Continental TSIO-360-FB
Service difficulty reports · 49
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 = 'TSIO360FB' 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 engine_model_key = 'TSIO360FB' 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 2015FA0000189Cable · wornCOWL FLAP CABLE RUBBING ON EXHAUST ON LT SIDE OF ENGINE. RUBBED THROUGH THE OUTER COVER AND HALF THROUGH THE INNER CORE. THIS ACFT HAS HAD A REPLACEMENT COWL INSTALLED UNDER STC SA03470AT.SDR 2015FA0000190Housing · wornREPLACED COWL FLAP CABLE, PN LSM-SCD-032-1 DUE TO WORN SPOT NEAR CONNECTION TO COWL. COWL HAS BEEN REPLACE IAW STC SA03470AT. ACFT HAD TO MAKE AN UNSCHEDULED STOP DO TO SMOKE IN THE CABIN. INSPECTION FOUND CABLE COVERING MELTED DO TO BEING TO CLOSE TO THE EXSDR 2013FA0000438Switch · shortedACFT DEPARTED, DURING INITIAL CLIMB, EXPERIENCED A LOSS OF POWER AT APPROX 1000 FT AGL. PILOT SWITCHED FUEL TANKS, CYCLED FUEL PUMP, AND MAGNETOS IN AN ATTEMPT TO REGAIN TAKEOFF POWER. ACFT CRASHED IN A RURAL AREA. DAMAGED RT WING ASSY AND LANDING GEAR.SDR CA130412007Hub · damaged(CAN) UPON DISASEMBLY OF THE PROPELLER THE PRELOAD SHELVES SHOWED EVIDENCE OF PREVIOUS SEVERE PROPELLER IMPACT DAMAGE. ACCORDING TO PROPELLER MANUAL 202A THERE IS NO DAMAGE ALLOWED IN THIS AREA. THE CYLINDER CONTAINED IMPROPER REPAIRS TO THE SCREW HOLES. ITSDR CA120607009Coupling · failed(CAN) ELECTRICAL FAILURE REPORTED. INSPECTED CHARGING SYS AND FOUND ALTERNATOR DRIVE COUPLING FAILED.SDR CA111107008Fairing · damaged(CAN) VERTICAL FIN AFT TIP FAIRING FOUND CONTACTING RUDDER TOP SURFACE DURING GROUND HANDLING AND PRE-FLIGHT INSPECTION. FAIRING REMOVED AND FOUND MOUNTING HARDWARE HOLE ABNORMALLY OVERSIZED ALLOWING FOR AIRSTREAM TO MOVE FAIRING BOTTOM T/E TO CONTACT RUDDERSDR CA110906002Fork · damaged(CAN) UPON DISASSEMBLY AND VISUAL INSP OF THIS PROPELLER, WE FOUND 1 EA, A-2202 BEARING TO BE DENTED BEYOND REPAIR, THE HUB PRELOAD SHELVES TO BE DAMAGED FROM PREVIOUS IMPACT AT WHICH TIME THE HUB SHOULD HAVE BEEN SCRAPED OUT AND THE B-3252 FORK HAD BEEN DRILLSDR 2011FA0000406Seal · failedOVERHAULED AND INSTALLED CYLINDERS, PN EC641370CN IAW SERVICE INFO AND MFG SERVICE INFORMATION. DURING THE OVERHAUL INTAKE VALVE SEALS PN 646678 WERE INSTALLED ONTO INTAKE VALVE GUIDES IAW MFG ILLUSTRATED PARTS CATALOG. THE INTAKE VALVE SEALS FAILED AFTER APSDR 2011FA0000407Seal · failedOVERHAULED AND INSTALLED CYLINDERS, PN EC641370CN IAW SERVICE INFO AND MFG SERVICE INFORMATION. DURING THE OVERHAUL INTAKE VALVE SEALS PN 646678 WERE INSTALLED ONTO INTAKE VALVE GUIDES IAW MFG