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 = 'V35A' 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 = 'V35A' 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 2026FA0000624Bolt · corrodedPER BEECH SI 0572-031 AND BEECH SERVICE MANUAL, 35590096B, REISSUED: NOVEMBER 15, 1960; 35-590096B21, REVISED: AUGUST 29, 2003, PAGE 4-4M, THE WING BOLTS ARE TO BE MAGNETICALLY INSPECTED EVERY FIVE (5) YEARS AND REPLACED EVERY FIFTEEN (15) YEARS. SINCE MOST SDR 2011FA0000716Control Cable · misroutedDURING THE PERFORMANCE OF AN ANNUAL INSPECTION, FOUND THE RT RUDDERVATOR TRIM CONTROL CABLE WAS ROUTED INCORRECTLY AND HAD CUT THROUGH THE RT RUDDERVATOR CONTROL TUBE APPROX 75 PERCENT. THE TUBE ALSO HAS SIGNS OF A CRACK ORIGINATING FROM THE DAMAGED SECTION OSDR GYN2006F00000Alternator · damagedREMOVED ALTERNATOR PN 1100715, SN 5050822, FOR REPLACEMENT DUE TO NO VOLTAGE OUTPUT, INSPECTED ALTERNATOR AND CRANKSHAFT GEARS BEFORE INSTALLING ANOTHER SERVICEABLE ALTERNATOR. FOUND TEETH ON BOTH GEARS DAMAGED BEYOND SERVICEABLE LIMITS. PITTING/FLAKING. THISDR UIEA200600185Thrust Reverser · delaminatedMINOR LIGHTNING STRIKE EXIT NR 1 ENGINE LT THRUST REVERSER TRANSLATING SLEEVE 3" BY 1" TRAILING EDGE CARBON FIBER DELAMINATION APPROX 7 O/C LOOKING FORWARD.SDR UIEA200600093Acoustic Panel · damagedON DAILY CHECK, MAIN DECK CARGO STAIRS HANDLE WALL STOWAGE BRACKETS (2) FOUND DETACHED FROM LHS SIDE WALL PANEL ADJACENT MED 1L STA 520-540 WITH APPROX 3 INCH TEAR ON SURFACE COVERING OF FIBERGLASS PANEL. REPAIRED PER SRM 747-400F 51-70-06 ATLAS EO XEO 53-050SDR 2005FA0000955Wheel · corrodedTHIS KIT WAS PURCHASED NEW AND OF THE 4 WHEEL HALVES THAT ARE PART OF THE KIT, AFTER ONLY ONE YEAR OF USE, 3 SHOWED SUCH SIGNS OF CORROSION THAT IT IS QUESTIONABLE IF THE LIFE OF THE 3 WHEEL HALVES WOULD BE OVER 2 YEARS. AFTER ITS OWN INSPECTION, THE MANUFACTSDR 2005FA0000954Wheel · corrodedTHIS KIT WAS PURCHASED NEW AND OF THE 4 WHEEL HALVES THAT ARE PART OF THE KIT, AFTER ONLY ONE YEAR OF USE, 3 SHOWED SUCH SIGNS OF CORROSION THAT IT IS QUESTIONABLE IF THE LIFE OF THE 3 WHEEL HALVES WOULD BE OVER 2 YEARS. AFTER ITS OWN INSPECTION, THE MANUFACTSDR RE401338Lifter · chipped732 HRS TOTAL TIME, 622 HRS TIME SINCE OVERHAUL DUE TO PROP STRIKE. DURING ANNUAL INSPECTION OF AIRCRAFT, NUMBER 3 CYLINDER WAS REMOVED FOR LOW COMPRESSION 10/80. FOUND METAL, STEEL, ON SKIRT OF CYLINDER. NOTED VISUALLY THAT CAM WAS WORN DOWN IN CONTACT ARSDR 2002FA0001316Elt · will not testELT NOT TRANSMITTING ON AM RADIO OR 121.5 VHF FREQUENCIES. DOES NOT PASS CFR PART 91.207D TEST. ELT WAS INSTALLED DEC, 2001 (NEW) AND TESTED PROPERLY AT THAT TIME UNIT HAS BEEN SENT FOR REPAIR.SDR AUS20021119Pump · leaking(AUS) ENGINE DRIVEN FUEL PUMP LEAKING. SUSPECT FAULTY SHAFT SEAL.SDR AUS20021032Bracket · corroded(AUS) RH MAIN LANDING GEAR STRUT SQUAT SWITCH ATTACHMENT BRACKETCORRODED THROUGH.SDR 2001FA0000057Channel · corrodedUPON REMOVAL OF THE LARGE FLOORBOARD AFT OF THE SPAR, IT WAS NOTED THAT THE TEW MIDDLE/CENTER CHANNEL ASSEMBLIES WERE CORRODED. THE CORROSION WAS SO BAD THAT A TWO INCH AREA AND ONE INCH AREA ON THE OTHER THAT PROVIDES THE MOUNTING FOR