Continental TSIO-360-E

Service difficulty reports · 37

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 = 'TSIO360E'
  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 CA131121009Shimmy Dampener · broken(CAN) DURING A WALK AROUND, THE STUDENT PILOT NOTED THE SHIMMY DAMPENER AT AN AWKWARD ANGLE. THE SHAFT WAS BROKEN NEXT TO THE ROD END. NO OTHER VISIBLE DAMAGE WAS EVIDENT. THE PART WAS REPLACED.Nov 13, 2013 · Piper PA34200T · Nose/Tail Landing GearSDR 2012FA0000230Link Assy · brokenON LANDING, LINK ASSY ON MAIN GEAR TRUSS ASSY BROKE AT STRUT ATTACHMENT AREA, CAUSING ACFT TO VEER OFF RUNWAY.Apr 20, 2012 · N1724H · Piper PA34200T · Landing Gear Retraction/Extension SystemSDR APC2010F00000Bolt · brokenON PREFLIGHT, THE PILOT FOUND THE STABILATOR TO BE EXTREMELY LOOSE AND NOTIFIED MX. WHEN REMOVED TAIL CONE FOUND A BROKEN BOLT ON THE RT THAT HAD BACKED OUT. IMMEDIATELY GROUNDED THE WHOLE FLEET UNTIL SUCH TIME AS WE COULD INSPECT ATTACHING POINTS, BEARINGS Mar 12, 2010 · N36319 · Piper PA34200T · Flight Control SystemSDR 2007FA0000547Pulley Bracket · chafedROLL SPOILER CABLE PN:S3779-4P233.7M WAS ROUTED INCORRECTLY OVER LOW FRICTION PULLEY P/N:S3504-4.5 (THROUGH A TOOLING HOLE) IN PULLEY BRACKET P/N:6960236-17. THIS CAUSED AN INTERFERENCE AND WEAR IN THE PULLEY BRACKET, AND FLAT AREAS TO THE CABLE. CABLE AND Jun 20, 2007 · N301Q · Glasfl H301LIBELLE · Drag Control SystemSDR NOB2007F00000Spring · obstructedNLG WOULD NOT EXTEND WHILE ON APPROACH. AC RETURNED & THROUGH G-LOAD MANUEVERS, MANAGED TO GET NLG TO EXTEND PRIOR TO LANDING. PROBLEM WAS DETERMINED TO BE INTERFERENCE BETWEEN NLG CENTERING SPRING ROD END ATTACHMENT CLEVIS BOLT HEAD AND REAR TORQUE TUBE FOMar 9, 2007 · N38858 · Piper PA34200T · Nose/Tail Landing GearSDR CA060502008Battery · leaking(CAN) ELT BATTERIES LEAKED. (TC NR 20060502008)Apr 27, 2006 · Piper PA34200T · Emergency Locator BeaconSDR AU510002146Hinge · corrodedRUDDER HINGE BRACKET CORRODED.Dec 12, 2005 · Piper PA34200T · Rudder StructureSDR 2005FA0000108Shaft · out of roundUPON INSTALLING A SHAFT INTO A ROCKER WITH INADEQUATE TOLERANCE LIMITS, NOTED BINDING IN THREE CLOCK POSITIONS. WITH PRUSSION BLUE, FOUND THAT THE SHAFT IS FORMED IN AN ELIPTICAL OR, MODIFIED TRI-ANGULAR SHAPE WITH REDUCED WEAR SURFACE AREA DUE TO INCONSISTANTJan 30, 2005 · N123AP · Piper PA34200T · Reciprocating Engine Power SectionSDR 2005FA0000484Shaft · out of roundUPON INSTALLING A SHAFT INTO A ROCKER WITH INADEQUATE TOLERANCE LIMITS, NOTED BINDING IN 3 O`CLOCK POSITIONS. WITH PRUSSION BLUE FOUND SHAFT IS FORMED IN ELIPTICAL OR, MODIFIED TRIANGULAR SHAPE WITH REDUCED WEAR SURFACE AREA DUE TO INCONSISTANT DIA OF SHAFT. Jan 30, 2005 · N123AP · Piper PA34200T · Reciprocating Engine Power SectionSDR CA040901001Tube · out of tolerance(CAN) TUBE PURCHASED NEW. INSTALLED NEW. TEE SHOOTING AT VARIOUS REPAIR STATIONS DISCOVER CIRCLIP GROOVE TOO SMALL TO ACCOMODATE FULL CLIP SEATING. (GROOVE UNDERSIZED)NEW TUBE PURCHASED AND REPLACED. NO FAULT TO DATE. INITIAL RECURRING FAULTS INC LUDED, LOSS Aug 18, 2004 · Piper PA34200T · Nose/Tail Landing Gear Strut/AxleSDR AUS20040204Tube · worn(AUS) NOSE LANDING GEAR EXTENSION HYDRAULIC PIPE WORN THROUGH BY CONTACT WITH THE NLG BRAKE FLUID COVER ASSEMBLY. LOSS OF HYDRAULIC