# Service difficulty reports: Continental IO-360-G

A list on [Continental IO-360-G](https://openairdocs.org/engine/continental-io-360-g.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 53 reports

- [SDR CA150810002](https://openairdocs.org/sdr/CA150810002.md): Clamp · malfunctioned · Aug 7, 2015 · Cessna 337G · Landing Gear Door Retract Section
  > (CAN) ON LANDING PILOT REPORTED GEAR DOORS OPEN BUT GEAR DID NOT FULLY EXTEND. THERE WAS NO GREEN GEAR DOWN LIGHT AND GEAR WAS NOT VISIBLE. ELECTRIC GEAR POWER PAK MOTOR WAS RUNNING CONTINOUSLY. THE PILOT DID A LOW OVERHEAD AND IT WAS NOTED THAT THE GEAR WAS H
- [SDR CA140506006](https://openairdocs.org/sdr/CA140506006.md): Drive Gear · cracked · May 6, 2014 · Reciprocating Engine Oil System
  > (CAN) OIL PUMP DRIVE GEAR FOUND CRACKED AT RADIUS BETWEEN GEAR FACE AND SHAFT. CRACK LENGTH IS APPROXIMATELY 1/3 THE CIRCUMFERENCE OF SHAFT. NO PREVIOUS HISTORY OF PROP-STRIKE. SUSPECTED OVER-TORQUE OF THE OIL PUMP DRIVE GEAR NUT OF 23.3-25.0 FT LBS.
- [SDR CA131002004](https://openairdocs.org/sdr/CA131002004.md): Clamp · broken · Oct 1, 2013 · Cessna 337G · Magneto/Distributor
  > (CAN) DURING OPS CHECKS OF THE ENGINE AFTER ENGINE INSPECTION, IT WAS NOTED THAT THE FRONT ENGINE LT MAG HAD A DROP OF 250. THE MAGNETO WAS REMOVED AND DISASSEMBLED FOR INSPECTION. IT WAS THEN NOTICED THAT THE CLAMPS THAT BOTH OF THE CLAMPS THAT HOLD DOWN TH
- [SDR CA120507018](https://openairdocs.org/sdr/CA120507018.md): Cable · frayed · Mar 16, 2012 · Cessna 337G · Trailing Edge Flaps
  > (CAN) INSPECTED FLAP CABLES AND FOUND FLAP CABLES 1460100-7 AND 1460100-8. FRAYED AT LOCATIONS SHOWN IN ALERT. CABLES R & R WITH NEW.
- [SDR CA110707004](https://openairdocs.org/sdr/CA110707004.md): Line · cracked · Jul 5, 2011 · Cessna 337G · Engine Fuel Distribution
  > PILOT REPORTED REAR ENGINE RUNNING TO LEAN CONDITION. NO MIXTURE ADJUSTMENT AVAILABLE. FOUND A CRACK IN THE NR 6 CYLINDER FUEL SUPPLY LINE TO NR 6 CYLINDER. REPLACED LINE WITH NEW LINE PN 630662, LEAK TESTED AND TEST FLIGHT PERFORMED, SATISFACTORY.
- [SDR CA101214008](https://openairdocs.org/sdr/CA101214008.md): Piston Rod · mismanufactured · Dec 14, 2010 · Propeller Assembly
  > (CAN) PISTON ROD PURCHASE (NEW) AND RECEIVED - VISUALLY ACCEPTABLE. PISTON ROD MACHINED INCORRECTLY FROM MCCAULEY - WHEN TRYING TO INSTALL BETA TUBE THREW THE PISTON ROD IT WILL NOT ALLOW THE TUBE ALL THE WAY IN. THE PISTON ROD INSIDE DIAMETER IS TOO SMALL AN
- [SDR 2010FA0000005](https://openairdocs.org/sdr/2010FA0000005.md): Stud · damaged · Dec 18, 2009 · N337LC · Cessna 337G · Reciprocating Engine Cylinder Section
  > DURING THE TORQUE SEQUENCE FOR THE ENG O/H FINAL ASSY, FASTENERS ON THE ENG CASE WERE BROUGHT TO HALF THEIR FINAL TORQUE VALUES WITHOUT ISSUE IAW THE CURRENT MM AND PERTINENT SB`S. THEN WHILE ATTEMPTING TO REACH FINAL TORQUE VALUES, NOTED THAT MANY OF THE STU
