# Lycoming I0-360 series

- Type: Engine model (FAA registry)
- Registry code: 41558
- Manufacturer (registry): LYCOMING
- Model: I0-360 SER
- Engine type: Turbo-shaft
- Power: 200 hp
- Data sheet: [TCDS 1E10](https://openairdocs.org/tcds/1E10) (OpenAirDocs)
- Holder: Lycoming Engines
- Installed in: 7 registered aircraft
- Page: https://openairdocs.org/engine/lycoming-i0-360-series

The registry names only the engine series, so ADs for every model in the series are matched.

## 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 2022-16-03](https://openairdocs.org/ad/2022-16-03): Engine (RECIPROCATING) · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-F and 236 more. Effective Aug 15, 2022
- [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 2015-19-07](https://openairdocs.org/ad/2015-19-07): Fuel injector fuel lines · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 187 more. Effective Nov 3, 2015
- [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 2012-03-06](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 2010-07-08](https://openairdocs.org/ad/2010-07-08): Turbochargers · Kelly Aerospace Energy Systems HIO-360-E1AD, HIO-360-E1BD, HIO-360-F1AD and 137 more. Effective Apr 19, 2010
- [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 2009-02-03](https://openairdocs.org/ad/2009-02-03): Fuel injection servos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 261 more. Effective Feb 9, 2009
- [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 2006-06-16](https://openairdocs.org/ad/2006-06-16): Crankshaft · Lycoming Engines AEIO-360-A1B6, AEIO-360-A1E6, IO-360-A1B6 and 18 more. Effective Apr 27, 2006
- [AD 2005-19-11](https://openairdocs.org/ad/2005-19-11): Crankshafts · Lycoming Engines AEIO-360-A1B6, AEIO-360-A1E6, AEIO-540-D4A5 and 59 more. Effective Oct 21, 2005
- [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 2003-14-03](https://openairdocs.org/ad/2003-14-03): Rotary fuel pumps · Lycoming Engines AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 262 more. Effective Aug 14, 2003
- [AD 2002-12-07](https://openairdocs.org/ad/2002-12-07): Oil Filter Converter Plate Gasket or the Converter Plate Kit · Lycoming Engines HIO-360-E1AD, HIO-360-E1BD, HIO-360-F1AD and 95 more. Effective Jul 3, 2002
- [AD 98-17-11](https://openairdocs.org/ad/98-17-11): Crankshafts · Continental Motors A-65-3, A-65-8, A75-8 and 90 more. Effective Oct 19, 1998
- [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 96-23-03](https://openairdocs.org/ad/96-23-03): High pressure fuel pumps · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 174 more. Effective Dec 23, 1996
- [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 95-26-02](https://openairdocs.org/ad/95-26-02): Aviation Gasoline · Lycoming Engines IO-320-B1A, IO-320-B1B, IO-320-B1C and 182 more. Effective Jan 24, 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 93-14-15](https://openairdocs.org/ad/93-14-15): Instrument Panel Placard, · Lycoming Engines IO-360-A1B6D and IO-360-A3B6D with STC SA4758NM or SE4757NM. Effective Aug 23, 1993
- [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 79-04-05](https://openairdocs.org/ad/79-04-05): Regulator Diaphragm Stem Assembly · Lycoming Engines AEIO-320-D1B, AEIO-320-E1A, AEIO-320-E1B and 215 more. Effective Sep 26, 1979
- [AD 78-23-10](https://openairdocs.org/ad/78-23-10): Center Body Bellows Seal Assembly · Lycoming Engines AEIO-320-D1B, AEIO-320-E1A, AEIO-320-E1B and 218 more. Effective Nov 7, 1978
- [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 73-23-01](https://openairdocs.org/ad/73-23-01): Piston Pin Assembly · Lycoming Engines AIO-360-A1A, AIO-360-A1B, AIO-360-A2A and 215 more. Effective Jan 13, 1977
- [AD 75-09-15](https://openairdocs.org/ad/75-09-15): Fuel Starvation To The Engine · Lycoming Engines AIO-320-A1A, AIO-320-A1B, AIO-320-A2A and 130 more. Effective Apr 30, 1975
- [AD 73-10-02](https://openairdocs.org/ad/73-10-02): Bendix Fuel Injectors · Bendix Fuel Injectors, AIO-320-A1A, AIO-320-A1B and 88 more. Effective May 16, 1973
- [AD 71-05-02](https://openairdocs.org/ad/71-05-02): Crankcase Main Bearings · Lycoming Engines IO-360-A1A, IO-360-A1B, IO-360-A1B6 and 9 more. Effective Feb 13, 1973
- [AD 71-11-02](https://openairdocs.org/ad/71-11-02): Intake and Exhaust Hydraulic Tappet Plunger Assembly · Lycoming Engines IO-360-A1A, IO-360-A1B, IO-360-A1B6 and 9 more. Effective Mar 14, 1972
- [AD 66-06-03](https://openairdocs.org/ad/66-06-03): Connecting Rod Assemblies · Lycoming Engines GO-435-C2 (O-435-17), GO-435-C2A, GO-435-C2A2 and 317 more. Effective Jan 16, 1969
- [AD 67-22-06](https://openairdocs.org/ad/67-22-06): Fuel Injectors · Lycoming Engines HIO-360-A1A, HIO-360-B1A, HIO-360-B1B and 28 more. Effective Aug 9, 1967
- [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 66-20-04](https://openairdocs.org/ad/66-20-04): Oil Filter Adapter Gasket · Lycoming Engines IO-320-A1A, IO-320-A2A, IO-320-B1A and 121 more. Effective Aug 27, 1966
- [AD 64-16-05](https://openairdocs.org/ad/64-16-05): AC Pumps · Lycoming Engines HIO-360-B1A, HIO-360-B1B, IO-320-B1A and 86 more. Effective Jul 10, 1964

