# Continental LTSIO-360-EB

- Type: Engine model (FAA registry)
- Registry code: 17290
- Manufacturer (registry): CONT MOTOR
- Model: LTSIO-360-EB
- Engine type: Reciprocating
- Power: 200 hp
- Data sheet: [TCDS E9CE](https://openairdocs.org/tcds/E9CE) (OpenAirDocs)
- Holder: Continental Aerospace Technologies, Inc.
- Installed in: 4 registered aircraft
- Page: https://openairdocs.org/engine/continental-ltsio-360-eb

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 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 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 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 95-08-10](https://openairdocs.org/ad/95-08-10): Oil Outlet Check Valve · Continental Motors LTSIO-360-E, LTSIO-360-EB, LTSIO-360-KB and 9 more. Effective Jul 10, 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 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 81-23-02](https://openairdocs.org/ad/81-23-02): Oil Filter Adapter Gasket · Continental Motors LTSIO-360-EB, LTSIO-360-KB, TSIO-360-EB and 2 more

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 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) (6)

- [SAIB NE-20-05](https://openairdocs.org/saib/NE-20-05): POWERPLANT - Engine Camshaft Gear Tooth Fracture. Issued Apr 6, 2020
- [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 NE-09-04](https://openairdocs.org/saib/NE-09-04): Fuel Control/Reciprocating Engines. Issued Jan 10, 2009

## Registered aircraft (4)

- [N14JN](https://openairdocs.org/aircraft/N14JN): [National Test Pilot School](https://openairdocs.org/faa-owner/NATIONAL%20TEST%20PILOT%20SCHOOL), [Mojave, CA](https://openairdocs.org/faa-place/CA/Mojave), built 1975, S/N 34-7570254
- [N234FY](https://openairdocs.org/aircraft/N234FY): [Vee Two Inc](https://openairdocs.org/faa-owner/VEE%20TWO%20INC), [Merritt Island, FL](https://openairdocs.org/faa-place/FL/Merritt%20Island), built 1978, S/N 347870428
- [N37PF](https://openairdocs.org/aircraft/N37PF): [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 1980, S/N 34-8070359
- [N912LL](https://openairdocs.org/aircraft/N912LL): [Legacy Air LLC](https://openairdocs.org/faa-owner/LEGACY%20AIR%20LLC), [Cadillac, MI](https://openairdocs.org/faa-place/MI/Cadillac), built 1978, S/N 34-7870020

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports (1)

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 19961224044549I](https://openairdocs.org/incident/19961224044549I), Dec 24, 1996: Piper PA34200T (N14JN), Seattle, WA, Minor damage. Narrative: upon clearing runway 34R, right engine propeller came in contact with taxiway light, half way up propeller blade. PIC stated that rainy conditions…

