# Service difficulty reports: Lycoming IO-360-C1C6

A list on [Lycoming IO-360-C1C6](https://openairdocs.org/engine/lycoming-io-360-c1c6.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 103 reports

- [SDR ECPR20260731002](https://openairdocs.org/sdr/ECPR20260731002.md): Spark Plug · cracked · Jul 30, 2026 · N8585Z · Piper PA28R201 · Spark Plug/Igniter
  > FOLLOWING DISCOVERY OF A CRACKED SPARK PLUG ON ANOTHER AIRCRAFT, A PRECAUTIONARY INSPECTION WAS CONDUCTED OF THE SPARK PLUG ON THIS AIRCRAFT AS IT WAS THE SAME LOT # AS A PREVIOUS SPARK PLUG FAILURE. VISUAL INSPECTION FOUND CRACKING AT A POINT BETWEEN THE SPA
- [SDR ECPR202304070001](https://openairdocs.org/sdr/ECPR202304070001.md): Switch · stuck · Apr 6, 2023 · N8587K · Piper PA28R201 · Landing Gear System
  > DURING THE PRE-TAXI CHECKLIST, STUDENT PILOT MISTAKENLY PLACED THE GEAR SELECTOR IN THE UP POSITION. THE NOSE GEAR RETRACTED, CAUSING THE NOSE OF THE AIRCRAFT TO COLLAPSE ON TO THE APRON DAMAGING THE PROPELLER AND ENGINE COWLING. INSPECTION FOUND THAT THE GE
- [SDR 2023FA0000205](https://openairdocs.org/sdr/2023FA0000205.md): Switch · stuck · Apr 5, 2023 · N8585Z · Piper PA28R201 · Landing Gear Retraction/Extension System
  > DURING SCHEDULED INSPECTION, LANDING GEAR ANTI-RETRACTION SYSTEM FAILED TO PREVENT GEAR RETRACTION WITH WEIGHT ON WHEELS. INSPECTION FOUND GEAR SAFETY SQUAT SWITCH WAS STUCK IN THE CLOSED POSITION INTERNALLY. THE SWITCH TAB WAS IN THE NORMAL DEACTIVATED POSI
- [SDR 2020FA0000446](https://openairdocs.org/sdr/2020FA0000446.md): Impulse Coupling · jammed · Sep 14, 2020 · N8288L · Piper PA28RT201 · Magneto/Distributor
  > DURING AN ENGINE RUN UP THE LEFT MAGNETO WAS OBSERVED TO BE NOT FIRING. UPON REMOVAL OF THE MAGNETO THE IMPULSE COUPLING WAS FOUND FAILED. ONE OF THE PAWLS WAS WEDGED BETWEEN THE PLATE OF THE COUPLING AND THE HOUSING OF THE MAGNETO. IT APPEARS THE RIVET ATT
- [SDR ECPR2019050383335](https://openairdocs.org/sdr/ECPR2019050383335.md): Stop Fitting · broken · May 3, 2019 · N8584T · Piper PA28R201 · Nose/Tail Landing Gear
  > DURING A SCHEDULED INSPECTION, THE OVERMOULDED RUBBER BUMPER ON THE NOSE GEAR RETRACTION STOP WAS FOUND BROKEN. THE RUBBER WAS SPLIT AT THE POINT OF CONTACT WITH THE RETRACTION DRAG LINK. THIS AICRAFT HAS HAD THIS PART REPLACED SEVEN TIMES PREVIOUSLY DURING TH
- [SDR ECPR2019011882002](https://openairdocs.org/sdr/ECPR2019011882002.md): Bumper · split · Jan 17, 2019 · N8586A · Piper PA28R201 · Nose/Tail Landing Gear
  > DURING A SCHEDULED INSPECTION, THE OVERMOULDED RUBBER BUMPER ON THE NOSE GEAR RETRACTION STOP WAS FOUND BROKEN. THE RUBBER WAS SPLIT AT THE POINT OF CONTACT WITH THE RETRACTION DRAG LINK. THIS AICRAFT HAS HAD THIS PART REPLACED THREE TIMES PREVIOUSLY DURING TH
- [SDR ECPR2018120768568](https://openairdocs.org/sdr/ECPR2018120768568.md): Stop · broken · Dec 6, 2018 · N8583N · Piper PA28R201 · Nose/Tail Landing Gear
