# Service difficulty reports: Continental TSIO-360-EB

A list on [Continental TSIO-360-EB](https://openairdocs.org/engine/continental-tsio-360-eb.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 76 reports

- [SDR AYKA20240403108](https://openairdocs.org/sdr/AYKA20240403108.md): Retainer · cracked · Apr 3, 2024 · N107AB · Piper PA34200T · Reciprocating Engine Cylinder Section
  > ROCKER ARM SHAFT RETAINER CONTINENTAL P/N # 631996. FOUND CRACKED RETAINERS DURING ANNUAL INSPECTION WHILE PERFORMING VISUAL INSPECTION. ORDER REPLACEMENTS. OLD PARTS ARE CAST AND NEW STYLE REPLACEMENT WITH SAME PART NUMBER LOOKS TO BE BILLET.
- [SDR 2024FA0000277](https://openairdocs.org/sdr/2024FA0000277.md): Retainer · cracked · Apr 2, 2024 · N107AB · Piper PA34200T · Reciprocating Engine Cylinder Section
  > ROCKER SHAFT RETAINERS CRACKED. X 8 4 ON LEFT ENGINE AND 4 ON RIGHT ENGINE.
- [SDR 2022FA0000485](https://openairdocs.org/sdr/2022FA0000485.md): Bolt · used · Aug 1, 2022 · N8111P · Piper PA34200T · Fasteners
  > LEFT LANDING GEAR SCISSOR LINK CENTER BOLT FAILED DURING TAXI
- [SDR CA190521033](https://openairdocs.org/sdr/CA190521033.md): Cotter Pin · broken · May 17, 2019 · Piper PA34200T · Reciprocating Engine Power Section
  > (CAN) DURING ROUTINE MAINTENANCE A PIECE OF METAL WAS FOUND IN THE L/H ENGINE OIL SUMP SCREEN. FURTHER INVESTIGATION FOUND THAT THE COTTER PIN INSTALLED INTO THE #4 CYLINDER CONNECTING ROD BOLT HAD BROKEN. THE HEAD OF THE COTTER PIN IS WHAT WAS FOUND IN THE OI
- [SDR CA190405018](https://openairdocs.org/sdr/CA190405018.md): Seal · inadequate · Apr 5, 2019 · Piper PA34200T · Flight Compartment Windows
  > (CAN) RH WINDSHIELD LOWER OUTBOARD CORNER WAS NOT SEALED SUFFICIENTLY AND CAUSED MOISTURE TO ENTER STRUCTURE. THE STEEL BRACKET BELOW THIS CORNER HAD ACCUMULATED EXCESSIVE CORROSION. ALL SURROUND STRUCTURE INSPECTED AND ONLY STEEL BRACKET WAS AFFECTED. BRACKET
- [SDR APCA2016072600001](https://openairdocs.org/sdr/APCA2016072600001.md): Stud · broken · Jul 26, 2016 · N36319 · Reciprocating Engine Cylinder Section
  > CYLINDER NR 6 HAD BROKEN BOTH EXHAUST ROCKER SHAFT STUDS. HAPPENED ON SAME CYLINDER APPROXIMATELY 200 HOURS AGO ON A FACTORY CYLINDER WITH 1000 HOURS. PUSH ROD IS NOT BENT, LIFTER DOES NOT SHOW ANY SCORING. OUR ASSUMPTION IS THE LIFTER HYDRAULICALLY LOCKED
- [SDR CA140822003](https://openairdocs.org/sdr/CA140822003.md): Crankshaft · cracked · Aug 7, 2014 · Piper PA34200T · Reciprocating Engine Power Section
  > (CAN) DURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED ON THE ENGINE CRANKSHAFT FLANGE, WHERE THE PROPELLER MOUNTS. THE CRACK WAS VERY SEVERE AS VERY TINY PIECES OF THE FLANGE HAD BROKEN OFF. THE CRACK APPEARS TO EXTEND THROUGH THE FLANGE OTBD OF THE DOWE
- [SDR CA121214007](https://openairdocs.org/sdr/CA121214007.md): Trunnion · cracked · Dec 14, 2012 · Piper PA34200T · Fuselage, Landing Gear Attach Fittings
  > (CAN) DURING ANNUAL INSPECTION, THE ENGINEER VISUALLY INSPECTING THE MAIN LANDING GEAR NOTICED A CRACK MIGRATING OUT OF THE LOWER BOLT HOLE OF LT FWD MLG ATTACH TRUNNION.
