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 = 'A36' 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 = 'A36' 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 96ZZZX2456Battery · leakingCONDUCTING A 91.207 INSPECTION OF ELT, FOUND BATTERY LEAKING 12 MONTHS AFTER INSTALLATION. THIS IS THE SECOND MERL BATTERY FOUND IN THIS CONDITION.SDR 96ZZZX1933Control Cable · brokeRIGHT RUDDER CABLE BROKE IN TAIL SECTION AT THE LAST PULLEY. APPARENTLY, THE CABLE HAD BEEN ROUTED INCORRECTLY FROM THE FACTORY. THE ROUTING OF THIS CABLE AT THE PULLEY IS VERY DIFFICULT TO SEE UNDER NORMAL INSPECTION CONDITIONS. THERE WAS NEVER ANY CONTROLSDR 96ZZZX1625Handle · misinstalledTHE AFT DOOR HANDLE INSIDE AFT CABIN ON BEECH A36 BONANZA AND BEECH 58 BARON AIRCRAFT USE A HANDLE WITH A PUSH BUTTON. A PROBLEM WAS FOUND ON THE AIRCRAFT IN QUESTION DURING A PRE-PURCHASE INSPECTION. THE DOOR HANDLE WAS IMPROPERLY INDEXED ON THE SQUARE MOUNTSDR EY2R9600390Dowel · corrodedDOWEL FOUND CORRODED.SDR EY2R9600389Blade · corrodedBLADE, SN BF318, FOUND CORRODED.SDR EY2R9600388Blade · corrodedBLADE, SN BF307, FOUND CORRODED.SDR EY2R9600387Blade · corrodedBLADE, SN BF319, FOUND CORRODED.SDR EY2R9600310Retain Bearing · corrodedRETAIN BEARING FOUND CORRODED.SDR 96ZZZX951Brake Disc · holes brokenDURING ROUTINE INSPECTION, FOUND BRAKE DISC LOOSE ON WHEEL. FOUND ALL 3 BRAKE DISC BOLT HOLES BROKEN OUT. WHEEL HALF BOLTS PROPERLY TORQUED. LOOSE BRAKE DISC CAUSED DAMAGE TO LOWER TORQUE LINK AND TO BRAKE CARRIER. SUBMITTER RECOMMENDS CLOSE INSPECTION DURSDR 95ZZZX6611Valve · burnedPILOT REPORTED LOSS OF RPM, ENGINE ROUGHNESS IN CRUISE FLIGHT, CONFIRMED BY EXTREMELY HOT INDICATION ON AIRCRAFT EGT SCANNER. NR 6 CYLINDER POSITION, FOUND NR 6 CYLINDER EXHAUST VALVE BURNED THROUGH, SEAT DETERIORATED BEYOND LIMITS. REMOVED NR 4 CYLINDER TO SDR 95ZZZX6610Cylinder · guide wornPILOT REPORTED LOSS OF RPM, ENGINE ROUGHNESS IN CRUISE FLIGHT, CONFIRMED BY EXTREMELY HOT INDICATION ON AIRCRAFT EGT SCANNER. NR 6 CYLINDER POSITION, FOUND NR 6 CYLINDER EXHAUST VALVE BURNED THROUGH, SEAT DETERIORATED BEYOND LIMITS. REMOVED NR 4 CYLINDER TO SDR 95ZZZX6818Seal · misgluedDURING THIS AIRCRAFT'S FIRST ANNUAL INSPECTION, THE LT EMERGENCY EXIT WINDOW WAS EXTREMELY DIFFICULT TO OPEN. IT WAS LATER DISCOVERED THE SEAL HAD BEEN GLUED ON BOTH SIDES AND, THEREFORE, HAD GLUED THE EMERGENCY EXIT