THE RT NOSE GEAR DOOR, AFT HINGE DURING LANDING GEAR CYCLE. IT WAS ALSO NOTED THAT THE NOSE WHEEL ASSY WOULD CONTACT THE NOSE WHEEL WELL STRUCTURE WHEN FULLY RETRACTED. PSDR CA101123004Shaft · brokenSHAFT GEAR BROKE JUST AFTER THE END OF THE SCAVENGE GEAR DRIVE SPLINE UPON LANDING.SDR 2009FA0000838Tie Bolt · missingDURING AN INCOMING INSPECTION A MISSING WHEEL ASSY TIE BOLT WAS MISSING. (UNKNOWN OPERATOR, UNKNOWN REPAIR STATION...ADP)SDR 2008FA0000317Bolt · shearedTHE PILOT REPORTED A "POP" AS HE WAS GROUND HANDLING THE AIRCRAFT ON THE RAMP (IN A STRAIGHT DIRECTION USING AN AIRTUG). FURTHER INVESTIGATION REVEALED 1 NUT/BOLT COMBINATION HAD SHEARED ON THE INBOARD WHEEL HALF OF THE RIGHT MAIN LANDING GEAR ASSEMBLY. THE SDR 20080506FA001Bolt · shearedTHE PILOT REPORTED A "POP" AS HE WAS GROUND HANDLING THE AIRCRAFT ON THE RAMP (IN A STRAIGHT DIRECTION USING AN AIRTUG). FURTHER INVESTIGATION REVEALED 1 NUT/BOLT COMBINATION HAD SHEARED ON THE INBOARD WHEEL HALF OF THE RIGHT HAND MAIN LANDING GEAR ASSEMBLY. SDR CA070514010Engine · making metal(CAN) ON A TRAINING MISSION, THE ENGINE EXPERIENCED A LOSS OF THRUST (DURING TRAFFIC PATTERN STALLS) ACCOMPANIED BY A NOISE AND A CHIP DETECTOR INDICATION. THE PILOT DECLARED AN EMERGENCY AND ABORTED THE MISSION. SUBSEQUENT INSPECTION REVEALED METAL PARTICLSDR CA070314021Engine · making metal(CAN) DURING A TRAINING MISSION, THE ENGINE EXPERIENCED AN UNCOMMANDED REDUCTION IN POWER ACCOMPANIED BY A NOISE AND A CHIP DETECTOR INDICATION. SUBSEQUENT INSPECTION REVEALED METALLIC DEBRIS IN THE ENGINE OIL SYSTEM. MFG WILL INVESTIGATE THE EVENT AND ADVIS
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