- [SDR 2012FA0000133](https://openairdocs.org/sdr/2012FA0000133.md): Trunnion · worn · Feb 24, 2012 · N449S · Piper PA34200T · Fuselage, Landing Gear Attach Fittings
  > DURING AN INSPECTION OF THE MLG, THE GEAR TRUNNION MOUNTING PLATES BOLTS WERE FOUND TO BE WITHIN TORQUE LIMITS, BUT LOOSE IN THE PLATES AND SPARS, REMOVED PLATES AND FOUND MOUNTING HOLES ELONGATED, REAMED HOLES FOR OVERSIZED HARDWARE IAW SB 956, RECOMMEND CHE
- [SDR 2012FA0000134](https://openairdocs.org/sdr/2012FA0000134.md): Trunnion · worn · Feb 24, 2012 · N863N · Piper PA34200T · Fuselage, Landing Gear Attach Fittings
  > DURING AN INSPECTION OF THE MLG, TRUNNION MOUNTING PLATES BOLTS FOUND TO BE WITHIN TORQUE LIMITS, BUT LOOSE IN THE PLATES AND SPARS, REMOVED PLATES AND FOUND MOUNTING HOLES ELONGATED, REAMED HOLES FOR OVERSIZED HARDWARE PER SB 956, RECOMMEND CHECKING THE TORQU
- [SDR 2012FA0000089](https://openairdocs.org/sdr/2012FA0000089.md): Seal · frozen · Feb 1, 2012 · N969WA · Piper PA34200T · Aileron Control System
  > DEPARTED AND CLIMBED THROUGH MODERATE TO HEAVY PARTICIPATION FOR 10-15 MINUTES, LEVELED OFF AT 9,000 FT WHICH WAS AN ALTITUDE THAT WAS BELOW FREEZING. SET AUTOPILOT FOR STRAIGHT AND LEVEL FLIGHT AND AFTER ABOUT 10 MINUTES, NOTICED THAT THE AIRPLANE WAS VEERIN
- [SDR CA110719006](https://openairdocs.org/sdr/CA110719006.md): Magneto · departed · Jul 19, 2011 · Piper PA34200T · Magneto/Distributor
  > DURING ENGINE THE PRE-FLIGHT RUN UP THE PILOTS NOTICED RT ENGINE ROUGHNESS AND LT MAGNETO DROP WAS EXCESSIVE. ACFT RETURNED TO CHOCKS AND FLIGHT WAS CANCELLED. A LARGE AMOUNT OF OIL WAS THEN DISCOVERED UNDER THE COWLING. MX DISCOVERED THAT THE LT MAGNETO HAD
- [SDR 2011FA0000402](https://openairdocs.org/sdr/2011FA0000402.md): Adapter · slipped · Jun 7, 2011 · N5561V · Piper PA34200T · Engine Starter
  > THE STARTER ADAPTER WAS SENT IN FOR REPAIR, UPON DISASSEMBLY, OUR FINDINGS, THE STARTER ADAPTER WAS SLIPPING DUE TO EXCESSIVE STARTER ENGAGEMENT WHICH OVERHEATED THE SAFT GEAR AND CLUTCH SPRING BOTH ITEMS HAVE REJECTED.
- [SDR 2011F00018](https://openairdocs.org/sdr/2011F00018.md): Cylinder · failed · Jan 16, 2011 · N51157 · Piper PA34200T · Reciprocating Engine Cylinder Section
  > PILOT NOTED REDUCTION IN MANIFOLD PRESSURE AND OIL PRESSURE ON LT ENGINE. PILOT REDUCED POWER TO IDLE AND REQUESTED LANDING AT NEAREST AIRPORT. POST LANDING INSP OF ENGINE REVEALED CRACK IN CYLINDER WALL AND PART OF PISTON MISSING.
