# Lycoming O-360-C2E - Type: Engine model (FAA registry) - Registry code: 42288 - Manufacturer (registry): LYCOMING - Model: O-360-C2E - Engine type: Reciprocating - Power: 180 hp - Data sheet: [TCDS E-286](https://openairdocs.org/tcds/E-286) (OpenAirDocs) - Holder: Lycoming Engines - Installed in: 5 registered aircraft - Page: https://openairdocs.org/engine/lycoming-o-360-c2e 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 2026-04-11](https://openairdocs.org/ad/2026-04-11): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 605 more. Effective Apr 8, 2026 - [AD 2020-25-12](https://openairdocs.org/ad/2020-25-12): Reciprocating Engine Power Section · Superior Air Parts IO-360-A1A1, IO-360-A1A2, IO-360-A2A1 and 146 more. Effective Jan 15, 2021 - [AD 2017-16-11](https://openairdocs.org/ad/2017-16-11): Reciprocating Engine Power Section · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-360-B1G6 and 93 more. Effective Aug 15, 2017 - [AD 2012-19-01](https://openairdocs.org/ad/2012-19-01): Crankshafts · Lycoming Engines AEIO-360-A1A, AEIO-360-A1B, AEIO-360-A1B6 and 321 more. Effective Oct 24, 2012 - [AD 2012-03-07](https://openairdocs.org/ad/2012-03-07): Carburetor · Lycoming Engines GO-435, GO-435-C2 (O-435-17), GO-435-C2A and 389 more. Effective Mar 27, 2012 - [AD 2009-26-12](https://openairdocs.org/ad/2009-26-12): Cylinder assemblies · Engine Components Reciprocating Engine Cylinder Assemblies, AEIO-320-D1B, AEIO-320-D2B and 264 more. Effective Feb 4, 2010 - [AD 2007-04-19 R1](https://openairdocs.org/ad/2007-04-19-R1): SAP cylinder assemblies · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 314 more. Effective May 7, 2007 - [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006 - [AD 2006-10-21](https://openairdocs.org/ad/2006-10-21): ECi connecting rods · Engine Components Reciprocating Engine Connecting Rods, AEIO-360-B1B, AEIO-360-B1D and 171 more. Effective Jun 22, 2006 - [AD 2004-10-14](https://openairdocs.org/ad/2004-10-14): Crankshaft gear · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 642 more. Effective Jun 25, 2004 - [AD 98-02-08](https://openairdocs.org/ad/98-02-08): Crankshaft · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 216 more. Effective Mar 30, 1998 - [AD 97-15-11](https://openairdocs.org/ad/97-15-11): Cylinder kits · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 538 more. Effective Aug 12, 1997 - [AD 96-09-10](https://openairdocs.org/ad/96-09-10): Oil pump · Lycoming Engines AEIO-320-E1A, AEIO-320-E1B, AEIO-320-E2A and 334 more. Effective Jul 15, 1996 - [AD 95-07-01](https://openairdocs.org/ad/95-07-01): Connecting Rod Bolt · Lycoming Engines AEIO-360-A1E, AEIO-360-B1G6, AEIO-360-H1A and 177 more. Effective Apr 12, 1995 - [AD 92-12-05](https://openairdocs.org/ad/92-12-05): Piston Pins · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 532 more. Effective Jul 10, 1992 - [AD 90-04-06 R1](https://openairdocs.org/ad/90-04-06-R1): Propeller Governor External Oil Line · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 427 more. Effective May 28, 1991 - [AD 87-10-06 R1](https://openairdocs.org/ad/87-10-06-R1): Rocker Arm Assembly · Lycoming Engines IO-360-B4, IVO-360-A1A, O-340-A1A and 243 more. Effective Sep 1, 