Continental TSIO-360-RB
Service difficulty reports · 96
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 = 'TSIO360RB' 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 = 'TSIO360RB' 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 2022FA0000739Magneto · failedMISFIRE FROM ENGINE IN FLIGHT, AND 200+ RPM DROP ON MAGNETO CHECK AFTER LANDING APPROXIMATELY 120 HOURS SMOH ON ENGINE, TSIO-360-RB2 CONTINENTAL. NORMAL MAGNETO DROP IS 75 RPM, SO OUTSIDE OF TOLERANCE. MAGNETOS WERE OVERHAULED BY QAA IN OKLAHOMA AT THE TIME OFSDR CA190530009Probe · malfunctioned(CAN) ON JANUARY 24, 2019 THE LEFT HAND ENGINE CHT SHOWED AN OVER TEMP INDICATION AND ACTIVATED THE MASTER CAUTION. THE CHT WAS REPLACED WITH A NEW UNIT AT 2738.8 TAT. ON MAR 19, 2019 THE R/H CHT FAILED CAUSING A MASTER CAUTION INDICATION. THE CHT PROBE WAS RESDR 2009FA0000463Crankshaft · crackedDURING ANNUAL INSP, OIL WAS FOUND AT FRONT OF ENGINE. FURTHER INVESTIGATION REVEALED A CRACK OF THE CRANKSHAFT AT THE PROP MOUNTING FLANGE. CAUSE HAS NOT BEEN DETERMINED. (K)SDR 2008FA0000003Strut · crackedDURING ANNUAL INSPECTION IT WAS NOTED THAT A CRACK WAS FOUND ON THE RT MAIN GEAR LOWER FORK ASSY PN 39489-003. THE CRACK IS LOCATED IN THE MILLED SECTION OF THE CASTING AT THE 11 O'CLOCK AND 1 O'CLOCK POSITIONS. THIS MILLED SECTION IS USED TO BOLT THE TORQUE SDR 2008FA0000004Strut · crackedDURING ANNUAL INSPECTION, IT WAS NOTED THAT A CRACK WAS FOUND ON THE RT MAIN GEAR LOWER FORK ASSEMBLY PN 39489-003. THE CRACK IS LOCATED IN THE MILLED SECTION OF THE CASTING AT THE 11 O'CLOCK AND 1 O'CLOCK POSITIONS. THIS MILLED SECTION IS USED TO BOLT THE TOSDR 2007FA0000729Bushing · misinstalledDURING THE PROCESS OF INSPECTING (6 EA) CONNECTING RODS IAW SB 07-1 AND SB 00-3, IT WAS FOUND THAT ALL WRIST PIN BUSHINGS WERE INSTALLED NOT IAW THEIR POSITIONS AS REQUIRED IN THE APPLICABLE SB AS REFERENCED. SPLIT LINE OF BUSHING ON WRONG SIDE OF CENTERLINE.SDR 2007FA0000288Floor Panel · debondedFLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM. THE SEAT MOUNTING BRACKETS ARE BOLTED THSDR 2007FA0000289Floor Panel · debondedFLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM. THE SEAT MOUNTING BRACKETS ARE BOLTED TSDR 2007FA0000290Floor Panel · debondedFLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM. THE SEAT MOUNTING BRACKETS ARE BOLTED THSDR 2007FA0000291Floor Panel · debondedFLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM. THE SEAT MOUNTING BRACKETS ARE BOLTED TSDR 2007FA0000292Floor Panel · debondedFLOORPANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM. THE SEAT MOUNTING BRACKETS ARE BOLTED THRSDR AU510002022Shaft · wornENGINE DRIVEN FUEL PUMP LEAKING. THE PUMP WAS DISMANTLED AND THE FOLLOWING DEFECTS WERE FOUND, ROTOR SHAFT FOUND WITH EXCESSIVE WEAR AND EXTREME SCORING, DEEP SCORING IN SHAFT BEARING (BUSHING), LOWER FACE OF ROTOR SHAFT HAS CONTACTED AND DAMAGED LOWER THRUSTSDR AU510002134Pump · contaminatedLT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.SDR