- [SDR FFKA139](https://openairdocs.org/sdr/FFKA139.md): Stud · sheared · Jul 6, 2009 · N8076N · Piper PA34200T · Reciprocating Engine Cylinder Section
  > PILOT REPORTED-ENG ROUGHNESS, WAS NOTICED ON THE LT ENGINE, TURNED ON THE AUXILIARY FUEL PUMP AND ENGINE BEGAN TO RUN BETTER BUT UNABLE TO MATCH MANIFOLD TO RT ENGINE. VISIBLE OIL FROM RT SIDE OF COWLING WAS NOTICED AND ENG WAS SHUTDOWN AND FEATHERED. MX INVE
- [SDR FFKA138](https://openairdocs.org/sdr/FFKA138.md): Oil Cooler · leaking · May 11, 2009 · N21407 · Piper PA34200T · Engine Oil Cooler
  > IN CRUISE FLIGHT PILOT NOTICED LOW OIL PRESSURE LIGHT ILLUMINATED AND THE LEFT ENGINE OIL PRESSURE GAUGE DROPPING TO ZERO. PILOT PERFORMED ENGINE SHUTDOWN AND LANDING WAS UNEVENTFUL. POST INSPECTION REVEALED THAT THE ENGINE OIL COOLER WAS LEAKING FROM WITHIN
- [SDR FFK2008F00002](https://openairdocs.org/sdr/FFK2008F00002.md): Cam · worn · Sep 2, 2008 · N3570M · Piper PA34200T · Magneto/Distributor
  > PILOT REPORTED A "POPPING" SOUND COMING FROM THE LT ENGINE, AFTER INVESTIGATION MAINT FOUND THAT THE LT ENGINE LT MAGNETO CAM FOLLOWER EXCESSIVELY WORN. REPLACED MAGNETO AS NEEDED NO FURTHER PROBLEMS NOTED. (K)
- [SDR CA080317004](https://openairdocs.org/sdr/CA080317004.md): Gear · failed · Feb 14, 2008 · Piper PA34200T · Accessory Gearboxes
  > (CAN) LOW OIL PRESSURE LIGHT CAME ON IMMEDIATELY AFTER TAKEOFF. PWR WAS BROUGHT BACK AND AC RETURNED FOR SAFE LANDING. ENGINE WAS SHUTDOWN OFF RUNWAY, PROP FEATHERED AUTOMATICALLY. BOTH SUCTION SCREEN AS WELL AS OIL FILTER INSPECTED, NO METAL CONTAMINANTS FOU
- [SDR FFKA118](https://openairdocs.org/sdr/FFKA118.md): Crankshaft · cracked · May 17, 2007 · N6935C · Piper PA34200T · Reciprocating Engine Power Section
  > PILOT REPORTED AN OIL LEAK COMING FROM THE LEFT (NR 1) ENGINE AFTER FINISHING THEIR FLIGHT FOR THE DAY. MAINTENANCE INVESTIGATED THE OIL LEAK AND FOUND THE CRANKSHAFT CRACKED AROUND THE CIRCUMFERENCE OF THE PROPELLER FLANGE. WHEN MAINTENANCE STARTED TO REMOV
- [SDR 2007FA0000277](https://openairdocs.org/sdr/2007FA0000277.md): Crankshaft · failed · Mar 22, 2007 · Reciprocating Engine Power Section
  > CRANKSHAFT FAILED NDI SB MSB96-10. (K)
- [SDR FFKA1020112](https://openairdocs.org/sdr/FFKA1020112.md): Adapter · broken · Oct 19, 2006 · N39545 · Piper PA34200T · Engine Fuel Distribution
  > FUEL FITTING ADAPTER P/N 630119 BROKE IN HALF CAUSING A LOSS OF POWER.
