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 = 'U206C' 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 = 'U206C' 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 4DSR2020701400001Reservoir · chafedDURING ANNUAL INSPECTION FOUND SEVERE CHAFING TO THE RT FUEL RESERVOIR TANK UNDER CO-PILOT'S FLOOR OUTBOARD. PART WAS WORN AT STANDPIPE AREA TO A DEPTH OF .043 INCH, CAUSED BY FLOOR CLOSEOUT PANEL INTERFERENCE.SDR 2014FA0000305Drag Link · failedNOSE GEAR COLLAPSE, ON LANDING. STRUCTURAL, PROPELLER, AND SUSPECTED ENGINE DAMAGE OCCURRED. INVESTIGATION REVEALED THAT THE NOSE GEAR DRAG LINK ASSEMBLY BROKEN AT THE WELD AT THE UPPER ATTACH POINT. IN CONTACT WITH MFG CONCERNING DISPOSITION.SDR CA130611007Bar · cracked(CAN) UPON LANDING FRONT SPREADER BAR DETACHED FROM LT FLOAT. UPON SUBSEQUENT INSPECTION FRONT SPREADER BAR SPAR EXHIBITS EVIDENCE OF PREVIOUS CRACKING TO WATER LANDING.SDR 2007FA0000036Lifter · deterioratedAFTER DRAINING OIL AND INSPECTING FILTER, LARGE FLAKES OF METAL WERE FOUND. DISASSEMBLED VALVE TRAIN AND FOUND SPALLING ON CYLINDER NR 6 INTAKE LIFTER. DAMAGE OCCURRED TO THE CORRESPONDING CAM LOBE AND CLYINDER NR 5 INTAKE LIFTER DUE TO DETERIORATION OF CYLISDR CA050302003Doubler · cracked(CAN) THE BULKHEAD DOUBLER REINFORCES THE HOLE WHERE THE HORIZONTAL STAB ATTACHES. DOULBER SPLIT IN TWO THROUGH ANCHOR NUT RIVIT HOLE. RESULTED IN BULKHEAD STA 209.0 P/N 1212402-2 CRACKING. THIS DOUBLER IS FOUND ON EARLY MODEL. LATER MODELS HAVE TWO DOUBLERSDR CA041110012Bolt · sheared(CAN) BOLT SHEARD ON LANDING CAUSING NOSE GEAR TO PIVOT FORWARD.NOTE - THIS BOLT WAS LAST CHANGED SEPT.9/94 AT 2875.1 T.T. (AIRCRAFT PRESENT T.T. IS 6238.7 HRS) THIS AIRCRAFT HAS OPERATED ON SKIS (SUSPECT THAT BOLT WAS OVERSTRESSED IN THIS CONFIGURATION) THIS SDR CA041125004Bolt · sheared(CAN) BOLT SHEARED ON LANDING CAUSING NOSE GEAR TO PIVOT FORWARD. NOTE: THIS BOLT WAS LAST CHANGED SEPTEMBER 9/94 AT 2875 I.T.T. (AIRCRAFT PRESENT TT IS 6238.7 HOURS) THIS AIRCRAFT HAS OPERATED ON SKIS (SUSPECT THAT BOLT WAS OVERSTRESSED IN THIS CONFIGURATION)SDR CA030410004Door Frame · cracked(CAN) UPON ANNUAL INSPECTION OF AIRCRAFT THE FORWARD LT DOOR POST WAS FOUND CRACKED ALMOST 1/2 WAY AROUND THE STRUCTURE. THE AIRCRAFT IS OPERATED ON WIPLINE FLOATS SO CONDITIONS FROM ROUGH WATER IS A POSSIBLE CONTRIBUTING FACTOR. THE AIRCRAFT HAS BEEN MAINTAINSDR CA030131005Bracket · cracked(CAN) HORIZONTAL STABILILZER REAR RT REINFORCEMENT ATTACH BRACKET WAS FOUND CRACKED .250 INCH LONG.SDR 010203Rib · misrepairedHORIZONTAL STABILIZER WAS REPAIRED AT AIRCRAFT TOTAL TIME OF 6658.5. 