AU510002137Pump · contaminatedRT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.SDR AU510002138Pump · contaminatedRT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.SDR AU510002139Pump · contaminatedLT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.SDR AU510002140Pump · contaminatedLT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.SDR AU510002142Pump · contaminatedLT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.SDR AUS20040227Bearing · failed(AUS) ENGINE DRIVEN FUEL PUMP FAULTY. PUMP CONTAMINATED WITH A BLACK CARBON POWDER TYPE SUBSTANCE. POOR PUMP LUBRICATION CAUSED EXCESSIVE BEARING WEAR.SDR AUS20040238Pump · contaminated(AUS) INSPECTION OF ENGINE DRIVEN FUEL PUMP FOLLOWING STRIP FOR OVERHAUL. THE PUMP WAS FOUND TO CONTAMINATED WITH WHAT APPEARS TO BE CARBON POWDER. PUMP SHAFT BUSHING CONTAMINATED, CAUSING PUMP ROTATION TO BE RESTRICTED.SDR AUS20040255Servo · leaking(AUS) ENGINE FCU SERVO STEM SEAL LEAKING FUEL. FURTHER INVESTIGATION FOUND THAT THERE WERE MANY SMALL PARTS OF BLUE RUBBER THROUGH OUT THE UNIT. THESE RUBBER PARTS HAD COME FROM A POSSIBLE DAMAGED O RING SEAL DURING ASSEMBLY. ON TOTAL STRIP OF THE UNIT NONE OFSDR AUS20031119Bolt · loose(AUS) AILERON CONTROL COLUMN IDLER SPROCKET BOLT LOW TORQUE. SUSPECTBOLTS LOOSENED DURING RIGGING AT MANUFACTURE AND NOT RETORQUED.SDR AUS20031120Bolt · loose(AUS) AILERON CONTROL COLUMN IDLER SPROCKET BOLT LOW TORQUE. SUSPECT BOLTS LOOSENED DURING RIGGING AT MANUFACTURE AND NOT RETORQUED. PERSONNEL/MAINTENANCE ERROR.SDR AUS20031118Bolt · loose(AUS) AILERON CONTROL COLUMN IDLER SPROCKET BOLT LOW TORQUE. SUSPECT BOLTS LOOSENED DURING RIGGING AT MANUFACTURE AND NOT RETORQUED.SDR AUS20021323Pin · chafed(AUS) MAGNETO HARD TO TIME. INVESTIGATION FOUND THE SPLIT PIN SECURING THE MAGNETO COUPLING NUT WAS CONTACTING THE END OF THE DRIVE CUSHION BEARING STUD ON THE CRANKCASE. MAGNETO WAS A NEWLY FITTED UNIT. FURTHER INVESTIGATION FOUND OTHER SIMILAR MAGNETOS. THESDR AUS20021210Control Valve · loose(AUS) LANDING GEAR HYDRAULIC PUMP PRESSURE CONTROL VALVE LOOSE IN HOUSING.SDR AUS20021177Line · corroded(AUS) LANDING GEAR DOWN HYDRAULIC TUBE LOCATED IN NLG WHEEL WELL CORRODED BEYOND LIMITS.SDR AUS20021178Line · corroded(AUS) LANDING GEAR UP HYDRAULIC TUBE LOCATED IN NLG WHEEL WELL CORRODED BEYOND LIMITS.SDR AUS20021160Line · leaking(AUS) HEATER FUEL LINE LEAKING. INVESTIGATION FOUND THE ALUMINIUM FUEL LINE HAD BEEN CHAFED BY ELECTRICAL WIRING RUNNING ADJACENT TO THE FUEL LINE. THE WIRE WAS WORN TO THE EXTENT OF ARCING AND BURNING THROUGH THE FUEL LINE. ELECTRICAL WIRING WAS POORLY FITTEDSDR AUS20021172Plate · cracked(AUS) PROPELLER CONTROL FEATHER GATE STOP PLATE ASSEMBLY LOCATED IN COCKPIT CONTROL QUADRANT CRACKED.SDR 3399Line · chafedFUEL INJECTION LINE TO NR 3 CYLINDER CHAFED BY CLAMP SECURING RUBBER INDUCTION COUPLING FROM INDUCTION SPIDER TO NR 5 CYLINDER INTAKE TUBE.SDR AUS20020986Line · corroded(AUS) NOSE LANDING GEAR, DOWN