1989 - [AD 89-04-02](https://openairdocs.org/ad/89-04-02): Carburetors · Continental Motors O-470-11, O-470-11-CI, O-470-11B and 175 more. Effective Mar 8, 1989 - [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 - [AD 80-06-05](https://openairdocs.org/ad/80-06-05): Magnetos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 254 more. Effective Mar 28, 1980 - [AD 75-08-09](https://openairdocs.org/ad/75-08-09): Oil Pump Drive Shaft · Lycoming Engines AEIO-360-A1B, AEIO-360-A1B6, AEIO-360-A1C and 365 more. Effective Aug 18, 1977 - [AD 69-24-03](https://openairdocs.org/ad/69-24-03): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 321 more. Effective Nov 29, 1969 - [AD 67-01-04](https://openairdocs.org/ad/67-01-04): Oil Filters · Full flow oil filter (Superior Flow STC SA401SW or 2 others). Effective Jan 2, 1967 - [AD 63-22-03](https://openairdocs.org/ad/63-22-03): Carburetors · Continental Motors GO-300-A, GO-300-B, GO-300-C and 143 more. Effective Dec 2, 1963 Historical (superseded or no longer in force): - [AD 2024-21-02](https://openairdocs.org/ad/2024-21-02) (historical): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 548 more. Effective Dec 5, 2024 - [AD 2008-19-05](https://openairdocs.org/ad/2008-19-05) (historical): Parallel Valve'' reciprocating engines · Engine Components Reciprocating Engine Cylinder Assemblies, AEIO-320-D1B, AEIO-320-D2B and 262 more. Effective Oct 20, 2008 - [AD 2005-26-10](https://openairdocs.org/ad/2005-26-10) (historical): ECi cylinder assemblies. · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 413 more. Effective Jan 31, 2006 - [AD 81-18-04 R2](https://openairdocs.org/ad/81-18-04-R2) (historical): Engine Oil Pump Driven Impeller and Shaft · Textron Lycoming, AVCO AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 376 more. Effective Jun 7, 1982 ## Information bulletins (advisory) (6) - [SAIB NE-19-08](https://openairdocs.org/saib/NE-19-08): Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve Cylinders. Issued May 2, 2019 - [SAIB NE-08-32R1](https://openairdocs.org/saib/NE-08-32R1): Propeller Governor Idler Gear Shaft Set Screw. Issued May 13, 2016 - [SAIB NE-14-13](https://openairdocs.org/saib/NE-14-13): Reciprocating Engine - Cylinder Mounting Studs. Issued Mar 24, 2014 - [SAIB NE-13-06](https://openairdocs.org/saib/NE-13-06): Pushrod Shroud Spring Retainers, Engine Components Part No. AEL14995, for Lycoming Engines 320, 360, and 540 Series Engines. Issued Nov 21, 2012 - [SAIB NE-06-32R1](https://openairdocs.org/saib/NE-06-32R1): Reciprocating Engine - Crankshaft. Issued Sep 10, 2008 - [SAIB NE-08-32](https://openairdocs.org/saib/NE-08-32) (historical): Propeller Governor Set Screw. Issued Jul 3, 2008 ## Registered aircraft (5) - [N181AK](https://openairdocs.org/aircraft/N181AK): [Weflen Arvid W](https://openairdocs.org/faa-owner/WEFLEN%20ARVID%20W), [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks), built 1992, S/N W1991 - [N7680S](https://openairdocs.org/aircraft/N7680S): [Hallsten Stephen B](https://openairdocs.org/faa-owner/HALLSTEN%20STEPHEN%20B), [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks), built 1976, S/N 221-76 - [N88297](https://openairdocs.org/aircraft/N88297): [Naber David