Continental TSIO-360-KB
Service difficulty reports · 54
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 = 'TSIO360KB' 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 = 'TSIO360KB' 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 2024FA0000239Tire · failedPILOT REPORTED ON LANDING THAT HE FELT THE AIRCRAFT YAWING TO THE RIGHT AND REALIZED HE HAD A FLAT TIRE. AIRPORT USED A SET OF DOLLIES TO MOVE THE AIRCRAFT BACK TO WINGS OF HOPE RAMP AREA. BOTH MAIN TIRES AND TUBES WERE REPLACED WITH NEW. WHEEL WAS DISASSEMBLESDR 2021FA0000101Rod End · shearedFAILURE OF THE NOSE GEAR DOWN-LOCK LINK ASSEMBLY, CAUSING A NOSE LANDING GEAR COLLAPSE, AND A DUAL ENGINE PROPELLER STRIKE. THE NOSE GEAR DOWN-LOCK LINK ASSEMBLY BENT, AND THEN SHEARED AT THE ADJUSTABLE ROD END.SDR YBBA201908280001Warning Light · inoperativePIC REPORTS NOSE GEAR INDICATION INOP DURING GEAR DOWN CYCLE, CYCLED GEAR 3 TIMES AND CONFIRMED GEAR DOWN WITH ATC ACKNOWLEDGEMENT DURING FLY BY, AFTER CYCLING GEAR ALL THREE INDICATIONS WERE PRESENT.SDR 2013FA0000094Cap · departedFUEL CAP ON THE WING INCORRECTLY INSTALLED AFTER REFUELING, FUEL CAP EVENTUALLY DEPARTED THE ACFT INFLIGHT. CAP WAS CHECKED DURING THE PREFLIGHT, AFTER REFUELING, AND THE CAP PLACEMENT WAS CLEARLY FLUSH WITH THE WING, AND THE "HANDLE" WAS FOLDED DOWN AND FLUSSDR 2007FA0000942Landing Gear · collapsedAIRCRAFT TAXIED TO RUNWAY AFTER LOADING CARGO. AFTER NORMAL RUNUP, THE PILOT TAXIED ONTO THE RUNWAY AND STOPPED. THE PILOT ADVANCED THROTTLES AND RELEASED BRAKES, AFTER RELEASING BRAKE, THE NOSE GEAR COLLAPSED. AIRCRAFT WAS RECOVERED AND TOWED OFF RUNWAY TOSDR 2007FA0000076Coupling · failedALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATORS, IN IMC SIMULTANEOUSLY. 1 PIECE COUPLING WITH A RUBBER LORD BUSHING BONDED/INTERFERENCE FIT SLIPPED, CAUSING THE ALTERNATORS FAILURES. PILOTS LOST ELECTRICAL AND DESCENDED THROUGH ICE, UNABLE TO SHED SDR 2007FA0000077Coupling · failedALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATORS, IN IMC SIMULTANEOUSLY. 1 PIECE COUPLING WITH A RUBBER LORD BUSHING BONDED/INTERFERENCE FIT SLIPPED, CAUSING THE ALTERNATORS FAILURES. PILOTS LOST ELECTRICAL AND DESCENDED THROUGH ICE, UNABLE TO SHED SDR 2007FA0000085Coupling · failedALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATOR, IN IMC SIMULTANEOUSLY. COUPLING FAILURE RESULTED IN TOTAL ELECTRICAL FAILURE, RT ENGINE.SDR 2006FA0000571Points · failedTHE POINTS WHICH ONLY HAD A TOTAL OF 9.3 HR, HAD THE PLASTIC PORTION WHICH RIDES THE CAM, MELT ON THE METAL OF THE POINTS WHICH REDUCED THE GAP TO CAUSE MISFIREING. CAPACITOR CHECKED GOOD AND WAS NOT REPLACED ON THE 500 HR INSP. AFTER A NEW POINT SET WERE INSDR CA070207006Trunnion · failed(CAN) NOSE GEAR TRUNNION DAMAGED AND REPAIRED. (TC NR 20070207006)SDR AU510001779Alternator · faultyLT AND RT ALTERNATORS REMOVED FROM AIRCRAFT FOR INTERNAL INSPECTION FOLLOWING PURCHASE OF AIRCRAFT. BOTH ALTERNATORS WERE FOUND TO CONTAIN NUMEROUS DEFECTS. ALTERNATORS HAD ONLY 12 HOURS TSO. ALTERNATORS WERE `KELLY AEROSPACE` ITEMS.SDR 2005FA0001192Adapter · crackedSTARTER ASSEMBLY BOLT HOLE FLANGE CRACKED AT THE 10 O'CLOCK BOLT POSITION. MANUFACTURER DESIGN FLAW. ONGOING NUMEROUS REOCCURENCES WITH THESE ADAPTER ASSEMBLY ACCESSORY DRIVE HOUSINGS, LEFT SIDE ONLY, IN FLEET AIRCRAFT.SDR 2005FA0001193Adapter · crackedSTARTER ASSEMBLY BOLT HOLE FLANGE CRACKED AT THE 10 O'CLOCK BOLT POSITION. MANUFACTURER DESIGN FLAW. ONGOING NUMEROUS REOCCURENCES WITH THESE ADAPTER ASSEMBLY ACCESSORY DRIVE HOUSINGS, LEFT SIDE ONLY, IN FLEET AIRCRAFT.SDR 2005FA0000670Gear · brokenENGINE LOST POWER FOR UNKNOWN REASONS. ENGINE WAS DISASSEMBLED AND INSPECTED. INVESTIGATION FOUND BROKEN DRIVE DOGS ON THE OIL PUMP GEAR, AS WELL AS GEAR TEETH ON THE CRANKSHAFT GEAR AND OUTSIDE DIAMETER OF THE CAM GEAR. THE REASON FOR THE FAILURE OF THE OISDR AUS20030654Washer · wrong part(AUS) LT AND RT MAIN LANDING GEAR FORWARD TRUNNION WASHERS INCORRECT PARTS. CORRECT WASHERS HAVE A CHAMFER ON THE INTERNAL BORE WHICH ALLOWS CLEARANCE FOR THE TRUNNION SHOULDER RADIUS. THE WASHERS FITTED DID NOT HAVE THE CHAMFER. IN THIS CASE THE DAMAGE WAS MSDR NCL2003F00000Rib · crackedTHE LT AND RT FORWARD TRUNNION FITTING ASSEMBLIES WERE REMOVED TO REPLACE THE BEARINGS. WHILE THE FITTINGS WERE REMOVED THE TECH NOTICED THAT BOTH LT AND RT RIBS WERE CRACKED AT THE FORWARD OUTBOARD FLANGES OF THE RIBS. THIS FLANGE IS UNDER THE TRUNNION FITTSDR AUS20021279Lever · binding(AUS) FLAP LEVER FOULING ON ENGINE CONTROL FRICTION LEVER.SDR AUS20021102Tube · corroded(AUS) LANDING GEAR UP' HYDRAULIC PIPE CORRODED.SDR AUS20021103Tube · corroded(AUS) LANDING GEAR DOWN' PIPE CORRODED.SDR AUS20021104Tube · corroded(AUS) LANDING GEAR DOWN' HYDRAULIC PIPE CORRODED.SDR AUS20021105Tube · corroded(AUS) LANDING GEAR UP' HYDRAULIC PIPE CORRODED.SDR AUS20020950Plate · cracked(AUS) PROPELLER PITCH LEVER FEATHER STOP PLATE CRACKED PREVENTING OPERATION OF PITCH LEVER.SDR AUS20020951Plate · cracked(AUS) PROPELLER PITCH CONTROL LEVER FEATHER STOP GATE PLATE CRACKED.SDR AUS20020823Shaft · scored(AUS) ROCKER SHAFT AND BUSH SCORED. SUSPECT CAUSED BY LACK OF LUBRICATION.SDR AUS20020855Exhaust Valve · worn(AUS) NO3 CYLINDER EXHAUST VALVE TIP WORN EXCESSIVELY. CORRESPONDINGROCKER DAMAGED ON CONTACT AREA. EXHAUST VALVES PNO 646460 AND INLET VALVES PNO 646459 IN OTHER CYLINDERS ALSO SHOWING SIGNS OFPITTING ON THE TIPS.SDR AUS20020948Tube · corroded(AUS) LANDING GEAR UP' HYDRAULIC TUBE CORRODED AND LEAKING THROUGH CORROSION HOLE LOCATED UNDER P' CLAMP.SDR AUS20020949Tube · corroded(AUS) LANDING GEAR HYDRAULIC PIPE CORRODED IN