FLUID.Feb 25, 2004 · Piper PA34200T · Landing Gear Retraction/Extension SystemSDR CA030729020Door · cracked(CAN) CRACKS ON THE MAIN LANDING GEAR DOOR FLANGE. BOTH LT AND RT DOOR. DOOR IS FIBERGLASS COMPOSITE STRUCTURE. MAIN LANDING GEAR DOOR LT PN 67090-10 MAIN LANDING GEAR DOOR RT PN 67090-11.Jul 21, 2003 · Piper PA34200T · Landing Gear DoorsSDR AUS20030413Fitting · fractured(AUS) LEFT ENGINE FUEL LINE FITTING FAILED. FUEL LEAK.Apr 3, 2003 · Piper PA34200T · Engine Fuel DistributionSDR AUS20030371Spar Cap · corroded(AUS) RH STABILATOR LOWER SPAR CAP CORRODED.Feb 26, 2003 · Piper PA34200T · Empennage StructureSDR CA030107018Line · corroded(CAN) DURING A GROUND RUN FOR CALIBRATION OF AN UNRELATED SYSTEM THE ENGINEER NOTICED A STRONG FUEL SMELL IN THE CABIN. THE SOURCE WAS FOUND TO BE A CORRODED HEATER FUEL LINE AT APPROXIMATELY FS 165. THE CARPET AHEAD OF PASSENGER SEAT NR 6 WAS SOAKED WITH FUELDec 24, 2002 · Piper PA34200T · Heating SystemSDR AUS20020713Cable · separated(AUS) FORWARD LH STABILATOR TRIM CABLE DISCONNECTED FROM TRIM WHEEL.BALL END OF CABLE HAD COME OUT OF THE SOCKET ON THE SIDE OF THE WHEEL.Jun 18, 2002 · Piper PA34200T · Elevator Tab Control SystemSDR AUS20011341Bolt · broken(AUS) STABILISER ATTACHMENT FITTING BOLTS BENT (2OFF) AND BROKEN(2OFF). INVESTIGATION FOUND THAT THE BOLTS WERE THE INCORRECT TYPE. THE PART NUMBER OF THE INCORRECT BOLTS WAS PNO NAS425-3-7.UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR.Dec 14, 2001 · Piper PA34200T · Fuselage, Stabilizer Attach FittingsSDR AUS20011183Housing · cracked(AUS) LH AND RH ENGINE TURBOCHARGER TURBINE HOUSINGS CRACKED. FOUND DURING INSPECTION IAW AD/TURBO/1. LH ENGINE - CONTINENTAL TSIO-360-E - SERIAL NUMBER 307156 TSO 338.6 HOURS - TSLSV 119.6 HOURS RH ENGINE - CONTINENTAL LTSIO-360-E - SERIAL NUMBER 306161TSO 33Nov 2, 2001 · Piper PA34200T · Exhaust TurbochargerSDR AU000624Stud · wrong part(AUS) BOTH PROPELLERS COULD NOT BE FITTED CORRECTLY DURING INSTALLATION TO RECENTLY OVERHAULED ENGINES. SUBSEQUENT INVESTIGATION FOUND THE ATTACHING STUDS WERE TOO LONG (-4 STUDS HAD BEEN FITTED INLIEU OF -3 STUDS). (X)Sep 1, 2000 · Piper PA34200T · Reciprocating Engine Power SectionSDR 20000809SH004Magneto · failedTEST RUN SHOWED MAGNETO TO BE DEAD. REMOVED AND DISASSEMBLED MAGNETO. FOUND WIPER TAB FOR DISTRIBUTOR GEAR TO BE SHEARED OFF OF GEAR. (X)Aug 1, 2000 · N4128M · Piper PA34220T · Magneto/DistributorSDR AU000330Crankcase · cracked(AUS) CRANKCASE CRACKED IN NUMEROUS PLACES. CRANKCASE HAD BEENPREVIOUSLY WELD REPAIRED.Jan 31, 2000 · Piper PA34200T · Reciprocating Engine Power SectionSDR AU991037Stall Warning · malfunctioned(AUS) STALL WARNING SYSTEM FAULTY. SYSTEM WORKS PERFECTLY ON THE GROUND BUT FAILS TO OPERATE IN THE AIR. THE SYSTEM HAS BEEN THOROUGHLY CHECKED WITH NUMEROUS COMPONENT CHANGES TO NO AVAIL.Aug 26, 1999 · Piper PA34200T · Stall Warning SystemSDR 2000ZZZX163Fuel Pump · brokenAIRCRAFT WAS EN ROUTE FROM OWA TO HTO, CRUISE AT 4,500 MSL. EXPERIENCED ENGINE AND FUEL FLOW FLUCTUATIONS, THEN COMPLETE LOSS OF POWER. WAS CLOSE TO WST, SECURED LEFT ENGINE AND LANDED. REEVES AIR INSPECTED AND FOUND LEFT ENGINE DRIVEN FUEL PUMP INOPERABLE.Aug 18, 1999 · N797MT · Piper PA34200T · Engine Fuel PumpSDR AU990854Co2 Detector · faulty(AUS) CARBON