Textron T206H

Service difficulty reports · 157

Newest first. General aviation reporting is voluntary.

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 = 'T206H'
  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.

SDR 20010305CW002Landing Gear · collapsedGOT RT GEAR UNSAFE LIGHT, UNABLE TO GET LIGHT TO GO OUT. ON LANDING, ROLL OUT RT MAIN GEAR COLLAPSED, DAMAGING THE RT FLOAT. INSPECTION FOUND RT MAIN GEAR ACTUATING CONTROL SHAFT BROKEN. INSTALLED KIT, REPAIRED RT FLOAT KEEL AND SKINS THAT WERE DAMAGED.Aug 8, 2000 · N7255T · Cessna T206H · Main Landing GearSDR 20000802SH014Flow Divider · failedWHILE C/W TEXTRON-LYC SA 55-550 ENG RECALL, FUEL FOUND IN CRANKSCASE MIXED WITH OIL. TEXTRON CHECKED FUEL SYS, FOUND NO PROBLEMS. TECH REP INSPECTED INSTALL AND FOUND NO PROBLEMS WITH INSTALL, BUT NOTED FUEL DRIPPING FROM FUEL INJECTOR LINES WITH MIX AND THRJul 14, 2000 · N2467X · Cessna T206H · Fuel DividerSDR 20000714SH029Valve Seat · looseAIRCRAFT HAD ENGINE FAILURE AT 79 FLIGHT HOURS. THE NR 1 CYLINDER EXHAUST VALVE SEAT CAME LOOSE FROM THE CYLINDER AND CAUSED SIGNIFICANT DAMAGE TO THE ENGINE. THE OUTSIDE DIAMETER OF THE EXHAUST VALVE SEAT WAS FOUND UNDERSIZED. (X)Jul 14, 2000 · N2638U · Cessna T206H · Reciprocating Engine Cylinder SectionSDR 20000512SH020Nose Rib · crackedDURING ACFT''S FIRST 100-HR INSP, A .25 INCH LONG CRACK WAS FOUND IN A NOSE RIB OF THE LT AILERON. NOSE RIB IS AT THE AILERON''S CUT-OUT IN THE LEADING EDGE FOR THE INBD HINGE ATTACH POINT, ON THE OTBD SIDE. THE CRACK IS AT THE UPPER FWD CORNER OF THE NOSE Mar 23, 2000 · N2371H · Cessna T206H · AileronsSDR 20000512SH019Nose Rib · crackedDURING ACFT''S FIRST 100-HR INSP, A .25 INCH LONG CRACK WAS FOUND IN A NOSE RIB OF THE LT AILERON. NOSE RIB IS AT THE AILERON''S CUT-OUT IN THE LEADING EDGE FOR THE INBD HINGE ATTACH POINT, ON THE OTBD SIDE. THE CRACK IS AT THE UPPER FWD CORNER OF THE NOSE Mar 23, 2000 · N2371H · Cessna T206H · AileronsSDR 20000328SH008Gauge · leakingFOUND OXYGEN PRESSURE GAUGE IN OVERHEAD CONSOLE LEAKING. DISASSEMBLY OF THE OXYGEN MASK OUTLET PORTS TO GAIN ACCESS TO 2 RIVETS WAS NECESSARY. (X)Mar 7, 2000 · Cessna T206H · Crew Oxygen SystemSDR 20000403SH001Hose · burnedSCAVENGE OIL HOSE TO TURBOCHARGER BURNED UP BY EXHAUST PIPE. USED ALTERNATE ROUTE TO BYPASS EXHAUSE PIPE. (X)Jan 14, 2000 · N7264H · Cessna T206H · Exhaust Turbocharger
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