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 2011-26-04](https://openairdocs.org/ad/2011-26-04) (historical): Externally mounted fuel injector fuel lines · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 186 more. Effective Jan 25, 2012
- [AD 2011-15-10](https://openairdocs.org/ad/2011-15-10) (historical): Fuel servos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 256 more. Effective Aug 16, 2011
- [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 2008-14-07](https://openairdocs.org/ad/2008-14-07) (historical): Externally mounted fuel injector fuel lines · Textron Lycoming, AVCO AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 185 more. Effective Aug 14, 2008
- [AD 2008-08-14](https://openairdocs.org/ad/2008-08-14) (historical): Fuel injection servo plugs · Superior Air Parts AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 242 more. Effective Apr 29, 2008
- [AD 2008-06-51](https://openairdocs.org/ad/2008-06-51) (historical): Fuel injection servo plugs · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 235 more
- [AD 2006-20-09](https://openairdocs.org/ad/2006-20-09) (historical): Certain crankshafts replacing · Lycoming Engines AEIO-360-A1B6, AEIO-360-A1E6, AEIO-540-D4A5 and 82 more. Effective Nov 3, 2006
- [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 2002-26-01](https://openairdocs.org/ad/2002-26-01) (historical): Fuel injector fuel lines · Textron Lycoming, AVCO IGO-480-A1B6, IGO-540-B1A, IGO-540-B1C and 178 more. Effective Jan 31, 2003
- [AD 2000-18-53](https://openairdocs.org/ad/2000-18-53) (historical): Oil Filter Converter Plate Gaskets · Textron Lycoming, AVCO AEIO-540, IO-360-A1B6D, IO-360-A1D6D and 73 more
- [AD 98-18-12](https://openairdocs.org/ad/98-18-12) (historical): Fuel Pump · Textron Lycoming, AVCO AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 249 more. Effective Sep 28, 1998
- [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) (14)

- [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-08-26R3](https://openairdocs.org/saib/NE-08-26R3): Magneto/Distributor. Issued Mar 31, 2011
- [SAIB NE-08-26R2](https://openairdocs.org/saib/NE-08-26R2) (historical): Magneto/Distributor. Issued Apr 22, 2010
- [SAIB NE-09-04](https://openairdocs.org/saib/NE-09-04): Fuel Control/Reciprocating Engines. Issued Jan 10, 2009
- [SAIB NE-06-32R1](https://openairdocs.org/saib/NE-06-32R1): Reciprocating Engine - Crankshaft. Issued Sep 10, 2008
- [SAIB NE-08-26R1](https://openairdocs.org/saib/NE-08-26R1) (historical): Dual Magnetos. Issued Jul 8, 2008
- [SAIB NE-08-32](https://openairdocs.org/saib/NE-08-32) (historical): Propeller Governor Set Screw. Issued Jul 3, 2008
- [SAIB NE-05-89](https://openairdocs.org/saib/NE-05-89): . Issued Sep 30, 2005
- [SAIB NE-05-40](https://openairdocs.org/saib/NE-05-40): . Issued Mar 18, 2005
- [SAIB NE-03-18](https://openairdocs.org/saib/NE-03-18): . Issued Jan 22, 2003
- [SAIB NE-01-22](https://openairdocs.org/saib/NE-01-22): . Issued May 11, 2001