- [SDR 2009FA0000782](https://openairdocs.org/sdr/2009FA0000782.md): Control Cable · frayed · Sep 10, 2009 · N1873M · Cessna 337G · Trailing Edge Flap Control System
  > FOUND BOTH OF THE RT WING FLAP EXTEND CABLES WITH BROKEN INTERNAL WIRES. CABLES HAD TO BE REMOVED AND TWISTED AGAINST THEIR NORMAL WIND TO FIND THE TROUBLE. BOTH WERE DAMAGED AT THE POINT WHERE THEY GO AROUND THE BELLCRANKS IN THE WING, ABOUT 2 INCHES FROM TH
- [SDR CA090712001](https://openairdocs.org/sdr/CA090712001.md): Valve · failed · Jul 12, 2009 · Cessna 337G · Landing Gear Brake System
  > (CAN) ON LANDING, THE PILOT NOTED THE ACFT PULLED TO THE LT. AFTER LANDING, IT WAS NOTED THAT THE LT TIRE HAD A FLAT SPOT THAT MIGHT HAVE BEEN DUE TO BRAKE BEING ON. INSP OF THE PARKING BRAKE REVEALED THAT WHEN THE PARK BRAKE WAS PUT ON AND THEN TURNED OFF S
- [SDR CA080918003](https://openairdocs.org/sdr/CA080918003.md): Alternator · damaged · Sep 17, 2008 · Cessna 337G · DC Generator-Alternator
  > (CAN) THE ACFT, A CESSNA 337G WAS ON A RETURN FLIGHT TO MAIN BASE WHEN THE PILOT NOTICED A INDICATION OF A FAILED FRONT ENGINE ALTERNATOR. THE ACFT LANDED WITHOUT INCIDENT AND MX INVESTIGATED THE PROBLEM. DURING REMOVAL OF THE FRONT ALTERNATOR, IT WAS DISCOV
- [SDR CA070823009](https://openairdocs.org/sdr/CA070823009.md): Engine · failed · Jul 24, 2007 · Cessna 337G · Engine Oil Pressure
  > (CAN) REAR ENGINE EXPERIENCED A LOSS OF OIL PRESSURE DURING FLIGHT. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO BASE. ENGINE WAS REPLACED. UNABLE TO DETERMINE OIL PRESSURE PROBLEM WITH FAILED OIL PRESSURE ON ENGINE. ENGINE WAS SHIPPED TO ENGINE SHOP. (TC NR
- [SDR CA060508001](https://openairdocs.org/sdr/CA060508001.md): Fuel Line · broken · May 4, 2006 · Cessna 337G · Engine Fuel Distribution
  > SHORTLY AFTER TAKEOFF, THE PILOT OF A CESSNA 337 NOTICED THAT FUEL PRESSURE ON THE REAR ENGINE BEGAN TO DROP OFF AND THE ENGINE BEGAN TO RUN ROUGH. TURNED ON THE ELECTRIC BOOST PUMP AND THE ENGINE CONTINUED TO RUN NORMALLY. ELECTED TO RETURN TO THE AIRPORT AN
- [SDR SDR2006001](https://openairdocs.org/sdr/SDR2006001.md): Unknown · unknown · Jan 2, 2006 · N4AE · Aerosp ATR72212 · Fire Detection
  > WHILE HOLDING FOR TAKEOFF, NR 1 ENGINE FIRE WARNING INDICATION ACTIVATED. CREW DISCHARGED FIRE BOTTLE AS A PRECAUTIONARY PROCEDURE. PERFORMED FIRE DETECTION TEST AND FOUND OPERATING PROPERLY. (K)
- [SDR AU510001955](https://openairdocs.org/sdr/AU510001955.md): Shaft · loose · Dec 9, 2005 · Hughes 269C · Main Rotor Gearbox
  > (AUS) LATERAL CYCLIC CONTROL BELLCRANK LOOSE. DISASSEMBLY AND INVESTIGATION OF THE TRANSMISSION FOUND THAT THE BELLCRANK MOUNTING SHAFT ATTACHED TO THE TRANSMISSION HAD NO SPLIT PIN WHICH ALLOWED THE NUT TO WORK LOOSE AND COME OFF THE SHAFT. THE NUT AND WASHER