  > DURING A SCHEDULED INSPECTION, THE OVERMOULDED RUBBER BUMPER ON THE NOSE GEAR RETRACTION STOP WAS FOUND BROKEN. THE RUBBER WAS SPLIT AT THE POINT OF CONTACT WITH THE RETRACTION DRAG LINK. THIS AICRAFT HAS HAD THIS PART REPLACED THREE TIMES DURING THE PAST FO
- [SDR ECPR2018112981439](https://openairdocs.org/sdr/ECPR2018112981439.md): Bumper · broken · Nov 28, 2018 · N8584T · Piper PA28R201 · Nose/Tail Landing Gear
  > DURING A SCHEDULED INSPECTION, THE OVERMOULDED RUBBER BUMPER ON THE NOSE GEAR RETRACTION STOP WAS FOUND BROKEN. THE RUBBER WAS SPLIT AT THE POINT OF CONTACT WITH THE RETRACTION DRAG LINK. THIS AICRAFT HAS HAD THIS PART REPLACED FOUR TIMES DURING THE PAST SIX
- [SDR ECPR2018110768116](https://openairdocs.org/sdr/ECPR2018110768116.md): Exhaust Stack · cracked · Nov 6, 2018 · N8583N · Piper PA28R201 · Engine Collector/Tailpipe/Nozzle
  > ON DEPARTURE FOLLOWING A TOUCH AND GO LANDING THE CREW HEARD AN UNUSUAL METALLIC SOUND FROM THE ENGINE. THE CREW REMAINED IN THE PATTERN AND CONDUCTED A FULL STOP LANDING. UPON INVESTIGATION, THE #1 CYLINDER EXHAUST STACK WAS FOUND COMPLETELY CRACKED OFF ALO
- [SDR ECPR201811060001](https://openairdocs.org/sdr/ECPR201811060001.md): Bumper Block · broken · Nov 5, 2018 · N8587K · Piper PA28R201 · Nose/Tail Landing Gear
  > DURING A SCHEDULED INSPECTION, THE OVERMOULDED RUBBER BUMPER ON THE NOSE GEAR RETRACTION STOP WAS FOUND BROKEN. THE RUBBER WAS SPLIT AT THE POINT OF CONTACT WITH THE RETRACTION DRAG LINK. THIS AICRAFT HAS HAD THIS PART REPLACED FIVE TIMES DURING THE PAST FIF
- [SDR PK0S2016FA0000414](https://openairdocs.org/sdr/PK0S2016FA0000414.md): Ball Joint · disconnected · Aug 26, 2016 · N210SP · Piper PA28RT201 · Propeller Controlling System
  > DURING TAKEOFF, ENGINE RPM DECREASED TO 2200 RPM. THE PILOT MADE A SUCCESSFUL LANDING. UPON REMOVING THE TOP COWLING THE PROPELLER CONTROL CABLE BALL JOINT RECEIVER WAS FOUND DISCONNECTED FROM THE RECEPTACLE. THE RETENTION CLIP WAS IN PLACE AND WAS NOT FOUN
- [SDR 2016FA0000318](https://openairdocs.org/sdr/2016FA0000318.md): Rib · buckled · Jun 6, 2016 · N149DT · Piper PA28R201 · Wing, Rib/Bulkhead
  > RECEIVED A WRITE UP FOR 149DT SAYING IT HAD CUTS IN THE LEFT MAIN TIRE. ON INSPECTION OF TIRE, NOTICED THAT THE WHEEL SEEMED TO BE CANTED. PROCEEDED TO INSPECT THE LANDING GEAR AND FOUND DAMAGE FROM WHERE IT APPEARED THE AIRCRAFT HAD BEEN SIDE LOADED AND THE
- [SDR 2015FA0000424](https://openairdocs.org/sdr/2015FA0000424.md): Screen · damaged · Sep 2, 2015 · N751KS · Piper PA28R201 · Engine Air Intake System
  > PAPER INDUCTION AIR FILTER, PN 638876 WAS FOUND TO HAVE INNER SCREEN MESH DISTORTED, LOOSE AND PULLING AWAY FROM INSIDE OF FILTER ASSEMBLY. IF ALLOWED TO CONTINUE, THIS SCREEN MATERIAL COULD BE INGESTED BY THE ENGINE INDUCTION AIR SYSTEM.