Lowell](https://openairdocs.org/faa-owner/NABER%20DAVID%20LOWELL), [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks), built 1974, S/N 104-74 - [N95NH](https://openairdocs.org/aircraft/N95NH): [Oberlander Justin D](https://openairdocs.org/faa-owner/OBERLANDER%20JUSTIN%20D), [Colton, OR](https://openairdocs.org/faa-place/OR/Colton), built 1974, S/N 105-74 - [N977SD](https://openairdocs.org/aircraft/N977SD): [St Denis Elizbeth A](https://openairdocs.org/faa-owner/ST%20DENIS%20ELIZBETH%20A), [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks), built 1975, S/N 156-75 ## NTSB investigations (2) 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 ANC95LA033](https://openairdocs.org/ntsb/ANC95LA033), Mar 9, 1995: Champion 8GCBC (N88297), Fairbanks, AK, substantial damage. Probable cause: THE PILOT'S INADEQUATE PRE-FLIGHT PLANNING. A SHORT TAKEOFF AREA THAT WAS COVERED WITH SOFT SNOW WERE FACTORS IN THE ACCIDENT. - [NTSB ANC89LA145](https://openairdocs.org/ntsb/ANC89LA145), Aug 19, 1989: Bellanca 8GCBC (N88297), Galbraith Lake, AK, substantial damage. Probable cause: THE PILOTS FAILURE TO MAINTAIN DIRECTION CONTROL AFTER ABORTING TAKEOFF FOLLOWING FAILURE OF THE TAIL LANDING GEAR TIRE. ## 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. - [Accident 19950309009279A](https://openairdocs.org/incident/19950309009279A), Mar 9, 1995: Bbavia 8GCBC (N88297), Fairbanks, AK, Substantial damage. Tried depart snow covered remote area on skis. Slowed by soft snow as skid ag in. Struck tress end of open area. - [Incident 19910318011289I](https://openairdocs.org/incident/19910318011289I), Mar 18, 1991: Bbavia 8GCBC (N88297), Livengood, AK, Minor damage. Experienced a rough running engine. Precautionary landing. Landed on rough terrain and right axel bolt broke. - [Accident 19890819030839A](https://openairdocs.org/incident/19890819030839A), Aug 19, 1989: Bbavia 8GCBC (N88297), Galbraith Lake, AK, Substantial damage. Aborted takeoff from a gravel bar when the tailwheel tire ruptured. Veered sharply collapsed gear. Rock cut tire. ## Service difficulty reports (129, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CA190718001](https://openairdocs.org/sdr/CA190718001), Jul 16, 2019: SPAR. CRACKED. (CAN) ROUTINE INSPECTION BEFORE A/C WAS DEPARTING ON LONG CONTRACT AWAY BASE. CRACKS EMANATING FROM NAIL HOLES ON SPAR DOUBLER. (TC# 20190718001) - [SDR CA190723008](https://openairdocs.org/sdr/CA190723008), Jun 27, 2019: CYLINDER. CRACKED. (CAN) HIGHER THAN EXPECTED CYLINDER HEAD TEMPERATURE (CHT), FOLLOWED BY DECREASING RPM AND A KNOCKING NOISE THAT PROGRESSIVELY GOT LOUDER. ON INSPECTION IT WAS - [SDR CA190315010](https://openairdocs.org/sdr/CA190315010), Feb 12, 2019: TAB. CRACKED. (CAN) ON A 100HR INSPECTION OF THE ELEVATOR TRIM TAB, THE TAB WAS OBSERVED TO BE CRACKED AT THE TOP RIVET OF THE BELL CRANK. THE TRIM TAB WAS REMOVED AND SENT T - [SDR CA190315008](https://openairdocs.org/sdr/CA190315008), Feb 1, 2019: TAB. CRACKED. (CAN) ON A 100HR INSPECTION OF THE ELEVATOR TRIM TAB, THE TAB WAS FOUND TO BE CRACKED AT TOP RIVET ON THE BELL CRANK. THE TRIM WAS REMOVED AND SENT TO QUARANTIN - [SDR CA160301026](https://openairdocs.org/sdr/CA160301026), Mar 1, 2016: SWITCH. FAILED. (CAN) ELT