THE SEAT RAILS WAS MISSSDR 99ZZZX4617Tube · chafedLOST FLIGHT INSTRUMENTS SHORTLY AFTER TAKEOFF. FOUND THE GYRO INSTRUMENTS WOULD TUMBLE WHEN THE GEAR WAS RETRACTED AND INSTRUMENT AIR PRESSURE DROP TO NEAR ZERO. AIR PRESSURE AND INSTRUMENT OPERATION RETURNED TO NORMAL WHEN GEAR WAS EXTENDED. INSPECTION FOUNSDR 99ZZZX2644Bulb · mismanufacturedTHE OIL TEMPERATURE BULB WAS TO BE REPLACED DUE TO INACCURATE TEMPERATURE INDICATION. THE REPLACEMENT PART WAS REJECTED BECAUSE THE WIRE STUD WAS LOOSE AND COULD BE ROTATED WITH FINGERS. THE PART WAS SENT BACK TO THE VENDOR FOR REPLACEMENT. THE VENDOR (KRN SDR 99ZZZX1212Alternator · failedINSTALLED ALTERNATOR AND UNIT FAILED TO OPERATE. AFTER INSPECTION, CAUSE OF FAILURE WAS THE BRUSHES. DURING ASSEMBLY, SOMEONE HAD PUT SOME TYPE OF EPOXY ON BRUSHES TO HOLD THEM IN THE BRUSH HOLDER. THIS, IN EFFECT, KEPT THE BRUSHES FROM MAKING CONTACT.SDR 99ZZZX1206Flap Track · wornFOUND FLAP TRACKS WORN BY ROLLERS. CANNOT BE PROPERLY DETECTED WITH FLAP INSTALLED, BOTH FLAPS. THIS IS SECOND AIRCRAFT IN 2 MONTHS.SDR 99ZZZX1205Flap Track · wornFOUND FLAP TRACKS WORN BY ROLLERS. CANNOT BE PROPERLY DETECTED WITH FLAP INSTALLED, BOTH FLAPS. THIS IS SECOND AIRCRAFT IN 2 MONTHS.SDR 98ZZZX187Control Tube · seizedPER AD 06-11-97, FOUND LEFT RUDDERVATOR TUBE WAS HOLDING TRAPPED WATER AND INBOARD BEARING WAS COMPLETELY SEIZED WITH RUST.SDR 97ZZZX4042Intercooler · leaksLEAKAGE AT OUTLET CONNECTION OF INTERCOOLER FOR TURBOCHARGER ON ENGINE. OUTLET OF INTERCOOLER IS SQUARE AND A ROUND RUBBER HOSE IS CLAMPED TO THE SQUARE OUTLET. OVER TIGHTNING OF CLAMP COULD CAUSE COLLAPSE OF OUTLET. HOSE PINCHES DURING CONNECTION AND LEAKSSDR AU970619Hub · faulty(AUS) PROPELLER HUB THREADS FAILED EDDY CURRENT INSPECTION - NO2 BLADE LOOSE IN HUB DUE TO BLADE NUT NOT BEING TORQUED AT LAST ASSEMBLY (SUSPECT AT INITIAL ASSEMBLY AT FACTORY APPROXIMATELY 20 YEARSPREVIOUSLY) - PERSONNEL/MAINTENANCE ERRORSDR EY2R9600107Hub · crackedHUB CRACKED IN THREAD AREASDR 96ZZZX4823Blade · crackedPROPELLER SUBMITTED FOR OVERHAUL/COMPLIANCE WITH AD 89-26-08, OIL FILL MODIFICATION TO DETECT BLADE/HUB CRACKS. UPON PENETRANT INSPECTION OF BLADE, A 1.25 INCH LONG CRACK WAS DISCOVERED IN THE SECOND RETENTION THREAD. ALSO, THE PROPELLER HUB, S/N 685951, WASDR AU960480Spar · cracked(AUS) FUSELAGE FRONT SPAR CARRY THROUGH SECTION CRACKED AT BOTH OUTBOARD SIDESSDR 96ZZZX2516Shaft · sheared pinAIRCRAFT ALTERNATOR WAS REPORTED INOPERATIVE. TROUBLESHOT AND FOUND ALTERNATOR GEAR RETAINING NUT HAD UNSCREWED FROM THE ARMATURE SHAFT. DISCOVERED INTERNAL CONDITION OF ARMATURE SHAFT TO BE WORN AT BEARING POINT. ALTERNATOR SHAFT SEIZED AND ROTATION OF THESDR 95ZZZX6745Seal · leaksSHORTLY AFTER REPLACING A REPAIRED NR 5 CYLINDER, OIL LEAKS DEVELOPED AROUND OUTBOARD ENDS OF SHROUD TUBES. COMPARISON TO ORIGINAL TCM PARTS SHOWED REPLACEMENT SEAL TO BE LARGER IN OUTSIDE DIAMETER CAUSING SEAL NOT TO PROPERLY FIT IN MACHINED RECESS CAUSING LSDR 95ZZZX2663Cylinder · crackedCRACKED CYLINDER FROM EXHAUST PORT AROUND CYLINDER HEAD TO SPARK PLUG HOLE, THREE-FOURTHS SEPARATED FROM BARREL.
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