- [SDR CA050913008](https://openairdocs.org/sdr/CA050913008.md): O-Ring · worn · Sep 1, 2005 · Piper PA34200T · Landing Gear Actuator
  > (CAN) PILOT REPORTED THAT LANDING GEAR FAILED TO RETRACT. AIRCRAFT PLACED ON JACKS, LANDING GEAR SWUNG, FOUND NOSE GEAR ACTUATOR FAILED TO COMPLETELY RETRACT. REMOVED NOSE GEAR ACTUATOR, DISASSEMBLED, FOUND PISTON ORING EXCESSIVELY WORN. INSTALLED NEW ORINGS
- [SDR CA050505003](https://openairdocs.org/sdr/CA050505003.md): Wheel · cracked · Apr 25, 2005 · Piper PA34200T · Wheel/Ski/Float
  > (CAN) ON LANDING PILOT REPORTED A NOISE FROM THE LT MAIN LANDING GEAR. INSPECTION FOUND THE INNER WHEEL HALF CRACKED AT THE BASE OF THE WHEEL FLANGE FOR APPROX 4 INCHES AND THE WHEEL FLANGE BOWED OUTWARD AND INTERFERING WITH THE BRAKE CALIPER. THE WHEEL ASSY W
- [SDR CA050414009](https://openairdocs.org/sdr/CA050414009.md): Bearing · chipped · Apr 14, 2005 · Piper PA34200T · Propeller Hub Section
  > (CAN) HUB P/N D2201-18, CHIPPED IN TWO PLACES AND TOOL MARK ALL IN A 1 INCH AREA ON INSTALLATION SEAL LIP. FORK P/N WORN BEYOND MAXIMUN/M LIMITS T/2 BEARINGS P/N DENTED BEYOND SERVICABLE LIMITS. THESE US PARTS RETURNED TO CUSTOMER.
- [SDR CA050401008](https://openairdocs.org/sdr/CA050401008.md): Alternator · failed · Mar 24, 2005 · Piper PA34200T · Alternator-Generator Drive
  > (CAN) ALTERNATOR FAILURE, SEPARATION OF DRIVE GEAR DUE TO SHEARED ROTOR SHAFT. METAL CONTAMINATION OF ENGINE.
- [SDR 2004FA0000874](https://openairdocs.org/sdr/2004FA0000874.md): Impulse Coupling · missing · Oct 6, 2004 · N6935C · Piper PA34200T · Magneto/Distributor
  > WHILE PERFORMING AD 96-12-07, THE MECHANIC NOTICED THAT THE STOP PIN FOR THE IMPULSE COUPLING WAS MISSING. INSPECTED THE ACCESSORY SECTION AND FOUND THE PIN WEDGED BETWEEN THE CRANK CASE AND A GEAR. REMOVED THE PIN, NO FURTHER DAMAGE WAS FOUND.
- [SDR CA040830002](https://openairdocs.org/sdr/CA040830002.md): Nut · failed · Aug 26, 2004 · Piper PA34200T · Fasteners
  > (CAN) DISCOVERED RT FWD TRUNION FITTING ATTACH BOLT ANCHOR NUT NOT RETAINING TORQUE DURING INSPECTION OF LANDING GEAR. LANDING GEAR REMOVED TO FACILITATE ANCHOR NUT REPLACEMENT. ALL ANCHOR NUTS REPLACED ON BOTH MLG FWD FITTINGS. ALSO FOUND HEAVY CORROSION O
- [SDR CA030324004](https://openairdocs.org/sdr/CA030324004.md): Mount · cracked · Mar 17, 2003 · Piper PA34200T · Nose/Tail Landing Gear Attach Section
  > (CAN) LOWER PORTION OF MOUNT ASSEMBLY TUBULAR STRUCTURE CRACKED, MOUNT MUST BE REMOVED TO FURTHER EVALUATEI.E. STRIP AND NDT INSPECTION BEFORE REPAIR STATUS CAN BE DETERMINED.
- [SDR AYQ2004F00000](https://openairdocs.org/sdr/AYQ2004F00000.md): Impulse Coupling · inoperative · Jan 23, 2003 · N969WA · Piper PA34200T · Magneto/Distributor
  > DEAD MAGNETO ON RUN UP. FOUND MAGNETO ROTATED IN ITS CLAMPS, TIMING WAY OFF. REMOVED MAG AND FOUND IMPULSE COUPLING MISSING CORNER OF PAWL PLATE.