REMOTE SWITCH FAILED TO ACTIVATE THE ELT WHEN SWITCHED TO THE ON POSITION. THE SWITCH WAS RETURNED TO THE ARMED POSITION AND TRIED AGAIN WITH NO ACTIV - [SDR CA151020001](https://openairdocs.org/sdr/CA151020001), Oct 18, 2015: HANDLE. FAILED. (CAN) FLAP HANDLE MATERIAL FAILED JUST FWD OF CABLE ATTACHMENT. THIS IS OUR 3RD FAILURE OF THIS PART ALONG WITH 1 CRACKED AND REMOVED FROM SERVICE. - [SDR CA151020002](https://openairdocs.org/sdr/CA151020002), Oct 18, 2015: HANDLE. FAILED. (CAN) FLAP HANDLE MATERIAL FAILED JUST FWD OF CABLE ATTACHMENT. - [SDR 2015FA0000419](https://openairdocs.org/sdr/2015FA0000419), Sep 1, 2015: CYLINDER HEAD. SEPARATED. SEPARATION OF THE CYLINDER HEAD FROM THE BARREL. PART ID INDICATES THAT THE CYLINDER IS SUBJECT TO AD 2009-26-12, GROUP A REQUIREMENTS. - [SDR CA150106010](https://openairdocs.org/sdr/CA150106010), Jan 5, 2015: FRAME. CRACKED. (CAN) DURING THE DND STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), THE STABILIZER WAS REMOVED AND STRIPPED OF ITS FABRIC AND PAINT. AT THAT POINT A CRACK WAS - [SDR CA130722007](https://openairdocs.org/sdr/CA130722007), Jul 22, 2013: PEDAL. BROKEN. (CAN) THE FRONT RT RUDDER PEDAL BROKE INTO 2 PEICES. THIS RESULTED IN THE REAR PILOT TO BE UNABLE TO ACTIVATE THE RT BRAKE. - [SDR CA120710013](https://openairdocs.org/sdr/CA120710013), Jul 6, 2012: INDICATOR. INACCURATE. (CAN) DURING FUELING PROCEDURES, IT WAS NOTICED BY THE PILOT THAT THE LT FUEL GUAGE WAS READING INACCURATE. A DIP OF THE FUEL TANK CONFIRMED THAT THE FUEL INDIC - [SDR CA110826003](https://openairdocs.org/sdr/CA110826003), Aug 24, 2011: SOLENOID. LOOSE. (CAN) DURING A 100 HR INSPECTION, IT WAS DISCOVERED THAT ONE OF THE TERMINAL ENDS OF THE STARTER SOLENOID THAT IS RIVETED INTO POSITION BECAME LOOSE AND HAD APP - [SDR CA110629004](https://openairdocs.org/sdr/CA110629004), Jun 23, 2011: CYLINDER. CRACKED. DURING THE 100HR INSPECTION, A .5" TO 1" CRACK WAS DISCOVERED COMMING FROM THE LOWER SPARK PLUG HOLE ON NR 4 CYLINDER. CYLINDER WAS REPLACED. THIS ENGINE IS USE - [SDR CA110531006](https://openairdocs.org/sdr/CA110531006), May 26, 2011: CONTROL HANDLE. FAILED. PILOT WAS GOING FROM 2 ND TO 4 TH NOTCH OF FLAP AND THE HANDLE FAILED. TT ON PART 1502 HRS. - [SDR CA110512002](https://openairdocs.org/sdr/CA110512002), May 11, 2011: CYLINDER HEAD. CRACKED. DURING A 100HR INSP, A CRACK WAS DISCOVERED COMING FROM THE LOWER SPARK PLUG HOLE PROCEDING TOWARDS THE EXHAUST VALVE. IT IS COMMON PRACTICE IN THE FACILITY TO - [SDR CA110222006](https://openairdocs.org/sdr/CA110222006), Feb 18, 2011: CRANKSHAFT. CORRODED. (CAN) DURING A COMPANY DIRECTED 2 YEAR INSPECTION OF THE ID OF THE CRANKSHAFT IAW SB 505B, PITTING WAS DISCOVERED AND FOUND TO BE 0.082" DEEP. CRANKSHAFT HAS BE - [SDR CA110222004](https://openairdocs.org/sdr/CA110222004), Feb 15, 2011: CRANKSHAFT. CORRODED. (CAN) THE FRONT PLUG WAS REMOVED FOR A COMPANY DIRECTED 2 YEAR CORROSION INSPECTION OF THE ID OF THE CRANKSHAFT IAW SB 505B. THIS INSPECTION WAS BEING COMPLETED - [SDR CA110204004](https://openairdocs.org/sdr/CA110204004), Feb 3, 2011: REMOTE SWITCH. FAILED. (CAN) DURING A FUNCTION TEST IT WAS DISCOVERED THAT THE LED LIGHT FAILED TO WORK. AS WELL WHEN THE SWITCH WAS TURNED TO THE ON