- [SDR CA051108010](https://openairdocs.org/sdr/CA051108010.md): Circuit Breaker · arced · Oct 28, 2005 · Cessna 337C · Landing Gear System Wiring
  > (CAN) DURING APPROACH FLIGHT, PILOT SELECTED LANDING GEAR DOWN. LANDING GEAR CONTROL CIRCUIT BREAKER POPPED AND WOULD NOT RESET. PILOT WAS INSTRUCTED TO CARRY OUT AN EMERGENCY GEAR EXTENSION AND FOLLOW LANDING PROCEDURES IN PILOT'S OPERATING HANDBOOK. UPON
- [SDR CA051027005](https://openairdocs.org/sdr/CA051027005.md): Ignition Lead · deteriorated · Oct 14, 2005 · Cessna 337G · Ignition Harness (Distribution)
  > (CAN) ON GROUND RUN, LT MAGNETO ON FRONT ENGINE HAD A 200 RPM DROP. DURING TROUBLESHOOTING FOUND NR 4 CYLINDER TOP LEAD SHORTING FROM INNER COIL THROUGH INSULATOR TO CAP. LEAD REPAIRED, AIRCRAFT RELEASED INTO SERVICE. AFTER A FEW HOURS OF FLIGHT, THE PROBLEM R
- [SDR CA050404009](https://openairdocs.org/sdr/CA050404009.md): Crankcase · cracked · Apr 4, 2005 · Cessna 337G · Reciprocating Engine Power Section
  > (CAN) THE INITIAL PROBLEM WAS AN OIL LEAK FOUND DURING INSPECTION, AFTER SEVERAL ENGINE GROUND RUN-UPS, CRACK OF 2 INCHES FOUND FWD OF CYLINDER NR 5 ON CRANKCASE UPPER SECTION, ENGINE REMOVED AND SEND TO REPAIR SHOP.
- [SDR CA040130007](https://openairdocs.org/sdr/CA040130007.md): Housing · cracked · Jan 6, 2004 · Cessna 337G · DC Generator-Alternator
  > (CAN) ON INSPECTION OF ALTERNATOR HOUSING 2 RIBS WERE FOUND CRACKED COMPLETELY THROUGH. THERE HAVE BEEN TWO OTHER SIMILAR ALTERNATORS FOUND WITH CRACKED RIBS.
- [SDR AUS20031296](https://openairdocs.org/sdr/AUS20031296.md): Hose · deteriorated · Nov 28, 2003 · Cessna 337G · Aircraft Fuel Distribution System
  > (AUS) REAR ENGINE FUEL PRESSURE HOSE LOCATED BETWEEN FIREWALL AND FUEL MANIFOLD DETERIORATED AND LEAKING ONTO LT EXHAUST STACK.
- [SDR AUS20031318](https://openairdocs.org/sdr/AUS20031318.md): Control Cable · frayed · Nov 28, 2003 · Cessna 337H · Trailing Edge Flap Control System
  > (AUS) IB FLAP CABLE CONTAINED BROKEN WIRES LOCATED AT TIGHT BEND AROUND THE BELLCRANK. APPROXIMATELY 50 PERCENT OF THE WIRES WERE BROKEN. INSPECTION CARRIED OUT IN RESPONSE TO MFG ALERT.
- [SDR CA031001009](https://openairdocs.org/sdr/CA031001009.md): Control Cable · damaged · Sep 23, 2003 · Cessna 337G · Trailing Edge Flap Control System
  > (CAN) A SPECIAL INSPECTION WAS INITIATED TO COMPLY WITH REMOVAL AND INSPECTION OF FLAP CONTROL CABLES THAT ARE CONNECTED TO THE INBOARD FLAP BELLCRANK. CABLE P/N 1460 100-7 AND 1460100-8 WERE BOTH FOUND TO HAVE SEVERAL BROKEN STRANDS AND REQUIRED REPLACEMENT.
- [SDR AUS20030912](https://openairdocs.org/sdr/AUS20030912.md): Structure · corroded · Sep 8, 2003 · Cessna 337G · Fuselage Main, Structure
  > (AUS) LT TAILBOOM LOWER STRUCTURE CORRODED IN AREA OF ATTACHMENT TO WING STRUCTURE. CORROSION IS BOTH INTERNAL AND EXTERNAL. RT TAILBOOM CONTAINED INTERNAL CORROSION ONLY.