ILLUSTRATED PARTS CATALOG. THE INTAKE VALVE SEALS FAILED AFTER APSDR 2011FA0000408Seal · failedOVERHAULED AND INSTALLED CYLINDERS, PN EC641370CN IAW SERVICE INFO AND MFG SERVICE INFORMATION. DURING THE OVERHAUL INTAKE VALVE SEALS PN 646678 WERE INSTALLED ONTO INTAKE VALVE GUIDES IAW MFG ILLUSTRATED PARTS CATALOG. THE INTAKE VALVE SEALS FAILED AFTER APSDR 2011FA0000409Seal · failedOVERHAULED AND INSTALLED CYLINDERS, PN EC641370CN IAW SERVICE INFO AND MFG SERVICE INFORMATION. DURING THE OVERHAUL INTAKE VALVE SEALS PN 646678 WERE INSTALLED ONTO INTAKE VALVE GUIDES IAW MFG ILLUSTRATED PARTS CATALOG. THE INTAKE VALVE SEALS FAILED AFTER APSDR 2011FA0000410Seal · failedOVERHAULED AND INSTALLED CYLINDERS, PN EC641370CN IAW SERVICE INFO AND MFG SERVICE INFORMATION. DURING THE OVERHAUL INTAKE VALVE SEALS PN 646678 WERE INSTALLED ONTO INTAKE VALVE GUIDES IAW MFG ILLUSTRATED PARTS CATALOG. THE INTAKE VALVE SEALS FAILED AFTER APSDR 2011FA0000411Seal · failedOVERHAULED AND INSTALLED CYLINDERS, PN EC641370CN IAW SERVICE INFO AND MFG SERVICE INFORMATION. DURING THE OVERHAUL INTAKE VALVE SEALS PN 646678 WERE INSTALLED ONTO INTAKE VALVE GUIDES IAW MFG ILLUSTRATED PARTS CATALOG. THE INTAKE VALVE SEALS FAILED AFTER APSDR CA110215006Tube · looseDURING THE ANNUAL INSP OF THE ACFT, THE STABILATOR BALANCE WEIGHT TUBE WAS FOUND TO BE LOOSE. THERE ARE 2 ATTACH BOLTS. THE FWD ATTACH BOLT WAS LOOSE AND WAS RE-TORQUED. THE AFT ATTACH BOLT WAS LOOSE WITH SOME PLAY, THE BOLT WAS REMOVED AND INSPECTED, WEAR WASSDR 2011FA0000168Link · crackedCRACK DISCOVERED IN FWD FACING RADIUS OF NOSE GEAR RETRACTION CYLINDER AND DOWN LOCK ATTACHMENT TANG DURING ANNUAL INSP. REPLACED ENTIRE NOSE GEAR LINK AND BRACE DOWN-LOCK ASSY WITH NEW TO RETURN ACFT TO AIRWORTHINESS.SDR CA090520002Packing · mismanufactured(CAN) ENGINE WAS REMOVED DUE TO LOW OIL PRESSURE IN FLIGHT. UPON INSP IT WAS FOUND THAT THE NYLON PACKING INSIDE THE FRONT MAIN BEARING SHELLS WERE TOO SHORT. THEY DID NOT REACH THE FULL LENGTH OF THE GROOVE THAT THEY ARE SET IN. IT IS SUSPECTED THAT THIS MASDR CA090326013Dimmer · overheated(CAN) PILOT OBSERVED SMOKE AND ODOR COMING FROM INSTRUMENT PANEL IN THE AREA OF ELECTRICAL SWITCHES, ELECTRICAL SYS WAS SWITCHED OFF AND ACFT LANDED SUCCESSFULLY. AFTER EXTENSIVE INSP TO DETERMINE CAUSE THE NAV LIGHT/RADIO DIMMER SWITCH WAS FOUND INOPERATIVE SDR CA090112008Gasket · leaking(CAN) ENGINE INSPECTED FOR OIL LEAK AT REAR ACCESSORY SECTION, FOUND OIL COMING FROM RIGHT MAGNETO ATTACH GASKET. MAGNETO REMOVED, GASKET AND ENGINE MATING SURFACE INSPECTED OK. MOUNTING FLANGE