- [SDR 2002FA0001153](https://openairdocs.org/sdr/2002FA0001153.md): Drive Shaft · failed · Aug 22, 2002 · N8385C · Piper PA34200T · Reciprocating Engine Oil System
  > RT ENGINE LOST OIL PRESSURE AFTER TAKEOFF DISASSEMBLY REVEALED BROKEN OIL PUMP DRIVE SHAFT/GEAR. SHAFT IS THE WEAK LINK.
- [SDR 2002FA0000953](https://openairdocs.org/sdr/2002FA0000953.md): Retainer · cracked · Jul 24, 2002 · N9712C · Piper PA34200T · Reciprocating Engine Cylinder Section
  > DURING AN ANNUAL INSPECTION, ONE ROCKER BOX COVER ON THE LEFT ENGINE WAS REMOVED IN THE PROCESS OF REPLACING PUSHROD TUBE SEALS. DISCOVERED ONE ROCKER SHAFT RETAINER CRACKED INTO TWO PIECES. DECIDED TO INSPECT REMAINDER OF CYLINDERS AND FOUND 19 OF 24 ROCKER
- [SDR CA020725006](https://openairdocs.org/sdr/CA020725006.md): Bearing · broken · Jul 7, 2002 · Piper PA34200T · Engine Starter
  > (CAN) ON A TRAINING FLIGHT IN CRUISE PILOTS OBSERVED LOW OIL PRESSURE LIGHT ILLUMINATION ON THE LT ENGINE AND NO OIL PRESSURE ON THE GAUGE. THE PROPELLER FEATHERED ON ITS OWN DUE TO NO OIL PRESSURE. ENGINE WAS SHUT DOWN ACCORDING TO THE EMERGENCY PROCEDURES AN
- [SDR CA020521005](https://openairdocs.org/sdr/CA020521005.md): Cylinder · cracked · May 13, 2002 · Piper PA34200T · Reciprocating Engine Cylinder Section
  > (CAN) STEEL BARREL CRACKED AROUND CIRCUMFERENCE JUST BELOW HEAD ATTACH AREA. 90 PERCENT.
- [SDR 2002FA0000310](https://openairdocs.org/sdr/2002FA0000310.md): Master Switch · broken · Feb 22, 2002 · N3054K · Piper PA34200T · Instrument Panel
  > THE MASTER SWITCH IS DIVIDED INTO TWO SWITCHES A THAT ARE COUPLED TOGETHER WITH A PLASTIC TAB. THE HALF OF THE SWITCH THAT CONTROLS THE ALTERNATOR FIELDS IS HIDDEN UNDER THE SIDE PANEL. WHEN THE TAB THAT COUPLES THE TWO TOGETHER BROKE, THE ALTERNATORS DROPPE
- [SDR CTU2002F00003](https://openairdocs.org/sdr/CTU2002F00003.md): Master Switch · broken · Feb 22, 2002 · N3054K · Piper PA34200T · Instrument Panel
  > THE MASTER SWITCH IS DIVIDED INTO TWO SWITCHES THAT ARE COUPLED TOGETHER WITH A PLASTIC TAB. THE HALF OF THE SWITCH THAT CONTROLS THE ALTERNATOR FIELDS IS HIDDEN UNDER THE SIDE PANEL. WHEN THE TAB THAT COUPLES THE TWO TOGETHER BROKE, THE ALTERNATORS DROPPED
- [SDR 2004FA0000626](https://openairdocs.org/sdr/2004FA0000626.md): Crankcase · cracked · Jan 16, 2002 · N35597 · Piper PA34200T · Reciprocating Engine Power Section
  > THE TURBOCHARGER ATTACHES TO THE ENGINE RT CRANKCASE, THROUGH A 21 INCH MOUNTING BRACKET, WHICH ATTACHES TO THE RT AFT ENGINE MOUNT. DURING A ROUTINE 100 HR INSPECTION, A 1.75 INCH CRACK WAS FOUND ON THE RT CRANKCASE HALF, RT AFT ENGINE MOUNT ATTACH. IT APPE