- [SDR CA030602001](https://openairdocs.org/sdr/CA030602001.md): Control Cable · damaged · May 30, 2003 · Cessna 337G · Trailing Edge Flap Actuator
  > (CAN) AFTER RECEIVING SDR ALERT AL-2003-05 AN INSPECTION WAS CARRIED OUT ON OUR 337G. TWO CABLES ON BOTH SIDES WERE FOUND DAMAGED. THE DAMAGE WAS LOCATED EXACTLY IN THE SAME LOCATION AS MENTION IN THE ALERT IE AROUND THE SHARP BEND OF THE BELLCRANK. ALL CABLES
- [SDR CA020611006](https://openairdocs.org/sdr/CA020611006.md): Bevel Gear · failed · Jun 3, 2002 · Cessna 337G · Reciprocating Engine Rear Section
  > (CAN) - VACUUM PUMP DRIVE NOT TURNING.- INSPECTION REVEALS NO TEETH ON DRIVE BEVEL GEAR.- METAL CONTAMINANTS CONTAINED INSIDE STARTER ADAPTER.- TCM SB 01-5 ADDRESSES PROBLEM.- TCM WARRANTS FULL REPLACEMENT.
- [SDR LU42001F00002](https://openairdocs.org/sdr/LU42001F00002.md): Bearing · failed · Oct 17, 2001 · N11FT · Cessna 337G · Propeller Assembly
  > RELEVANT INDICATION.
- [SDR CA010627062](https://openairdocs.org/sdr/CA010627062.md): Piston · broken · Jun 18, 2001 · Cessna 337G · Reciprocating Engine Cylinder Section
  > (CAN) ON A GROUND RUN-UP PRIOR TO A SCHEDULED INSPECTION A PARTIAL POWER LOSS WAS DETECTED. A MOTO-STAT WAS CARRIED OUT AND #6 CYL. HAD VERY LOW COMPRESSION. A FILTER CHECK WAS CARRIED OUT AND SUBSTANIAL METAL PARTS, ALM, CHROME AND STEEL WERE FOUND THAT ARE C
- [SDR 20010605CW017](https://openairdocs.org/sdr/20010605CW017.md): Alternator · failed · May 16, 2001 · N297DC · Cessna 337G · DC Generator-Alternator
  > OWNER OF THIS AIRCRAFT EXPERIENCED FWD ENGINE ALTERNATOR FAILURE (AS INDICATOR BY FAILURE LIGHT) DURING FLIGHT. TECHNICIAN AND OWNER REMOVED ALTERNATOR FROM ENGINE AND DISCOVERED THE DRIVE SHAFT SHEARED. THE GEAR RETAINING BOLT HAD RUBBED INTERNALLY AND BUS
- [SDR CA010504017](https://openairdocs.org/sdr/CA010504017.md): Support Bracket · cracked · Apr 16, 2001 · Cessna 337C · Rudder Control System
  > (CAN) DURING A 100 HOUR INSPECTION IT WAS OBSERVED THERE WA A CRACK IN THE ABOVE MENTIONED BRACKET. A NEW BRACKET WAS INSTALLED AND AIRCRAFT RELEASED FOR RETURN TO SERVICE.
- [SDR AU001098](https://openairdocs.org/sdr/AU001098.md): Gear · failed · Nov 21, 2000 · Cessna 337G · Reciprocating Engine Rear Section
  > (AUS) VACUUM PUMP DRIVE GEAR FAILED. (X)
- [SDR CA001228030](https://openairdocs.org/sdr/CA001228030.md): Fuel Tank · cracked · Nov 15, 2000 · Cessna 337H · Fuel Storage
  > (CAN) WHILE BEING STORED IN A HANGAR RIGHT WING WAS DISCOVERED TO BE LEAKING FUEL. UPON FURTHER INSPECTION NR3 FUEL TANK P/N 1516132-16 HAD A CRACK ON TOP NEAR THE TRAILING EDGE. FUEL TANK WAS THEN REMOVED, REPAIRED AND REINSTALLED.
- [SDR CA001211004](https://openairdocs.org/sdr/CA001211004.md): Cam · cracked · Oct 20, 2000 · Cessna 337H · Steering Unit
  > (CAN) DISCOVERED DURING A 100-HOUR INSPECTION. THE SHIMMY DAMPER ATTACH BRACKET WAS FOUND CRACKED. DUE TO THIS, THE LANDING GEAR (NOSE) WAS REMOVED AND THE STEERING CAM WAS SENT OUT FOR NDT. THE CAM WAS FOUND CRACKED AT THE LOWER FORWARD SHIMMY DAMPER ATTACH
- [SDR CA001211005](https://openairdocs.org/sdr/CA001211005.md): Bracket · cracked · Oct 20, 2000 · Cessna 337H · Landing Gear Steering System
  > (CAN) DISCOVERED DURING A 100 HOUR INSPECTION. THE TOP OF THE BRACKET WHERE THE SHIMMY DAMPER ATTACHES WAS FOUND CRACKED.