## Registered aircraft (7)

- [N18NG](https://openairdocs.org/aircraft/N18NG): [Gaar John L](https://openairdocs.org/faa-owner/GAAR%20JOHN%20L), [Leawood, KS](https://openairdocs.org/faa-place/KS/Leawood), built 1998, S/N 1
- [N3235B](https://openairdocs.org/aircraft/N3235B): [Hbhis LLC](https://openairdocs.org/faa-owner/HBHIS%20LLC), [Gnadenhutten, OH](https://openairdocs.org/faa-place/OH/Gnadenhutten), S/N 1010
- [N36CE](https://openairdocs.org/aircraft/N36CE): [Hawkes Delray](https://openairdocs.org/faa-owner/HAWKES%20DELRAY), [Sequim, WA](https://openairdocs.org/faa-place/WA/Sequim), built 1982, S/N 24-1321
- [N377JD](https://openairdocs.org/aircraft/N377JD): [Styer David](https://openairdocs.org/faa-owner/STYER%20DAVID), [Milton Freewater, OR](https://openairdocs.org/faa-place/OR/Milton%20Freewater), S/N 2007
- [N4200](https://openairdocs.org/aircraft/N4200): [Burdick Rich](https://openairdocs.org/faa-owner/BURDICK%20RICH), [Montrose, CO](https://openairdocs.org/faa-place/CO/Montrose), built 1975, S/N 674
- [N62VA](https://openairdocs.org/aircraft/N62VA): [Tiger 17 LLC](https://openairdocs.org/faa-owner/TIGER%2017%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1997, S/N 2081
- [N92DA](https://openairdocs.org/aircraft/N92DA): [Delory Dana E](https://openairdocs.org/faa-owner/DELORY%20DANA%20E), [Shoreacres, TX](https://openairdocs.org/faa-place/TX/Shoreacres), built 1992, S/N 28-37057

## NTSB investigations (4)

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 FTW96LA381](https://openairdocs.org/ntsb/FTW96LA381), Sep 7, 1996: Mooney M20J (N311SM), Biscoe, AR, destroyed. Probable cause: Binding of the flight control system for an undetermined reason.
- [NTSB SEA92LA073](https://openairdocs.org/ntsb/SEA92LA073), Apr 11, 1992: Enstrom 280 FX (N377JD), Mount Vernon, WA, substantial damage. Probable cause: A HARD LANDING BY THE PILOT, AFTER A POWER LOSS DUE TO FUEL EXHAUSTION.
- [NTSB NYC90LA090](https://openairdocs.org/ntsb/NYC90LA090), Apr 22, 1990: Enstrom 280 (N493H), Thornton, PA, substantial damage. Probable cause: FAILURE TO ATTAIN A PROPER CLIMB RATE AFTER TAKEOFF FROM A CONFINED AREA. FACTORS INCLUDE GUSTY WINDS AND HIGH OBSTRUCTIONS.
- [NTSB DEN76AD040](https://openairdocs.org/ntsb/DEN76AD040), Mar 14, 1976: Hiller Acft UH-12E (N67159), Bluff, UT, destroyed

## FAA accident and incident reports (7)

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 20020603012909I](https://openairdocs.org/incident/20020603012909I), Jun 3, 2002: Enstrm 280FX (N377JD), Snoqualmie, WA, Minor damage. (-23) The aircraft rolled on its side after landing on an uneven surface.
- [Incident 19990103005809I](https://openairdocs.org/incident/19990103005809I), Jan 3, 1999: Piper PA28R201 (N92DA), Longview, TX, Minor damage. (-5)Pilot took-off and flew with alternator switch off, lost battery power. On approach, gear would not extend using normal procedure. Pilot confused if…
- [Accident 19960907026719A](https://openairdocs.org/incident/19960907026719A), Sep 7, 1996: Mooney M20J (N311SM), Biscoe, AR, Substantial damage. Flight control problems in flight, rolled left, nose dropped, emergency landing in bean field, struck trees, burned (-23) on September 7, 1996, at 1259 central…
- [Accident 19920411035179A](https://openairdocs.org/incident/19920411035179A), Apr 11, 1992: Enstrm 280FX (N377JD), Mount Vernon, WA, Substantial damage. Engine quit on sightseeing flight. Autorotated but rocked forward on landing. Used aft cylic. Rotors chopped boom.
- [Accident 19900422011739A](https://openairdocs.org/incident/19900422011739A), Apr 22, 1990: Enstrm 280 (N493H), Thornton, PA, Substantial damage. Departing a confined Private helipad,struck trees. Gusty wind and near gross weight contributed.
- [Incident 19801014074119I](https://openairdocs.org/incident/19801014074119I), Oct 14, 1980: Enstrm 280 (N88HB), Mount Laurel, NJ, Minor damage. Emergency landing after engine made a loud noise found a broken cooling fan blade. .
- [Incident 19780422012749I](https://openairdocs.org/incident/19780422012749I), Apr 22, 1978: Enstrm 280 (N280RS), Coconut Grove, FL, Minor damage. Pilot made approach to hover to intended landing site on shore. Could not maintain rp. Settled in water.