CLOSED. SUBMITTER SUGGESTS UPON DELIVERY SDR 95ZZZX6551Rocker Shaft · bolt shearedNR 2 CYLINDER VALVE COVER REMOVED FROM PUSHROD TUBE SEAL REPLACEMENT. FOUND FORWARD ROCKER SHAFT THROUGH-BOLT IN 3 PIECES. BOLT SHEARED FLUSH IN CYL HEAD, ALSO, INSIDE ROCKER SHAFT. APPROX .3125 INCH HOLE IN FWD SHAFT HOLDER WAS FND ENLARGED TO .50 INCH. ESDR 95ZZZX6164Relay · wrong partELECTRICAL SYSTEM WOULD MOMENTARILY DROP OFF-LINE WHEN GEAR WAS RETRACTED. FOUND BATTERY AND STARTER RELAY TYPES REVERSED, INTERMITTENT DUTY RELAY INSTALLED IN BATTERY POSITION. INSTALLED NEW CORRECT P/N RELAYS IN BATTERY AND STARTER POSITIONS. NEW DIODES FSDR 95ZZZX6922O-Ring · leakingFUEL STAINS NOTED ON OIL FILTER, LOWER LEFT FIREWALL. FUEL WAS LEAKING IN A HIGH PRESSURE STREAM FROM A BAD 'AN' 123956 O-RING ON THE LEFT SIDE OF ENGINE DRIVEN FUEL INJECTOR PUMP HIGH PRESSURE METERING SCREW. THIS FUEL GLANCED OFF THE OIL FILTER, HIT THE LOSDR 95ZZZX6764Seal · leakingTHE GARLOCK SEAL OR LIPPED SEAL ON THE AIR CONDITIONER PULLEY SHAFT WHICH STICKS OUT THE AFT SIDE OF THE STARTER ADAPTER (THE SHAFT WITH THE CASTELATTED NUT AND COTTER PIN ON THE AFT FORWARD OF IT), WAS LEAKING OIL. HARD TO LOCATE LEAK AT THIS SEAL AS IT LOOKSDR 95ZZZX5921Filter Assy · brokenPILOT REPORTED A FUEL LEAK FROM THE ENGINE. INVESTIGATION REVEALED A LOOSE FILTER BOWL. ON A CLOSER EXAMINATION, FOUND FILTER BOWL HAD ALMOST DETACHED ITSELF FROM THE UPPER HOUSING. WHEN THE BOWL WAS FINALLY REMOVED, PART OF THE UPPER HOUSING TO WHICH THE FSDR 95ZZZX2729Pan · crackedHOLE HAD BROKEN OUT IN CENTER OF PAN. PAN IS FORMED FROM .032. NOTIFIED BEECH OF PROBLEM. INSTALLED A NEW PART. BEECH INDICATED THEY MAY USE .061 MATERIAL SOMETIME IN THE FUTURE.SDR 95ZZZX4018Regulator · malfunctionAIRCRAFT MADE FORCED LANDING (NO ELECTRICAL POWER). PILOT HAD TO PERFORM MANUAL LANDING GEAR EXTENSION. ON LANDING, NOSE GEAR COLLAPSED (GEAR WAS NOT FULLY EXTENDED). NEW PROPELLER INSTALLED AND ENGINE RUN-UP, TROUBLESHOOTING DETERMINED A FAULTY VOLTAGE REGSDR 95ZZZX3192Pump · defectiveENGINE RAN ROUGH AT ALTITUDE, AUTOMIX NOT WORKING. WOULD NOT AUTOLEAN.SDR 95ZZZX2902Anti-Ice System · contaminatedAEROSPACE SYSTEMS AND TECHNOLOGY, INC., TKS ANTI-ICE SYSTEM WAS INSTALLED IN THIS AIRCRAFT IAW STC SA2239C3 AND A 337 FORM. A BLADDER IN THE RIGHT WING HOLDS THE TKS FLUID WITH A FILLER CAP ON THE TOP WING SURFACE. THERE ARE WARNINGS ON EITHER