- [SDR CA000505013](https://openairdocs.org/sdr/CA000505013.md): Crankcase · cracked · Apr 20, 2000 · Cessna 337B · Reciprocating Engine Power Section
  > (CAN) CRANKCASE FOUND TO BE A LIGHT DUTY CASE.ENGINE SHOP DISCARDED CASE AND REPLACED IT WITH A NEW HEAVY CASE.
- [SDR AU990090](https://openairdocs.org/sdr/AU990090.md): Piston · damaged · Jan 27, 1999 · Cessna 337G · Reciprocating Engine Cylinder Section
  > (AUS) NR 6 CYLINDER PISTON DAMAGED DUE TO DETONATION. METAL CONTAMINATION OF THE ENGINE. ENGINE FACTORY REMANUFACTURED 457.1 HOURS PREVIOUSLY. PART TC: 457.
- [SDR CA981027005](https://openairdocs.org/sdr/CA981027005.md): Cylinder · cracked · Oct 27, 1998 · Cessna 337D · Reciprocating Engine Cylinder Section
  > (CAN) DURING CRUISE, THE FRONT ENGINE HAD A CYLINDER FAILURE. THE CYLINDER WAS REPLACED AFTER LANDING.
- [SDR CA981109010](https://openairdocs.org/sdr/CA981109010.md): Crankcase · cracked · Oct 9, 1998 · Cessna 337G · Reciprocating Engine Power Section
  > (CAN) THE REAR ENGINE OF A 337G SKYMASTER WAS REPORTED AS RUNNING ROUGH. INSPECTION FOUND THE SPARK PLUGS FOULED, SO THE PLUGS WERE REPLACED. THE ENGINE RAN SMOOTH AND IT WAS RELEASED FOR RETURN TO SERVICE. ON THE SECOND FLIGHT WHEN POWER WAS REDUCED, THE EN
- [SDR AU981084](https://openairdocs.org/sdr/AU981084.md): Cylinder · damaged · Aug 20, 1998 · Cessna 337G · Reciprocating Engine Cylinder Section
  > (AUS) NR 2 CYLINDER ROCKER ARM SHEARED OFF AT ATTACHMENT POINT.
- [SDR CA980602057](https://openairdocs.org/sdr/CA980602057.md): Wing · bird strike · May 15, 1998 · Cessna 337G · Wing Main, Frame Structure
  > (CAN) IN CRUISE, PILOT CAUGHT A FLASH OF MOTION AND HEARD A BIRD IMPACT WITH HIS LEFT WING. DAMAGE WAS VISIBLE FROM THE COCKPIT. WIRES WERE VISIBLE SO ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO BASE. DAMAGE WAS FOUND TO EXTEND FROM STN 204 TO 222. LEADIN
- [SDR CA980504019](https://openairdocs.org/sdr/CA980504019.md): Bearing · corroded · Apr 29, 1998 · Cessna 337G · Propeller Blade Section
  > (CAN) PROPELLER RECEIVED FOR FIVE YEAR CORROSION INSPECTION. INSPECTION FOUND NR 1 BLADE BEARING RACE CORRODED. BEARING RACE REPLACED.
- [SDR CA980311016](https://openairdocs.org/sdr/CA980311016.md): Blade · damaged · Mar 3, 1998 · Cessna 337G · Propeller Blade Section
  > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER BLADES WERE REPAIRED IN THE FIELD AND FOUND TO BE BELOW MANUFACTURERS MINIMUM WIDTHS (LIMITS).
