# Continental IO-360-G

- Type: Engine model (FAA registry)
- Registry code: 17152
- Manufacturer (registry): CONT MOTOR
- Model: IO-360-G
- Engine type: Reciprocating
- Power: 210 hp
- Data sheet: [TCDS E1CE](https://openairdocs.org/tcds/E1CE) (OpenAirDocs)
- Holder: Continental Aerospace Technologies, Inc.
- Installed in: 10 registered aircraft
- Page: https://openairdocs.org/engine/continental-io-360-g

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2023-17-04](https://openairdocs.org/ad/2023-17-04): Reciprocating Engine Oil System · F & M Enterprises' Model C6LC, C6LC-S or C6LC-L oil filter… (Stratus Tool Technologies STC SE09356SC or 2 others). Effective Oct 26, 2023
- [AD 2023-05-16](https://openairdocs.org/ad/2023-05-16): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 147 more. Effective Mar 15, 2023
- [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 2012
- [AD 2011-26-07](https://openairdocs.org/ad/2011-26-07): Engine · Continental Motors C-125-1, C-125-2, C145-2 and 48 more. Effective Jan 24, 2012
- [AD 2010-11-04](https://openairdocs.org/ad/2010-11-04): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 190 more. Effective Jun 16, 2010
- [AD 2000-23-21](https://openairdocs.org/ad/2000-23-21): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 164 more. Effective Dec 12, 2000
- [AD 98-19-02](https://openairdocs.org/ad/98-19-02): Piston Pins · Continental Motors IO-360-A, IO-360-AB, IO-360-C and 31 more. Effective Nov 9, 1998
- [AD 97-26-17](https://openairdocs.org/ad/97-26-17): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 90 more. Effective Jan 23, 1998
- [AD 95-21-15](https://openairdocs.org/ad/95-21-15): Aviation Gasoline · Continental Motors A-65-8, C85-12F, C85-12FJ and 77 more. Effective Nov 28, 1995
- [AD 93-10-02](https://openairdocs.org/ad/93-10-02): Missing Cylinder Valve Retainer Key · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 180 more. Effective Aug 12, 1993
- [AD 92-04-09](https://openairdocs.org/ad/92-04-09): Rocker Shaft Hold Down Stud · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 41 more. Effective Jun 22, 1993
- [AD 91-19-03](https://openairdocs.org/ad/91-19-03): Oil Filter · Continental Motors 6-285-A, 6-285-B, 6-285-BA and 169 more. Effective Sep 29, 1991
- [AD 88-03-06](https://openairdocs.org/ad/88-03-06): Oil Filter · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 155 more. Effective Apr 15, 1988
- [AD 81-13-10 R1](https://openairdocs.org/ad/81-13-10-R1): Oil Pressure · Continental Motors IO-360-A, IO-360-AB, IO-360-C and 28 more. Effective Nov 20, 1981
- [AD 81-16-05](https://openairdocs.org/ad/81-16-05): Magnetos · Lycoming Engines AEIO-320-E1B, AEIO-320-E2B, AEIO-360-B1G6 and 234 more. Effective Aug 6, 1981

Historical (superseded or no longer in force):

- [AD 2023-04-08](https://openairdocs.org/ad/2023-04-08) (historical): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 141 more. Effective Feb 23, 2023
- [AD 2009-24-52](https://openairdocs.org/ad/2009-24-52) (historical): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 192 more
- [AD 2009-24-51](https://openairdocs.org/ad/2009-24-51) (historical): Hydraulic lifters · Teledyne Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 156 more
- [AD 2002-13-04](https://openairdocs.org/ad/2002-13-04) (historical): Magneto impulse coupling stop pin · Teledyne Continental Motors C-125-1, C-125-2, C145-2 and 48 more. Effective Jul 12, 2002
- [AD 2000-08-51](https://openairdocs.org/ad/2000-08-51) (historical): Crankshaft · Teledyne Continental Motors IO-360-A, IO-360-AB, IO-360-B and 158 more
- [AD 94-14-12](https://openairdocs.org/ad/94-14-12) (historical): Octane Aviation Gasoline · Teledyne Continental Motors A-65-8, C85-12, E185-11 and 68 more

