# Lycoming I0-360-ES

- Type: Engine model (FAA registry)
- Registry code: 41596
- Manufacturer (registry): LYCOMING
- Model: I0-360-ES
- Engine type: Reciprocating
- Power: 210 hp
- Data sheet: [TCDS E1CE](https://openairdocs.org/tcds/E1CE) (OpenAirDocs)
- Holder: Continental Aerospace Technologies, Inc.
- Installed in: 18 registered aircraft
- Page: https://openairdocs.org/engine/lycoming-i0-360-es

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 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 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 81-16-05](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

## Information bulletins (advisory) (4)

- [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

## Registered aircraft (18)

- [N1249C](https://openairdocs.org/aircraft/N1249C): [Dane Aviators LLC](https://openairdocs.org/faa-owner/DANE%20AVIATORS%20LLC), [Waunakee, WI](https://openairdocs.org/faa-place/WI/Waunakee), built 2003, S/N 1268
- [N1432C](https://openairdocs.org/aircraft/N1432C): [Knoxville Flyers Inc](https://openairdocs.org/faa-owner/KNOXVILLE%20FLYERS%20INC), [Knoxville, TN](https://openairdocs.org/faa-place/TN/Knoxville), built 2003, S/N 1332
- [N1857](https://openairdocs.org/aircraft/N1857): [Saigal Sanjay](https://openairdocs.org/faa-owner/SAIGAL%20SANJAY), [Menlo Park, CA](https://openairdocs.org/faa-place/CA/Menlo%20Park), built 2003, S/N 1298
- [N200GR](https://openairdocs.org/aircraft/N200GR): [Lpc Aviation Inc](https://openairdocs.org/faa-owner/LPC%20AVIATION%20INC), [Punta Gorda, FL](https://openairdocs.org/faa-place/FL/Punta%20Gorda), S/N 1300
- [N360WT](https://openairdocs.org/aircraft/N360WT): [Thompson William E](https://openairdocs.org/faa-owner/THOMPSON%20WILLIAM%20E), [Columbus, OH](https://openairdocs.org/faa-place/OH/Columbus), built 2001, S/N 964-320-804-SFB
- [N459BT](https://openairdocs.org/aircraft/N459BT): [Air Conrad LLC](https://openairdocs.org/faa-owner/AIR%20CONRAD%20LLC), [Duncansville, PA](https://openairdocs.org/faa-place/PA/Duncansville), built 2002, S/N 1225
- [N50BZ](https://openairdocs.org/aircraft/N50BZ): [2fly-Safety LLC Trustee](https://openairdocs.org/faa-owner/2FLY-SAFETY%20LLC%20TRUSTEE), [Azle, TX](https://openairdocs.org/faa-place/TX/Azle), built 2003, S/N 1327
- [N5454M](https://openairdocs.org/aircraft/N5454M): [Mid-South Consultant Pharmacy Services Pllc](https://openairdocs.org/faa-owner/MID-SOUTH%20CONSULTANT%20PHARMACY%20SERVICES%20PLLC), [Cookeville, TN](https://openairdocs.org/faa-place/TN/Cookeville), built 2002, S/N 1226
- [N5MP](https://openairdocs.org/aircraft/N5MP): [Turlock Air LLC](https://openairdocs.org/faa-owner/TURLOCK%20AIR%20LLC), [Wilmington, NC](https://openairdocs.org/faa-place/NC/Wilmington), built 2003, S/N 1294
- [N61EW](https://openairdocs.org/aircraft/N61EW): [Wrede Emil F](https://openairdocs.org/faa-owner/WREDE%20EMIL%20F), [Lincroft, NJ](https://openairdocs.org/faa-place/NJ/Lincroft), built 2003, S/N 1302
- [N705DM](https://openairdocs.org/aircraft/N705DM): [Hysmith Nicholas Daniel](https://openairdocs.org/faa-owner/HYSMITH%20NICHOLAS%20DANIEL), [Germantown, TN](https://openairdocs.org/faa-place/TN/Germantown), built 2001, S/N 1150
- [N742C](https://openairdocs.org/aircraft/N742C): [Qualitair LLC Trustee](https://openairdocs.org/faa-owner/QUALITAIR%20LLC%20TRUSTEE), Michelstadt, built 2003, S/N 1274
- [N8017D](https://openairdocs.org/aircraft/N8017D): [Pepper Enterprises LLC](https://openairdocs.org/faa-owner/PEPPER%20ENTERPRISES%20LLC), [El Paso, TX](https://openairdocs.org/faa-place/TX/El%20Paso), built 2003, S/N 1339
- [N832JH](https://openairdocs.org/aircraft/N832JH): [Bluepoint Air LLC](https://openairdocs.org/faa-owner/BLUEPOINT%20AIR%20LLC), [Pinehurst, NC](https://openairdocs.org/faa-place/NC/Pinehurst), built 2003, S/N 1296
- [N860P](https://openairdocs.org/aircraft/N860P): [Lunsford Group Inc](https://openairdocs.org/faa-owner/LUNSFORD%20GROUP%20INC), [Winnsboro, SC](https://openairdocs.org/faa-place/SC/Winnsboro), built 2001, S/N 1149
- [N907MM](https://openairdocs.org/aircraft/N907MM): [Upwind Inc Trustee](https://openairdocs.org/faa-owner/UPWIND%20INC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2003, S/N 1270
- [N932CD](https://openairdocs.org/aircraft/N932CD): [Team Aviation II LLC](https://openairdocs.org/faa-owner/TEAM%20AVIATION%20II%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2002, S/N 1231
- [N939CD](https://openairdocs.org/aircraft/N939CD): built 2003, S/N 1295

