# Service difficulty reports: Lycoming IO-360-C1E6

A list on [Lycoming IO-360-C1E6](https://openairdocs.org/engine/lycoming-io-360-c1e6.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 67 reports

- [SDR 2017FA0000257](https://openairdocs.org/sdr/2017FA0000257.md): Trunnion · broken · Jun 26, 2017 · N101SA · Piper PA34200 · Wing, Landing Gear Attach Fittings
  > LEFT MAIN LANDING GEAR REAR TRUNNION BROKE ON LANDING. THIS CAUSED LEFT MAIN GEAR FORWARD TRUNNION TO BREAK AND GEAR TO MOVE UPWARD IN GEAR WELL.
- [SDR 2017FA0000040](https://openairdocs.org/sdr/2017FA0000040.md): Alternator · shorted · Feb 3, 2017 · N41285 · Piper PA34200 · DC Generator-Alternator
  > AIRCRAFT EXPERIENCED A FAILURE OF THE LEFT ALTERNATOR IN FLIGHT THAT RESULTED IN SMOKE COMING FROM THE COWL. AIRCRAFT LANDED SAFELY AND UPON INSPECTION FOUND THAT THE ALTERNATOR WOULD NOT TURN WHEN TURNING THE PROPELLER. UPON REMOVAL OF THE ALTERNATOR FROM THE
- [SDR 2017FA0000091](https://openairdocs.org/sdr/2017FA0000091.md): Alternator · seized · Jan 15, 2017 · N4128 · Piper PA34200 · AC Inverter
  > THE ALTERNATOR SEIZED IN FLIGHT CAUSING THE BELT TO BURN AND SMOKE OVER THE PULLEY.
- [SDR CA150424001](https://openairdocs.org/sdr/CA150424001.md): Spring · broken · Apr 23, 2015 · Piper PA34200 · Nose/Tail Landing Gear Strut/Axle
  > (CAN) AFTER TAKEOFF PILOT REPORTED GEAR UNSAFE LIGHT CAME ON AND STAYED ON AFTER SELECTING GEAR UP. PILOT SELECTED GEAR DOWN AND GOT A 3 GREEN LIGHT INDICATION AND LANDED SAFELY. ACFT WAS SNAGGED AND REPORTED TO MAINTENANCE. UPON INSPECTION IT WAS FOUND THA
- [SDR CA140820006](https://openairdocs.org/sdr/CA140820006.md): Bracket · unsecure · Aug 7, 2014 · Piper PA34200 · Nose/Tail Landing Gear
  > (CAN) AFTER TOUCHDOWN, DURING ROLL OUT, THE NOSE GEAR RETRACTED CAUSING BOTH PROPELLERS TO STRIKE THE GROUND. DURING ASSESSMENT INSPECTION, LOWER TUNNEL BRACKET, PN 95554-00 WAS FOUND TO HAVE 4 RIVETS PULLED THROUGH CAUSING THE GEOMETRY TO CHANGE ON DOWN LINK
- [SDR CA130920012](https://openairdocs.org/sdr/CA130920012.md): Squat Switch · defective · Sep 11, 2013 · Piper PA34200 · Landing Gear Position and Warning
  > (CAN) NOSE GEAR FAILED TO RETACT AFTER TAKEOFF. ACFT PLACED ON JACKS AND INSPECTED. SQUAT SWITCH FOUND DEFECTIVE. SWITCH REPLACED AND GEAR SWING COMPLETED. ACFT RETURNED TO SERVICE.
- [SDR CA130220012](https://openairdocs.org/sdr/CA130220012.md): Attach Fitting · corroded · Feb 20, 2013 · Piper PA34200 · Vertical Stabilizer, Attach Fittings
  > (CAN) EXCESSIVE DISSIMILAR CORROSION FOUND BETWEEN BULKHEAD ASSEMBLY AND STEEL FITTING THAT IS THE FWD ATTACH POINT FOR THE VERTICAL STABILIZER. RIVETS APPEARED TO BE IN PLACE BUT WERE FOUND TO BE NOT HOLDING ANYTHING. DAMAGE WAS FOUND TO BE SAME AS DAMAGE R
- [SDR CA120525002](https://openairdocs.org/sdr/CA120525002.md): Spring · broken · May 18, 2012 · Piper PA34200 · Trailing Edge Flaps
  > (CAN) FLAP RETURN SPRING WAS FOUND BROKEN AT ATTACH POINT DURRING PREFLIGHT INSPECTION.
