Continental TSIO-520-K

Service difficulty reports · 26

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 = 'TSIO520K'
  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 IKBR2019051709088Pulley · wornWHILE PERFORMING AN ANNUAL INSPECTION WE FOUND AIR CONDITIONING DRIVE PULLEY FOUND SEVERELY LOOSE. WE REMOVED PULLEY AND FOUND BEARING HAD SPUN INSIDE THE ALUMINUM PULLEY AND WORE THE PULLEY SEVERELY. PARTS AND NOT AVAILABLE FROM CIRRUS AT THIS TIME WE REMOVEDMay 14, 2019 · N512RD · Cirrus SR22T · Cabin Cooling SystemSDR AUS20040243Wire · broken(AUS) RT MAIN LANDING GEAR DOWNLOCK SWITCH WIRE BROKEN IN AREA APPROXIMATELY 763MM (3IN) FROM SWITCH.Mar 27, 2004 · Cessna 340CESSNA · Landing Gear System WiringSDR AUS20031197Diode · failed(AUS) LANDING GEAR ELECTRICAL CIRCUIT DIODE FAILED. INVESTIGATION FOUND POWER WAS BACK FEEDING FROM THE PRESS TO TEST CIRCUIT.Nov 14, 2003 · Cessna 340CESSNA · Landing Gear System WiringSDR AUS20031135Governor · cracked(AUS) LT PROPELLER GOVERNOR HEAD CRACKED. LOSS OF ENGINE OIL.Nov 7, 2003 · Cessna 340CESSNA · Propeller GovernorSDR AUS20030131Rod End · separated(AUS) MIXTURE CONTROL SYSTEM ROD END FAULTY.Jan 13, 2003 · Cessna 340CESSNA · Mixture ControlSDR AUS20020644Gearbox · worn(AUS) LANDING GEAR ACTUATOR REDUCTION GEARBOX GEAR TEETH WORN. ELECTRIC DRIVE MOTOR INTERMITTENT IN OPERATION AND CLUTCH INEFFECTIVE.May 21, 2002 · Cessna 340CESSNA · Landing Gear Retraction/Extension SystemSDR AUS20020433Bracket · cracked(AUS) LT ENGINE INDUCTION SYSTEM BALANCE TUBE FORWARD ATTACHMENT BRACKET BROKEN ALLOWING THE BALANCE TUBE TO SEPARATE FROM THE MANIFOLD.Apr 14, 2002 · Cessna 340CESSNA · Reciprocating Engine Cylinder SectionSDR 2002FA0000326Cylinder · brokenPILOT REPORTED PARTIAL LOSS OF POWER AND VIBRATION FROM RIGHT ENGINE ON CLIMB-OUT. UPON INSPECTION FOUND RIGHT ENGINE NR 2 CYINDER HEAD BROKEN IN THE AREA OF THE FOURTH AND FIFTH COOLING FINS. HEAD WAS COMPLETELY SEPARATED FROM THE BARREL AND WAS HELD IN PLAFeb 26, 2002 · N986CB · Cessna 340CESSNA · Reciprocating Engine Cylinder SectionSDR AUS20011386Bulb · burned out(AUS) NOSE LANDING GEAR DOWN AND LOCKED LIGHT BULBS (2OFF) BLOWN.Dec 18, 2001 · Cessna 340CESSNA · Landing Gear Position and WarningSDR AUS20011279Indicator · reads high(AUS) AIRSPEED INDICATOR FAULTY. INDICATOR WAS READING 180 KNOTS WHEN THE AIRCRAFT WAS STATIONARY. PITOT AND STATIC LINES CHECKED WITH NO FAULTS. ARTIFICIAL HORIZON ALSO TOPPLING IN FLIGHT.Oct 23, 2001 · Cessna 340CESSNA · Airspeed/Mach IndicatorSDR AUS20011007Pin · sheared(AUS) LANDING GEAR UPPER MANUAL EMERGENCY EXTENSION SYSTEM INTERCONNECT SHAFT SPROCKET ROLL PIN SHEARED.Aug 30, 2001 · Cessna 340CESSNA · Landing Gear Retraction/Extension SystemSDR AU010303Actuator · broken(AUS) RT MAIN LANDING GEAR MICROSWITCH ACTUATOR FAILED.Mar 31, 2001 · Cessna 340CESSNA · Landing Gear Position and WarningSDR AU010077Gear · faulty(AUS) ENGINE