- [SDR 2015FA0000437](https://openairdocs.org/sdr/2015FA0000437.md): Magneto · inoperative · Aug 21, 2015 · N125MT · Piper PA28R201 · Magneto/Distributor
  > THE ACFT WOULD NOT START OR EVEN HIT DESPITE MULTIPLE ATTEMPTS. WHEN THE TIMING WAS CHECKED IT WAS FOUND THAT THE IMPULSE COUPLING WOULD RELEASE AT VARYING TIMES. THIS ACFT ONLY HAS ONE IMPULSE COUPLED MAGNETO. THIS MAGNETO HAS BEEN RETURNED FOR WARRANTY.
- [SDR 2015FA0000197](https://openairdocs.org/sdr/2015FA0000197.md): Adapter · not seated · Apr 15, 2015 · N772FT · Piper PA28R201 · Reciprocating Engine Oil System
  > AIRCRAFT WAS WRITTEN UP FOR HIGH OIL TEMPERATURE 4/18/15. T 47.2, H-9010.5. OIL FILTER ADAPTER WAS REMOVED AND INSPECTED. THERMO VALVE SEAT AND SEAT IN ADAPTER SHOWED SIGNS THAT FULL SEAT WAS NOT HAPPENING, ALLOWING BYPASS. WO-C15-040.
- [SDR CA140124002](https://openairdocs.org/sdr/CA140124002.md): Cable · frayed · Jan 17, 2014 · Piper PA28RT201 · Elevator Tab Control System
  > (CAN) DURING AN AVIONICS INSTALLATION, WHILE A TECH WAS IN THE TAIL, THEY DISCOVERED THE FORWARD LT STABILATOR TRIM CABLE WAS FRAYED. THIS CABLE WAS FRAYED WHERE THE CABLE RUNS AROUND THE ELECTRIC TRIM SERVO. ALL TRIM CABLES WERE REPLACED. SYSTEM RIGGED.
- [SDR 2013FA0000319](https://openairdocs.org/sdr/2013FA0000319.md): Distributor Gear · failed · Jun 5, 2013 · N36120 · Piper PA28R201 · Magneto/Distributor
  > ACFT RAN ROUGH AND SKIPPED. OPENED MAGNETO FOR INSPECTION. FOUND DISTRIBUTOR GEAR K3008 METAL FINGER BECAME DISLODGED FROM THE CENTER POST. GEAR WAS REPLACED WITH NEW ONE. ENGINE RAN FINE WITHOUT ISSUES. MAGNETO WAS GIVEN A 500 HR MAGNETO INSPECTION 98.6 HR
- [SDR CA130423009](https://openairdocs.org/sdr/CA130423009.md): Trunnion · cracked · Mar 20, 2013 · Piper PA28RT201 · Fuselage, Landing Gear Attach Fittings
  > (CAN) WHILE ATTEMPTING TO REMOVE THE COWLING, AME LOOKED UP THRU THE NOSE GEAR DOORS AND NOTICED CRACKED NOSE GEAR TRUNNION WHERE DRAG BRACE ATTACHES. DRAG BRACE AND DOWNLOCK AND NO OTHER CRACKS FOUND. NO REPORTED EXCESSIVE SHIMMY, ALTHOUGH SHIMMY DAPENER HA
- [SDR 2011FA0000661](https://openairdocs.org/sdr/2011FA0000661.md): Bolt · failed · Sep 17, 2011 · N82821 · Piper PA28RT201 · Main Landing Gear
  > AFTER LANDING, WHILE TURNING, LT WING SAGGED. CONTINUED TAXI, LT MLG COLLAPSED. BOLT HOLDING REAR TRUNNION FRACTURED AT THE HEAD DUE TO CORROSION. ALL THE LOAD WAS TRANSFERRED TO THE FRONT TRUNNION WHICH FRACTURED AT THE END OF THE MACHINED MAIN TRUNNION ST
- [SDR 2011FA0000632](https://openairdocs.org/sdr/2011FA0000632.md): Tappet · damaged · Aug 15, 2011 · N5163M · Piper PA28R201 · Engine (Reciprocating)
  > AFTER FINDING MAGNETIC METAL FLAKES IN OIL FILTER AT ANNUAL INSP, ENGINE WAS REMOVED FROM SERVICE AND DISASSEMBLED. INSP REVEALED SEVERE FLAKING AND SPALLING OF 2 EA TAPPET FACES AND DAMAGE TO THE CORRESPONDING CAM LOBES. NONE AT THIS TIME. SUSPECT MFG PROB
- [SDR OG5R20110719001](https://openairdocs.org/sdr/OG5R20110719001.md): Tire · deflated · Jul 12, 2011 · N384ND · Piper PA28R201 · Tire
  > FLAT TIRE DURING LANDING ROLL OUT; WHILE TAXIING TO PARK THE ACFT.