- [SDR 98ZZZX874](https://openairdocs.org/sdr/98ZZZX874.md): Pump · failed · Feb 5, 1998 · N132CM · Cessna 337H · Reciprocating Engine Oil System
  > FOLLOWING TAKEOFF, AIRSPEED SLOWED. REAR ENGINE INSTRUMENTS INDICATED ENGINE WAS LOSING POWER. OIL PRESSURE WAS DROPPING AND THE PROPELLER WENT INTO FEATHER. THE ENGINE WAS SHUT DOWN AND A LANDING WAS MADE. AN INSPECTION OF THE ENGINE DETERMINED THE OIL PU
- [SDR 97ZZZX3017](https://openairdocs.org/sdr/97ZZZX3017.md): Spring · broken · Jun 24, 1997 · Cessna 337G · Magneto/Distributor
  > CUSTOMER COMPLAINED THAT UPON PERFORMING REAR ENGINE MAGNETO CHECK, ONE MAGNETO PRODUCED NO DROP, THE OTHER MAGNETO WOULD CAUSE ENGINE DECELERATE TO THE POINT OF STOPPING. MAGNETO'S WERE REMOVED AND INSPECTED. FOUND IMPULSE COUPLING SPRING BROKEN. THIS IS T
- [SDR CA970722043](https://openairdocs.org/sdr/CA970722043.md): Gear Switch · bent · May 28, 1997 · Cessna 337G · Landing Gear Retraction/Extension System
  > (CAN) NOSE WHEEL RETRACTED AND COULD NOT BE EXTENDED DUE TO FAILURE OF THE SQUAT SWITCH BRACKET TO MAKE POSITIVE CONTACT WITH THE SWITCH. THE AIRCRAFT MADE A NOSE WHEEL GEAR UP LANDING.
- [SDR CA960927007](https://openairdocs.org/sdr/CA960927007.md): Alternator · broken drive · Sep 18, 1996 · Cessna 337G · DC Generator-Alternator
  > (CAN) THE ALTERNATOR FAILED IN FLIGHT AND GROUND INSPECTION REVEALED THE DRIVE SHAFT HAD SHEARED.
- [SDR CA960715011](https://openairdocs.org/sdr/CA960715011.md): Alternator · broken shaft · Jul 1, 1996 · Cessna 337G · DC Generator-Alternator
  > (CAN) THE ALTERNATOR DRIVE SHAFT FAILED AT THE BASE OF THE ALTERNATOR. THIS SHAFT APPEARED TO BE CRACKED OR HAD A PREVIOUS FLAW. THIS ALLOWED THE REMAINING SHAFT AND DRIVE GEAR TO MOVE FORWARD RUBBING ON THE CAM GEAR. THE RUBBER BUSHING, P/N 632050, AND METAL
- [SDR CA960619031](https://openairdocs.org/sdr/CA960619031.md): Counterweight Pl · broken · Jun 10, 1996 · Mooney M20K · Reciprocating Engine Power Section
  > (CAN) THE ENGINE DEVELOPED A SLIGHT VIBRATION INFLIGHT. THE ENGINE OIL PRESSURE & VACUUM SUCTION DROPPED TO ZERO. THE STANDBY VACUUM RESTORED SUCTION. THE ENGINE OPERATING TEMPERATURE INCREASED BUT STAYED IN THE GREEN. THE MANIFOLD PRESSURE WAS NORMAL. POST FL
- [SDR CA960604003](https://openairdocs.org/sdr/CA960604003.md): Cylinder · not firing · May 24, 1996 · Cessna 337G · Reciprocating Engine Cylinder Section
  > (CAN)IN CRUISE AT 9.5K, ENGINE RAN ROUGH AND BACKFIRED, SHUTDOWN.
- [SDR CA960502049](https://openairdocs.org/sdr/CA960502049.md): Piston Pin · fractured · Apr 15, 1996 · Cessna 337G · Reciprocating Engine Cylinder Section
  > (CAN) CLIMBING THROUGH 5,200 FEET, REAR ENGINE RPM STARTED FLUCTUATING 200-300 RPM. OIL PRESSURE DROPPED TO ZERO, ENGINE FEATHERED. ENGINE TEARDOWN REVEALED BROKEN PISTON PIN. SUPERIOR AIR PART.
- [SDR CA960422008](https://openairdocs.org/sdr/CA960422008.md): Cylinder Head · cracked · Apr 11, 1996 · Cessna 337G · Reciprocating Engine Cylinder Section
  > (CAN)FRONT ENGINE #5 CYLINDER CRACKED APPROXIMATELY 3 INCHES LONG ACROSS THE ROCKER ARM CAVITY AREA.
- [SDR CA960422009](https://openairdocs.org/sdr/CA960422009.md): Bulkhead · cracked · Apr 11, 1996 · Cessna 337G · Propeller Spinner Section
  > (CAN)REAR ENGINE PROP SPINNER BULKHEAD ASSEMBLY CRACKED IN NUMEROUS PLACES STARTING AT THE PROP MOUNTING HOLES RUNNING RADIALLY TO OUTER DIAMETER.

Next page: https://openairdocs.org/engine/continental-io-360-g/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 = 'IO360G'
ORDER BY difficulty_date DESC
```

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

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