## NTSB investigations (3)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ERA22LA352](https://openairdocs.org/ntsb/ERA22LA352), Aug 3, 2022: Cirrus Design SR20 (N459BT), Nixon, PA, substantial damage. Probable cause: The pilot’s failure to maintain directional control while landing, resulting in a runway excursion. Contributing to the outcome was the pilot’s failure to ensure that the airplane’s right side door…
- [NTSB ERA20CA142](https://openairdocs.org/ntsb/ERA20CA142), Mar 27, 2020: Cirrus SR20 (N586C), Stow, MA, substantial damage. Probable cause: The pilot's failure to maintain directional control during landing in gusting crosswind conditions, which resulted in a runway excursion and impact with vegetation.
- [NTSB DCA07MA003](https://openairdocs.org/ntsb/DCA07MA003), Oct 11, 2006: Cirrus Design SR-20 (N929CD), Manhattan, NYC, NY, destroyed, 2 fatal. Probable cause: The pilots' inadequate planning, judgment, and airmanship in the performance of a 180º turn maneuver inside of a limited turning space.

## FAA accident and incident reports (4)

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.

- [Accident 20220803014029A](https://openairdocs.org/incident/20220803014029A), Aug 3, 2022: Cirrus Design Corp SR20 (N459BT), Butler, PA, Substantial damage. During departure and climb, the pilot noticed the copilot door ajar. The pilot attempted to close the door with no success. The pilot flew the normal pattern…
- [Accident 20200327004479A](https://openairdocs.org/incident/20200327004479A), Mar 27, 2020: Cirrus Design Corp SR20 (N586C), Stow, MA, Substantial damage. Pilot stated he was attempting to land runway 3 at 6B6, winds reported 12KTS, gust to 21 from 340. Upon touch down the aircraft veered to the left. He…
- [Accident 20061011029619A](https://openairdocs.org/incident/20061011029619A), Oct 11, 2006: Cirrus SR20 (N929CD), Manhattan, NY, Destroyed, 2 fatal. (-23) Aircraft impacted building during unsuccessful attempt to remain within class b exclusionary airspace over east river, Manhattan, new york, NY, during…
- [Incident 20030324006249I](https://openairdocs.org/incident/20030324006249I), Mar 24, 2003: Cirrus SR20 (N61EW), Grand Rapids, MN, Minor damage. (-23) While giving initial training in customers new airplane, flight encountered severe turbulence during the final approach. Decision to reject landing was…