## Service difficulty reports (45)

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

- [SDR GAJA2016F00164](https://openairdocs.org/sdr/GAJA2016F00164), Jul 22, 2016: ACTUATOR. LEAKING. LANDING GEAR UNSAFE LIGHT ILLUMINATED IN FLIGHT. PERFORMED EMERGENCY LANDING GEAR EXTENSION PROCEDURES LANDING GEAR WENT DOWN AND LOCKED. LANDED SAFE AND OBSERV
- [SDR CA160222009](https://openairdocs.org/sdr/CA160222009), Feb 19, 2016: FUEL CONTROL. MALFUNCTIONED. (CAN) DURING CRUISE FLIGHT, THE PILOT NOTED THAT THE RH ENGINE FUEL FLOW WAS LOW AND THE EGT WAS HIGH AT FULL RICH MIXTURE SETTING. THE FUEL SERVO WAS REMOVED A
- [SDR CA151002007](https://openairdocs.org/sdr/CA151002007), Sep 30, 2015: CYLINDER. DAMAGED. (CAN) FUEL PUMP SET UP IAW SID97-3F. AFTER GROUND ADJUSTMENTS, ENGINE PERFORMED WELL AND WITHIN LIMITS EXCEPT THAT AT ALTITUDE, THE FUEL FLOW COULD NOT BE OBTAI
- [SDR CA150916016](https://openairdocs.org/sdr/CA150916016), Sep 8, 2015: DISPLAY. FAILED. (CAN) PRIMARY FLIGHT DISPLAY`S ATTITUDE DISPLAY FAILED DURING FLIGHT. AFTER FAILURE, UPON GROUND TESTING THE PFD, IT WAS NOTICED TO HAVE ERRONEOUS AND WANDERING
- [SDR CA150721004](https://openairdocs.org/sdr/CA150721004), Jul 16, 2015: BRACKET. BROKEN. (CAN) LEFT MLG DOWN LOCK SPRING BRACKET FOUND BROKEN DURING WALK AROUND.
- [SDR CA150316010](https://openairdocs.org/sdr/CA150316010), Mar 11, 2015: ACTUATOR. BROKEN. (CAN) NOSE GEAR ACTUATOR BROKE AT AFT ATTACH END.
- [SDR CA130923015](https://openairdocs.org/sdr/CA130923015), Sep 19, 2013: TRUNNION. LOOSE. (CAN) RT MAIN GEAR FORWARD TRUNNION ATTACH BOLTS FOUND LOOSE. BOLTS REPLACED WITH NEW AND TORQUED.
- [SDR CA130118007](https://openairdocs.org/sdr/CA130118007), Jan 16, 2013: DRIVE ASSY. SLIPPED. (CAN) LT ENGINE ALTERNATOR DRIVE COUPLING FOUND TO BE SLIPPING.
- [SDR 2013FA0000068](https://openairdocs.org/sdr/2013FA0000068), Dec 19, 2012: GEAR. OUT OF TOLERANCE. UPON REMOVAL OF STARTER ADAPTOR FOR REPAIR DUE TO SLIPPAGE, IT WAS FOUND THA THE SCAVENGER PUMP HAD OUT OF TOLERANCE IMPESSER GEARS, PITTING AND CORROSION. ALSO
- [SDR CA121203007](https://openairdocs.org/sdr/CA121203007), Nov 27, 2012: WHEEL HALF. CRACKED. (CAN) RIGHT INNER WHEEL HALF FOUND CRACKED AND RUBBING ON THE BRAKE BACK-PLATE. CRACK WAS ABOUT .1250" WIDE AND 4" LONG. WRONG PN FOUND INSTALLED IAW PARTS MANU
- [SDR CA121119012](https://openairdocs.org/sdr/CA121119012), Nov 19, 2012: OIL FILTER. MISMANUFACTURED. (CAN) ONE OF THE END CAPS THAT HOLD THE PAPER FILTER WAS NOT CRIMPED LIKE THE OTHER END WHEN THE FILTER WAS CUT FOR EXAMINATION DURING ROUTINE MAINTENANCE AND I
- [SDR CA120430008](https://openairdocs.org/sdr/CA120430008), Mar 19, 2012: TIRE. FLAT. (CAN) NOSE TIRE WENT FLAT DURING TAXI.
- [SDR CA111107004](https://openairdocs.org/sdr/CA111107004), Nov 1, 2011: MASTER SWITCH. UNSERVICEABLE. (CAN) MASTER SWITCH WILL NOT SHUTOFF WHEN SET TO OFF POSITION. SWITCH VERY DIFFICULT TO MOVE TO ON OR OFF POSITION. SWITCH R & R WITH NEW. SWITCH OPENED UP, FOU
- [SDR KRTR200110223001](https://openairdocs.org/sdr/KRTR200110223001), Jan 25, 2011: ENGINE. MISOVERHAULED. DURING REPLACEMENT OF THE STARTER ADAPTER, P/N 635048A16. NOTICED THAT THE CRANKSHAFT GEAR LOCATED AT THE AFT END OF THE CRANSHAFT DID NOT HAVE SAFETY WIRE ON T
- [SDR CA101110008](https://openairdocs.org/sdr/CA101110008), Nov 5, 2010: LATCH. BENT. (CAN) PILOT’S REPORT -- NOSE BAGGAGE DOOR HANDLE/LOCKING SYSTEM SHOULD NOT ALLOW THE KEY TO BE REMOVED, UNLESS THE HANDLE IS IN THE CLOSED POSITION - THIS IS DE