POSITION, THE ELT ACTIVATED PROPE - [SDR CA110204005](https://openairdocs.org/sdr/CA110204005), Feb 3, 2011: REMOTE SWITCH. FAILED. (CAN) DURING THE TROUBLESHOOTING OF ANOTER ELT SYSTEM. IT WAS DISCOVERED THAT THE ELT REMOTE SWITCH WOULD TURN THE ELT ON PROPERLY BUT WOULD NOT RESET THE SYSTE - [SDR CA110225007](https://openairdocs.org/sdr/CA110225007), Jan 11, 2011: CRANKSHAFT. CORRODED. (CAN) DURING A COMPANY DIRECTED 2 YEAR INSPECTION OF THE ID OF THE CRANKSHAFT TO BE COMPLETED IAW SB 505B. DURING THE INSPECTION IT WAS DISCOVERED THAT THE ID W - [SDR CA100816006](https://openairdocs.org/sdr/CA100816006), Aug 10, 2010: BRUSHES. BROKEN. FAA-PMA PART AM-3215 CARBON BRUSH AND SPRING WAS FOUND BROKEN OFF FLUSH WITH THE SPRING AND FELL INTO THE MAGNETO. CONTACT WAS MAINTAINED BY THE REMAINING PART - [SDR CA100816003](https://openairdocs.org/sdr/CA100816003), Aug 9, 2010: MOUNT. CRACKED. (CAN) THE ENGINE MOUNT WAS FOUND CRACKED ON THE LT SIDE ON THE ARM GOING FROM THE FIRE WALL TO THE UPPER LORD MOUNT JUST ABOVE THE WELD LOCATED AT THE FIRE WALL - [SDR CA090225003](https://openairdocs.org/sdr/CA090225003), Feb 24, 2009: TRANSFER TUBE. CRACKED. (CAN) DURING THE REPAIR OF CORROSION PITTING IN THE CRANKSHAFT BORE, A CRACK WAS DISCOVERED COMING FROM THE CUTOUT ON THE OIL TRANSFER TUBE. THE CRACK APPEARS T - [SDR CA090223015](https://openairdocs.org/sdr/CA090223015), Feb 23, 2009: CRANKSHAFT. CORRODED. UPON REMOVAL OF THE EXPANSION PLUG TO FACILITATE SLUG REMOVAL IT WAS DISCOVERED THAT THEIR WAS BUBBLING IN THE PID. BASED UPON PREVIOUS EXPERIENCE WITH THIS PRO - [SDR CA090112002](https://openairdocs.org/sdr/CA090112002), Jan 8, 2009: CRANKSHAFT. CORRODED. (CAN) UPON REMOVAL OF THE EXPANSION PLUG TO FACILITATE SLUG REMOVAL IT WAS DISCOVERED THAT THERE WAS BUBBLING IN THE PID. BASED UPON PREVIOUS EXPERIENCE WITH TH - [SDR CA080806012](https://openairdocs.org/sdr/CA080806012), Aug 1, 2008: CYLINDER HEAD. CRACKED. (CAN) DURING CLIMB OUT WITH GLIDER IN TOW, THE PILOT REPORTED AN ENGINE VIBRATION. THEY IMMEDIATELY INSTRUCTED THE GLIDER TO RELEASE AND THEN PREFORMED A DOWN W - [SDR CA080806013](https://openairdocs.org/sdr/CA080806013), Jul 28, 2008: TIRE. DAMAGED. (CAN) TAIL WHEEL FOUND FLAT DURING TAXI, UPON DISASSEMBLY IT WAS FOUND THAT THE INNER CORDS WERE FOUND LET GO AND CUT THE TUBE. TIRE, BATCH NR WAS EITHER 032167 - [SDR CA080806014](https://openairdocs.org/sdr/CA080806014), Jul 27, 2008: TIRE. DAMAGED. (CAN) TAIL WHEEL FOUND FLAT DURING TAXI, UPON DISASSEMBLY IT WAS FOUND THAT THE INNER CORDS WERE FOUND LET GO AND CUT THE TUBE. TIRE, BATCH NR WAS EITHER 032167 - [SDR CA080123007](https://openairdocs.org/sdr/CA080123007), Jan 15, 2008: FUEL TANK. CRACKED. (CAN) GAS FUMES WERE DETECTED AROUND AC. WHEN RT OB FUEL TANK WAS REMOVED A CRACK WAS FOUND ON A REPAIRED RADIUS OF THE LATERAL RE-ENFORCEMENT INDENT OF THE TAN - [SDR CA080123008](https://openairdocs.org/sdr/CA080123008), Jan 15, 2008: FUEL TANK. CRACKED. (CAN) GAS FUMES WERE DETECTED AROUND AC. WHEN THE RT IB FUEL TANK WAS REMOVED A CRACK WAS FOUND AROUND THE FUEL VENT INTERCONNECT WELD. (TC NR 20080123008) - [SDR CA080111002](https://openairdocs.org/sdr/CA080111002), Jan 7, 2008: HINGE. CRACKED. (CAN) ON INSPECTION, 4 CRACKS FOUND