- [SDR OG5R20110714002](https://openairdocs.org/sdr/OG5R20110714002.md): Tire · deflated · Jun 9, 2011 · N278ND · Piper PA28R201 · Tire
  > LT MAIN TIRE WENT FLAT ON TAXI.
- [SDR 2010FA0001176](https://openairdocs.org/sdr/2010FA0001176.md): Gascolator · worn · Oct 29, 2010 · N98UA · Piper PA28RT201 · Fuel Control/Reciprocating Engines
  > EXPERIENCED A SIGNIFICANT LOSS OF ENGINE POWER & ROUGHNESS DURING CLIMBOUT WHEN POWER WAS REDUCED AT 1500 FEET MSL. POWER WAS RESTORED AT FULL THROTTLE AND FULL RICH. A SECOND ATTEMPT TO REDUCE POWER AT 3000 FEET RESULTED IN THE SAME LOSS OF POWER. AFTER L
- [SDR 2010FA0000731](https://openairdocs.org/sdr/2010FA0000731.md): Rod End · weak · Jun 28, 2010 · N5163M · Piper PA28R201 · Propeller Governor
  > (UC2R) THE PILOT REPORTED THA THE PROP GOVEERNOR CONTROL WAS UNRESPONSIVE. THE TECH FOUND THE PROP GOVERNOR ROD END OFF OF THE GOVERNOR ATTACH BALL. THE SPRING SAFETY DEVICE HAD ROTATED AND ALLOWED THE ROD END TO POP OFF OF THE ATTACH BALL. THE ROD END WA
- [SDR 2010FA0000415](https://openairdocs.org/sdr/2010FA0000415.md): Intake Valve · broken · Apr 20, 2010 · N630AC · Piper PA28R201 · Reciprocating Engine Power Section
  > (ECPS) DURING THIRD TOUCH AND GO CLIMB OUT AT APPROXIMATELY 400 FT. A LOUD BANG WAS HEARD AND A SMOKE / BURNT OIL SMELL APPEARED. ONLY PARTIAL ENGINE POWER WAS AVAILABLE BUT WAS ENOUGH TO TURN AROUND AND LAND ON THE SAME RUNWAY, WITHOUT INCIDENT. ENGINE WAS SH
- [SDR 2010FA0000021](https://openairdocs.org/sdr/2010FA0000021.md): Control Unit · worn · Jan 4, 2010 · N4160F · Piper PA28R201 · Propeller Governor
  > DURING ANNUAL INSP OF ENG, FOUND PROP GOVERNOR CONTROL UNIT CONTROL ARM HIGH RPM ADJUSTABLE STOP SCREW AND STOP PIN EXCESSIVELY WORN. CONTROL ARM STOP PIN HAS A GROOVE IN WHICH CONTROL ARM RETURN SPRING IS HOOKED IN. THE WEAR BETWEEN THE ADJUSTABLE HIGH RPM
- [SDR 2009FA0000913](https://openairdocs.org/sdr/2009FA0000913.md): Camshaft · sheared · Sep 1, 2009 · N2241N · Piper PA28RT201 · Magneto/Distributor
  > MAGNETO FAILURE DUE TO ROTATING MAGNETO CAM SHAFT SHEARING OFF JUST BELOW THE CAM, AT THE FORK. THE PROBABLE CAUSE OF THE BREAK IS METAL FATIGUE AT THE FORKED GROOVE WHICH CAUSES CRACKS AND THEN LEADS TO FAILURE. THIS IS THE SECOND MAGNETO THIS SHOP HAS SEEN
- [SDR 2009FA0000624](https://openairdocs.org/sdr/2009FA0000624.md): Wire Harness · broken · Jun 26, 2009 · N1386T · Piper PA28R201 · Landing Gear System Wiring
  > AFTER GEAR EXTENSION, RT MLG DOWN LIGHT FAILED TO LIGHT. PROBLEM FOUND IN WIRING HARNESS AT RT MLG DOWNLOCK SWITCH. WIRE INSIDE THE CASTING AT THE WIRING HARNESS WAS BROKEN.