## Service difficulty reports (176, newest 50)

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

- [SDR 2024FA0000534](https://openairdocs.org/sdr/2024FA0000534), Jul 26, 2024: DRIVE COUPLING. BROKEN. GEAR PORTION OF COUPLER SLIPS INSIDE METAL/RUBBER HOUSING, CAUSING ALTERNATOR #2 TO REMAIN OFFLINE. A SECOND ALTERNATOR EXISTS WITHIN THE SYSTEM, SO NO INITIAL 
- [SDR 2024FA0000147](https://openairdocs.org/sdr/2024FA0000147), Feb 5, 2024: MAGNETO. MISOVERHAULED. REBUILT T WAS DETERMINED TO BE FAULTY OUT OF THE BOX BY THE SHOP TECHNICIAN PERFORMING INSTALL OF MAGNETO TO THE AIRCRAFT. TECHNICIAN TESTED AND VERIFIED REBUIL
- [SDR 2023FA0000241](https://openairdocs.org/sdr/2023FA0000241), May 1, 2023: FUEL DIVIDER. INOPERATIVE. PILOT COMPLETED A SATISFACTORY ENGINE RUN. CLIMBING OUT, ENGINE STARTS TO RUN ROUGH. PILOT NOTICES FUEL DROPLETS ON WINDSCREEN. ENGINE QUITS WHILE THROTTLE IS F
- [SDR 2021FA0000269](https://openairdocs.org/sdr/2021FA0000269), Sep 30, 2021: EXHAUST ROCKER. SHEARED. AIRCRAFT LANDED AFTER NOTICEABLE POWER LOSS. DURING DETAILED VISUAL INSPECTION, DISCOVERED #3 CYLINDER EXHAUST ROCKER ATTACH STUDS SHEARED AT CYLINDER. ROCKER W
- [SDR 2019FA0000399](https://openairdocs.org/sdr/2019FA0000399), Dec 9, 2019: BRACKET. WORN. RUDDER AILERON INTERCONNECT STOPPED FUNCTIONING. DISCOVERED BRACKETS WORN THROUGH. NO CHAFING ON CONTROL CABLES FORTUNATELY. PART NO LONGER MANUFACTURED.
- [SDR 2019FA0000096](https://openairdocs.org/sdr/2019FA0000096), Mar 4, 2019: SPARK PLUG. DAMAGED. AIRCRAFT RETURNED TO AIRPORT SHORTLY AFTER TAKEOFF CLIMB DUE TO SMOKE AND FUMES IN COCKPIT. PILOT ALSO RECEIVED HIGH CHT AND HIGH EGT INDICATIONS FROM #1 CYLIND
- [SDR O6WR201812130001](https://openairdocs.org/sdr/O6WR201812130001), Dec 12, 2018: KEYWAY. WORN. KEY ON DRIVE SHAFT FROM ENGINE TO TACHOMETER GENERATOR WORE AWAY CAUSING LOW/NO RPM INDICATION. FAILURE AFTER ONLY 106HRS MAY INDICATE POSSIBLE MANUFACTURE DEFE
- [SDR 2018FA0000117](https://openairdocs.org/sdr/2018FA0000117), Mar 23, 2018: HINGE BRACKET. CORRODED. PROBLEM AREA BY VISUAL INSPECTION - RIGHT AND LEFT FLAP HINGE BRACKET SEVERE CORROSION AND PRONE TO CRACKS LEADING UP TO THE BOLT HOLES THAT ATTACH THE BRACKET 
- [SDR 2017FA0000049](https://openairdocs.org/sdr/2017FA0000049), Feb 8, 2017: PROBE. ERRATIC. PERFORMED INITIAL ENGINE RUNUP, BECAUSE HIGH NR 2 CHT WAS REPORTED. AFTER ENGINE WAS WARMED UP DID FULL POWER STAIC RUN UP, NO ABNORMAL TEMPS WERE NOTED. BORESC
- [SDR CG9S2016FA0000409](https://openairdocs.org/sdr/CG9S2016FA0000409), Aug 30, 2016: PUMP. LOW PRESSURE. DURING A MAINTENANCE CHECK FLIGHT, THE AIRCRAFT LOST ENGINE POWER APPROXIMATELY 2-3 MILES FROM AIRPORT ON APPROACH. ACFT WAS ABLE TO LAND UNEVENTFULLY ON ANOTHE
