Continental TSIO-520-H

Service difficulty reports · 28

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 = 'TSIO520H'
  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 2014FA0000560Tube · failedENROUTE, MANIFOLD PRESSURE DROPPED TO 24". INDUCTION TUBE FROM COMPRESSOR TO THROTTLEBODY FAILED WITH A 2" TO 3" HOLE ONLEFT SIDE BLEW OUT.Jul 29, 2014 · N100BG · Cessna T210L · Aircraft Fuel Distribution SystemSDR CA090826018Cable · failedOWNER/PILOT REPORTED THAT AFTER LANDING, FLAPS WOULD NOT RETRACT TO FULL UP NOR DID FLAP INDICATOR INDICATE CORRECT POSITION OF FLAPS. TROUBLESHOOTING REVEALED THAT FLAP FOLLOW UP CABLE OUTER CASING SHATTERED JUST INBD OF ATTACH CLAMP IN ROOF ABOVE PILOTS HEAug 24, 2009 · Cessna T210K · Trailing Edge Flap Control SystemSDR 2009FA0000004Bolt · failedDURING CLIMB TO CRUISE ENGINE MADE A LOUD NOISE AND QUIT RUNNING, ENGINE REMAINED WINDMILLING TO LANDING. VISUAL INSP REVEALED NR 3 CYLINDER ROD BOLT MISSING, ROD CAP EXITED ENG THRU UPPER CASE, NO EVIDENCE OF OIL STARVATION.Dec 10, 2008 · N9426K · Cessna T210L · Reciprocating Engine Power SectionSDR CA061019009Spring · broken(CAN) NOTE THE SERIAL NUMBER ON THE ENGINE ON THIS FORM IS INCORRECT IT IS 217469-R. THE IMPULSE COUPLING SPRING WAS FOUND BROKEN. CUSTOMER HAD COMPLAINED OF ROUGH RUNNING CHECK MAG DROP, REMOVED MAGS AND INSPECTED. THE SPRINGS WERE BROKEN IN BOTH MAGNETOS,Oct 18, 2006 · Cessna T210L · Magneto/DistributorSDR CA061109004Bracket · loose(CAN) BRACKET P/N 1243019-2 FOUND LOOSE AGAINST TORQUE TUBE P/N 1234650-2. LOOSE FASTENERS REMOVED AND REPLACED. (TC NR 20061109004)Sep 22, 2006 · Cessna T210L · Elevator StructureSDR AU510001486Crankcase · damaged(AUS) CRANKCASE HOLED. LOSS OF POWER IN NR 4 AND NR 6 CYLINDERS. (CASA# 510001486)Dec 12, 2005 · Cessna T210L · Reciprocating Engine Power SectionSDR CA050302004Doubler · cracked(CAN) THE BULKHEAD DOUBLER REINFORCES THE HOLE WHERE THE HORIZONTAL STAB ATTCHES. DOUBLER SPLIT IN TWO THROUGH THE ANCHOR NUT RIVIT HOLE. THIS DOUBLER IS ONLY FOUND ON EARLY MODELS.Mar 21, 2005 · Cessna T210K · Horizontal Stabilizer, Attach FittingsSDR 2004FA0000580Bolt · missingWHILE MAKING A APPROACH TO THE AIRPORT FOR LANDING, THE PILOT ADDED POWER WITH NO ENGINE RESPONSE. THE THROTTLE CABLE DISCONNECTED FROM THE ENGINE CONTROL ARM DUE TO THE THROTTLE ATTACHING BOLT MISSING ALONG WITH THE WASHER, NUT AND COTTER PIN. THROTTLE WORKEDJul 14, 2004 · N2KD · Cessna T210J · FastenersSDR CA040622005Belt · failed(CAN) THE ALTERNATOR DRIVE BELT CAME OFF IN FLIGHT.Jun 6, 2004 · Cessna T210L · Alternator-Generator DriveSDR 2004FA0000432Pump · inoperativeENGINE DRIVEN FUEL PUMP NO METERED OR UN METERED FUEL PRESSURE WHILE ENGINE