- [SDR CA120518002](https://openairdocs.org/sdr/CA120518002.md): Air Box · cracked · May 17, 2012 · Piper PA34200 · Engine Air Intake System
  > (CAN) WHILE COMPLETING 100 HR INSPECTION, A CRACK WAS FOUND ON THE RT ENGINE ALTERNATE AIR BOX AT THE FLANGE ATTACHING THE AIR BOX TO THE FUEL SERVO. THE CRACK WAS ON A WELDED FLANGE. THE CRACK WAS VISIBLE FROM THE BOTTOM ONLY. AIR BOX WAS REMOVED AND SENT
- [SDR CA120426002](https://openairdocs.org/sdr/CA120426002.md): Rib · cracked · Apr 19, 2012 · Piper PA34200 · Wing Spar
  > (CAN) ADDITIONAL CRACKS AT THE LOCATION OF RIB REPAIR INSIDE OF GEAR WELL ARE VISIBLE TO NAKED EYE BUT ARE COVERED BY DRAG BRACE PICK UP. THERE ARE HAIRLINE CRACKS IN SPAR AT DRAG BRACE PICK UP POINT WHICH ARE ALSO COVERED BY THE FITTING, MORE EASILY DISTINGU
- [SDR CA110930013](https://openairdocs.org/sdr/CA110930013.md): Stringer · corroded · Sep 28, 2011 · Piper PA34200 · Fuselage Main, Longeron/Stringer
  > (CAN) WHEN REMOVING THE RT INBD FUEL TANK DUE TO A LEAK, CORROSION WAS NOTED ON THE FORWARD STRINGER, DIRECTLY BEHIND THE EXHAUST PIPE. THE CORROSION PRODUCED A HOLE THAT WAS APPROX 1.0" X 0.75". AN APPROVED REPAIR IS BEING CARRIED OUT.
- [SDR CA110504008](https://openairdocs.org/sdr/CA110504008.md): Wheel Half · broken · May 2, 2011 · Piper PA34200 · Wheel/Ski/Float
  > (CAN) DURING TAXI, THE PILOT NOTED A STRONG VIBRATION FROM THE LANDING GEAR. THE PILOT SHUTDOWN THE ACFT ON THE TAXIWAY AND NOTED A PROBLEM WITH THE LT WHEEL, BRAKE. UPON INSPECTION BY AMO, IT WAS FOUND THAT A PIECE OF THE INNER WHEEL HALF HAD BROKEN FREE, AB
- [SDR CA101217010](https://openairdocs.org/sdr/CA101217010.md): Tube · cracked · Dec 17, 2010 · Piper PA34200 · Heating System
  > (CAN) WHILE PERFORMING A PRESSURE DECAY TEST AS REQUIRED BY AD 2004-21-05 AN EXTENSIVE LEAK WAS DISCOVERED IN THE COMBUSTION TUBE. THE COMBUSTION TUBE WOULD NOT HOLD PRESSURE (6 PSIG) FOR MORE THAN A COUPLE OF SECONDS. UPON REMOVAL OF THE FORWARD DUCT A LARGE
- [SDR CA100805008](https://openairdocs.org/sdr/CA100805008.md): Torque Tube · broken · May 15, 2010 · Piper PA34200 · Rudder Control System
  > (CAN) TAXING FOR REFUELING PILOT REPORTED LOSS OF LT RUDDER FEEDBACK PRESSURE. AT INSP LT RUDDER CONTROL CABLE ARM WELD WAS FOUND TO BE BROKEN AT TORQUE TUBE. RUDDER BAR (TORQUE TUBE).