- [SDR CA090710001](https://openairdocs.org/sdr/CA090710001.md): Actuator · broken · Jun 8, 2009 · Piper PA28R201 · Landing Gear Retraction/Extension System
  > (CAN) GEAR SELECTED DOWN FOR LANDING. NO NOSE GEAR DOWN INDICATION IN COCKPIT. FLYBY CARRIED OUT. TOWER CONFIRMED GEAR APPEARED DOWN. LANDING UNEVENTFUL. GEAR DOWNLOCK ACTUATOR FOUND BROKEN.
- [SDR CA090126002](https://openairdocs.org/sdr/CA090126002.md): Spring · misinstalled · Jan 24, 2009 · Piper PA28R201 · Magneto/Distributor
  > ENGINE DISPLAYED EXCESSIVE MAG DROP DURING PRE-FLIGHT RUNUP. MAGNETO REMOVED FOR INSPECTION. IMPULSE COUPLING SPRING FOUND INCORRECTLY INSTALLED IN HOUSING RESULTING IN DAMAGE TO HOUSING. IMPULSE COUPLING FAILED MANDATORY INSPECTION REQUIREMENTS IN SERVICE
- [SDR 2008FA0000195](https://openairdocs.org/sdr/2008FA0000195.md): Fuel Control · loose · Feb 29, 2008 · N540PU · Piper PA28R201 · Fuel Controlling System
  > RAN ENGINE AFTER INSPECTION AND FOUND FUEL FLOW AT TO POWER SETTING TO BE QUITE LOW. INVESTIGATED AND FOUND PLUG LOOSE ON SIDE OF INJECTION SERVO. CONTACTED ENGINE SHOP FOR FIX.
- [SDR 2006FA0001068](https://openairdocs.org/sdr/2006FA0001068.md): Oil Cooler · leaking · Nov 3, 2006 · N287ND · Piper PA28R201 · Engine Oil Cooler
  > PILOT REPORTED FLICKERING OIL PRESSURE ANNUCIATOR DURING TAKE-OFF. LANDED AND FOUND OIL LEAKING FROM OIL COOLER AREA. UPON CLOSER EXAMINATION BY A&P DETERMINED COOLER WAS LEAKING IN BETWEEN THE COOLING FINS. COOLER WAS REPLACED RUN UP AND LEAK CHECKED GOOD. OI
- [SDR CA060421017](https://openairdocs.org/sdr/CA060421017.md): Alternator · failed · Apr 13, 2006 · Piper PA28R201T · Alternator-Generator Drive
  > THE ALTERNATOR HAS BEEN OVERHAULED AND FAILED.
- [SDR 2006FA0000328](https://openairdocs.org/sdr/2006FA0000328.md): Shaft · sheared · Mar 9, 2006 · N5321U · Piper PA28R201 · Magneto/Distributor
  > ENGINE RUNUP INDICATED A DEAD MAGNETO. REMOVED AND DISASSEMBLED MAGNETO HOUSING. FOUND ROTOR SHAFT SHEARED OFF AT BOTTOM OF CAM SLOT. A FEW CRACKED SHAFTS HAVE BEEN FOUND AT 500 HR INSPECTIONS. RECOMMEND CLOSE INSPECTION OF THIS AREA AT REPAIR AND OVERHAUL
- [SDR 2006FA0000161](https://openairdocs.org/sdr/2006FA0000161.md): Fuel · contaminated · Feb 9, 2006 · N384ND · Piper PA28R201 · Engine Fuel Distribution
  > BROWNISH FUEL WAS DETECTED FROM THE FUEL GASCOLATOR. AFTER TROUBLESHOOTING IT WAS DETERMINED THAT THE BROWNISH FUEL COLOR PRESENT IN THE FUEL SYSTEM.
- [SDR AU510002068](https://openairdocs.org/sdr/AU510002068.md): Frame · cracked · Dec 12, 2005 · Piper PA28R201 · Fuselage Main, Frame
  > REAR FUSELAGE FRAME P/N 62444-005 AND DOUBLER P/N 79272-000 CRACKED AND CORRODED.