- [SDR 2016FA0000407](https://openairdocs.org/sdr/2016FA0000407), Aug 28, 2016: PUMP. LEAKING. LEAKAGE IN THE ELECTRIC FUEL PUMP.
- [SDR 2016FA0000228](https://openairdocs.org/sdr/2016FA0000228), May 11, 2016: VALVE. STUCK. STUCK EXHAUST VALVE IN THE OPEN POSITION HAS CAUSED THE NR 5 CYLINDER PISTON TO PUSH IT CLOSED AND BENDING THE PUSHROD IN THE PROCESS. CYL ASSY'S NR 3, 5 & 6 DI
- [SDR 2016FA0000168](https://openairdocs.org/sdr/2016FA0000168), Apr 6, 2016: ROTOR SHAFT. WORN. DURING A PHASE NR 2 INSPECTION TECH NOTED BROWN DUST COMING OUT OF NR 2 ALTERNATOR FAN AREA. WHEN ALTERNATOR WAS DISASSEMBLED FOR INSPECTION, DISCOVERED WEAR ON
- [SDR 2016FA0000164](https://openairdocs.org/sdr/2016FA0000164), Apr 5, 2016: BOLT. BROKEN. ALTERNATOR NR 1 FAILED DURING A TRAINING FLIGHT. MAINTENANCE TECH NOTED A BROKEN ALTERNATOR CASE BOLT. THE CASE HALVES LOOSENED WHICH THEN CAUSED MORE DAMAGE WH
- [SDR CG9S2016FA0000121](https://openairdocs.org/sdr/CG9S2016FA0000121), Mar 9, 2016: ROTOR SHAFT. CRACKED. DURING MAGNETO 500 HOUR INSPECTION, DISCOVERED ROTOR SHAFT CRACKED AT KEYWAY FOR INTERNAL GEAR. THE KEY WAY AREA WAS ALSO CHIPPED FROM UNKNOWN REASONS. MAGNETO 
- [SDR 2016FA0000119](https://openairdocs.org/sdr/2016FA0000119), Mar 4, 2016: BOLT. BROKEN. DURING A PHASE 2 INSPECTION, TECH NOTED A BROKEN ALTERNATOR CASE BOLT. THE CASE HALVES HAD NOT LOOSENED UP AND NO FURTHER DAMAGE TO ALTERNATOR WAS NOTED. ALL TH
- [SDR 2016FA0000120](https://openairdocs.org/sdr/2016FA0000120), Mar 4, 2016: BOLT. BROKEN. DURING A PHASE 2 INSPECTION, THE TECH NOTED A BROKEN ALTERNATOR CASE BOLT. THE CASE HALVES HAD NOT LOOSENED UP AND NO FURTHER DAMAGE TO ALTERNATOR WAS NOTED. AL
- [SDR CG9S2016022400096](https://openairdocs.org/sdr/CG9S2016022400096), Feb 24, 2016: ALTERNATOR. DAMAGED. DURING A TRAINING FLIGHT, IT WAS NOTED THE NR 2 ALTERNATOR WAS NOT FUNCTIONING. TROUBLESHOOTING BY MAINTENANCE DISCOVERED THE NUT FOR THE STATOR TERMINAL WAS MI
- [SDR CG9S2016022600097](https://openairdocs.org/sdr/CG9S2016022600097), Feb 22, 2016: ALTERNATOR. INOPERATIVE. DURING A TRAINING FLIGHT, IT WAS NOTED THE NR 2 ALTERNATOR WAS NOT FUNCTIONING. INVESTIGATION BY MAINTENANCE DISCOVERED THE FIELD WAS OPEN ON ALTERNATOR. DURING
- [SDR 2016FA0000088](https://openairdocs.org/sdr/2016FA0000088), Feb 15, 2016: IMPULSE COUPLING. MISINSTALLED. DURING 500 HOUR MAGNETO INSPECTION IT WAS NOTED THE IMPULSE COUPLING ON MAGNETO WAS NOT FUNCTIONING PROPERLY. UPON REMOVAL OF IMPULSE COUPLING IT WAS NOTED THAT