## Information bulletins (advisory) (5)

- [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016
- [SAIB NE-13-15](https://openairdocs.org/saib/NE-13-15): Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control Levers. Issued Feb 8, 2013
- [SAIB NE-13-04](https://openairdocs.org/saib/NE-13-04): Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing Inspection. Issued Oct 31, 2012
- [SAIB NE-10-09](https://openairdocs.org/saib/NE-10-09): Reciprocating Engine Power Section: Hydraulic Valve Lifters. Issued Nov 20, 2009
- [SAIB CE-02-09](https://openairdocs.org/saib/CE-02-09): . Issued Dec 28, 2001

## Registered aircraft (10)

- [N1375L](https://openairdocs.org/aircraft/N1375L): [Aviation Specialty Services LLC](https://openairdocs.org/faa-owner/AVIATION%20SPECIALTY%20SERVICES%20LLC), [Beaufort, NC](https://openairdocs.org/faa-place/NC/Beaufort), built 1978, S/N 33701867
- [N337BD](https://openairdocs.org/aircraft/N337BD): [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE), [Casper, WY](https://openairdocs.org/faa-place/WY/Casper), built 1973, S/N 0062
- [N472MT](https://openairdocs.org/aircraft/N472MT): [Flight 915 LLC](https://openairdocs.org/faa-owner/FLIGHT%20915%20LLC), [El Paso, TX](https://openairdocs.org/faa-place/TX/El%20Paso), built 2013, S/N 72924
- [N5RZ](https://openairdocs.org/aircraft/N5RZ): [Bbz Consulting LLC](https://openairdocs.org/faa-owner/BBZ%20CONSULTING%20LLC), [Cody, WY](https://openairdocs.org/faa-place/WY/Cody), built 1974, S/N 33701554
- [N72342](https://openairdocs.org/aircraft/N72342): [Ampaire Inc](https://openairdocs.org/faa-owner/AMPAIRE%20INC), [Long Beach, CA](https://openairdocs.org/faa-place/CA/Long%20Beach), built 1973, S/N 33701567
- [N72446](https://openairdocs.org/aircraft/N72446): [Minerals 66 LLC](https://openairdocs.org/faa-owner/MINERALS%2066%20LLC), [Molt, MT](https://openairdocs.org/faa-place/MT/Molt), built 1973, S/N 33701587
- [N726AS](https://openairdocs.org/aircraft/N726AS): [A2g International LLC](https://openairdocs.org/faa-owner/A2G%20INTERNATIONAL%20LLC), [San Juan Capo, CA](https://openairdocs.org/faa-place/CA/San%20Juan%20Capo), built 1975, S/N 33701661
- [N743AS](https://openairdocs.org/aircraft/N743AS): [A2g International LLC](https://openairdocs.org/faa-owner/A2G%20INTERNATIONAL%20LLC), [San Juan Capo, CA](https://openairdocs.org/faa-place/CA/San%20Juan%20Capo), built 1975, S/N 33701647
- [N746AS](https://openairdocs.org/aircraft/N746AS): [A2g International LLC](https://openairdocs.org/faa-owner/A2G%20INTERNATIONAL%20LLC), [San Juan Capo, CA](https://openairdocs.org/faa-place/CA/San%20Juan%20Capo), built 1978, S/N 33701850
- [N797KW](https://openairdocs.org/aircraft/N797KW): [Dawson Wayne R](https://openairdocs.org/faa-owner/DAWSON%20WAYNE%20R), [Arlington, TX](https://openairdocs.org/faa-place/TX/Arlington), built 2007, S/N 72288

