Continental TSIO-360-F

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 = 'TSIO360F'
  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 2012FA0000228Spark Plug · damagedPILOT REPORTED ENGINE BEGAN RUNNING ROUGH AT 11,000 FT. DESCENDED TO 5,000 FT AND ENGINE OPERATED CORRECTLY. RETURNED TO AIRPORT, LANDED WITHOUT FURTHER INCIDENT. REMOVED TOP COWLING AND ALL 12 SPARK PLUGS, PN RMH38E. ALL SPART PLUGS RUSTED ON OUTSIDE AND Mar 2, 2012 · N151JF · Piper PA28R201T · Spark Plug/IgniterSDR CA090303006Main Bearing · failed(CAN) LARGE PIECE OF FERROUS MATERIAL FOUND IN OIL PICKUP SCREEN DURING ROUTINE INSP, PIECE IDENTIFIED AS PORTION OF CTR MAIN BRG. ENGINE REMOVED FROM ACFT, DISASSEMBLED, INSP CONFIRMS COMPLETE FAILURE OF NR 2 CTR MAIN BRG. IN CONJUNCTION, CRANKCASE BRG SADDLMar 2, 2009 · Piper PA28R201T · Reciprocating Engine Power SectionSDR CA090220005Plug · missingON APPROACH TO YBL, THE PILOT DETECTED BURNING OIL AND SAW SMOKE, THE PILOT LANDED THE AIRCRAFT AND NOTICED A LARGE AMOUNT OF OIL ON THE BELLY OF THE AIRCRAFT AND DRIPPING FROM THE COWLS, AFTER THE TECHNICIAN INVESTIGATED THE OIL LEAK HE FOUND A HOLE WHERE A PFeb 13, 2009 · Piper PA28R201T · Accessory GearboxesSDR NTB2008F00000Impulse Coupling · brokenIMPULSE COUPLING SPRING BROKEN. EVIDENCE OF PRE-EXISTING CRACK AND CORROSION. VERY LOW TIME IN SERVICE. MAG TO ENGINE TIMING LOST. BOTH MAGS EXPERIENCED THE SAME FAILURE ALMOST SIMULTANEOUSLY. (K)Aug 8, 2008 · N5880V · Piper PA28R201T · Magneto/DistributorSDR NTB2008F00001Spring · brokenIMPULSE COUPLING SPRING BROKEN. EVIDENCE OF PRE-EXISTING CRACK AND CORROSION. VERY LOW TIME IS SERVICE. MAG TO ENGINE TIMING LOST. BOTH MAGS EXPERIENCED THE SAME FAILURE ALMOST SIMULTANEOUSLY. (K)Aug 8, 2008 · N5880V · Piper PA28R201T · Magneto/DistributorSDR CA070919001Tube · broken(CAN) FUEL DISCHARGE TUBE BROKE, ENGINE LOST POWER. SUSPECT MID-TUBE CLIP P/N: 626477-2 MAY HAVE FAILED FIRST. (TC NR 20070919001)Sep 17, 2007 · Piper PA28R201T · Aircraft Fuel Distribution SystemSDR CA070502008Control Cable · damaged(CAN) MIXTURE CONTROL WAS FOUND TO BE STIFF BY MAINT ON AN ENGINE START FOR TAXI TO HANGER. CABLE WAS REMOVED. THE CABLE ROUTING POSITIONS THE CABLE LESS THAN (6) INCHES FROM THE TURBOCHARGER. AN ASBESTOS COVER HAD PREVIOUSLY BEEN PLACED OVER THE CABLE AND STIApr 27, 2007 · Piper PA28R201T · Mixture ControlSDR CA070118003Pump · faulty(CAN) ENGINE DRIVEN FUEL PUMP OUTPUT IS LOW AT RATED RPM 2600. (TC NR 20070118003)Jan 10, 2007 · Piper PA28R201T · Engine Fuel PumpSDR 2004FA0000845Shaft · mismanufacturedDURING 100 