- [SDR 2015FA0000638](https://openairdocs.org/sdr/2015FA0000638), Dec 9, 2015: PUMP. MALFUNCTIONED. DURING A CIRRUS PROGRESSIVE INSPECTION PROGRAM PHASE 2 INSPECTION DISCOVERED ENGINE FUEL FLOW TO BE 15.7 GALLONS PER HOUR. THE PUMP WAS REPLACED.
- [SDR 2015FA0000629](https://openairdocs.org/sdr/2015FA0000629), Dec 2, 2015: KEYWAY. WORN. DURING A PROGRESSIVE INSPECTION PROGRAM, 50 HOUR INSPECTION DISCOVERED ALTERNATOR NR 2 COOLING FAN LOOSE ON ALTERNATOR SHAFT. FAN PN: ES4137 IS PART OF ALTERNAT
- [SDR CG9S2015112500618](https://openairdocs.org/sdr/CG9S2015112500618), Nov 25, 2015: CAM. CRACKED. DURING A MAGNETO 500 HR INSPECTION, DISCOVERED MAGNETO IMPULSE COUPLING CAM ASSY CRACKED AT KEYWAY. THIS MAGNETO WAS 442 HOURS SINCE ENGINE REMANUFACTURE.
- [SDR 2015FA0000614](https://openairdocs.org/sdr/2015FA0000614), Nov 20, 2015: ALTERNATOR. INOPERATIVE. PILOTS REPORTED ALTERNATOR NR 2 INOPERATIVE WITH ASSOCIATED CAS WARNING MESSAGE. TROUBLESHOOTING BY MAINTENANCE REVEALED HIGH RESISTANCE OF THE FIELD CIRCUIT OF
- [SDR 2015FA0000615](https://openairdocs.org/sdr/2015FA0000615), Nov 18, 2015: COOLING FAN. LOOSE. DURING A PROGRESSIVE INSPECTION PROGRAM, PHASE 2 INSPECTION DISCOVERED ALTERNATOR NR 2 COOLING FAN LOOSE ON ALTERNATOR SHAFT. FAN, PN: ES4137 IS PART OF ALTERNA
- [SDR 2015FA0000589](https://openairdocs.org/sdr/2015FA0000589), Nov 15, 2015: SPRING. BROKEN. PILOT REPORTED DURING ATTEMPTED ENGINE START, A GRINDING NOISE WAS HEARD AND PROPELLER DIDN'T TURN. DISCOVERED CLUTCH SPRING IN STARTER ADAPTER HAD BROKEN.
- [SDR 2015FA0000594](https://openairdocs.org/sdr/2015FA0000594), Nov 12, 2015: COOLING FAN. LOOSE. DURING A CIRRUS PROGRESSIVE INSPECTION PROGRAM PHASE 2 INSPECTION DISCOVERED ALTERNATOR NR 2 COOLING FAN LOOSE ON ALTERNATOR SHAFT. FAN, PN: ES4137 IS PART OF A
- [SDR 2015FA0000561](https://openairdocs.org/sdr/2015FA0000561), Nov 11, 2015: CYLINDER HEAD. SEPARATED. ACFT EXPERIENCED ENGINE OIL LOSS DURING CLIMB OUT, ACFT ALSO EXPERIENCED LOSS OF ENGINE OIL PRESSURE. ACFT LANDED SAFELY. UPON INSPECTION BY MAINTENANCE THE NR 
- [SDR 2015FA0000590](https://openairdocs.org/sdr/2015FA0000590), Nov 11, 2015: COOLING FAN. LOOSE. DURING A PROGRESSIVE INSPECTION PROGRAM, PHASE 2 INSPECTION DISCOVERED ALTERNATOR NR 2 COOLING FAN LOOSE ON ALTERNATOR SHAFT. FAN PN: ES4137 IS PART OF ALTERNAT
- [SDR 2015FA0000592](https://openairdocs.org/sdr/2015FA0000592), Nov 11, 2015: SHAFT. CRACKED. DURING MAGNETO 500 HOUR INSPECTION, DISCOVERED ROTOR SHAFT CRACKED NEAR DRIVE GEAR AT WOODRUFF KEY WAY. THIS MAGNETO WAS REMANUFACTURED WITH ONLY 442 HOURS SINC