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports (3)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20140630011089I](https://openairdocs.org/incident/20140630011089I), Jun 30, 2014: Cessna 337G (N72446), Oneonta, AL, Minor damage. On June 30, 2014 the certificated private pilot of aircraft N72446 was enroute from albertville, AL (8A0) to Oneonta, AL (20A). The pilot stated he made a…
- [Incident 20071017828629I](https://openairdocs.org/incident/20071017828629I), Oct 17, 2007: Cessna 337G (N727AS), Titusville, FL, Minor damage. (-23) The aircraft was being used for a local part 91 orientation flight and touch & go landing practice. After the flight, the crew noticed a jagged hole in…
- [Incident 19850322025149I](https://openairdocs.org/incident/19850322025149I), Mar 22, 1985: Cessna 337G (N72342), Youngstown, OH, Minor damage. Struck newly installed wood pole while taxiing at dusk. Airport owner has erected signs restricting taxi in area.

## Service difficulty reports (53, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR CA150810002](https://openairdocs.org/sdr/CA150810002), Aug 7, 2015: CLAMP. MALFUNCTIONED. (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 
- [SDR CA140506006](https://openairdocs.org/sdr/CA140506006), May 6, 2014: DRIVE GEAR. CRACKED. (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
- [SDR CA131002004](https://openairdocs.org/sdr/CA131002004), Oct 1, 2013: CLAMP. BROKEN. (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 DISASSEM
- [SDR CA120507018](https://openairdocs.org/sdr/CA120507018), Mar 16, 2012: CABLE. FRAYED. (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), Jul 5, 2011: LINE. CRACKED. 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. REP
- [SDR CA101214008](https://openairdocs.org/sdr/CA101214008), Dec 14, 2010: PISTON ROD. MISMANUFACTURED. (CAN) PISTON ROD PURCHASE (NEW) AND RECEIVED - VISUALLY ACCEPTABLE. PISTON ROD MACHINED INCORRECTLY FROM MCCAULEY - WHEN TRYING TO INSTALL BETA TUBE THREW THE P
- [SDR 2010FA0000005](https://openairdocs.org/sdr/2010FA0000005), Dec 18, 2009: STUD. DAMAGED. 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
- [SDR 2009FA0000782](https://openairdocs.org/sdr/2009FA0000782), Sep 10, 2009: CONTROL CABLE. FRAYED. 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. BOT
- [SDR CA090712001](https://openairdocs.org/sdr/CA090712001), Jul 12, 2009: VALVE. FAILED. (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 BEIN
- [SDR CA080918003](https://openairdocs.org/sdr/CA080918003), Sep 17, 2008: ALTERNATOR. DAMAGED. (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 WITHO
- [SDR CA070823009](https://openairdocs.org/sdr/CA070823009), Jul 24, 2007: ENGINE. FAILED. (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
- [SDR CA060508001](https://openairdocs.org/sdr/CA060508001), May 4, 2006: FUEL LINE. BROKEN. 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 TH
- [SDR SDR2006001](https://openairdocs.org/sdr/SDR2006001), Jan 2, 2006: UNKNOWN. UNKNOWN. WHILE HOLDING FOR TAKEOFF, NR 1 ENGINE FIRE WARNING INDICATION ACTIVATED. CREW DISCHARGED FIRE BOTTLE AS A PRECAUTIONARY PROCEDURE. PERFORMED FIRE DETECTION TES