HOUR INSP AT 1V5, LT CONTROL COLUMN, P/N 62834-02, WAS REMOVED FOR REPLACEMENT DUE TO EXCESS PLAY. UPON REMOVAL, CONTROL COLUMN SHAFT, P/N 62716-02, WAS FOUND TO BE DRILLED (FOR AN-386-1-6A TAPER PIN) LESS THAN 0.025 INCH FROM AFT END OF SHAFT. HOLOct 18, 2004 · N43761 · Piper PA28R201T · Control Column SectionSDR 2004FA0000846Shaft · mismanufacturedDURING 100 HR INSP AT 1V5, LT CONTOL COLUMN UNIVERSAL,P/N 62834-02, WAS REMOVED FOR REPLACEMENT DUE TO EXCESS PLAY. CONTROL COLUMN SHAFT, P/N 62716-02, WAS FOUND TO BE DRILLED (FOR THE AN-386-1-6A TAPER PIN) LESS THAN 0.025 INCH FROM AFT END OF SHAFT. HOLE IOct 18, 2004 · N43761 · Piper PA28R201T · Control Column SectionSDR AUS20030626Stud · cracked(AUS) MAIN LANDING GEAR SIDE BRACE STUD CONTAINED LONGITUDINAL MPI INDICATIONS. FOUND DURING INSPECTION IAW AD/PA28/91 AMDT1.Jun 20, 2003 · Piper PA28R201T · Landing Gear Retraction/Extension SystemSDR AUS20030367Link · failed(AUS) NOSE LANDING GEAR DRAG LINK ASSEMBLY SHEARED IN AREA LOCATEDFORWARD OF THE RH ATTACHMENT POINT.Mar 25, 2003 · Piper PA28R201T · Landing Gear Retraction/Extension SystemSDR AUS20020155Capacitor · faulty(AUS) LH MAGNETO CAPACITOR WIRE INTERMITTENT CONTACT.Mar 1, 2002 · Piper PA28R201T · Magneto/DistributorSDR AUS20020156Capacitor · faulty(AUS) RH MAGNETO CAPACITOR WIRE INTERMITTENT CONTACT.Feb 5, 2002 · Piper PA28R201T · Magneto/DistributorSDR AU000534Stud · cracked(AUS) LEFT AND RIGHT MAIN LANDING GEAR SIDE BRACE STUDS CRACKED. FOUND DURING MAGNETIC PARTICLE INSPECTION IAW AD/PA28/91. (X)Jul 10, 2000 · Piper PA28R201T · Wing, Landing Gear Attach FittingsSDR CA000530031Trunnion · cracked(CAN) DURING A 50-HOUR INSPECTION OF THE LANDING GEAR, THE NOSE GEAR TRUNNION WAS FOUND CRACKED AT SHIMMY DAMPENER ATTACHMENT POINT. POSSIBLE CAUSE - OVERSTEER.May 1, 2000 · Piper PA28RT201T · Nose/Tail Landing Gear Strut/AxleSDR AU000342Fuel Tank · leaking(AUS) FUEL TANK LEAKING. INSPECTION FOUND FAULTY SEALANT. FOUND FOLLOWING COMPLIANCE WITH AD/GEN/80.Apr 7, 2000 · Piper PA28R201T · Fuel StorageSDR 99ZZZX1076Bypass Pipe · not installedA TURBO HEAT BLANKET WAS INSTALLED ON 1-28-99. SUBMITTER STATED DURING THE INSTALLATION OF THE TURBO HEAT BLANKET, THE MECHANIC FAILED TO REINSTALL THE EXHAUST BYPASS VALVE PIPE (STC SA4731 NM/STC 4731 NM) THAT DIRECTED EXHAUST GAS OUTBOARD OF THE ENGINE. THMar 5, 1999 · N6140H · Piper PA28R201T · Exhaust TurbochargerSDR CA990318049Flyweight · loose(CAN) PILOT REPORTED ROUGH RUNNING ENGINE ON RUN-UP. INSPECTION FOUND RIGHT HAND MAGNETO DEAD. DURING REMOVAL OF THE MAGNETO, THE IMPULSE