OIL SCAVENGE PUMP GEAR FAULTY. ROCKWELL HARDNESS TEST GAVE A READING OF 34 WHICH IS BELOW SPECIFICATION.Feb 6, 2001 · Reciprocating Engine Oil SystemSDR AU001054Pump · shorted(AUS) FUEL TRANSFER PUMP FAILED AFTER 287.8 HOURS OPERATION SINCE NEW. PREVIOUS FUEL PUMP AND FUEL TANKS HAD BEEN CONTAMINATED WITH EDA. (X)Nov 7, 2000 · Cessna 340CESSNA · Fuel Boost PumpSDR AU001053Relay · corroded(AUS) BATTERY RELAY COIL OPEN CIRCUITED DUE TO CORROSION CAUSED BY MOISTURE INGRESS. (X)Oct 31, 2000 · Cessna 340CESSNA · DC Generating SystemSDR AU000685Clamp · inadequate(AUS) ENGINE EXHAUST CLAMPS HAD UNKNOWN HOURS IN SERVICE. CLAMPS ARE LIFED AT 500 HOURS. C LAMPS WERE IN POOR CONDITION. (X)Sep 1, 2000 · Cessna 340CESSNA · Engine Collector/Tailpipe/NozzleSDR AU000686Seat Belt · inadequate(AUS) FORWARD SEAT BELT SHOULDER HARNESSES NOT FITTED. ITEMS HAD NOT BEEN REINSTALLED FOLLOWING INTERIOR REFURBISHMENT. (X)Sep 1, 2000 · Cessna 340CESSNA · Flight Compartment EquipmentSDR AU000687Control Cable · failed(AUS) LEFT AND RIGHT PROPELLER OUTER CONTROL CABLES SEPARATED AT SLIDE JOINT LOCATED AT PROPELLER GOVERNOR END. LEFT CABLE HAD BEEN REPAIRED BY LOCKWIRING THE ENDS TOGETHER. CABLES P/N 9910269-15 AND P/N 9910269-16. (X)Sep 1, 2000 · Cessna 340CESSNA · Propeller Controlling SystemSDR AU000688Bolt · misinstalled(AUS) LEFT AILERON TRIM ACTUATING ROD ATTACHMENT BOLT AND NUT NOT SPLIT PINNED. (X)Sep 1, 2000 · Cessna 340CESSNA · Aileron Tab Control SystemSDR AU000739Window · separated(AUS) COPILOT SIDE WINDOW SEPARATED IN-FLIGHT. (X)Sep 1, 2000 · Cessna 340CESSNA · Flight Compartment WindowsSDR AU000766Wire · shorted(AUS) PRESS TO TALK (PTT) SWITCH STUCK IN THE TRANSMIT' POSITION. INVESTIGATION FOUND THE THE PVT WIRE LOCATED IN THE CENTRE PEDESTAL UNDER THE THROTTLE QUADRANT WAS SHORTING OUT.Sep 1, 2000 · Cessna 340CESSNA · Communications System WiringSDR AU000779Aileron · seized(AUS) AILERONS JAMMED DURING CRUISE. AILERONS FREED DURING DESCENT. INVESTIGATION COULD FIND NO CAUSE OF JAMMING. SUSPECT ICING. (X)Aug 28, 2000 · Cessna 340CESSNA · Aileron Control SystemSDR AU000587Bolt · broken(AUS) ENGINE EXHAUST BOLTS BROKEN, ALLOWING EXHAUST GASSES TO INITIATE BURNING A HOLE IN THE AIRFRAME.Jul 7, 2000 · Cessna 340CESSNA · Engine Collector/Tailpipe/NozzleSDR AU990521Cylinder · separated(AUS) LT ENGINE NR 1 CYLINDER HEAD SEPARATED FROM THE CYLINDER BARREL. METAL CONTAMINATION OF OIL SYSTEM.May 22, 1999 · Cessna 340CESSNA · Reciprocating Engine Cylinder SectionSDR AU971459Gps System · faulty(AUS) GPS INTERFACE TO HSI AND AIRDATA SYSTEM FAULTY ALLOWING AIRCRAFT TO WANDER IN AUTOPILOT NAV MODE.Nov 24, 1997 · Cessna 340CESSNA · Global Positioning SystemSDR AU961162Bearing · loose(AUS) ALTERNATOR SLIP RING END BEARING INNER RACE LOOSE ON ROTOR SHAFTJun 27, 1996 · Cessna 340CESSNA · DC Generator-Alternator
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