IN CORNERS (TC NR 20080111002) - [SDR CA080111003](https://openairdocs.org/sdr/CA080111003), Jan 2, 2008: HINGE. CRACKED. (CAN) CRACK FOUND DURING SIRP INSP (TC NR 20080111003) - [SDR CA071122004](https://openairdocs.org/sdr/CA071122004), Nov 23, 2007: TANK. CRACKED. (CAN) AIRCRAFT WAS IN FOR A 50 HR INSPECTION. AFTER ENGINE RUN UP, MECHANIC DETECTED GAS FUMES AND LOOKED ON THE RT SIDE ON THE AC WINGS NEAR TRAILING EDGE NOTI - [SDR CA070320006](https://openairdocs.org/sdr/CA070320006), Feb 26, 2007: CONTROL CABLE. FRAYED. (CAN) FLAP CABLE FOUND FRAYED AT ALLUMINUM PULLEY IN LT WING GAP AREA. (TC NR 20070320006) - [SDR CA070320008](https://openairdocs.org/sdr/CA070320008), Feb 26, 2007: CONTROL CABLE. FRAYED. (CAN) FLAP CABLE FOUND FRAYED AT ALLUMINUM PULLEY IN RT WING GAP AREA. (TC NR 20070320008) - [SDR CA070227004](https://openairdocs.org/sdr/CA070227004), Feb 21, 2007: TRANSFER TUBE. LOOSE. (CAN) CRANKSHAFT FWD CAVITY OIL TRANSFER TUBE LOOSE LATERALLY AND ROTATIONALLY. CRANKSHAFT WAS REPAIRED APPROX 500 HOURS AGO. (TC NR 20070227004) - [SDR CA061201004](https://openairdocs.org/sdr/CA061201004), Nov 24, 2006: TANK. CRACKED. (CAN) AIRCRAFT HAD RETURNED TO MAINTENANCE FACILITY FOR WINTER STORAGE. FUEL STAINS WERE NOTICED ON THE BOTTOM OF THE WING NEAR THE TRAILING EDGE. LT IB TANK WA - [SDR CA060424006](https://openairdocs.org/sdr/CA060424006), Apr 24, 2006: SPAR. DAMAGED. 2 HOLES FOR MOUNTING INBD FLAP HINGE BRACKET LWR ATTACH AND INBD BOLT FOR SHIM PLATE BOTH FOUND CRUDELY DRILLED AND VERY OVAL. - [SDR CA060421019](https://openairdocs.org/sdr/CA060421019), Mar 23, 2006: CRANKSHAFT. CORRODED. (CAN) FWD INNER DIA CRANKSHAFT CORRODED BEYOND LIMITS IAW AWD 98-02-08. (TC NR 20060421019) - [SDR CA060421020](https://openairdocs.org/sdr/CA060421020), Mar 23, 2006: CRANKSHAFT. CORRODED. CORROSION FOUND UNDER PID AT FWD ID. - [SDR CA060421021](https://openairdocs.org/sdr/CA060421021), Mar 23, 2006: CRANKSHAFT. CORRODED. CORROSION FOUND UNDER PID FWD ID. - [SDR CA060127006](https://openairdocs.org/sdr/CA060127006), Jan 27, 2006: LANDING GEAR. CRACKED. (CAN) 2 SMALL CRACKS UNDER UPPER RADIUS OF LANDING GEAR. - [SDR CA060124002](https://openairdocs.org/sdr/CA060124002), Jan 20, 2006: RUDDER PEDAL. CRACKED. (CAN) DURING THE COMPANY STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), THE AIRCRAFT RUDDER PEDALS WERE SENT FOR NDT INSPECTION WHERE IT WAS DISCOVERED THAT B - [SDR CA060116006](https://openairdocs.org/sdr/CA060116006), Jan 11, 2006: CRANKSHAFT. CORRODED. THE CRANKSHAFT A/C WAS INSPECTED DUE TO A FAILURE OF A CRANKSHAFT ON ANOTHER AIRCRAFT IN THE FLEET (INTERNAL CORROSION). UPON REMOVAL OF THE FRONT CRANK PLUG AN - [SDR CA051205007](https://openairdocs.org/sdr/CA051205007), Dec 1, 2005: CRANKSHAFT. CORRODED. (CAN) THE CRANKSHAFT OF THIS AIRCRAFT WAS INSPECTED DUE TO A FAILURE OF A CRANKSHAFT OF ANOTHER AIRCRAFT IN THE FLEET (INTERNAL CORROSION). UPON REMOVAL OF THE - [SDR CA051101003](https://openairdocs.org/sdr/CA051101003), Oct 17, 2005: CRANKSHAFT. CORRODED. (CAN) ENGINE WAS REMOVED FROM THE AIRCRAFT AND SENT TO AN OVERHAUL FACILITY FOR AN INSPECTION DUE TO A PROP STRIKE. DURING THE INSPECTION OF THE CRANKSHAFT, IT - [SDR CA050927002](https://openairdocs.org/sdr/CA050927002), Sep 