- [SDR CA091203005](https://openairdocs.org/sdr/CA091203005), Nov 24, 2009: ALTERNATOR. FAILED. (CAN) RT ALTERNATOR QUIT FUNCTIONING DURING FLIGHT.
- [SDR CA091027003](https://openairdocs.org/sdr/CA091027003), Sep 30, 2009: COUPLING. FAILED. (CAN) ON FINAL APROACH FOR LANDING IN IFR CONDITIONS, THE PILOT LOST ALL ELECTRICAL POWER. PILOT INITIATED A "GO AROUND" AND LANDED AT A VFR AIRPORT NEARBY. (TC
- [SDR FFKA141](https://openairdocs.org/sdr/FFKA141), Sep 24, 2009: TURBOCHARGER. LEAKING. AFTER INSTALLING AN O/H TURBOCHARGER, SN TR0109050, 1 HOUR OF FLIGHT TIME WAS PUT ON PART, AFTER SEVERAL DAYS OF OTHER UNRELATED MX AND WAITING FOR VFR WEATHER,
- [SDR VOX2009F00000](https://openairdocs.org/sdr/VOX2009F00000), Dec 26, 2008: BOLT. BROKEN. NR 3 CYL INTAKE ROCKER ARM RETAIN BOLTS BROKEN.
- [SDR FFKA127](https://openairdocs.org/sdr/FFKA127), Mar 27, 2008: CYLINDER. FAILED. DURING CRUISE FLIGHT, THE PILOT NOTICED THAT THE MANIFOLD PRESSURE ON THE RIGHT ENGINE WAS CREEPING LOWER AND LOWER, PILOT COMPENSATED BY ADVANCING RIGHT ENGINE
- [SDR FFKA123](https://openairdocs.org/sdr/FFKA123), Dec 17, 2007: PISTON. BURNED. PILOT REPORTED A LOSS OF POWER ON THE RT ENGINE AND DECLARED AN EMERGENCY. MAINTENANCE PERFORMED A COMPRESSION CHECK ON THE CYLINDERS AND FOUND ZERO PRESSURE ON
- [SDR TVD2006F00001](https://openairdocs.org/sdr/TVD2006F00001), Oct 30, 2006: MOTOR. FAILED. LANDING GEAR FAILED TO FULLY RETRACT. FOUND ELECTRIC MOTOR ON HYDRAULIC POWERPACK FAILED. REPLACED POWER PACK AND LANDING GEAR FUNCTIONED PROPERLY. (K)
- [SDR 2005FA0001116](https://openairdocs.org/sdr/2005FA0001116), Aug 10, 2005: REGULATOR VALVE. RUPTURED. UPON RUN UP, PILOT CYCLED BOOTS. BOOT CYCLE STATUS LIGHT CAME ON BUT EXTINGUISHED BEFORE 6 SECOND INFLATION CYCLE TIMED OUT. (PRESS TO TEST SHOWED LAMP OK). BOO
- [SDR 2005FA0001117](https://openairdocs.org/sdr/2005FA0001117), Aug 10, 2005: REGULATOR VALVE. RUPTURED. UPON RUN UP, PILOT CYCLED BOOTS. BOOT CYCLE STATUS LIGHT CAME ON BUT EXTINGUISHED BEFORE 6 SECOND INFLATION CYCLE TIMED OUT. (PRESS TO TEST SHOWED LAMP OK) BOOT
- [SDR 101](https://openairdocs.org/sdr/101), Mar 28, 2005: PUMP. INOPERATIVE. PILOT SQUAWKED THAT THE FUEL FLOW FOR THE RIGHT ENGINE WAS LOW AND ERRATIC IN-FLIGHT. MAINTENANCE INSPECTED AND TRIED TO ADJUST THE FUEL SYSTEM, REPLACED FUEL P
- [SDR 100](https://openairdocs.org/sdr/100), Mar 16, 2005: PUMP. INOPERATIVE. INSTALLED A FACTORY REMANUFACTURED ENGINE FROM CONTINENTAL THAT CAME WITH A NEW FUEL PUMP. UPON DOING THE ENGINE GROUND RUNS AND INITIAL ENGINE SET UP THE FUEL 
- [SDR 2005FA0000255](https://openairdocs.org/sdr/2005FA0000255), Jan 21, 2005: FITTING. SHEARED. AIRCRAFT WAS IN CRUISE FLIGHT WHEN IT EXPERIENCED AN IMMEDIATE ENGINE FAILURE ON THE RIGHT ENGINE, PILOT COULD NOT RESTART ENGINE. AFTER LANDING MAINTENANCE REP
- [SDR CA040921006](https://openairdocs.org/sdr/CA040921006), Aug 27, 2004: BEARING. DESTROYED. (CAN) PILOT REPORTED MINOR DIFFICULTY IN MAINTAINING A CONSTANT: RPM SELECTION, RPM WOULD WANDER +/- 50 RPM (RT SIDE. PROPS NEW. CONTROL LINKAGE AND GOVERNORS I
- [SDR CA040720002](https://openairdocs.org/sdr/CA040720002), Jul 13, 2004: SPAR. WORN. DURNG 100 HOURS INSPECTION, RT WING REAR SPAR ATTACHMENT BOLT P/N NAS464P6LA6 FOUND LOOSE. BOLT WAS REMOVED AND FOUND SEVERLY DAMAGED (DEFORMED) AND BOTH SPAR F
- [SDR 2004FA0000277](https://openairdocs.org/sdr/2004FA0000277), Feb 24, 2004: CYLINDER. LEAKING. VALVE COVER GASKETS ON RT ENGINE WERE SEEPING. PROCEEDED TO CHANGE GASKETS ON NR 1 CYLINDER AND DISCOVERED THE LOCKING SAFETY FOR THE NUTS ON THE VALVE ROCKER A
