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 = '767204' 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 = '767204' 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 AUS20010803Actuator · faulty(AUS) LH MAIN LANDING GEAR FORWARD DRAG BRACE DOWNLOCK ACTUATOR FAULTY. INVESTIGATION FOUND THE ACTUATOR PISTON ROD DETACHED FROM THE ACTUATOR BODY DUE TO FAILURE OF THE PISTON ROD IN THE THREADEDAREA WHICH ENGAGES THE PISTON RETAINING NUT.SDR AUS20010672Pin · missing(AUS) FLAP BYPASS VALVE ROTARY ACTUATOR PIN MIGRATED OUT OF POSITIONLEVER.SDR AUS20010580Oxygen Mask · faulty(AUS) PASSENGER OXYGEN MASKS (7OFF) SUSPECT FAULTY. FOUND DURINGINSPECTION IAW AD/B767/125.SDR AU010383Stringer · cracked(AUS) STRINGER 32L LOCATED AT STN 1085 CRACKED. CRACK LENGTH 114.3MM(4.5IN).SDR AU010351Slide · misinstalled(AUS) ESCAPE SLIDE FITTED TO DOOR LT 1 INCORRECTLY FITTED FOLLOWINGHEAVY MAINTENANCE. INSPECTION FOUND THAT THE SLIDE BAR WAS IN THE STOWED (TRANSPORT) POSITION AND WAS NOT CONNECTED TO THE GIRT BAR. FURTHER INVESTIGATION FOUND THAT THE ESCAPE SLIDES ONTHE OTSDR AU001331Seat Back · cracked(AUS) CAPTAINS SEAT BACK VERTICAL ADJUSTMENT TRACKS PNO 812072-7 ANDPNO 812072-8 CRACKED FROM THE UPPER EDGE OF THE AFT TRACK FLANGE. CRACK LENGTH 30MM (1.18IN).SDR AU000442Structure · damaged(AUS) NOSE LANDING GEAR INADVERTANTLY RETRACTED DURING OVERNIGHT MAINTENANCE. EXTENSIVE DAMAGE WAS CAUSED TO THE FUSELAGESTRUCTURE IN THE NOSESDR AU000398Hose · leaking(AUS) HORIZONTAL STABILISER TRIM CONTROL MODULE HYDRAULIC HOSE LEAKING. LOSS OF HYDRAULIC FLUID. HOSE IS ORIGINAL FITMENT ITEM FROM AUGUST 1987.SDR AU000116Pin · cracked(AUS) RT ENGINE PYLON MIDSPAR FITTING INBOARD FUSE PIN CRACKEDINTERNALLY. CRACK LENGTH 19.050MM (0.75IN). FOUND DURING EDDY CURRENT INSPECTION.SDR AU000350Frame · cracked(AUS) LT ENGINE PYLON TOP WEB CRACKED AT THE FORWARD INBOARD CORNER OFTHE POWER FEEDER CABLE CUTOUT. CRACK LENGTH 9.525MM (0.375IN).SDR AU000887Cvr · faulty(AUS) COCKPIT VOICE RECORDER (CVR) FAULTY. WORKSHOP INVESTIGATION FOUND INTERMITTENT FAILURE DUE TO TAPE DEPOSIT ON RECORDING HEADS CAUSING LOW AUDIO ON TRACK 2.SDR AU000066Wire Rope · frayed(AUS) RT AILERON CONTROL CABLE A4B-3 FOUND FRAYED AT WING STATION 531 FAIR LEAD. ALL STRANDS EXCEPT THE HEART STRAND WERE BROKEN. THE ADJACENT WIRE ROPE A4A-3 HAD BROKEN WIRES AND THE ENTIRE LENGTH OF BOTH WIRE ROPE RUNS WAS WORN AT THE FAIR LEAD LOCATIONS.SDR AU000053Valve · fractured(AUS) LEFT HYDRAULIC SYSTEM HP FILTER MODULE PRESSURE RELIEF VALVE BODY FAILED AT O- RING GROOVE.SDR AU990453Structure · damaged(AUS) AIRCRAFT SUFFERED HAIL DAMAGE TO THE FOLLOWING AREAS: 1. LT INBOARD AND OUTBOARD AILERONS. 2. LT AND RT LEADING EDGE SLAT WEDGES. 3. LT AND RT INBOARD AND OUTBOARD FLAP TRAILING EDGES. 4. NR 10 SPOILER. 5. VERTICAL STABILIZER RT SIDE LEASDR AU990407Wedge · disbonded(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES DISBONDED AND CORRODED ON THE FOLLOWING SLATS: SLAT NR 1. DISBOND 150 MM BY 40 MM (5.905 INCHES BY 1.574 INCH) AT INBOARD END, 30 MM (1.181 INCH) FORWARD OF TRAILING EDGE. DISBOND 180 MM BY 12 MM (7.086 INCHES BSDR AU990146Gear · corroded(AUS) NR 3 OUTBOARD AND NR 4 INBOARD LEADING EDGE SLAT ROTARY ACTUATORS CONTAINED INTERNAL CORROSION ON THE RING GEAR BEARING SURFACES AND THE PLANET GEAR P/N 256T2152. FOUND DURING VISUAL INSPECTION IAW ER B76-27-80-27 (AD/B767/095). PART TC: 51,949.SDR AU990037Wedge · disbonded(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES FOUND WITH DISBONDED AREAS ON A TOTAL OF SEVEN SLATS. FOUND DURING VISUAL AND ULTRASONIC INSPECTIONS IAW BOEING ALERT SB 767-57A0039.SDR AU990036Web · cracked(AUS) LEFT ENGINE PYLON TOP WEB CRACKED AT THE REAR OUTBOARD CORNER OF ONE WEB CUT-OUT. CRACK LENGTH 9.53 MM (0.375 INCH). FOUND DURING EDDY CURRENT INSPECTION.SDR AU981478Apu · failed(AUS) APU FAILED. REAR BEARING HOUSING AND OIL SCAVENGE PUMP FOUND ON THE RAMP. PART TC: 27,149.SDR AU981222Slat · delaminated(AUS) NR 1 AND NR 3 LEADING EDGE SLAT TRAILING EDGES DELAMINATING.SDR AU981170Seat Belt · faulty(AUS) PASSENGER SEAT BELTS LOCATED AT 19D, 23E, 30C, 32E, 33E AND 34C AS WELL AS THE FIRST OFFICER'S SEAT BELT HAD MISSING ID LABELS. FOUND DURING INSPECTION IAW ER Z1-25-00-10J (AD/RES/29).SDR AU981152Slat · delaminated(AUS) NR 2 LEADING EDGE SLAT TRAILING EDGE WEDGE DELAMINATED IN FOUR AREAS. FOUND DURING INSPECTION IAW AD/B767/73.SDR AU980063Skin · damaged(AUS) FUSELAGE SKIN AND STRINGER 31R LOCATED AT STN 485 DAMAGED BY FORK LIFT DURING LOADING OF FORWARD CARGO HOLD.SDR AU971069Seal · leaking(AUS) RAM AIR TURBINE (RAT) HYDRAULIC PUMP HOUSING SEALS LEAKING.SDR AU970698Cylinder · corroded(AUS) LH MAIN LANDING GEAR OUTER CYLINDER FORWARD TRUNNION CONTAINEDSEVERAL AREAS OF CORROSION
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