- [SDR 2015FA0000559](https://openairdocs.org/sdr/2015FA0000559), Nov 10, 2015: KEYWAY. WORN. DURING AN ACFT PROGRESSIVE 50 HOUR INSPECTION, DISCOVERED ALTERNATOR NR 2 COOLING FAN LOOSE ON ALTERNATOR SHAFT. THE FAN IS PART OF ALTERNATOR. THE KEY WAY OF T
- [SDR CG9S2015FA0000550](https://openairdocs.org/sdr/CG9S2015FA0000550), Nov 6, 2015: PUMP. MALFUNCTIONED. DURING A CIRRUS PROGRESSIVE INSPECTION PROGRAM, PHASE 2 INSPECTION DISCOVERED ENGINE FUEL FLOW TO BE 13.8 GALLONS PER HOUR. THIS ACFT HAD BEEN FLOWN AN UNDERMIN
- [SDR 2015FA0000546](https://openairdocs.org/sdr/2015FA0000546), Nov 4, 2015: PUMP. LOW PRESSURE. PILOT REPORTED LOW FUEL FLOW ON CLIMB OUT IN THE RANGE OF 13.4 TO 13.6 GALLON PER HOUR. WE HAVE ESTABLISHED AN OPERATIONAL MINIMUM FUEL FLOW OF 16.0 GALLONS PER
- [SDR 2015FA0000557](https://openairdocs.org/sdr/2015FA0000557), Nov 2, 2015: ADAPTER. MAKING METAL. DISCOVERED FERROUS METAL FLAKES IN OIL FILTER. DURING INVESTIGATION DETERMINED SOURCE WAS THE DRIVE SHAFT WITHIN THE STARTER ADAPTER. APPEARS THE DRIVE CLUTCH S
- [SDR 2015FA0000547](https://openairdocs.org/sdr/2015FA0000547), Nov 1, 2015: PUMP. LOW PRESSURE. PILOTS REPORTED LOW FUEL FLOW ON CLIMBOUT IN THE RANGE OF 14 GALLONS IAW HOUR. ESTABLISHED AN OPERATIONAL MINIMUM FUEL FLOW OF 16.0 GALLONS PER HOUR DUE TO OUR 
- [SDR 2015FA0000593](https://openairdocs.org/sdr/2015FA0000593), Oct 13, 2015: MOUNT BRACKET. CRACKED. DURING A MFG PROGRESSIVE INSPECTION PROGRAM 50 HOUR INSPECTION, DISCOVERED THE NR 1 ALTERNATOR MOUNTING BRACKET CRACKED IN THE FORWARD ALTERNATOR MOUNTING HOLE.
- [SDR 2015FA0000549](https://openairdocs.org/sdr/2015FA0000549), Sep 21, 2015: PUMP. MALFUNCTIONED. DURING A MFG PROGRESSIVE INSPECTION PROGRAM 50 HOUR INSPECTION, DISCOVERED ENGINE FUEL FLOW TO BE 13.9 GALLONS PER HOUR. IN THIS CASE WE WERE NOT ABLE TO ADJUST
- [SDR 2015FA0000548](https://openairdocs.org/sdr/2015FA0000548), Sep 16, 2015: PUMP. MALFUNCTIONED. DURING A PROGRESSIVE INSPECTION PROGRAM, 50 HOUR INSPECTION, DISCOVERED ENGINE FUEL FLOW TO BE 14.4 GALLONS IAW HOUR. WE HAVE ESTABLISHED AN OPERATIONAL MINIMUM
- [SDR 2015FA0000562](https://openairdocs.org/sdr/2015FA0000562), Sep 3, 2015: PUMP. LOW PRESSURE. PILOTS REPORTED LOW FUEL FLOW ON CLIMBOUT AT 13 GALLONS PER HOUR. WE HAVE ESTABLISHED AN OPERATIONAL MINIMUM FUEL FLOW OF 16.0 GALLONS PER HOUR DUE TO OUR EXPER
- [SDR 2015FA0000563](https://openairdocs.org/sdr/2015FA0000563), Sep 2, 2015: PUMP. LOW PRESSURE. PILOTS REPORTED HIGHER THAN NORMAL CHT ON CYLINDERS NR 1 AND NR 3 ALONG WITH LOW FUEL FLOW ON CLIMB, IN THE RANGE OF 12 TO 14 GALLONS PER HOUR. WE HAVE ESTABLIS