- [SDR AU510001955](https://openairdocs.org/sdr/AU510001955), Dec 9, 2005: SHAFT. LOOSE. (AUS) LATERAL CYCLIC CONTROL BELLCRANK LOOSE. DISASSEMBLY AND INVESTIGATION OF THE TRANSMISSION FOUND THAT THE BELLCRANK MOUNTING SHAFT ATTACHED TO THE TRANSMIS
- [SDR CA051108010](https://openairdocs.org/sdr/CA051108010), Oct 28, 2005: CIRCUIT BREAKER. ARCED. (CAN) DURING APPROACH FLIGHT, PILOT SELECTED LANDING GEAR DOWN. LANDING GEAR CONTROL CIRCUIT BREAKER POPPED AND WOULD NOT RESET. PILOT WAS INSTRUCTED TO CARRY O
- [SDR CA051027005](https://openairdocs.org/sdr/CA051027005), Oct 14, 2005: IGNITION LEAD. DETERIORATED. (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 INSULAT
- [SDR CA050404009](https://openairdocs.org/sdr/CA050404009), Apr 4, 2005: CRANKCASE. CRACKED. (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 CRANKCAS
- [SDR CA040130007](https://openairdocs.org/sdr/CA040130007), Jan 6, 2004: HOUSING. CRACKED. (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), Nov 28, 2003: HOSE. DETERIORATED. (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), Nov 28, 2003: CONTROL CABLE. FRAYED. (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
- [SDR CA031001009](https://openairdocs.org/sdr/CA031001009), Sep 23, 2003: CONTROL CABLE. DAMAGED. (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/
- [SDR AUS20030912](https://openairdocs.org/sdr/AUS20030912), Sep 8, 2003: STRUCTURE. CORRODED. (AUS) LT TAILBOOM LOWER STRUCTURE CORRODED IN AREA OF ATTACHMENT TO WING STRUCTURE. CORROSION IS BOTH INTERNAL AND EXTERNAL. RT TAILBOOM CONTAINED INTERNAL CORR
- [SDR CA030602001](https://openairdocs.org/sdr/CA030602001), May 30, 2003: CONTROL CABLE. DAMAGED. (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 EXACTL
- [SDR CA020611006](https://openairdocs.org/sdr/CA020611006), Jun 3, 2002: BEVEL GEAR. FAILED. (CAN) - VACUUM PUMP DRIVE NOT TURNING.- INSPECTION REVEALS NO TEETH ON DRIVE BEVEL GEAR.- METAL CONTAMINANTS CONTAINED INSIDE STARTER ADAPTER.- TCM SB 01-5 ADDR
- [SDR LU42001F00002](https://openairdocs.org/sdr/LU42001F00002), Oct 17, 2001: BEARING. FAILED. RELEVANT INDICATION.
- [SDR CA010627062](https://openairdocs.org/sdr/CA010627062), Jun 18, 2001: PISTON. BROKEN. (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 
- [SDR 20010605CW017](https://openairdocs.org/sdr/20010605CW017), May 16, 2001: ALTERNATOR. FAILED. OWNER OF THIS AIRCRAFT EXPERIENCED FWD ENGINE ALTERNATOR FAILURE (AS INDICATOR BY FAILURE LIGHT) DURING FLIGHT. TECHNICIAN AND OWNER REMOVED ALTERNATOR FROM ENG
- [SDR CA010504017](https://openairdocs.org/sdr/CA010504017), Apr 16, 2001: SUPPORT BRACKET. CRACKED. (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
- [SDR AU001098](https://openairdocs.org/sdr/AU001098), Nov 21, 2000: GEAR. FAILED. (AUS) VACUUM PUMP DRIVE GEAR FAILED. (X)
- [SDR CA001228030](https://openairdocs.org/sdr/CA001228030), Nov 15, 2000: FUEL TANK. CRACKED. (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 
- [SDR CA001211004](https://openairdocs.org/sdr/CA001211004), Oct 20, 2000: CAM. CRACKED. (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 STEE
