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 = '560' 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 = '560' 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 96ZZZX5323Elbow · looseDURING REPAIR OF FUEL PANEL, PN 611BB, RT CENTER STUB WING, THE STATED ELBOW WAS FOUND LOOSE AT BOTH B-NUTS, ONE ONLY ENGAGED BY HALF OF A TURN. NUTS WERE TIGHTENED AND TORQUED IAW MAINTENCE. THIS AREA IS NOT INSPECTED UNTIL THE PHASE 5 1,200-HOUR INSPECTIONSDR 96ZZZX5358Rib · crackedDURING PHASE INSPECTION, FOUND RUDDER TO HAVE UNUSUAL NOISE WHEN MOVED. NO EXTERNAL DEFECTS NOTED. INSPECTED WITH BORESCOPE AND FOUND RIB WITH APPROXIMATELY 2.3750 INCH CRACK ORIGINATING AT FORWARD LIGHTENING HOLE. NEW RIB INSTALLED AND RUDDER BALANCED.SDR 96ZZZX5966Duct · crackedDURING A PHASE INSPECTION, BOTH THE LT AND RT ENGINE INLET OUTER DUCT SKINS WERE FOUND TO HAVE SEVERAL CRACKS EMANATING FROM THE RIVET HOLES TO THE SKIN EDGES WHERE THE DUCT IS RIVETED TO THE INLET LIP. DISCUSSION WITH MANUFACTURER DETERMINED THE SUSPECT CAUSSDR 96ZZZX3457Transducer · out of calibCOMPARING AOA TRANSDUCER VANE WITH SISTER ACFT, FND VANE TRAVEL SUSPECT. CHECKED WITH ELEC PROTRACTOR, FND TRANSDUCER OUT OF CALIBRATION. INTERNAL STOPS HAD MOVED. ON PRE-FLIGHT, PILOT'S AOA ROTARY TEST WITH POWER ON ACFT SYS TESTS OK. STICK SHAKER, IND, LISDR 96ZZZX1955Switch Wire · chafedAIRCRAFT WAS EXPERIENCING PERIODIC UNCOMMANDED LT BOOST PUMP OPERATION WITH LT BOOST PUMP AND LT FUEL LOW PRESSURE ANNUNCIATOR LIGHTS COMING ON. PROBLEM FOUND TO BE CAUSED BY THE LT ENGINE FUEL PRESSURE SWITCH WIRES HAD CHAFED THROUGH AGAINST THE SHARP EDGE OSDR 96ZZZX762Wire · chafedFLIGHT CREW REPORTED A GEAR UNSAFE LIGHT WITH GEAR DOWN AND THREE GREEN (NO HYDRAULIC POWER ON LIGHT), ANTI-SKID INOPERATIVE LIGHT ON AND GEAR HORN SOUNDING. FOUND WIRING CHAFED/DAMAGED AT RT WS 54.07 RIB FEED-THROUGH IN THE TRAILING EDGE. REPAIRED WIRING, SSDR 95ZZZX7036Brake · defectiveAIRCRAFT HAD BEEN TO NUMEROUS SHOPS WITH WEAK OR NO BRAKES (THE BRAKES WOULD NOT HOLD THE AIRCRAFT STILL WITH MORE THAN 1700 RPM). MAINTENANCE MANUAL SAYS THAT ALL THICK PADS MAY BE NEEDED OR IT MAY NEED THIN PADS ON ANVIL SIDE AND THICK PADS ON PISTON SIDE. SDR 95ZZZX6307Switch · failedWHILE PERFORMING A GEAR RETRACTION CHECK PER A PHASE 2 INSPECTION, THE FOLLOWING PROBLEM WAS NOTED. UPON SELECTION OF GEAR UP, MAIN GEAR WENT UP AND LOCKED, BUT NOSE GEAR DID NOT. NOSE GEAR DID COME OFF OF DOWNLOCK, BUT WHEN MAINS WENT UP AND LOCKED, NOSE GESDR 95ZZZX3641Controller · inoperativePRESSURE CONTROLLER INOP. REPLACED CONTROLLER, SYSTEM OPERATES NORMALLY. NO FURTHER PROBLEMS.SDR 95ZZZX2249Bypass Duct · crackedWHILE PERFORMING OTHER MAINTENANCE ON THE AIRCRAFT, A TECHNICIAN NOTED LIGHT SHOWING THROUGH THE TAILPIPE FROM THE BYPASS DUCT TO THRUST REVERSER ATTACH FLANGE. THE COWLING RING WAS REMOVED AND THE OUTBOARD T/R ATTACH FLANGE WAS FOUND CRACKED AND DEFORMED. OSDR 95ZZZX2101Inlet · duct crackedDURING INSPECTION, THE DEICE DUCT OF THE LEFT ENGINE INLET WAS FOUND CRACKED AT THE BLEED PIPE FLANGE. THIS INLET WAS THE LATEST MOD, UPDATED TO RE-ENFORCE THIS AREA TO PREVENT CRACKING. CESSNA HAS BEEN ALERTED TO THIS SITUATION. INLET WAS INSTALLED AS A RESDR 95ZZZX2100Inlet · duct crackedDURING INSPECTION, THE DEICE DUCT OF THE RIGHT ENGINE INLET WAS FOUND CRACKED AT THE BLEED PIPE FLANGE. THIS INLET IS THE LATEST MOD, UPDATED TO RE-ENFORCE THIS AREA TO PREVENT CRACKING. CESSNA HAS BEEN ALERTED TO THIS SITUATION. INLET WAS INSTALLED AS A RESDR 95ZZZX1172Duct · tornPILOTS SQUAWKED THE RT ENGINE ANTI-ICE LIGHT CAME ON DURING DESCENT WHEN THE POWER WAS REDUCED TO 76 PERCENT N2. TROUBLESHOOTING THE SYSTEM REVEALED TWO PROBLEMS. NR 1: THE 300 DEGREE TEMPERATURE SWITCH WAS ACTUATING AT 340 DEGREES. NR 2: THE RAM AIR DUCTSDR 95ZZZX1171Switch · defectivePILOTS SQUAWKED THE RT ENGINE ANTI-ICE LIGHT CAME ON DURING DESCENT WHEN THE POWER WAS REDUCED TO 76 PERCENT N2. TROUBLESHOOTING THE SYSTEM REVEALED TWO PROBLEMS. NR 1: THE 300 DEGREE TEMPERATURE SWITCH WAS ACTUATING AT 340 DEGREES. NR 2: THE RAM AIR DUCT
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