- [SDR 2004FA0000627](https://openairdocs.org/sdr/2004FA0000627.md): Crankcase · cracked · Jan 16, 2002 · N35597 · Piper PA34200T · Reciprocating Engine Power Section
  > THE TURBOCHARGER ATTACHES TO THE ENGINE RT CRANKCASE, THROUGH A 21 INCH MOUNTING BRACKET, WHICH ATTACHES TO THE RT AFT ENGINE MOUNT. DURING A ROUTINE 100 HR INSPECTION, A.75 INCH CRACK WAS FOUND ON THE RT CRANKCASE HALF, RT AFT ENGINE MOUNT ATTACH. IT APPEA
- [SDR 2002FA0000154](https://openairdocs.org/sdr/2002FA0000154.md): Cylinder Head · separated · Dec 31, 2001 · N2931L · Piper PA34200T · Reciprocating Engine Cylinder Section
  > DURING LEVEL FLIGHT THE LEFT ENGINE STARTED RUNNING VERY ROUGH. ENGINE FEATHERED AND AIRCRAFT RETURNED TO AIRPORT. ENGINE UNCOWLED AND NR 5 CYLINDER HEAD WAS FOUND SEPARATED FROM BARREL.
- [SDR EEJ2001F00001](https://openairdocs.org/sdr/EEJ2001F00001.md): Channel · cracked · Oct 12, 2001 · N81659 · Piper PA34200T · Landing Gear Steering System
  > NOSE WHEEL STEERING CHANNEL CRACKED AT RIGHT REAR WELD. MADE POPPING NOISE WHILE TAXING. DUE TO STEERING AIRCRAFT ON GROUND, NOSE WHEEL STEERING (WHERE BALL GOES INTO SAID CHANNEL) STRESSES THE WELDS ON FORWARD AND AFT ENDS THUS CRACKING THE WELDS.
- [SDR CA010322002](https://openairdocs.org/sdr/CA010322002.md): Liner · destroyed · Feb 8, 2001 · Piper PA34200T · Brake
  > (CAN) WHILE CONDUCTING A GENERAL WALK AROUND FOR A PRE-PURCHASE, THE INBOARD PRESSURE PLATE SIDE OF THE BRAKE CALIPERS, THE BRAKE LINERS WERE TOTALLY DESTROYED, RESULTING IN THE STEEL PRESSURE PLATE TO COME IN FULL CONTACT WITH THE BRAKE DISC WHICH CREATED DEE
- [SDR 20010305CW012](https://openairdocs.org/sdr/20010305CW012.md): Adapter · failed · Jan 25, 2001 · N2240D · Piper PA34200T · Engine RPM Indicating System
  > 90 DEGREE TACH DRIVE ADAPTER PUT ON AIRCRAFT. WHEN ADAPTER FAILS, THERE IS NO RPM INDICATION TO TACH. PROBLEM, APPARENTLY VIBRATION INDUCED. SOME PROVISIONS SHOULD BE MADE TO REINFORCE UNIT, OR RELOCATE IT TO AN AREA NOT AS PRONE TO VIBRATIONS.
- [SDR 20010222CW002](https://openairdocs.org/sdr/20010222CW002.md): Coupler · failed · Jan 23, 2001 · N304CW · Piper PA34200T · Alternator-Generator Drive
  > RT ALTERNATOR FAILED IN FLIGHT AT NIGHT. ALTERNATOR FAILURE CAUSED BY DRIVE COUPLER FAILURE.
- [SDR 20010301CW007](https://openairdocs.org/sdr/20010301CW007.md): Coupler · failed · Jan 23, 2001 · N304CW · Piper PA34200T · Alternator-Generator Drive
  > LT ALTERNATOR FAILED IN FLIGHT AT NIGHT. ALTERNATOR FAILURE CAUSE: DRIVE COUPLER FAILURE.