- [SDR 2015FA0000412](https://openairdocs.org/sdr/2015FA0000412), Aug 26, 2015: ROD. FAILED. ENGINE FAILURE IN FLIGHT. ROD WAS FOUND TO HAVE EXITED CRANK CASE.
- [SDR 2015FA0000441](https://openairdocs.org/sdr/2015FA0000441), Aug 25, 2015: PUMP. LEAKING. (B9582) LEAKING SEAL IN THE ELECTRIC FUEL PUMP.
- [SDR 2015FA0000297](https://openairdocs.org/sdr/2015FA0000297), Jun 28, 2015: ENGINE. FLAMED OUT. (B9739) ENGINE FLAMEOUT WHILE IDLE.
- [SDR 2015FA0000296](https://openairdocs.org/sdr/2015FA0000296), Jun 15, 2015: WARNING LIGHT. ILLUMINATED. (B9570) LOW FUEL FLOW WAS INDICATED.
- [SDR 2015FA0000295](https://openairdocs.org/sdr/2015FA0000295), Jun 14, 2015: WARNING MESSAGE. ILLUMINATED. (B9581) LOW FUEL FLOW WAS INDICATED DURING TAKEOFF.
- [SDR 2015FA0000302](https://openairdocs.org/sdr/2015FA0000302), Jun 14, 2015: WARNING MESSAGE. ILLUMINATED. (B9575) LOW FUEL FLOW AT IDLE ON THE GROUND.
- [SDR 2015FA0000321](https://openairdocs.org/sdr/2015FA0000321), Jun 8, 2015: DISTRIBUTOR BLK. LOOSE. COMPLAINT OF AN INTERMITTENT ENGINE VIBRATION. SUSPECTED AN IGNITION SYSTEM PROBLEM. FOUND 1 MAGNETO HAD JUMPED INTERNAL TIMING DUE TO DISTRIBUTOR BLOCK BEARING
- [SDR 2015FA0000301](https://openairdocs.org/sdr/2015FA0000301), May 24, 2015: PUMP. LOW PRESSURE. THE ENGINE DRIVEN PUMP PRODUCED LOW FUEL FLOW DURING TAKING OFF.
- [SDR 2015FA0000289](https://openairdocs.org/sdr/2015FA0000289), May 22, 2015: PUMP. LEAKING. FUEL PUMP FAILED AND THE ENGINE STOPPED DURING TAXI.
- [SDR 2015FA0000300](https://openairdocs.org/sdr/2015FA0000300), May 21, 2015: PUMP. LOW PRESSURE. THE ENGINE DRIVEN FUEL PUMP PRODUCED LOW FUEL FLOW DURING TAKING OFF.

All 176: https://openairdocs.org/engine/lycoming-i0-360-es/reports.md

## STCs that may be installed (OpenAirDocs) (21)

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 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 SE04577CH](https://openairdocs.org/stc/SE04577CH): Install an electronic engine ignition system. Electroair Acquisition Corp
- [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 SE09846SC](https://openairdocs.org/stc/SE09846SC): Installation of S539800M30 starter adapter springs. Aircraft Specialties Services Inc. Lists IO-360 Series
- [STC SE01559SE](https://openairdocs.org/stc/SE01559SE): Modify the existing fuel induction system to install the Continental ES tuned induction system. Merlyn Sales Inc
- [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 SE09963SC](https://openairdocs.org/stc/SE09963SC): Installation of modified fuel injector nozzles. General Aviation Modifications, Inc
- [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

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