- [SDR CA001211005](https://openairdocs.org/sdr/CA001211005), Oct 20, 2000: BRACKET. CRACKED. (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), Apr 20, 2000: CRANKCASE. CRACKED. (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), Jan 27, 1999: PISTON. DAMAGED. (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), Oct 27, 1998: CYLINDER. CRACKED. (CAN) DURING CRUISE, THE FRONT ENGINE HAD A CYLINDER FAILURE. THE CYLINDER WAS REPLACED AFTER LANDING.
- [SDR CA981109010](https://openairdocs.org/sdr/CA981109010), Oct 9, 1998: CRANKCASE. CRACKED. (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 SMO
- [SDR AU981084](https://openairdocs.org/sdr/AU981084), Aug 20, 1998: CYLINDER. DAMAGED. (AUS) NR 2 CYLINDER ROCKER ARM SHEARED OFF AT ATTACHMENT POINT.
- [SDR CA980602057](https://openairdocs.org/sdr/CA980602057), May 15, 1998: WING. BIRD STRIKE. (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 WA
- [SDR CA980504019](https://openairdocs.org/sdr/CA980504019), Apr 29, 1998: BEARING. CORRODED. (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), Mar 3, 1998: BLADE. DAMAGED. (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), Feb 5, 1998: PUMP. FAILED. FOLLOWING TAKEOFF, AIRSPEED SLOWED. REAR ENGINE INSTRUMENTS INDICATED ENGINE WAS LOSING POWER. OIL PRESSURE WAS DROPPING AND THE PROPELLER WENT INTO FEATHER. TH
- [SDR 97ZZZX3017](https://openairdocs.org/sdr/97ZZZX3017), Jun 24, 1997: SPRING. BROKEN. CUSTOMER COMPLAINED THAT UPON PERFORMING REAR ENGINE MAGNETO CHECK, ONE MAGNETO PRODUCED NO DROP, THE OTHER MAGNETO WOULD CAUSE ENGINE DECELERATE TO THE POINT O
- [SDR CA970722043](https://openairdocs.org/sdr/CA970722043), May 28, 1997: GEAR SWITCH. BENT. (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 NO
- [SDR CA960927007](https://openairdocs.org/sdr/CA960927007), Sep 18, 1996: ALTERNATOR. BROKEN DRIVE. (CAN) THE ALTERNATOR FAILED IN FLIGHT AND GROUND INSPECTION REVEALED THE DRIVE SHAFT HAD SHEARED.
- [SDR CA960715011](https://openairdocs.org/sdr/CA960715011), Jul 1, 1996: ALTERNATOR. BROKEN SHAFT. (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 SHAF
- [SDR CA960619031](https://openairdocs.org/sdr/CA960619031), Jun 10, 1996: COUNTERWEIGHT PL. BROKEN. (CAN) THE ENGINE DEVELOPED A SLIGHT VIBRATION INFLIGHT. THE ENGINE OIL PRESSURE & VACUUM SUCTION DROPPED TO ZERO. THE STANDBY VACUUM RESTORED SUCTION. THE ENGIN
- [SDR CA960604003](https://openairdocs.org/sdr/CA960604003), May 24, 1996: CYLINDER. NOT FIRING. (CAN)IN CRUISE AT 9.5K, ENGINE RAN ROUGH AND BACKFIRED, SHUTDOWN.
- [SDR CA960502049](https://openairdocs.org/sdr/CA960502049), Apr 15, 1996: PISTON PIN. FRACTURED. (CAN) CLIMBING THROUGH 5,200 FEET, REAR ENGINE RPM STARTED FLUCTUATING 200-300 RPM. OIL PRESSURE DROPPED TO ZERO, ENGINE FEATHERED. ENGINE TEARDOWN REVEALED BRO
- [SDR CA960422008](https://openairdocs.org/sdr/CA960422008), Apr 11, 1996: CYLINDER HEAD. CRACKED. (CAN)FRONT ENGINE #5 CYLINDER CRACKED APPROXIMATELY 3 INCHES LONG ACROSS THE ROCKER ARM CAVITY AREA.
- [SDR CA960422009](https://openairdocs.org/sdr/CA960422009), Apr 11, 1996: BULKHEAD. CRACKED. (CAN)REAR ENGINE PROP SPINNER BULKHEAD ASSEMBLY CRACKED IN NUMEROUS PLACES STARTING AT THE PROP MOUNTING HOLES RUNNING RADIALLY TO OUTER DIAMETER.