AREA UNDER P' CLAMP.SDR AUS20020822Piston Pin · damaged(AUS) NO1 ENGINE PISTON PINS (6OFF) HAD SEVERE DAMAGE TO THE ALUMINIUMEND CAPS. THE END CAPS HAD MIGRATED OUTWARDS AND WERE RUBBING ONTHE CYLINDER WALLS. METAL CONTAMINATION OF ENGINE OIL SYSTEM.SDR CA020403004Pump · leaking(CAN) WHILE CARRYING AT AD 2001-17-13 (JANAERO SOLENOID/SHUTOFF VALVE LEAK CHECK) THE HEATER FUEL PUMP WAS FOUND TO BE LEAKING OUT OF THE POWER WIRE GROMMET. THIS PUMP IS UNDER THE CENTRE FLOOR BOARD IN THE CABIN AND ALTHOUGH THERE IS A DRAIN UNDER THE PUMP FUSDR CA041213001Skin · mismarked(CAN) SKIN ASSY P/N 7861901 MATERIAL AND SKIN THICKNESS IDENTIFIED IN PIPER SENECA SERVICE MANUAL STRUCTURES SECTION FIG.4-9 NR 5 AS 2024-T3 0.032SDR 2001FA0000583Wire · missingNEW EXCHANGE ALTERNATOR SUPPLIED. ALTERNATOR OUTPUT OK. PANEL INOPERATIVE LIGHT STAYS ILLUMINATED. INSPECTION OF ALTERNATOR REVEALED MISSING LEAD WIRE FROM STATOR TO STATOR. ALT LIGHT TERMINAL ON ALTERNATOR. ALTERNATOR REQUIRES ADDITIONAL LEAD WIRE FOR ASDR CA010831004Fastener · missing(CAN) 1. FITTING, ASSY OUTBOARD LOWER ENGINE MOUNT. ONE MISSING FASTENER ON OUTBOARD LOWER SIDE FITTING (P/N: 37437-01).2. FITTING, ASSY INBOARD LOWER ENGINE MOUNT. ONE MISSING FASTENER ON INBOARD LOWER SIDE OF FITTING (P/N: 37442-01)SDR 20001017SH008Controller · looseEXCESS PLAY IN ARM TO LINKAGE. (X)SDR CA000824030Ground Wire · broken(CAN) THIS AIRCRAFT SUFFERED A PARTIAL GEAR UP LANDING ON JUNE 19, 2000. TEMPORARY REPAIRS WERE MADE AND THE AIRCRAFT WAS FERRIED TO CYEG FOR FURTHER INSPECTION AND REPAIR. NECESSARY REPAIRS WERE MADE. INSPECTION BEFORE FURTHER FLIGHT REVEALED THAT THE STAKOSDR 20000829SH011Duct · crackedPILOT REPORTED THOTTLE SPLIT AND UNABLE TO OBTAIN RATED POWER ON LEFT ENGINE. INSPECTION OF LEFT ENGINE REVEALED EXHAUST V-DUCT ASSY AT TURBOCHARGER CRACKED. THIS PART WAS INSTALLED NEW AS A COMPONENT OF A FACTORY RE-MANUFACTURED ENGINE. TOTAL TIME SINCE INSDR 20000626SH017Fuel Control · failedENGINE DIED ON LANDING ROLL-OUT. AIRCRAFT WAS TAKEN TO MAINTENANCE AND A GROUND RUN PERFORMED. THE FUEL SERVO ON THIS ENGINE WAS RICH AT IDLE AND UNABLE TO ADJUST MIXTURE. SERVO WAS REMOVED FROM ENGINE AND SENT FOR REPLACEMENT. TOTAL TIME ON UNIT WAS 54 HOSDR 2000ZZZX603Magneto · failedMAGNETO FAILED IN-FLIGHT. FOUND SEVERE DAMAGE TO DISTRIBUTOR FROM ARCING. ARCING APPEARED TO HAVE STARTED BEWEEN COIL AND REAR BEARING HOUSING. SUBMITTER STATED CAUSE UNKNOWN. (X)SDR 99ZZZX4653Crankshaft · crackedTRANSIT ACFT LANDED EN ROUTE WITH LT ENGINE SHUT DOWN DUE IN-FLIGHT OIL LEAK. CLEANED ENG AND DID A SHORT RUN AND FOUND OIL COMING FROM PROP SHAFT AREA. REMOVED PROP AND CHECKED O-RING AND IT CHECKED OK. UPON FURTHER INVEST, APPEARED TO BE A CRACK BEHIND PRSDR 99ZZZX3583Mixture Plate · scoredENGINE OPERATING SQUAWKS INCLUDE STIFF