- [SDR CA100115004](https://openairdocs.org/sdr/CA100115004.md): Rib · cracked · Jan 15, 2010 · Piper PA34200 · Trailing Edge Flaps
  > (CAN) DURING DISASSEMBLY FOR REPAIR TO THE FLAP ATTACH BRACKET, NOSE RIBS PN 62328-00 AND 62328-01 WERE FOUND TO BE CRACKED AT THE FLAP HINGE BRACKET ATTACH POINT. THIS BRACKET ALSO FORMS THE ATTACHING POINT FOR THE FLAP CONTROL ROD. BOTH LT AND RT FLAPS WE
- [SDR CA091008002](https://openairdocs.org/sdr/CA091008002.md): Bolt · sheared · Oct 7, 2009 · Piper PA34200 · Wheel/Ski/Float
  > (CAN) WHILE TOWING THE ACFT, GROUND CREW NOTICED AN ABNORMAL SOUND COMMING FROM THE LT MAIN WHEEL. UPON INSP BY MX STAFF, THE LT WHEEL WAS FOUND TO HAVE 2 OUT OF 3 WHEEL-HALF BOLTS BROKEN. BOLTS WERE SHEARED AT THE HEAD. WHEEL ASSY WAS REMOVED. GEAR LEG AND A
- [SDR CA090504006](https://openairdocs.org/sdr/CA090504006.md): Wire · chafed · Apr 29, 2009 · Piper PA34200 · Landing Gear System Wiring
  > (CAN) PILOT REPORTED THAT ON APPROACH TO LANDING, THE RT MAIN GEAR "DOWN AND LOCKED" LIGHT WAS UNSERVICEABLE. THE LANDING GEAR WAS CYCLED 3 TIMES BUT THE LIGHT JUST FLICKERED. THE PILOT THEN HAD THE CONTROL TOWER CHECK AND CONFIRM THAT THE GEAR WAS DOWN. A NOR
- [SDR CA090223014](https://openairdocs.org/sdr/CA090223014.md): Mount · cracked · Feb 20, 2009 · Piper PA34200 · Engine Mount Section
  > (CAN) CRACK FOUND DURING A ROUTINE 400 HOUR INSP. REPLACEMENT PART ORDERED AND RECEIVED. CRACKED APPEARED TO BE NEW. TUBING CRACKED AND SEPARATED. CRACK APPEARED ON LWR PORTION OF ENGINE MOUNT WITHIN 1.5 CM OF WELD.
- [SDR CA090223016](https://openairdocs.org/sdr/CA090223016.md): Landing Gear · cracked · Feb 20, 2009 · Piper PA34200 · Nose/Tail Landing Gear
  > (CAN) CRACK FOUND DURING 400 HOUR ACFT INSP. SMALL CRACK FOUND WHEN INSPECTING NOSE LANDING GEAR. CRACK WAS AT THE ATTACHMENT POINT OF THE PIVOT CHANNEL FOR THE NOSE GEAR STEERING. PART REPLACED WITH OVERHAULED PART.
- [SDR CA090302002](https://openairdocs.org/sdr/CA090302002.md): Pump · failed · Jan 16, 2009 · Piper PA34200 · Engine Fuel Pump
  > (CAN) INSTALLED OVERHAULED FUEL PUMP ON ACFT 30/01/08, PUMP FAILED 16/01/09.
- [SDR CA081113006](https://openairdocs.org/sdr/CA081113006.md): Wheel · cracked · Nov 7, 2008 · Piper PA34200 · Wheel/Ski/Float
  > (CAN) DURING A TIRE CHANGE, THE AME NOTICED A 4 INCH CRACK ALONG THE WHEEL, WHERE THE TIRE BEAD SITS. THIS TYPE OF FINDING IS RATHER UNUSUAL AT THE AMO. NO HARD OR UNUSUAL LANDINGS WERE REPORTED. THE WHEEL HALF WAS REPLACED, AND THE ACFT RETURNED TO SERVICE.