27, 2005: CONTROL CABLE. FRAYED. (CAN) ELEVATOR UP CONTROL CABLED FRAYED AT AFT PULLEY. - [SDR CA050819006](https://openairdocs.org/sdr/CA050819006), Aug 19, 2005: LEAF SPRING. BROKEN. (CAN) MAIN LEAF SPRING BROKEN AT ALIGNMENT DIMPLE. - [SDR CA050819007](https://openairdocs.org/sdr/CA050819007), Aug 19, 2005: CONTROL CABLE. FRAYED. (CAN) RT FLAP WING ROOT CABLE FRAYED AT PULLEY. - [SDR CA050819008](https://openairdocs.org/sdr/CA050819008), Aug 19, 2005: CONTROL CABLE. FRAYED. (CAN) LT RUDDER CABLE FRAYED AT CABIN PULLEY. All 129: https://openairdocs.org/engine/lycoming-o-360-c2e/reports.md ## STCs that may be installed (OpenAirDocs) (36) 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 SE04651CH](https://openairdocs.org/stc/SE04651CH): To allow use of l00R grade aviation fuel meeting Swift Fuel, LLC specification SPEC-l00R-22. Swift Fuels LLC - [STC SE00825WI](https://openairdocs.org/stc/SE00825WI): Installation of Specialty Products Spin-on oil filter on Lycoming Engines. B & C Specialty Products Inc - [STC SE208SO](https://openairdocs.org/stc/SE208SO): Installation of ice indicator in the carburetor. LegacySTC.com. Lists O-360 Series - [STC SE04349CH](https://openairdocs.org/stc/SE04349CH): Installation of SureFly electronic ignition. SureFly Partners Ltd - [STC SE01954SE](https://openairdocs.org/stc/SE01954SE): Installation of engine crankcase seal. Ly-Con Rebuilding Company - [STC SE02352CH](https://openairdocs.org/stc/SE02352CH): Installation of Challenger cleanable oil filter assembly. Challenger Aviation Products Inc - [STC SE00939WI](https://openairdocs.org/stc/SE00939WI): Installation of B&C Specialty Products Model BC 315-( ) Starter on Lycoming engines. B & C Specialty Products Inc - [STC SE2390CE](https://openairdocs.org/stc/SE2390CE): Installation of B & C Speciality Products. B & C Specialty Products Inc. Lists O-360 Series - [STC SE03232CH](https://openairdocs.org/stc/SE03232CH): Installation of Engine Preheat Kit p/n TA2925-1 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 SE4408SW](https://openairdocs.org/stc/SE4408SW): Miscellaneous engine cylinder replacement parts. Continental Motors, Inc. Lists O-360 Series - [STC SE8776SW](https://openairdocs.org/stc/SE8776SW): Installation of coated cylinders and piston rings. Continental Motors, Inc. Lists O-360 Series - [STC SE00218NY](https://openairdocs.org/stc/SE00218NY): Replacement of Lycoming starter with SKY-TEC 12 volt starter installed. Hartzell Engine Technologies, LLC. Lists O-360 Series - [STC SE00226NY](https://openairdocs.org/stc/SE00226NY): Replacement of Lycoming starter with SKY-TEC 24-volt starter Models 149-24HT and 122-24HT. Approval limited to 24-volt DC source available to the starter. Hartzell Engine Technologies, LLC - [STC SE00357NY](https://openairdocs.org/stc/SE00357NY): Replacement of Lycoming starter with SKY-TEC 24-volt starter installed. Hartzell Engine Technologies, LLC. Lists O-360 Series - [STC SE2901NM](https://openairdocs.org/stc/SE2901NM): Lycoming valve cover gasket. Real Gaskets Tennessee - [STC SE02291AT](https://openairdocs.org/stc/SE02291AT): Conversion of the engine from a carburetor fuel system and magneto ignition system to a full authority