ON MAGNETO INSPECTED AND FOUND CRACKED IN AREA WHERE BOTH HOLD DSDR 2008FA0000243Turbocharger · fodTURBOCHARGER COMPRESSOR DAMAGED BY FOD INGESTED THROUGH THE ALTERNATE AIR DOOR. THIS DOOR IS ON TOP OF THE AIR FILTER BOX ALLOWING ANY OBJECT THROWN UP BY THE NOSE WHEEL TO ENTER THE INDUCTION SYSTEM WHEN THE DOOR IS ACTIVATED DURING PREFLIGHT CHECKS.SDR UQM2005F00000Crankshaft · brokenAFTER INSTALLING REBUILT MAGS, TEST RAN AND WAS KNOCKING. REMOVED NR 1 CYLINDER AND FOUND CRANKSHAFT BROKEN AT THE JOURNAL. I FEEL THE CRANK MAY BE BROKEN IN ANOTHER SPOT. MFG IS AWARE OF THIS AND A REPLACEMENT ENGINE HAS BEEN SENT. PILOT WAS FLYING AT 700SDR UQM2005F00001Magneto · failedPILOT WAS FLYING AT 7000 FT AND LOST POWER. ENGINE WENT TO IDLE. MADE A SAFE LANDING. AFTER COMING TO A STOP THE ENGINE WS NOT RUNNING. FOUND THE MAGS BOTH LT AND RT HAVE NO SPARK. REMOVED P LEADS AND STILL NO SPARK. REPLACED CONDENSORS AND STILL NO SPARSDR UQM2005F00002Magneto · failedPILOT WAS FLYING AT 7000 FT AND LOST POWER. HE SAID ENGINE WENT TO IDLE. HE MADE A SAFE LANDING. AFTER COMING TO A STOP THE ENGINE WAS NOT RUNNING. FOUND THE MAGS BOTH LT AND RT HAVE NO SPARK. REMOVED P LEADS AND STILL NO SPARK. REPLACED CONDENSERS AND SSDR CA041013007Fitting · cracked(CAN) BRASS OUTLET ANGLE FITTING ON FUEL PUMP CRACKED CAUSING FUEL TO LEAK OUT IN FLIGHT.SDR 2004FA0000339Housing · crackedREMOVED TURBO FOR OTHER WORK, INSPECTED HOUSING PN 600510-04 AND FOUND IT TO BE CRACKED AS SHOWN IN AD 82-27-03 FIGURE 2, AD 82-27-03 DOES NOT APPLY TO THIS HOUSING NUMBER, RECOMMEND INSPECTING ALL TURBOS REGARDLESS OF AD.SDR 2003FA0000939Attach Fitting · crackedCOMPONENT WAS CRACKED IN THREE PLACES, THIS IS IN THE DRIVE ATTACHMENT BASE. (JUST FORWARD OF THE ATTACHMENT PLATE), ON THE WEB THAT SECURES THE ALTERNATOR. OWNER SAID THAT HE HAD REPLACED THE ALTERNATOR 7 MONTHS AGO FOR THE SAME PROBLEM, CRACKED JUST AFT OFSDR 920DMValve Guide · brokenCYLINDER WAS REMOVED FOR LEAKING EXHAUST VALVE BY CUSTOMER. UPON DISASSEMBLY AND REMOVAL OF LOWER VALVE SPRING RETAINER, THE GUIDE WAS FOUND TO BE IN TWO PIECES. THE LOWER HALF WAS STILL IN THE CYLINDER HEAD AND ID WAS EXTREMELY WORN AND OVAL SHAPED. THE FRSDR 2002FA0000217Line · wornENGINE LOST OIL PRESSURE IN CRUISE FLIGHT. THE PILOT MADE AN UNSCHEDULED LANDING. INVESTIGATION REVEALED THAT THE OIL FILLER CAP HAD COME OFF AND THE ENGINE LOST OIL. THE INTERNAL AREA OF THE OIL FILLER TUBE HAD WORN AND WOULD NO LONGER PUT SUFFICIENT PRESSSDR 2001FA0000376Isolator · burned outIN CRUISE FLIGHT NOTICED THE AMP GAUGE WAS SHOWING THE ALTERNATOR PUTTING OUT OVER 45 TO 50 AMPS. DME DROPPED OF LINE, LOST THE TRANSPONDER SIGNAL. VFR CONDITIONS AND CANCLED FLIGHT. LANDED AT THE CLOSEST AIRPORT. STARTED AIRCRAFT. RADIOS WORKING. 