- [SDR 2008FA0000578](https://openairdocs.org/sdr/2008FA0000578.md): Valve Seat · damaged · Jul 16, 2008 · Reciprocating Engine Cylinder Section
  > INTAKE VALVE SEAT CAME LOOSE FROM THE SEAT BORE IN THE CYLINDER HEAD. THE LOOSE SEAT DAMAGE TO CYLINDER HEAD, VALVE, AND VALVE SEAT. INTERFERENCE FIT BETWEEN THE VALVE SEAT AND THE CYLINDER HEAD WAS NOT CORRECT. THIS WAS AN OVERHAULED CYLINDER. (K)
- [SDR ZB0R20070009](https://openairdocs.org/sdr/ZB0R20070009.md): Rod End · separated · Dec 14, 2007 · N15412 · Piper PA34200 · Power Lever
  > IN CRUISE, PILOT ATTEMPTED TO REDUCE POWER FOR MANEUVERS PRACTICE. LT ENGINE WAS UNRESPONSIVE. INSTRUCTOR IDENTIFIED LT ENGINE THROTTLE PROBLEM, ENGINE RPM WAS STABLE AT NEAR FULL POWER. RETURNED TO HOME BASE. PILOT FEATHERED AND SHUTDOWN LT ENGINE ON APPROACH
- [SDR 2007FA0000144](https://openairdocs.org/sdr/2007FA0000144.md): Switch · frozen · Feb 5, 2007 · N1533E · Piper PA34200 · Landing Gear Retraction/Extension System
  > UPON LANDING, GEAR EXTENSION, DURING APPROACH TO LANDING, PILOT NOTED AN EXCEPTIONALLY LONG TIME BETWEEN GEAR SWITCH ACTUATION AND INDICATION OF ALL DOWN AND LOCKED. OUTSIDE TEMP +9 F. BELIEVE THAT SWITCH ARM FOR DOWNLOCK HAD FROZEN IN PLACE (UP) AND REQUIR
- [SDR CA061227005](https://openairdocs.org/sdr/CA061227005.md): Crankshaft · cracked · Dec 18, 2006 · Piper PA34200 · Reciprocating Engine Power Section
  > (CAN) LT ENGINE DEVELOPED AN OIL LEAK FROM CRANKSHAFT SEAL. DURING SEAL REPLACEMENT, IT WAS NOTICED THAT THE CRANKSHAFT FLANGE WHERE PROPELLER BOLTS ON, WAS CRACKED FROM ONE LIGHTNING HOLE TO THE OTHER. IT LOOKED AS IF THERE WAS AN INDENTATION ON THE BACK SID
- [SDR X6PA200500006](https://openairdocs.org/sdr/X6PA200500006.md): Bulkhead · cracked · Jul 11, 2005 · N152BW · Piper PA34200 · Propeller Spinner Section
  > LT SPINNER BULKHEAD FOUND CRACKED, PIPER P/N 453-978. 1.5 IN CRACK EXTENDING FROM LAST SPINNER ATTACH FASTENER AT 10 O’CLOCK POSITION AND ANOTHER AT 2 O’CLOCK POSITION. BOTH CRACKS RUN INWARD TOWARD BULKHEAD/PROPELLER ATTACH POINT.
- [SDR X6PA200500002](https://openairdocs.org/sdr/X6PA200500002.md): Servo · leaking · Feb 16, 2005 · N997BW · Piper PA34200 · Engine Fuel Distribution
  > DURING A 100 HR INSPECTION, FUEL WAS FOUND DRIPPING FROM MIXTURE CONTROL ARM SHAFT. FUEL INJECTION SERVO REMOVED AND REPLACED.
- [SDR MW22004F00001](https://openairdocs.org/sdr/MW22004F00001.md): Stud · failed · Jun 16, 2004 · N4818T · Piper PA34200 · Reciprocating Engine Cylinder Section
  > NR 3 CLYINDER DECK STUDS FAILED AND CYLINDER LT ENGINE. CONNECTING ROD AND PISTON ALSO NOT FOUND.
- [SDR AUS20031102](https://openairdocs.org/sdr/AUS20031102.md): Mount · separated · Oct 22, 2003 · Piper PA34200 · Fuselage, Landing Gear Attach Fittings
  > (AUS) NOSE LANDING GEAR ACTUATOR MOUNT BRACKET RIVETS FAILED. SUSPECT CAUSED BY HEAVY LANDING AND SUBSTANDARD RIVETING. PERSONNEL/MAINTENANCE ERROR.
- [SDR 2003FA0000959](https://openairdocs.org/sdr/2003FA0000959.md): Cylinder · separated · Sep 23, 2003 · N439CT · Piper PA34200 · Reciprocating Engine Cylinder Section
  > THE AIRCRAFT WAS PREPARING FOR LANDING AT ARB, PILOT REDUCED POWER. WITHOUT WARNING, LEFT ENGINE FWD OUTBOARD CYLINDER SEPARATED FROM ENGINE, WAS HELD ON BY FUEL LINES AND IGNITION HARNESS. OUTBOARD UPPER ENGINE COWLING, PISTON AND ROD DEPARTED AIRCRAFT. L
- [SDR 2003FA0001007](https://openairdocs.org/sdr/2003FA0001007.md): Stud · broken · Aug 8, 2003 · N1039U · Piper PA34200 · Reciprocating Engine Cylinder Section
  > CYL STUDS BROKEN. CYL BACKED OFF ENGINE.