- [SDR 20010305CW011](https://openairdocs.org/sdr/20010305CW011.md): Adapter · failed · Jan 23, 2001 · N2240D · Piper PA34200T · Engine RPM Indicating System
  > 90 DEGREE TACH DRIVE ADAPTER PUT ON AIRCRAFT. WHEN ADAPTER FAILS, THERE IS NO RPM INDICATION TO TACH. PROBLEM APPARENTLY VIBRATION INDUCED. SOME PROVISION SHOULD BE MADE TO REINFORCE UNIT OR RELOCATE IT TO AN AREA NOT AS PRONE TO VIBRATIONS.
- [SDR CA001212018](https://openairdocs.org/sdr/CA001212018.md): Nut · cracked · Nov 24, 2000 · Piper PA34200T · Wing, Fuselage Attach Fittings
  > (CAN) THREE NUTS USED TO ATTACH THE LOWER END OF THE MAIN WING LONGERON TO THE INTERIOR LONGERON WERE FOUND CRACKED.ACCORDING TO A PIPER REP FOR API, THE SAME TYPE OF INSPECTION SHOWN IN PIPER SB 602 WOULD APPLY TO OUR AIRCRAFT. THE PROBLEM IS HOWEVER THAT OU
- [SDR 2002FA0000131](https://openairdocs.org/sdr/2002FA0000131.md): Pushrod · cracked · Aug 28, 2000 · N91284 · Piper PA34200T · Reciprocating Engine Power Section
  > ON ANNUAL INSPECTION OF THE LEFT ENGINE THREE PUSHRODS WERE NOTED TO BE CRACKED ALONG WHAT LOOKS LIKE THEIR ENTIRE LENGTHS. THE THREE DEFECTIVE PUSHRODS WERE REPLACED WITH NEW ONES, AND THE REMAINDER OF THE PUSHRODS WERE OVERHAULED FOR BOTH ENGINES. CAUSE OF T
- [SDR 20000821SH001](https://openairdocs.org/sdr/20000821SH001.md): Seal · worn · Aug 8, 2000 · N1278H · Piper PA34200T · Reciprocating Engine Cylinder Section
  > 372 HOURS TOTAL TIME SINCE NEW. RETAINER SPRINGS FELL OFF OF SEAL AND INTO THE OIL SYSTEM. NO DAMAGE CAUSED. THEY WERE CAUGHT IN OIL SCREEN. UPON REMOVAL OF VALVE COVERS AND VALVE SPRINGS, ALL SEALS WERE FOUND WORN AND SPRINGS READY TO WEAR THROUGH. (X)
- [SDR 20000515SH009](https://openairdocs.org/sdr/20000515SH009.md): Gear · mismanufactured · Apr 20, 2000 · Reciprocating Engine Rear Section
  > NEW OIL PUMP DRIVEN GEAR DOES NOT HAVE THE CHAMFER ON THE INSIDE OF THE TWO DRIVE SLOTS. THIS IS A MFG''S DEFECT. WHEN THE DRIVE IMPELLER NR 653814 IS INSTALLED, AND TACH NUT TORQUED, THE NR 654720 GEAR BOTTOMS ON THE 2 RADIUSES OF THE DRIVE DOGS THAT ENGAGE T
- [SDR CA000301041](https://openairdocs.org/sdr/CA000301041.md): Fuel Cell · contaminated · Feb 17, 2000 · Piper PA34200T · Fuel Storage
  > (CAN) WATER AND ICE IN FUEL SYSTEM.
- [SDR CA990303003](https://openairdocs.org/sdr/CA990303003.md): Hub · corroded · Feb 19, 1999 · Piper PA34200T · Propeller Hub Section
  > (CAN) INSPECTION FOUND CORROSION ON THE HUB TO ENGINE MOUNTING FLANGE. THE BEARING RACES WERE ALSO DENTED BY THE BALLBEARINGS. THE HUB WAS OVERHAULED AND THE BEARINGS WERE REPLACED.

Next page: https://openairdocs.org/engine/continental-tsio-360-eb/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'TSIO360EB'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/continental-tsio-360-eb/reports

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