- [SDR 2005FA0001495](https://openairdocs.org/sdr/2005FA0001495.md): Mount · broken · Oct 18, 2005 · N283ND · Piper PA28R201 · Engine Mount Section
  > DURING ROUTING SCHEDULED MAINTENANCE INSPECTION NOTED ENG MOUNT WAS CRACKED JUST ABOVE WELD ON RT LOWER SIDE OF ENGINE MOUNT. JUST ABOVE AFT DRAGLINK MOUNT POINT. ALSO, UPON FURTHER INSPECTION THE LOWER HORIZONTAL TUBE MOST OB WAS ALSO BENT. MOS NOTED TOWAR
- [SDR 2005FA0000737](https://openairdocs.org/sdr/2005FA0000737.md): Stud · failed · May 6, 2005 · N9816C · Piper PA28R201 · Reciprocating Engine Power Section
  > NR 4 CYLINDER BASE STUD FAILED IN TENSION. NUT AND 30 PERCENT OF STUD LENGTH FOUND BETWEEN NR2 AND NR4 CYLINDERS ON THE INNER CYLINDER BAFFLE. NR 4 CYLINDER REMOVED AND REMAINING PARTIAL STUD REMOVED WITH STUD EXTRACTOR. INSTALLED NEW STUD, PN 50-15 AND RE
- [SDR 2005FA0000542](https://openairdocs.org/sdr/2005FA0000542.md): Starter · failed · Apr 12, 2005 · N146LH · Piper PA28R201 · Engine Starter
  > STARTER REPAIRED UNDER W/O 6900 FOR SB A-112. FAILED IN SERVICE 76.4 HOURS LATER.
- [SDR 2005FA0000581](https://openairdocs.org/sdr/2005FA0000581.md): Rib · cracked · Mar 22, 2005 · N703ER · Piper PA28R201 · Wing, Rib/Bulkhead
  > DURING A VISUAL INSPECTION, A SMALL CRACK WAS FOUND IN THE RT NOSE RIB. A MORE THOROUGH INSPECTION REVEALED THAT AN ADDITIONAL CRACK, MUCH LARGER (ABOUT 4 INCHES LONG), WAS FOUND ON THE RIB. THESE RIBS ARE INCLUDED IN THE MOUNTING ASSEMBLY FOR THE BRACKET(MAI
- [SDR 2005FA0000428](https://openairdocs.org/sdr/2005FA0000428.md): Rib · cracked · Mar 22, 2005 · N706ER · Piper PA28R201 · Wing, Rib/Bulkhead
  > DURING A VISUAL INSPECTION, A SMALL CRACK WAS FOUND IN THE RT NOSE RIB P/N-62021-005 AND -004. A MORE THOROUGH INSPECTION REVEALED THAT AN ADDITIONAL CRACK, MUCH LARGER (ABOUT4 INCHES LONG), WAS FOUND ON THE RIB P/N-78475-009 AND -008. THESE RIBS ARE INCLUDED
- [SDR 2005FA0000556](https://openairdocs.org/sdr/2005FA0000556.md): Rib · cracked · Mar 22, 2005 · N708ER · Piper PA28R201 · Wing, Rib/Bulkhead
  > DURING A VISUAL INSPECTION, A SMALL CRACK WAS FOUND IN THE RT NOSE RIB P/N-62021-005 AND -004. A MORE THOROUGH INSPECTION REVEALED THAT AN ADDITIONAL CRACK, MUCH LARGER (ABOUT 4 IN LONG), WAS FOUND ON THE RIB P/N-78475-009 AND -008. THESE RIBS ARE INCLUDED I
- [SDR 2005FA0000557](https://openairdocs.org/sdr/2005FA0000557.md): Rib · cracked · Mar 21, 2005 · N701ER · Piper PA28R201 · Wing, Rib/Bulkhead
  > DURING VISUAL INSPECTION, A SMALL CRACK WAS FOUND IN THE RT NOSE RIB P/N-62021-005 AND -004. A MORE THOROUGH INSPECTION REVEALED THAT AN ADDITIONAL CRACK, MUCH LARGER (ABOUT 4 INCHES LONG), WAS FOUND ON THE RIB P/N-78475-009 AND -008. THESE RIBS ARE INCLUDED I
- [SDR 2005FA0000555](https://openairdocs.org/sdr/2005FA0000555.md): Rib · cracked · Mar 21, 2005 · N492B · Piper PA28R201 · Wing, Rib/Bulkhead