- [SDR AUS20030777](https://openairdocs.org/sdr/AUS20030777.md): Wheel · collapsed · Aug 1, 2003 · Piper PA34200 · Wheel/Ski/Float
  > (AUS) NOSE WHEEL COLLAPSED DURING LANDING.
- [SDR CA030731006](https://openairdocs.org/sdr/CA030731006.md): Landing Gear · collapsed · Jun 29, 2003 · Piper PA34200 · Nose/Tail Landing Gear
  > (CAN) ON LANDING NOSE WHEEL COLLAPSED WHILE TOWING AIRCRAFT TO HANGAR. RIGHT MAIN GEAR COLLAPSED.
- [SDR AUS20030347](https://openairdocs.org/sdr/AUS20030347.md): Landing Gear · corroded · Mar 14, 2003 · Piper PA34200 · Main Landing Gear
  > (AUS) RT MAIN LANDING GEAR CORRODED (RUSTY).
- [SDR AUS20030358](https://openairdocs.org/sdr/AUS20030358.md): Rod End · failed · Feb 6, 2003 · Piper PA34200 · Power Lever
  > (AUS) RT ENGINE GOVERNOR RODEND FAILED UNDER LIGHT TORQUE DURING INSTALLATION.
- [SDR CA021007014](https://openairdocs.org/sdr/CA021007014.md): Rib · damaged · Sep 13, 2002 · Piper PA34200 · Nacelle/Pylon, Main Frame
  > (CAN) PILOT ON A RETURN FLIGHT HOME EXPERIENCED A SLOWER THAN NORMAL LANDING GEAR RETRACTION. A VISUAL INSPECTION WAS CARRIED OUT. INSPECTION OF THE LEFT MAIN GEAR AREA REVEALED TWO RIB ASSEMBLIES DAMAGED. THEY WERE LOCATED ADJACENT TO EACH SIDE OF THE GEAR
- [SDR AUS20020424](https://openairdocs.org/sdr/AUS20020424.md): Fitting · broken · May 2, 2002 · Piper PA34200 · Landing Gear Retraction/Extension System
  > (AUS) LANDING GEAR RETRACTION FITTING BROKEN. DOWNLOCKS JAMMED IN THE UP POSITION.
- [SDR AUS20011375](https://openairdocs.org/sdr/AUS20011375.md): Nut · missing · Dec 19, 2001 · Piper PA34200 · Main Landing Gear Strut/Axle/Truck
  > (AUS) LH MAIN LANDING GEAR TORQUE LINK CONNECTING BOLT NUT MISSING.
- [SDR CA011102002](https://openairdocs.org/sdr/CA011102002.md): Spar · failed · Oct 18, 2001 · Piper PA34200 · Vertical Stabilizer, Attach Fittings
  > (CAN) FAILURE OF RIVETS SECURING LOWER 4 INCHES OF SPAR FLANGES TO FITTING P/N 63501-00. FOUR RIVETS HAD FAILED ON LT SIDE AND ONE RIVET FAILED ON RT SIDE.
- [SDR CA010205024](https://openairdocs.org/sdr/CA010205024.md): Rib · cracked · Jan 15, 2001 · Piper PA34200 · Wing, Rib/Bulkhead
  > (CAN) DURING THE 50 HOURS INSPECTION, THE RIB MEMBRANE LOCATED OUTSIDE THE MAIN LANDING GEAR (LT SIDE) WAS FOUND CRACKED AND DEFORMED.
- [SDR AU010007](https://openairdocs.org/sdr/AU010007.md): Downlock · contaminated · Jan 6, 2001 · Piper PA34200 · Landing Gear Retraction/Extension System
  > (AUS) LT MAIN LANDING GEAR DOWNLOCK ARM JAMMED BY A STONE PREVENTING LANDING GEAR FROM CORRECTLY LOCKING IN THE DOWN POSITION.