- [SDR ZKG2003F00001](https://openairdocs.org/sdr/ZKG2003F00001), Feb 24, 2003: CYLINDER. SEPARATED. IN CRUSE FLIGHT ENGINE LOST POWER, OIL PRESSURE WAS DECREASING, PILOT SHUT ENGINE DOWN AND LANDED WITH NO TROUBLE UPON INSPECTION, FOUND NR 2 CYLINDER OFF OF CA
- [SDR 2002FA0000230](https://openairdocs.org/sdr/2002FA0000230), Jan 10, 2002: PUSHROD. CRACKED. ON ANNUAL INSPECTION OF THE LT ENGINE (TOTAL TIME 3197.9) THREE PUSH RODS WERE NOTED TO BE CRACKED ALONG ALMOST THE ENTIRE LENGTH OF THE PUSHRODS EXTENDING FROM
- [SDR CTU2002F00000](https://openairdocs.org/sdr/CTU2002F00000), Dec 13, 2001: REGULATOR. LEAKING. HEATER FUEL REGULATOR INSPECTED IAW AD, FOUND TO BE LEAKING.
- [SDR CTU2002F00002](https://openairdocs.org/sdr/CTU2002F00002), Dec 13, 2001: REGULATOR. LEAKING. HEATER FUEL REGULATOR INSPECTED IAW AD FOUND TO BE LEAKING.
- [SDR WD42002F00001](https://openairdocs.org/sdr/WD42002F00001), Sep 21, 2001: TUBE. CORRODED. SHORTLY AFTER AIRCRAFT DEPARTURE, THE PILOT SMELLED HYDRAULIC FLUID IN COCKPIT. DECISION WAS MADE TO DIVERT BACK TO AIRPORT. WHEN CYCLING GEAR DOWN, AN UNSAFE C
- [SDR 20001031SH017](https://openairdocs.org/sdr/20001031SH017), Sep 25, 2000: SPRING. BROKEN. PILOT REPORTED THAT OIL PSI WAS LOW AS HE REDUCED POWER FOR LANDING. THE SPRING BROKE DUE TO RUBBING ON THE INSIDE OF THE RELIEF VALVE PISTON. (X)
- [SDR 20001018SH012](https://openairdocs.org/sdr/20001018SH012), Sep 15, 2000: SERVO. DEFECTIVE. THROTTLE HARD TO MORE IN-FLIGHT, SERVO REMOVED AND A NEW ONE INSTALLED. OVER FOUR POUNDS TO MOVE CONTROL. (X)
- [SDR 98ZZZX3876](https://openairdocs.org/sdr/98ZZZX3876), Jul 17, 1998: CYLINDER. CRACKED. PILOT STATED IN CRUISE, THE RT ENGINE STARTED RUNNING SLIGHTLY ROUGH. AFTER A CHECK OF THE ENGINE GAUGES, PILOT NOTED A SLIGHT DROP IN THE MANIFOLD PRESSURE FOL
- [SDR 98ZZZX136](https://openairdocs.org/sdr/98ZZZX136), Dec 22, 1997: STUD. SHEARED. NOTICED BASE NUT AND PART OF STUD MISSING ON TOP REAR STUD LOCATION OF NR 1 CYLINDER. NUT HAD COME OFF OTHER END OF STUD. STUD HAD FAILED AT CYLINDER BASE FLANG
- [SDR 97ZZZX4149](https://openairdocs.org/sdr/97ZZZX4149), Sep 5, 1997: ADAPTER. BROKEN. TACHOMETER DRIVE ADAPTER IS A 90-DEGREE DRIVE THAT REVERSES OUTPUT ROTATION AND ANGLE OF OUTPUT FROM ENGINE TO DRIVE TACHOMETER SHAFT. FOUND MOUNTING NUT AND FL
- [SDR 97ZZZX2871](https://openairdocs.org/sdr/97ZZZX2871), May 28, 1997: BEARING. LOOSE. DRIVE END BEARING INNER RACE BECAME LOOSE ON SHAFT CAUSING OIL TO LEAK THOUGH SEAL. MAG HAD AN EXTREME AMOUNT OF OIL INTERNALLY AND STILL RAN NORMALLY.
- [SDR BIER970040](https://openairdocs.org/sdr/BIER970040), Jan 23, 1997: SEALING LIP. ERODED. DURING UNRELATED MAINTENANCE, FOUND SEALING LIP THAT HELPS SEAL THE TURBINE HOUSING TO THE TURBOCHARGER CENTER SECTION ERODED AWAY AND THE GASKET PARTIALY BLOWN
- [SDR 96ZZZX5263](https://openairdocs.org/sdr/96ZZZX5263), Sep 27, 1996: DISTRIBUTOR BLOC. OVERHEAT. DISTRIBUTOR BLOCK AND DISTRIBUTOR GEAR HAD EXCESSIVE HEAT BUILD-UP AND MELTING OF GEAR POSSIBLY DUE TO LACK OF SUFFICIENT CLEARANCE DURING MANUFACTURE OR IMPROP
- [SDR 95ZZZX3130](https://openairdocs.org/sdr/95ZZZX3130), May 16, 1995: PUMP. SEAL LEAK. ON 2-21-95, THE RIGHT ENGINE DEVELOPED A SURGE ON F.F. AND M.A.P. DURING CRUISE. AFTER TROUBLESHOOTING, DISCOVERED ANEROID SEAL HAD FAILED. THE PUMP WAS REPAIRE
- [SDR 95ZZZX604](https://openairdocs.org/sdr/95ZZZX604), Jan 8, 1995: ENGINE. MALFUNCTIONED. VFR FROM MARSHALLTOWN TO DSM. RT ENGINE QUIT, PILOT WENT THROUGH THE CHECK LIST AND FEATHERED THE ENGINE. THE FUEL SELECTOR COULD NOT MOVE. THE A/C HAD BEEN STO