  > DURING A VISUAL INSP, A SMALL CRACK WAS FOUND IN THE RT NOSE RIB P/N-62021-005 AND -004. A MORE THOROUGH INSPECTION REVEALED THAT AN ADDITIONAL CRACK, MUCH LARGER (ABOUT 4 INCH LONG), WAS FOUND ON THE RIB P/N-78475-009 AND -008. THESE RIBS ARE INCLUDED IN THE
- [SDR CA050105007](https://openairdocs.org/sdr/CA050105007.md): Camshaft · worn · Nov 30, 2004 · Piper PA28R201 · Reciprocating Engine Power Section
  > (CAN) AIRCRAFT IS OPERATED BY BUSY FLIGHT TRAINING UNIT NO COMPLAINTS OF ENGINE MALFUNCTIONS HAD BEEN REPORTED. ENGINE WAS RUN UP, FOUND NORMAL, PRIOR TO INSPECTION. OIL SUCTION SCREEN WAS INSPECTED AND FOUND CLEAN. OIL PRESSURE FILTER WAS CUT OPEN AND A SMA
- [SDR 2005FA0000538](https://openairdocs.org/sdr/2005FA0000538.md): Starter · failed · Nov 18, 2004 · N146LH · Piper PA28R201 · Engine Starter
  > NEW REPLACEMENT STARTER FAILED 76.4 HOURS AFTER INSTALLATION. BENDIX DRIVE JAMS, STARTER WILL NOT OPERATE. STARTER IS NOT EFFECTED BY SB A-112. 4TH STARTER CHANGE ON AIRPLANE, 3RD DUE TO MECHANICAL FAILURE ALL WITHIN 205 HOURS (APPROX. 1 YEAR). REVERTED TO HEA
- [SDR 2004FA0000513](https://openairdocs.org/sdr/2004FA0000513.md): Door · failed · May 19, 2004 · N2495M · Piper PA28R201 · Engine Air Intake System
  > PARTIAL LOSS OF ENGINE POWER OCCURRED JUST AFTER TAKEOFF. THE MANIFOLD PRESSURE DROPPED TO 15 INCHES HG, RPM DROPPED TO 1900. PRE TAKEOFF ENGINE RUN UP, ALTERNATE AIR CHECK WAS REPORTED AS NORMAL. A POST FLIGHT INSPECTION REVEALED THAT ALTERNATE AIR (HEAT
- [SDR 2004FA0000660](https://openairdocs.org/sdr/2004FA0000660.md): Door · ingested · May 19, 2004 · N2495M · Piper PA28R201 · Engine Air Intake System
  > PARTIAL LOSS OF ENG PWR OCCURRED JUST AFTER T/O. MANIFOLD PRESS DROPPED TO 15 INCHES HG AND RPM DROPPED TO 1900. PRE T/O ENG RUN UP, ALTERN AIR CHECK WAS REPORTED AS (NORMAL). POST FLT INSP REVEALED THAT ALTERN AIR (HEAT BOX) DOOR HAD SEPARATED FROM ALTERNA
- [SDR 2004FA0000374](https://openairdocs.org/sdr/2004FA0000374.md): Attach Fitting · loose · May 11, 2004 · N703ER · Piper PA28R201 · Fuselage, Wing Attach Fittings
  > DURING A ROUTINE INSPECTION, THE LT AFT WING ATTACHMENT FITTING WAS FOUND TO HAVE A LOOSE ATTACHING BOLT. THIS PROBLEM HAS BEEN TYPICAL ON A FLEET OF 6 AIRCRAFT OF THIS MODEL. THE PARTS IN QUESTION ARE: P/N-401-187 BOLT (AN5-7A), P/N-66762-00 (PLATE-AFT SPAR)
- [SDR 2004FA0000375](https://openairdocs.org/sdr/2004FA0000375.md): Bolt · sheared · May 4, 2004 · N708ER · Piper PA28R201 · Fasteners
  > DURING FLIGHT, THE PILOT REPORTED THAT THE GEAR UNSAFE LIGHT WAS ILLUMINATED DURING GEAR RETRACTION. THE GEAR WAS EXTENDED AND 3 GREEN LIGHTS WERE OBSERVED. DURING THE SUBSEQUENT INSPECTION, THE BOLT IDENTIFIED BELOW WAS FOUND SHEARED AND THE PORTION OF THE BO

Next page: https://openairdocs.org/engine/lycoming-io-360-c1c6/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 = 'IO360C1C6'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/lycoming-io-360-c1c6/reports

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