- [SDR 20001017SH024](https://openairdocs.org/sdr/20001017SH024.md): Rod Bolt · broken · Aug 28, 2000 · N56213 · Piper PA34200 · Reciprocating Engine Power Section
  > NR 3 CONNECTING ROD BOLT PN SL-75060 BROKE CAUSING THE CONNECTING ROD CAP TO SEPARATE RESULTING IN COMPLETE ENGINE FAILURE. AIRCRAFT LANDED WITHOUT INCIDENT. (X)
- [SDR CA000907024](https://openairdocs.org/sdr/CA000907024.md): Actuator · broken · Aug 6, 2000 · Piper PA34200 · Landing Gear Position and Warning
  > (CAN) GEAR WOULD NOT RETRACT AFTER TAKEOFF. AT RETURN TO BASE, SQUAT SWITCH ACTUATOR ARM WAS FOUND TO BE BROKEN. NEW ACTUATOR INSTALLED, NORMAL FUNCTION RETURNED. (X)
- [SDR AU000427](https://openairdocs.org/sdr/AU000427.md): Pipe · corroded · May 24, 2000 · Piper PA34200 · Hydraulic System, Main
  > (AUS) LANDING GEAR ''UP'' PIPE CORRODED AND LEAKING. LOSS OF HYDRAULIC FLUID. LEFT MLG DOWNLOCK STIFF TO OPERATE. AIRCRAFT OPERATES IN A SALT LADEN ENVIRONMENT.
- [SDR CA000427034](https://openairdocs.org/sdr/CA000427034.md): Pump · failed · Apr 4, 2000 · Piper PA34200 · Hydraulic Pump (Electric/Engine), Main
  > (CAN) THE LANDING GEAR WAS SELECTED DOWN BUT THE GEAR REMAINED IN THE UP POSITION. MAINTENANCE FOUND THE MOTOR OF THE POWER PACK TO BE UNSERVICEABLE. THE ASSEMBLY WAS REPLACED.
- [SDR CA000404044](https://openairdocs.org/sdr/CA000404044.md): Wire · corroded · Dec 20, 1999 · Piper PA34200 · Landing Gear System Wiring
  > (CAN) WITH GEAR SELECTED DOWN, RIGHT MAIN LANDING GEAR FAILED TO INDICATE DOWN AND LOCKED. INSPECTION REVEALED A CORRODED AND BROKEN WIRE AT A SPLICE APPROXIMATELY 1 FOOT FROM THE RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH. WIRING REPAIRED BY REPLACING SUBJECT
- [SDR AU990729](https://openairdocs.org/sdr/AU990729.md): Coupling · broken · Jul 10, 1999 · Piper PA34200 · Power Lever
  > (AUS) RIGHT ENGINE THROTTLE BALL COUPLING FAILED IN THE AREA BENEATH THE BALL. INVESTIGATION FOUND THAT THE BALL STUD WAS WORN APPROXIMATELY 40 PERCENT THROUGH.
- [SDR CA990514015](https://openairdocs.org/sdr/CA990514015.md): Pump · failed · May 6, 1999 · Piper PA34200 · Vacuum Distribution System
  > (CAN) PILOT REPORTED THE RIGHT RED BALL WAS VISIBLE IN THE VACUUM GAUGE. THE VACUUM PUMP WAS REMOVED AND INSPECTION FOUND THE DRIVE SHAFT WAS SHEARED. THE PUMP WAS REPLACED.
- [SDR CA990401015](https://openairdocs.org/sdr/CA990401015.md): Rib · cracked · Mar 22, 1999 · Piper PA34200 · Wing, Rib/Bulkhead
  > (CAN) AT 1,000-HOUR INSPECTION, FOUND TWO CRACKS (FORWARD TOP CORNER AND TOP MIDDLE) ON DOUBLE RIB STA 69.24 ON RT WING IN GEAR WHEELWELL.
- [SDR AU990310](https://openairdocs.org/sdr/AU990310.md): Swivel · worn · Jan 23, 1999 · Piper PA34200 · Power Lever
  > (AUS) THROTTLE CONTROL CABLE SWIVEL WORN AND SEPARATED FROM THE BALL JOINT.

Next page: https://openairdocs.org/engine/lycoming-io-360-c1e6/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 = 'IO360C1E6'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/lycoming-io-360-c1e6/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.