RUNNING. FUEL PUMP RECENTLY INSTALLED HAD 2.7 HOURS ON IT, AFTER OVERHAUL. INSTALLED NEWLY OVERHAULD PUMP. OPS CHECK GOOD. PROBABLE CAUSE OF PUMP FAILURE, UNKNOWN.May 21, 2004 · N93379 · Cessna T210L · Engine Fuel PumpSDR CA010503013Torque Link · cracked(CAN) UPPER NOSE GEAR TORQUE LINK FOUND CRACKED AS SHOWN. CRACK WAS IN TWO LOCATIONS ABOUT 1/8 INCH LONG. PART HAD NOT FAILED.THIS IS THE SECOND PART FOUND CRACKED ON CESSNA 210 AIRCRAFT, BOTH IN THE SAME LOCATION.Apr 18, 2001 · Cessna T210K · Nose/Tail Landing Gear Strut/AxleSDR 20010403CW012Rod · departedAIRCRAFT ARRIVED WITH RIGHT ENGINE OIL LEAK. FOUND OIL LINE TO BE LEAKING. REPAIRED OIL LINE AND SERVICED BACK UP WITH OIL. ENGINE WAS RERUN AND A ROD CAME LOOSE AND PENETRATED THE CRANKCASE. NO OTHER INFORMATION WAS RECEIVED, EXCEPT THAT THE ENGINE RAN OUFeb 24, 2001 · N5988M · Cessna 421B · Reciprocating Engine Power SectionSDR CA000802023Solenoid · failed(CAN) AFTER TAKEOFF AND LANDING SELECTED UP AND LOCKED. LANDING GEAR CIRCUIT BREAKER TRIPPED. (PROBLEM RETURNED INTERMITTENTLY.) PROBLEM TRACED TO DEFECTIVE LANDING GEAR SOLENOID. SOLENOID REPLACED, PROBLEM SOLVED.Jul 14, 2000 · Cessna T210L · Landing Gear Retraction/Extension SystemSDR CA000802024Bracket · cracked(CAN) DURING THE INSPECTION OF THE STABILIZER, A CRACK WAS FOUND ON THE INBOARD LT STABILIZER BRACKET TO ELEVATOR P/N 1232624-1 ATTACHED TO THE SPAR. PROBLEM WAS REPAIRED.Jul 14, 2000 · Cessna T210L · Elevator Control SystemSDR 20000522SH016Riser · crackedMAINTENANCE LOOKED AT ACFT BEFORE FLIGHT. COWLING WAS REMOVED AND EXHAUST SOOT WAS SEEN AROUND LOWER SIDE OF NR 4 CYLINDER. FURTHER INVESTIGATION REVEALED A CRACK AROUND THE EXHAUST RISER THAT WAS ABOUT 270 DEGREES AROUND THE PIPE. HEAT EXCHANGER PORTION OFMay 15, 2000 · N732JF · Cessna T210L · Engine Collector/Tailpipe/NozzleSDR 99ZZZX922Pin · mismanufacturedNEW VAR TYPE CRANK WAS RECEIVED TO REPLACE A NON-VAR TYPE. COUNTERWEIGHTS WERE AS INSTALLED BY TCM. COUNTERWEIGHTS WERE REMOVED TO CHECK PIN SIZES AND PART NUMBERS TO MAKE SURE TCM INSTALLED THE CORRECT ONES AND IN THE PROPER LOCATIONS. SUBMITTER FOUND THE TFeb 8, 1999 · Reciprocating Engine Power SectionSDR 98ZZZX1582Cylinder · separationINSPECTION FOUND NR 2 CYLINDER SEPARATED BETWEEN BORE AND HEAD.Apr 8, 1998 · Reciprocating Engine Cylinder SectionSDR AU980402Valve · worn(AUS) THREE ENGINE CYLINDERS REMOVED DUE TO LOW COMPRESSION. ALL EXHAUST VALVES PN 646286 AND VALVE GUIDES PN 636242 WERE FOUND TO BE WORN BEYOND LIMITS WITH 0.508MM (.020 INCH), 1.016MM (.041 INCH) AND 1.168MM (.046 INCH) CLEARANCES.Mar 24, 1998 · Cessna T210L · Reciprocating Engine Cylinder SectionSDR AU980392Structure · misinstalled(AUS) HORIZONTAL