SIDE OF THE FISDR 95ZZZX3144Magneto · mistimedINVESTIGATED PILOT COMPLAINT OF EXCESSIVE RPM DROP OF RIGHT MAGNETO ON RUN-UP. FOUND LEFT MAGNETO TIMED AT 24 DEGREES BTC AND RIGHT MAGNETO AT 13 DEGREES BTC. REMOVED AND PARTIALLY DISASSEMBLED RIGHT MAGNETO. FOUND INTERNAL TIMING CORRECT AND VISUAL INSPECTSDR 95ZZZW723Stop · worn on endPILOT REPORTED THAT THE CABIN ENTRANCE DOOR STOP WAS MISSING OR BROKEN. INVESTIGATION REVEALED THAT THE STOP HAD BECOME DISENGAGED FROM THE DOOR FRAME. THE AIRCRAFT HAS A HIGH NUMBER OF FLIGHT HOURS, AND THE STOP AND CHANNEL HAD BECOME WORN TO THE POINT THATSDR 95ZZZX2739Gear Warn · malfunctionAIRCRAFT STARTED TO LAND UNTIL PROP, FLAPS, AND STEP CONTACTED RUNWAY. A GO AROUND WAS INITIATED, LANDING GEAR WAS SELECTED DOWN AND A NORMAL LANDING WAS MADE. PILOT STATED HE DID NOT HEAR A GEAR WARNING HORN. AFTER AIRCRAFT WAS FERRIED HOME, GEAR SYSTEM CHSDR 95ZZZX2323Bracket · brokenSEVENTH STUD, CYLINDERS 2 AND 4: BRACKET BROKEN IN HALVES. ONE ONE-HALF FOUND LYING NEXT TO KEEL, OTHER ONE-HALF MISSING. (ANNUAL 100-HOUR INSPECTION.) REPLACED BRACKET AND NUT, PN 646312. SUSPECT CAUSE: PROGRESSIVE CRACK LEADING TO ULTIMATE FAILURE.SDR 95ZZZX1272Wire · chafedTHE WIRING BUNDLE FROM THE LANDING GEAR INDICATOR LIGHTS AND LANDING GEAR SELECTOR HANDLE ASSEMBLY CHAFED AGAINST THE LIGHTING BUS BAR ASSEMBLY PENETRATING THE INSULATION AND SHORTING THE WIRE TO THE BUS BAR. THIS ALLOWED UNREGULATED CURRENT FLOW THROUGH THE SDR 95ZZZX814Cell · delaminatedDURING A SCHEDULED INSPECTION OF THE AIRCRAFT, THE LT MAIN FUEL CELL INTERIOR WAS STARTING TO DELAMINATE. UPON REMOVAL OF THE FUEL CELL, INSPECTION OF THE INTERIOR DISCLOSED THAT CELL MATERIAL WAS PARTIALLY OBSTRUCTING THE FUEL CELL OUTLET STRAINER. SUBMITTESDR 95ZZZX635Cylinder · excess wearENGINE TT SINCE FACTORY OVERHAUL, 7726 HOURS. REBUILT 1-14-92. INSTALLED 2-12-92. CYLINDER HEAD DATES 8-91, ALL 6 CYLNDERS, LOW COMPRESSIONS ALL CYLINDERS. CYLINDERS ARE WORN BEYOND SERVICEABLE LIMITS AND SEVERE RING WEAR. ROCKER SHAFTS ARE SEVERELY WORN,SDR 95ZZZX556Field Wire · brokenINSPECTION OF THE AIRCRAFT'S ELECTRICAL SYSTEM FOUND A BROKEN FIELD WIRE AT THE TERMINAL END ATTACHMENT TO THE ALTERNATOR. THIS CAUSED A LOSS OF ELECTRICAL POWER AND DEAD BATTERY. PILOT PUT THE GEAR DOWN, GEAR ONLY WENT DOWN EST. 80 PERCENT, HOWEVER, LANDING
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