All 53: https://openairdocs.org/engine/continental-io-360-g/reports.md

## STCs that may be installed (OpenAirDocs) (23)

Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SE5583SW](https://openairdocs.org/stc/SE5583SW): Installation of fuel flow transducers (true-flow totalizer). Alcor LLC. Lists IO-360 Series
- [STC SE04349CH](https://openairdocs.org/stc/SE04349CH): Installation of SureFly electronic ignition. SureFly Partners Ltd
- [STC SE02352CH](https://openairdocs.org/stc/SE02352CH): Installation of Challenger cleanable oil filter assembly. Challenger Aviation Products Inc
- [STC SE03309CH](https://openairdocs.org/stc/SE03309CH): Installation of Engine Preheat Kit, p/n TSP6CYL-2927-115 for 115 volt application. Hartzell Propeller Inc
- [STC SE01966WI](https://openairdocs.org/stc/SE01966WI): Use of GAMI G100UL High Octane Unleaded Avgas in spark ignition piston aircraft engines. General Aviation Modifications Inc
- [STC SE8409SW](https://openairdocs.org/stc/SE8409SW): Installation of P/N CO-300-1 Oil Filter Adaptor with spin-on filter as a replacement for the existing oil screen. Stratus Tool Technologies LLC
- [STC SE3330NM](https://openairdocs.org/stc/SE3330NM): Continental valve cover gasket. Real Gaskets Tennessee
- [STC SE09846SC](https://openairdocs.org/stc/SE09846SC): Installation of S539800M30 starter adapter springs. Aircraft Specialties Services Inc
- [STC SE822GL](https://openairdocs.org/stc/SE822GL): Installation of a Shadin Co. fuel flow transducer. Shadin Avionics
- [STC SE1780NM](https://openairdocs.org/stc/SE1780NM): Installation of Precise Flight standby vacuum system (SVS III). Precise Flight Inc
- [STC SE5743NM](https://openairdocs.org/stc/SE5743NM): Intallation of adapter for externally mounted oil filter. Aviation Development Corporation
- [STC SE09513SC](https://openairdocs.org/stc/SE09513SC): Installation and usage of Exxon 20W50 Multigrade aircraft engine oil conforming to Exxon Oil Formulation WS-3013. Exxon Company USA. Lists IO-360 Series
- [STC SE09401SC](https://openairdocs.org/stc/SE09401SC): Installation of modified fuel injector nozzles. General Aviation Modifications, Inc
- [STC SE00577NY](https://openairdocs.org/stc/SE00577NY): Installation of Canadian Aero Mfg. (C.A.M.) Oil Coolers. Canadian Aero Manufacturing. Lists IO-360 Series
- [STC SE00350SE](https://openairdocs.org/stc/SE00350SE): Installation of sump mounted chip detector. Aviation Development Corporation
- [STC SE00427NY](https://openairdocs.org/stc/SE00427NY): Installation, operation and inspection of CAM oil coolers. Canadian Aero Manufacturing
- [STC SE8023SW](https://openairdocs.org/stc/SE8023SW): Installation and usage of AEROSHELL. Shell Development Co. Lists IO-360 Series
- [STC SE452NE](https://openairdocs.org/stc/SE452NE): Installation and usage of 'Mobil AV 1' aviation oil. Mobil Research & Development Corp. Lists IO-360 Series
- [STC SE5879SW](https://openairdocs.org/stc/SE5879SW): Use of Phillips X/C II 20W-50 and25W-60 oil (OSS 55875) in all Avco reciprocating aircraft engines from 65 to 450 BHP. Phillips Petroleum Co. Lists IO-360 Series
- [STC SE244NE](https://openairdocs.org/stc/SE244NE): Installation of Mattituck plasma flame sprayed cylinder barrels in Teledyne reciprocating engines. Mattituck Airbase, Inc. Lists IO-360 Series
- [STC SE1445SO](https://openairdocs.org/stc/SE1445SO): Use of Aero-blend oil additive in Teledyne (non turbocharged) aircraft engines. ProTec. Lists IO-360 Series
- [STC SE99WE](https://openairdocs.org/stc/SE99WE): Installation of Equa-Flo fuel/air induction system. Circle Machine Company
- [STC SE234GL](https://openairdocs.org/stc/SE234GL): Installation of a steel pin in Continental fuel pump, P/N 638157. Approved Aircraft Accessories, Inc

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