HYDRAULIC LINE CORRODED. SUSPECT CAUSED BY LACK OF CORROSION PREVENTION DURING MANUFACTURE.SDR AUS20020987Line · corroded(AUS) NOSE LANDING GEAR UP HYDRAULIC LINE CORRODED. SUSPECT CAUSED BY LACK OF CORROSION PREVENTION DURING MANUFACTURE.SDR AUS20020544Relay · faulty(AUS) BATTERY RELAY SEIZED IN THE ON' POSITION. INVESTIGATION FOUND THAT WATER HAD LEAKED PAST THE AFT CABIN DOOR SEAL AND DRIPPED ONTO THE RELAY.SDR U23R624YBracket · brokenUPON ANNUAL INSPECTION OF THE AIRCONDITIONING COMPRESSOR, IT WAS NOTED TO MOVE AROUND BY PRESSING ON THE AIRCONDITIONING BELT FURTHER INSPECTION REVEALED THE FORWARD AIRCONDITIONING BRACKET TO BE BROKEN. DURING REMOVAL OF THE BRAKET IT WAS ALSO FOUND TO BE BROSDR 20010124CW006Ignition Lead · shortedNR2 AND NR6 CYLINDER IGNITION LEADS ON BOTTOM PLUGS SHORTED OUT, BEHIND IGNITION LEAD SPRING ASSEMBLY.SDR 20001218SH029Distributor · wornDURING SCHEDULED 500-HOUR INSPECTION OF MAGNETO, FOUND DISTRIBUTOR GEARSHAFT AND BLOCK BEARINGS WORN. THIS WEAR HAD ALLOWED BRUSH TO WEAR WHICH CAUSED METAL CONTACT AND WEARING OF THE COIL, THE MAGNETO WAS REPLACED. GEAR AND BLOCK ASSY, PN K-3823. (X)SDR 20001218SH032Distributor · wornDURING SCHEDULED 500-HOUR INSPECTION OF MAGNETO, FOUND DISTRIBUTOR GEARSHAFT AND BLOCK BEARINGS WORN. PARTS WERE REPLACED. P/N M3828 GEAR REPLACED AND MAGNETO INSTALLED AND TIMED. (X)SDR 20001102SH004Servo · inoperativeUNABLE TO ADJUST MIXTURE AND IDLE. WILL NOT STAY SET. ENGINE QUITS WITH BOOST PUMP ON. (X)SDR 20001017SH012Controller · malfunctionedTHE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETTING IN-FLIGHT AND ON GROUND. CONTROLLER REPLACED. (X)SDR 20001018SH010Controller · stuckTHE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETTING IN-FLIGHT AND ON THE GROUND. CONTROLLER REPLACED. (X)SDR 20001019SH030Servo · faultyTHROTTLE HARD TO MOVE, CHECKED FORCE TO MOVE THROTTLE ON THE GROUND AND FOUND OVER SPECS. SERVO REMOVED AND A NEW ONE INSTALLED IAW PIPER MANUAL. (X)SDR 20001018SH013Servo · defectiveTHROTTLE HARD TO MOVE IN-FLIGHT, SERVO REMOVED AND A NEW ONE INSTALLED. OVER FOUR POUNDS TO MOVE CONTROL. (X)SDR 20001019SH016Tube · crackedINSPECTION OF INTAKE FOUND NR 2 INTAKE TUBE CRACKED AT THE FLANGE. (X)SDR 20001023SH002Tube · crackedINSPECTION OF INTAKE FOUND NR 2 INTAKE TUBE CRACKED AT THE FLANGE. (X)SDR 20000911SH040Servo · faultyUNABLE TO ADJUST FUEL FLOW AT IDLE. (X)SDR 20000925SH037Servo · failedTHROTTLE HARD TO MOVE IN FLIGHT, SERVO REMOVED AND A NEW ONE INSTALLED. OVER FOUR POUNDS TO MOVE CONTROL. (X)SDR 20000925SH035Servo · failedTHROTTLE END PLAY ON SHAFT. NEW FROM TCM. (X)SDR 20000911SH025Servo · failedON LANDING , LEFT ENGINE LAGGED POWER TO LANDING. THE RPM DROPPED FROM 2,400 TO 1,800. THROTTLE POWER TO 22 INCHES. (X)SDR 20000925SH029Servo · failedON LANDING AT GOODYEAR AIRPORT IN AZ, THE LEFT ENGINE LAGGED POWER TO LANDING. THE RPM DROPPED FROM 2,400 TO 1,800. THROTTLE POWER TO 22 INCHES. (X)
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