THROTTLES, ENGINES DYING, ROUGH RUNNING, AND IMPROPER FUEL MIXTURES. THE ENGINE PARAMETERS WERE RESET, BUT THE PROBLEMS RETURNED. THE MIXTURE CONTROL ON THE THROTTLE SIDE OF THE SERVO WAS DISASSEMBLED. FOUND THE BRASS SDR 99ZZZX3584Mixture Plate · scoredENGINE OPERATING SQUAWKS INCLUDE STIFF THROTTLES, ENGINES DYING, ROUGH RUNNING, AND IMPROPER FUEL MIXTURES. THE ENGINE PARAMETERS WERE RESET, BUT THE PROBLEMS RETURNED. THE MIXTURE CONTROL ON THE THROTTLE SIDE OF THE SERVO WAS DISASSEMBLED. FOUND THE BRASS SDR 99ZZZX984Fuel Servo · mismanufacturedNEW FUEL SERVO INSTALLED ON AIRCRAFT. FUEL LEAK AT FUEL INLET. REMOVED ADAPTER FROM UNIT, O-RING PACKING, PN 951789, WAS MISSING. SUBMITTER STATED THIS WAS A NEW SERVO AND ALL FITTINGS INSTALLED WERE TORQUED.SDR 99ZZZX191Cylinder Head · brokenCONDITION OCCURRED DURING CRUISE CONFIGURATION. PILOT REPORTED LOSS OF MANIFOLD PRESSURE AND DIMINISHED PERFORMANCE ON RT ENGINE. PILOT NOTED OIL COMING FROM ENGINE COWLING AND SHUT ENGINE DOWN. AN INSPECTION REVEALED CYL NR 4 HAD A BROKEN HEAD. THE BREAK SDR CA981109012Wire · broken(CAN) WHEN GEAR SELECTED DOWN, NO GREEN LIGHT FOR LEFT GEAR AND GEAR UNSAFE LIGHT ON. FLY-BY OK. AIRCRAFT LANDED SAFELY. INSPECTION FOUND A BROKEN WIRE AT THE CONNECTOR FOR THE GEAR SWITCH.SDR AU980897Fuel System · malfunctioned(AUS) LEFT AND RIGHT ENGINES CUT OUT. SUSPECT LEAN CUT-OUT DUE TO FUEL STARVATION.SDR 97ZZZX4670Through Bolt · brokenDURING AN ANNUAL INSPECTION, THE BOTTOM CRANKCASE THROUGH-BOLT LOCATED BETWEEN NR 1 AND NR 3 CYLINDER POSITION WAS FOUND BACKED OUT FROM THE CASE ALMOST TO THE POINT OF FALLING OUT OF ITS MOUNTING HOLE BY APPROXIMATELY 1.1250 INCHES. WHEN BOLT WAS REMOVED, FOSDR AU970648Combustor · cracked(AUS) CABIN HEATER COMBUSTION CAN SPLIT AROUND CIRCUMFERENCE FORAPPROXIMATELY 60MM (2.36IN) - HEATER WAS BEING OVERHAULED TO COMPLY WITH REQUIREMENTS OF AD/AIRCON/9 AMDT5 PARA3SDR CA970407008Hub · threads flatened(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION AND HUB THREADS WERE FOUND FLATTENED, DUE TO REMOVING AND INSTALLING THE PROPELLER.SDR CA970407009Blade · eroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION AND THE BLADES WERE FOUND ERODED AND REQUIRED FILING. THE TIP ANGLES WERE OUT OF SPECIFICATIONS AND REQUIRED TWISTING.SDR CA970407013Blade · eroded(CAN) INSPECTION FOUND PROPELLER LEADING EDGE ERODED/CORRODED, WHICH REQUIRED FILING. THE BLADE TIP ANGLES WERE OUT OF SPECIFICATIONS AND REQUIRED TWISTING.SDR 96ZZZX6146Engine · making metalDURING 100 HR INSPECTION, THE LEFT ENGINE OIL FILTER WAS FOUND TO BE CONTAMINATED WITH METAL. REMOVAL OF PROPELLER REVEALED METAL CONTAMINATION IN CRANKSHAFT. ENGINE WAS REMOVED FOR OVERHAUL. FURTHER DETAILS WILL BE PROVIDED UPON RECEIPT OF TEAR DOWN REPOR
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