30 TO SDR CA010627054Trunnion · cracked(CAN) WHILE INSPECTING SHIMMEY DAMPENER AS PART OF 100 HOUR INSPECTION. IT WAS DISCOVERED THAT THE NLG TRUNNION ASSEMBLY WAS CRACKED AT SHIMMEY DAMPENE R ATTACH POINT.SDR 20000425SH039Drive Gear · brokenPILOT WAS IN-FLIGHT WHEN ENGINE FAILED. PILOT PERFORMED EMERGENCY PROCEDURES AND RETURNED TO AIRPORT. INSPECTION REVEALED THE GOVERNOR DRIVE GEAR HAD FAILED. GOVERNOR DRIVE GEAR ALSO DRIVES THE ENGINE DRIVEN FUEL PUMP WHICH, WHEN GEAR FAILED, TOOK THE ENGINSDR 99ZZZX956Retainer · crackedUPON COMPLETION OF CSB 98-1A, FOUND THAT NR 2 CYLINDER EXHAUST ROCKER SHAFT RETAINER WAS CRACKED. SUBMITTER SUGGESTED A POSSIBLE CAUSE IS OVERTORQUING OF ROCKER SHAFT RETAINER NUT OR MANUFACTURER DEFECT.SDR 98ZZZX4047Stud · separatedNR 3 CYLINDER ROCKER ARM CAME LOOSE, STUDS PULLED OUT OF CYLINDER. TACHOMETER: 540.SDR 98ZZZX998Coupling · failedALTERNATOR FAILED WHEN GEAR WAS RETRACTED. GEAR LOWERED AND RETURNED TO FIELD. PILOT REPORTED ALTERNATOR CHANGED ABOUT 10 HOURS AGO AND REGULATOR CHANGED ABOUT 20 HOURS AGO FOR SAME PROBLEM. FOUND ALTERATOR DRIVE SHEARED. REF: SPECIAL AIRWORTHINESS BULLETSDR 97ZZZX574Inject Pump · pin detachedUPON REACHING AN ALT OF 4500 FEET, THE PILOT LEANED THE MIXTURE CONT. AT THE POINT OF ENG ROUGHNESS, HE ATTEMPTED TO ENRICHEN THE MIXTURE. THE MIXTURE WOULD NOT ADVANCE. IN THE PROCESS OF TRYING TO FREE THE MIXTURE, THE ENG QUIT, AND THE MIXTURE COULD NOT BSDR 96ZZZX5448Crankshaft · brokenENGINE LOST POWER IN-FLIGHT. ACFT ABLE TO LAND AND TAXIED IN UNDER ITS OWN POWER. ENG INSP REVEALED PROP COULD BE MOVED 15 TO 20 DEGREES WITHOUT RESISTANCE. WITH PLUGS REMOVED, FND THE FRONT 4 PISTONS WOULD MOVE IN THAT 15 TO 20 DEGREES, BUT NR 1 AND NR 2 CSDR 96ZZZX4383Stud · stretchENGINE WAS BEING REPAIRED FOR SEVERAL BROKEN CYLINDERS, BASE STUDS, AND LOOSE NUTS. MECHANIC RECEIVED 36 BRAND NEW STUDS FROM THREE DIFFERENT VENDORS IN TCM PACKAGING. UPON TORQUING TO THE REQUIRED MINIMUM TORQUE VALVE, A TOTAL OF 12 STRETCHED. THEY WERE ALSDR 96ZZZX3207Fill Tube · rustyTHE INSIDE OF THE OIL FILLER TUBE AND OIL CAP WERE RUSTED TO THE POINT OF FLAKES OF RUST BEING KNOCKED OFF OF THE SURFACE AND FALLING INTO THE CRANKCASE. SUBMITTER STATED THESE ASSEMBLIES SHOULD PROBABLY BE MADE OF STAINLESS STEEL. THEY ARE CADMIUM PLATED WHSDR 96ZZZX3072Coil · wire brokenINSTALLED NEW MAGNETO, WAS INOPERATIVE. TROUBLESHOOTING