## STCs that may be installed (OpenAirDocs) (22)

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 LTSIO-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 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 SE1796NM](https://openairdocs.org/stc/SE1796NM): Conversion of the Continental TSIO-360-EB and LTSIO-360-EB engines (200 HP-2575 RPM) to the operating limits of the *(-KB) engine. Turboplus Aircraft Systems, Inc
- [STC SE4177NM](https://openairdocs.org/stc/SE4177NM): Installation of a pressurized magneto system for Bendix Models S6RN-25 and S6LN-25, or Slick Models 6214 (6210 for LTSIO) or Model 6224 (6220 for LTSIO). Turboplus Aircraft Systems, Inc
- [STC SE4303NM](https://openairdocs.org/stc/SE4303NM): Installation of a magneto pressurization kit assembly and associated system for Bendix Models S6RN-25 and S6LN-25, or SLICK Models 6214 (6210 for LTSIO) or Model 6224 (6220 for LTSIO). Turboplus Aircraft Systems, Inc
- [STC SE8776SW](https://openairdocs.org/stc/SE8776SW): Installation of coated cylinders and piston rings. Continental Motors, Inc
- [STC SE02598CH](https://openairdocs.org/stc/SE02598CH): ONE ONLY STC; S/Ns 807783-R and 818341-R: Installation of AIR BP piston engine lubricating oil MDM100-QB2050AD-01 in Teledyne Continental Motors model TSIO-360-EB and LTSIO-360-EB horizontally opposed reciprocating engines. Air BP Lubricant
- [STC SE624GL](https://openairdocs.org/stc/SE624GL): Incorporation of a 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 LTSIO-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
- [STC SE4731NM](https://openairdocs.org/stc/SE4731NM): Replace fixed wastegate with a turbocharger differential pressure control system. Merlyn Products Inc
- [STC SE452NE](https://openairdocs.org/stc/SE452NE): Installation and usage of 'Mobil AV 1' aviation oil. Mobil Research & Development Corp. Lists LTSIO-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 LTSIO-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 LTSIO-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 LTSIO-360 Series

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