COUPLING FLYWEIGHT FELL OUT. THE AXLE/RIVET HEAD FOUND MISSING. ALL CYLINDERS, OIL SUMP AND ACCESSORY SECTION, WERE INFeb 18, 1999 · Piper PA28RT201T · Magneto/DistributorSDR CA980430038Tube Assy · cracked(CAN) TUBE CRACKED UNDER CLAMP. NOT VISIBLE WITH CLAMP ON. REPLACED.Apr 14, 1998 · Piper PA28R201T · Aircraft Fuel Distribution SystemSDR CA980331021Cable · stiff(CAN) BOTH PROP AND MIXTURE CONTROL CABLES VERY STIFF. AREA BEHIND TURBO BADLY CORRODED. CABLES REPLACED.Mar 9, 1998 · Piper PA28R201T · Mixture ControlSDR AU970577Elt · faulty(AUS) ELT FAULTY - `G' SWITCH UNSERVICEABLE - BATTERIES OF EUROPEAN ORIGIN FITTED - BATTERY INSULATORS WORN - EVIDENCE OF MOISTURE INGRESSJun 2, 1997 · Piper PA28RT201T · Emergency Locator BeaconSDR AU970450Cable · stuck(AUS) MIXTURE CONTROL CABLE STUCK - CABLE RUNS ADJACENT TO TURBOCHARGER - THROTTLE CABLE AND PROPELLER CONTROL CABLES ALSO RUN ADJACENT TO THE TURBOCHARGERApr 18, 1997 · Piper PA28R201T · Mixture ControlSDR 97ZZZX1589Cylinder · head separatedDURING ANNUAL INSPECTION, FOUND NR 2 CYLINDER HEAD SEPARATING FROM BARREL. THE HEAD WAS TURNED COUNTERCLOCKWISE 4 DEGREES AND WAS .0625 INCH FARTHER FROM FIRST CYLINDER FIN THAN OTHER CYLINDERS. LEAK CHECK (PARAGRAPH C TCM SB 96-12) REVEALED LEAK. COMPRESSIMar 21, 1997 · Reciprocating Engine Cylinder SectionSDR AU970140Actuator · failed(AUS) NOSE LANDING GEAR HYDRAULIC ACTUATOR FAILED AT FUSELAGE ATTACHMENT POINTJan 27, 1997 · Piper PA28R201T · Landing Gear ActuatorSDR 97ZZZX3739Stud · failedAS A RESULT OF AN ACCIDENT, FOLLOW-UP INVESTIGATION REVEALED THE ENGINE LOST POWER DUE TO FAILURE OF THE ROCKER ARM SHAFT HOLD-DOWN STUDS ON NR 2 CYLINDER. AD 92-04-09 WAS C/W. THE CYLINDER WAS AN EXCHANGE INSTALLED AT THE LAST OVERHAUL. STUDS FAILED MOST LDec 31, 1996 · N40437 · Piper PA28201T · Reciprocating Engine Cylinder SectionSDR 96ZZZX5470Lock Tab · failedCYLINDERS WERE SENT OUT FOR CHROMING AND OVERHAUL. CYLINDERS WERE RECEIVED BACK READY TO INSTALL. NEW SUPERIOR AIR PARTS ROCKER ARM SHAFT BOLT LOCK TABS WERE INSTALLED. UPON BENDING TANGS OVER BOLT HEADS, ALL TANGS EITHER CRACKED OR BROKE OFF COMPLETELY. SSep 10, 1996 · Piper PA28R201T · Reciprocating Engine Cylinder SectionSDR 95ZZZX5104Piston Pin · brokenNR 2 CYLINDER PISTON PIN FAILED AT MIDSECTION (BROKEN IN HALF). SUBSEQUENT FAILURE OF NR 2 PISTON AND METAL CONTAMINATED SUPERIOR AIR PARTS SUPPLIED PISTON PIN WITH A SHIP DATE OF 11-8-94. CAUSE UNKNOWN.Aug 1, 1995 · N327LP · Piper PA28R201T · Reciprocating Engine Cylinder Section
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