REVEALED THE COIL WIRE WAS BROKEN AT THE TERMINAL END. (INSULATION WAS STILL INTACT). SUBMITTER STATED CAUSE WAS DUE TO THE TERMINAL END BEING CRIMPED TOO HARD RESULTING IN BROKEN WIRE. RECOMMEND MANUSDR 96ZZZX3074Condenser · failedINVESTIGATION FOR MAG PROBLEM FOUND CONDENSER HAD NO CONTINUITY.SDR 96ZZZX3075Condenser · wire brokenRT MAG INOPERATIVE. INSTALLED NEW MAG, SN 1069532DR. THIS NEW MAG WAS INOPERATIVE. TROUBLESHOOTING BOTH MAGS REVEALED ORIGINAL MAG HAD BAD CONSENSER AND THE NEW MAGNETO HAD A BAD COIL. BOTH NEW MAGNETOS HAD A BAD COIL. BOTH THE CONDENSER AND COIL PROBLEMSSDR 96ZZZX3073Magneto · failedMAGNETO FAILED. DID NOT TROUBLESHOOT MAG DUE TO IT BEING UNDER WARRANTY.SDR MCA12BMVValve · leakingFUEL MANIFOLD VALVE FOUND LEAKING AROUND VALVE DIAPHRAGM. REASON FOR LEAK UNKNOWN. ENGINE AND COMPONENTS REBUILT BY TCM 5-12-95. (X)SDR 95ZZZX6417Rocker Shaft · wornDURING ROUTINE OIL CHANGE, OIL FILTER WAS FOUND CONTAMINATED WITH FERROUS MATERIAL. OIL ANALYSIS DETERMINED MATERIAL TO BE CASE HARDENED STEEL. UPON INSPECTION, FOUND SEVERE CORROSION IN CYLINDER WALLS, STARTER HOUSING, AND GEARS. ALSO, WORN ROCKER SHAFTS. SDR 95ZZZX5949Housing · crackedDURING COMPLIANCE WITH AD 82-27-03 AND AFTER REMOVING THE EXHAUST HOUSING OF THE TURBOCHARGER, A CRACK, APPROXIMATELY .75 INCH LONG, WAS NOTED IN THE WEB AREA NEAR THE INLET. PARAGRAPH J OF THE AD STATES THE 200-HOUR REPETITIVE INSPECTION REQUIREMENT IS RELIESDR 96ZZZX936Retainer · crackedDURING C/W CONTINENTAL SB CSB95-4, FOUND 2 ROCKER SHAFT RETAINERS CRACKED THROUGH THE BOLT HOLE.SDR 95ZZZX5765Gasket · failedREPLACED ROCKER BOX COVER GASKETS WITH NEW SUPERIOR SILICON GASKET. USED ALL NORMAL PROCEDURES FOR INSTALLATION. COVERS CAME OFF IN-FLIGHT CAUSING ENGINE OIL LOSS. AFTER FURTHER INVESTIGATION, SUPERIOR FOUND A SL NR P1B-93007, THAT SAYS TO USE LOCTITE ON SCSDR 95ZZZX3244Idle Shaft · wornOIL PUMP WOULD LOSE PRIME AND HAVE NO OIL PRESSURE AFTER START-UP. OIL PUMP IDLE SHAFT EXTREMELY WORN AND BOTH GEARS WORN. WORE THE PUMP HOUSING CAUSING AN OIL SHORTAGE TO THE ENGINE WITH BEARING AND CASE DAMAGE. THE PUMP HOUSING AND SHAFTS WERE TIGHT AND CSDR 95ZZZX1601Connect Rod · failedTHIS ENGINE, CONVERTED FROM A TSIO-360-GB, HAD NR 3 AND NR 4 CONNECTING RODS FAIL AT THE SAME TIME KNOCKING A HOLE IN THE UPPER CASE AREA OF ABOUT 8 INCHES DIAMETER. TELEDYNE-CONTINENTAL SB M86-11 R1 PERTAINS TO THIS SUB JECT.SDR 95ZZZX764Adapter · failedSTARTER ADAPTER FAILED. FOUND SPRING, PN 539800, BROKE AT LOCATION OF LOCK SCREW, PN 633845.
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