Pratt & Whitney Canada PW206C

Service difficulty reports · 63

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 engine_model_key = 'PW206C'
  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 CA080116008Fitting · contaminated(CAN) DURING CRUISE, THE ENGINE POWER DECREASED UNCOMMANDED TO IDLE SETTING, FOLLOWED BY LOSS OF OIL PRESSURE. THE CREW ELECTED TO SHUTDOWN THE ENGINE AND RETURN TO BASE. INVESTIGATION FOUND THE P3 FITTING TO BE CONTAMINATED WITH FOREIGN DEBRIS. FITTING AND SYDec 20, 2007 · Agusta A109E · Engine (Turbine/Turboprop)SDR BAQA200700038Blade · separatedDURING NORMAL FLIGHT PILOT EXPERIENCED ABNORMAL VIBRATIONS. THE PILOT INITIATED AN EMERGENCY LANDING AND LANDED WITH THE GEARS UP IN A FIELD. MAINTENANCE PERSONNEL INSPECTED THE AIRCRAFT AND FOUND THE TIP CAP UPPER SKIN ON MAIN ROTOR BLADE P/N 709-0103-01-109 Nov 13, 2007 · N1UW · Agusta A109E · Main Rotor BladesSDR CA071003013Engine · power loss(CAN) DURING TAKEOFF, THE PILOT REPORTED A POWER LOSS ACCOMPANIED BY AN LOW TORQUE WARNING INDICATION. THE AIRCRAFT WAS DAMAGED IN THE RESULTING FORCED LANDING.Aug 5, 2007 · Agusta A109E · Engine (Turbine/Turboprop)SDR CA070914013Line · contaminated(CAN) ON TAKEOFF ENGINE POWER REDUCED UNCOMMANDED. SUBSEQUENT INSPECTION REVEALED CONTAMINATION / BLOCKAGE OF THE FUEL CONTOL P3 AIR PRESSURE FITTING AT THE NR 8 BEARING CARBON SEAL LOCATION. (TC NR 20070914013)Jul 23, 2007 · Urocop EC135P1 · Fuel Controlling SystemSDR 200700006Ecu · failedNR 1 ECU WARNING LIGHT ILLUMINATED IN FLIGHT. ALONG WITH THE NR 1 ECU CAUTION LIGHT NR 1 ECU FAIL LIGHT ILLUMINATED. THE NR 1 ENGINE WENT INTO MANUAL MODE. NO LIMITS WERE EXCEEDED. AIRCRAFT IS CURRENTLY IN MAINTENANCE TO TROUBLESHOOT PROBLEM.Feb 1, 2007 · N109DK · Agusta A109E · Fuel Controlling SystemSDR BAQA200700006Ecu · failedNR 1 ECU WARNING LIGHT ILLUMINATED IN FLIGHT. ALONG WITH THE NR 1 ECU CAUTION LIGHT NR 1 ECU FAIL LIGHT ILLUMINATED. THE NR 1 ENGINE WENT INTO MANUAL MODE. NO LIMITS WERE EXCEEDED. AIRCRAFT IS CURRENTLY IN MAINTENANCE TO TROUBLESHOOT PROBLEM. THE AC LANDED.Jan 31, 2007 · N109DK · Agusta A109E · Fuel Controlling SystemSDR BAQ2006F00001Bearing Race · crackedBEARING INNER RACE CRACKED. NOTED UPON DISASSEMBLY. (K)Jul 5, 2006 · N109UP · Agusta A109E · Standard Practices/StructuresSDR CA050725014Engine · making metal(CAN) THE ENGINE WAS REPORTED TO EMIT A NOISE ACCOMPANIED BY A CHIP DETECTOR INDICATION. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED MAGNETIC DEBRIS IN THE ENGINE. P&WC WILL INVESTIGATE Jul 9, 2005 · Agusta A109E · Engine (Turbine/Turboprop)SDR CA050419005Fuel Control · failed(CAN) DURING TAKEOFF, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION TO IDLE SPEED. THE FUEL CONTROL UNIT (FMM) WAS SUBSEQUENTLY REPLACED.Apr 8, 2005 · Agusta A109E · Fuel Control/Turbine EnginesSDR NXT2005F00000Spar · crackedA (4) INCH CRACK WAS DISCOVERED IN THE L/E SPAR DOUBLER OF THE VERTICAL FIN. ADDITIONALLY, (2) CRACKS WERE FOUND IN THE VERTICAL STABILIZER ASSY (NOT DETACHABLE). ONE CRACK MEASURED APPROX 5 INCHES AND ONE APPROXIMATELY 7 INCHES. A DETAIL BREAKDOWN OF THISMar 25, 2005 · N144CF · Agusta A109E · Rotorcraft Tail BoomSDR CA050112005Engine · malfunctionedTHE ENGINE EXPERIENCED A RAPID, UNCOMMANDED DECREASE IN TORQUE IN FLIGHT, ACCOMPANIED BY AN INCREASE IN OTHER ENGINE PARAMETERS. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO BASE. SUBSEQUENT INSPECTION REVEALED POWER TURBINE BLADE DAMAGE. PWC WILL Jan 9, 2005 · Agusta A109 · Turbine SectionSDR 11072110704Blade · crackedPILOT FELT VIBRATION IN TAIL ROTOR PEDALS DURING APPROACH. POST FLIGHT INSPECTION REVEALED THAT 1 TAIL ROTOR BLADE HAD A CHORD WISE CRACK BEGINNING AFT OF THE SPAR AND EXTENDING THROUGH THE TRAILING EDGE OF THE BLADE. THE CRACK WAS THROUGH BOTH SKINS AND THENov 7, 2004 · N200BK · Agusta A109E · Tail Rotor BladesSDR CA041026002Engine · fluctuates(CAN) ON A 'CAT A' TAKE-OFF (DURING THE REVERSING PHASE) THE PILOT REPORTED TORQUE FLUCTUATIONS ON THE NR 1 ENGINE. ALL ENGINE PARAMETER THEN WENT TO ZERO (ENGINE OUT). THE PILOT LOST CONTROL OF THE A/C, ITTURNED LT AND THE TAIL HIT AN OBSTACLE. THE PILOT COMPOct 23, 2004 · Agusta A109 · Engine (Turbine/Turboprop)
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