6 EACH NEW AND IMPROVED NOSE RIBS WERE INSTALLED AND NUMEROUS RIVETS WERE NOT INSTALLED IN THE REPLACED RIBS. REFERENCE SERVICE NEWSLETTER NR 87-18R1. RIBS THAT WERE DETERMINED TO BE REPLASDR 1BShimmy Dampener · misinstalledSHIMMY DAMPENER SLIDING SHAFT INSTALLED 180 DEGREES OUT. UNIT WAS OVERHAULED.SDR 20000517SH022Hub · crackedCRACK STARTING FROM O-RING GROOVE EXTENDING ACROSS FLANGE AREA. (X)SDR AU990430044Actuating Pin · corroded(AU) DURING INSPECTION THE PROPELLER BLADE ACTUATING PIN WAS FOUND CORRODED. IT WAS NOT REUSABLE. THE PIN WAS REPLACED.SDR AU990430041Bearing · corroded(AU) INSPECTION FOUND THE BLADE BEARINGS CORRODED BEYOND LIMITS. THE BLADE BEARINGS WERE NOT WITHIN REPAIRABLE LIMITS. THE BEARINGS WERE REPLACED.SDR AU990430040Cylinder · corroded(AU) INSPECTION FOUND THE INSIDE DIAMETER OF THE PROPELLER BLADE CYLINDERS PITTED AND CORRODED. THE CYLINDERS WERE REPLACED.SDR CA981006006Cylinder · cracked(CAN) CYLINDERS NR 3 AND NR 6 FOUND CRACKED ON INSPECTION.SDR AU981431Hub · corroded(AUS) PROPELLER HUB SEVERELY CORRODED.SDR AU980949Pump · worn(AUS) ENGINE OIL PUMP GEAR BUSHES WORN CAUSING THE GEARS TO RUB AGAINST THE PUMP BODY AND CAUSE WEAR TO THE HOUSING.SDR AU980948Camshaft · worn(AUS) CAMSHAFT FRONT LOBE WORN.SDR AU980947Gear · cracked(AUS) STARTER SHAFT GEAR TOOTH CRACKED. SUSPECT CAUSED BT BACKFIRE DURING START. FOUND USING NDT.SDR CA980430004Cylinder · cracked(CAN) ENGINE RUNNING ROUGH IN-FLIGHT. POST-FLIGHT INSPECTION FOUND A CYLINDER CRACKED AROUND THE EXHAUST VALVE SEAT.SDR CA971024013Door Post · cracked(CAN) IT WAS OBSERVED ON ONE OCCASSION THE WINDSHIELD APPEARED TO BE MOVING IN ITS LOWER RETAINER DURING WATER LANDINGS. MAINTENANCE ACTION INVOLVED REMOVING LOWER RETAINER REVEALING FORWARD DOOR POSTCHANNEL WAS CRACKED THREE INCHES. AT CRACK LOCATION, THERESDR AU961129Fuel System · wrong fuel(AUS) AIRCRAFT FILLED WITH AVTUR - ENGINE DAMAGED DUE TO DETONATION - METAL CONTAMINATION OF OIL SYSTEM - PERSONNEL/MAINTENANCE ERROR- UNAPPROVED PART (FUEL)SDR CA960202013Aft Strut Fittng · cracked(CAN)INSPECTION OF THE FLOATS REVEALED A CRACK RADIATING FROM THE BOLT HOLE OF THE AFT LEFT HAND FITTING WE FOUND THAT THE AN7 BOLT WAS SEIZED IN THE FITTING BY CORROSION TO SUCH AN EXTENT THAT IT SHEARED WHILE ATTEMPTING TO REMOVE IT. THE CORROSION BETWEEN T
Back to Cessna U206C