DIOXIDE DETECTOR FAULTY.Aug 18, 1999 · Piper PA34200T · Emergency EquipmentSDR AU990836Liner · unserviceable(AUS) CABIN HEATER COMBUSTION LINER FAILED. FOUND DURING INSPECTION IAW AD/AIRCON/9 AMDT5.Aug 17, 1999 · Piper PA34200T · Heating SystemSDR CA991231062Cotter Pin · broken(CAN) COTTER PIN FOUND IN OIL SCREEN AT 100HR INSP.Feb 22, 1999 · Piper PA34200T · Reciprocating Engine Power SectionSDR CA991231063Crankshaft · cracked(CAN) TWO CRACKS FOUND BY NDI SHOP, CRANK REJECTED.Feb 22, 1999 · Piper PA34200T · Reciprocating Engine Power SectionSDR AU980280Crankcase · cracked(AUS) ENGINE CRANKCASE RT HALF CRACKED IN NR 4 MAIN BEARING TUNNEL AND LT HALF CRACKED IN NR 2 AND NR 3 MAIN BEARING TUNNELS. CRANKSHAFT CRACKED ON NR 4 MAIN BEARING. CRACK LENGTH APPROXIMATELY 50.8MM (2 INCHES).Feb 4, 1998 · Reciprocating Engine Power SectionSDR CA980302002Cylinder · separated(CAN) THE TOP OF THE CYLINDER CONTAINING THE VALVES AND THE ROCKER ARMS SEPARATED FROM THE CYLINDER.Nov 20, 1997 · Piper PA34200T · Reciprocating Engine Cylinder SectionSDR CA971016002Piston Ring · broken(CAN) DURING CYLINDER REMOVAL TO CORRECT AN OIL CONSUMPTION PROBLEM, IT WAS FOUND THAT PISTON RING (P/N 684042) WAS BROKEN. IT APPEARS THERE WAS A CASTING PROBLEM DURING MANUFACTURER.Oct 8, 1997 · Piper PA34200T · Reciprocating Engine Cylinder SectionSDR AU970799Cylinder · distorted(AUS) NO6 CYLINDER EXHAUST FLANGE DISTORTED - 2MM (0.078IN) GAP ON FORWARD SIDE - FURTHER INVESTIGATION FOUND NO2 AND NO4 CYLINDERS WITH APPROXIMATELY 1MM (0.039IN) GAPS - HEAT DAMAGE TO ENGINE COWLS FROM LEAKING EXHAUST GASSES - NEW GASKETS HAD BEEN FITTED APJun 20, 1997 · Piper PA34200T · Reciprocating Engine Cylinder SectionSDR AU970915Bearing · bindiing(AUS) LH ENGINE MIXTURE CONTROL ROD END BEARING AND CONTROL ARM BINDING ON FCUMay 20, 1997 · Piper PA34200T · Mixture ControlSDR AU960808Exhaust Valve · failed(AUS) LH ENGINE NO5 CYLINDER EXHAUST VALVE FAILED - SUSPECT CAUSED BY EXCESSIVE LEANING OF ENGINEMay 28, 1996 · Piper PA34200T · Reciprocating Engine Cylinder SectionSDR 96ZZZX938Line · brokeFUEL LINE FROM FLOW DIVIDER TO NR 6 NOZZLE BROKE AT B-NUT NOZZLE AND SPRAYED RAW FUEL ON ENGINE. ENGINE ROUGH, BUT NOT SHUT DOWN AND LANDED OK WITH NO FIRE. VERY LUCKY!Jan 30, 1996 · N999CC · Piper PA34200T · Fuel DividerSDR CA951218018Fuel Pump · faulty(CAN)DURING A TRAINING FLIGHT,AT 5,000 FEET,THE #2 ENGINE HAD A LOSS OF POWER & THE LOWERING OF PRESSURE ON THE FUEL FLOW INDICATOR.THE #2 ENGINE WAS SHUTDOWN & THE AIRCRAFT LANDED.AFTER ARRIVAL THE #2 ENG INE WAS RUN UP,THREE TIMES IT FAILED TO EXCEED 2,000 RDec 11, 1995 · Piper PA34200 · Engine Fuel PumpSDR BIER950010Adapter Shaft · shearedTACH INDICATED 0 RPM BUT ENGINE RAN NORM. FOUND TACH DRIVE ADAPTER SHEARED AT ATTACH NUT. REMOVED AND REPL WITH NEW.Apr 21, 1995 · N9211K · Piper PA34200T · Engine RPM Indicating SystemSDR 96ZZZX4786Crankcase · crackedDURING TROUBLESHOOTING TO DETERMINE ORIGIN OF AN OIL LEAK, FOUND CASE CRACKED ON BOTH VALVES AT NR 3 BEARING WEB. UPON TEAR DOWN, CASE HALVES WERE REJECTED DUE TO FAILING HARDNESS TEST. CRACKS WERE IN AREA OF A PREVIOUS REPAIR. CAUSE OF FAILURE UNKNOWN.Mar 13, 1995 · N321GS · Piper PA34200T · Reciprocating Engine Power Section
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