STABILIZER SPAR CAP CRACKED IN AREA OF THE LOWER REAR MOUNT BOLT HOLES. CRACK LENGTHS 12.7MM (0.5 INCH). INVESTIGATION FOUND NEW PN 1232624-1 REINFORCEMENTS (SE 84-17) HAD BEEN FITTED IN AMERICA (29JUL84), BUT HAD BEEN INSTALLED UPSIDE DOWN Feb 1, 1998 · Cessna T210M · Horizontal Stabilizer, Spar/RibSDR CA971027010Fuel Pump · rusted(CAN) RIGHT AUXILIARY FUEL PUMP FOUND RUSTED. ALSO LEFT AND RIGHT CHECK VALVES PART NO. FACKV-5-100-6 FOUND CLOGGED. THIS AS A RESULT OF INSTALLATION OF FLINT AUXILIARY SYSTEM STC SA2862WE, SA3266NM OR SA4300WE ACCORDING TO SUBMITTER.Jul 17, 1997 · Cessna T210L · Fuel Boost PumpSDR CA970506010Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. LEADING EDGE OF THE PROPELLER BLADE WAS FOUND DAMAGED. REWORK AND GRINDING WAS REQUIRED TO FIX THE AIRFOIL ON ALL BLADES.Apr 29, 1997 · Cessna T210L · Propeller Blade SectionSDR 97ZZZX2120Spring · brokenTROUBLESHOOTING OF 400 RPM MAG DROP FOUND LEFT MAGNETO TIMING AT 7 DEGREES BTC. REMOVED MAG AND FOUND IMPULSE COUPLING SPRING BROKEN TWO INCHES FROM OUTER END.Apr 23, 1997 · N93377 · Cessna T210L · Magneto/DistributorSDR 97ZZZX14Hub · crackedDURING 100 HOUR INSPECTION, FOUND PROP HUB CRACKED AT 5 OF THE 6 MOUNTING STUDS.Oct 31, 1996 · N8237M · Cessna T210K · Propeller Hub SectionSDR CA960826021Reinforcement · cracked(CAN) HORIZONTAL STAB REINFORCEMENT BRACKET REPLACED WITH HEAVIER REPLACEMENT PART SUPPLIED THROUGH CESSNA.Aug 8, 1996 · Cessna T210L · Horizontal Stabilizer StructureSDR 96ZZZX3774Cylinder · separatedPILOT REPORTED ROUGH ENGINE AND LARGE RPM DROP ON MAG CHECK. INSPECTION FOUND NR 3 CYLINDER CRACKED. WHEN CYLINDER REMOVED, IT WAS DISCOVERED THE HEAD WAS COMPLETELY SEPARATED. BOTTOM SPARK PLUG WAS FOULED.Jul 11, 1996 · N6308H · Cessna T207A · Reciprocating Engine Cylinder SectionSDR 96ZZZX4958Crankshaft · flange failedPROPELLER AND CRANKSHAFT PROPELLER FLANGE SEPARATED FROM ENGINE.Jul 5, 1996 · N7398M · Cessna T210M · Reciprocating Engine Power SectionSDR AU960602Link · broken(AUS) PROPELLER NO1 BLADE PITCH CHANGE LINK BROKEN - FURTHER INSPECTION FOUND INCORRECT BLADE RETENTION NUT 'O' RINGS FITTED - PROPELLER IS GREASE FILLED WITH OIL FILLED PROPELLER 'O' RINGS FITTED TO UNMODIFIED GROOVES - PERSONNEL/MAINTENANCE ERROR - UNAPPROVEMay 10, 1996 · Cessna T210L · Propeller Controlling SystemSDR 96ZZZX383Guide · wornINSTALLED 6 CERMICHROME CYLINDER REBUILT UNITS WITH 643767 GUIDES. 120 SMOA. COMPRESSION LEAK ON TWO CYLINDERS. PULLED ALL 6 AND RETURNED UNITS TO ECI. THEY DIAGNOSED AS JUST WORN OUT. THEY REPAIRED SAME AND SUGGESTED FULL FLOW LIFTERS AND DRILLED ROCKERSOct 15, 1995 · Reciprocating Engine Cylinder Section
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