digital electronic control (FADEC) system for fuel injection and ignition. Continental Motors, Inc - [STC SE01524CH](https://openairdocs.org/stc/SE01524CH): Replace Slick 6000, 6100, 6200, 6300, 4000, 4100, 4200, and 4300 series magnetos and TCM/Bendix S6-20, S6-200, S6-1200, S-20, S-200, and S-1200 series magnetos with Champion Limited Authority Spark Advance Regulator (LASAR ) Model 4755 and 6755 bush kit ignition systems. Champion Aerospace LLC - [STC SE524CH](https://openairdocs.org/stc/SE524CH): Replace Slick 4000, 4100, 4200, and 4300 series magnetos and TCM/Bendix S-20, S-200, and S-1200 series magnetos with the Champion Limited Authority Spark Advance Regulator (LASAR ). Champion Aerospace LLC - [STC SE8193SW](https://openairdocs.org/stc/SE8193SW): Grind nitriden high compression cylinder barrles to plus .010 oversize and install SL75089 P10 piston, SL74242 P10 compression ring, and SL73857 P10 oil ring. Superior Air Parts Inc - [STC SE1779NM](https://openairdocs.org/stc/SE1779NM): Installation of Precise Flight, Inc. 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 SE00889LA](https://openairdocs.org/stc/SE00889LA): Installation of Nickson's cylinder barrels on Lycoming reciprocating engine models. Nickson's Machine Shop Inc - [STC SE2563CE](https://openairdocs.org/stc/SE2563CE): Leaded and unleaded automotive gasoline, 91 minimum antiknock index (RON+MON) /2 per ASTM spec D-439. Intermixing with aviation gasoline also approved. Petersen Aviation Inc - [STC SE1-201](https://openairdocs.org/stc/SE1-201): Installation of the Richter Aero Equipment Type B-4 or B-5 Temperature Probe. (O-360 SERIES (excl. A1C, C2B, C2D)). MidContinent Instru Co Inc. Lists O-360 Series - [STC SE09492SC](https://openairdocs.org/stc/SE09492SC): Installation and usage of Exxon 20W50 multigrade aircraft engine oil conforming to Exxon Oil formulation WS-3013. Exxon Company USA. Lists O-360 Series - [STC SE00350SE](https://openairdocs.org/stc/SE00350SE): Installation of sump mounted chip detector. Aviation Development Corporation - [STC SE8023SW](https://openairdocs.org/stc/SE8023SW): Installation and usage of AEROSHELL. Shell Development Co. Lists O-360 Series - [STC SE370NE](https://openairdocs.org/stc/SE370NE): Installation of 'Auto-Vac 2' auxiliary vacuum system. Raymond Ives - [STC SE452NE](https://openairdocs.org/stc/SE452NE): Installation and usage of 'Mobil AV 1' aviation oil. Mobil Research & Development Corp. Lists O-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 O-360 Series - [STC SE5924SW](https://openairdocs.org/stc/SE5924SW): Installation of stainless steel replacement exhaust studs on AVCO engines. Perrigo & Steele Aircraft Engr Company. Lists O-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 O-360 Series - [STC SE80NE](https://openairdocs.org/stc/SE80NE): Installation and usage of Bel-Ray synthetic aviation oil, Bel-Ray Aero 1, (nonsupercharged), horizontally opposed direct drive, aircraft engines of 350 hp. or less. Bel-Ray Company, Inc. Lists O-360 Series - [STC SE128NE](https://openairdocs.org/stc/SE128NE): Use of AMS/OIL 15W 50 synthetic piston aircraft oil in Avco engines. AMS/OIL. Lists O-360 Series --- 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.