## Service difficulty reports (86, newest 50)

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

- [SDR 2023FA0000622](https://openairdocs.org/sdr/2023FA0000622), Oct 20, 2023: CYLINDER. CRACKED. PILOT REPORTED LOSS OF ENGINE POWER. BEGAN TO RUN ROUGH. MADE A PRECAUTIONARY NORMAL LANDING. MECHANIC REMOVED COWLING AND FOUND A CRACKED NR 4 CYLINDER. LB STA
- [SDR 2021FA0000407](https://openairdocs.org/sdr/2021FA0000407), Dec 16, 2021: NONE. LOOSE. DURING R/H AILERON BELLCRANK CABLES DISCONNECTION FOR CLEANING / INSPECTION / LUBE, FOUND BELLCRANK ASSY P/N 47350-2 CONSTITUTED OF PIVOT BALL BEARING HOUSING P
- [SDR 4RPA201307010001](https://openairdocs.org/sdr/4RPA201307010001), Jun 28, 2013: PUMP. FAILED. LEFT ENGINE FUEL FLOW DROPPED FROM 25 GALLONS AN HOUR AT TOP OF CLIMB TO 7 GALLONS AN HOUR AT ALL POWER SETTINGS. ELECTRIC FUEL PUMP SWITCH ALSO FAILED. PILOT U
- [SDR 2012FA0000727](https://openairdocs.org/sdr/2012FA0000727), Oct 25, 2012: POWER SUPPLY. FAILED. LEFT STROBE INOPERATIVE. TESTED FLASH TUBE WITH ANOTHER POWER SUPPLY - FUNCTION CHECK OK. PULLED THE POWER SUPPLY AND OPENED - EVIDENCE OF CAPACITOR EXPLOSION A
- [SDR 2012FA0000517](https://openairdocs.org/sdr/2012FA0000517), Jul 9, 2012: COWL DOOR. DEPARTED. DURING DESCENT THROUGH 7,000 FT, TOP COWL ASSEMBLY DEPARTED THE ACFT AND STRUCK THE LEFT WINDSCREEN CAUSING A LARGE HOLE. FURTHER INSPECTION REVEALED THAT THE R
- [SDR 2012FA0000343](https://openairdocs.org/sdr/2012FA0000343), May 29, 2012: CASE. CRACKED. DURRING PRE FLIGHT FOUND OIL ON COWLING. INVESTIGATION FOUND A CRACK IN THE RT FWD TOP OF THE ENGINE CASE.
- [SDR 2011FA0000544](https://openairdocs.org/sdr/2011FA0000544), Aug 22, 2011: BOLT. LOOSE. WHILE COMPLYING WITH AD 11-07-13 LT AND RT ELEVATOR SPAR, IT WAS NOTED THAT THE HORIZONTAL STAB WAS LOOSE AT BOTH THE FRONT AND REAR MOUNTING POINTS. MOVEMENT W
- [SDR 2011FA0000373](https://openairdocs.org/sdr/2011FA0000373), Jun 9, 2011: FILTER ELEMENT. SPLIT. DURING ROUTINE INSPECTION, AIR FILTER WAS FOUND SPLIT OPEN AT THE SEAM. IT IS A CYLINDRICAL SHAPE AND IT WRAPS AROUND A METAL SCREEN. THE SPLIT AREA COMPRISED S
- [SDR 2011FA0000334](https://openairdocs.org/sdr/2011FA0000334), May 18, 2011: SPAR. CORRODED. DURING REPAIR OF LT WING THE AFT SPAR ATTACH FITTING WAS REMOVED. SEVERE CORROSION WAS FOUND UNDER THE FITTING. PROBABLE CAUSE IS TRAPPED MOISTURE, LACK OF PREV
- [SDR NX4R000013](https://openairdocs.org/sdr/NX4R000013), Apr 28, 2011: MOUNT. CRACKED. DURING ROUNTINE MX, THE TECH WAS PERFORMING A PRELIMINARY/HIDDEN DAMAGE INSP OF THE AREA SURROUNDING THE AREA WHERE WORK WAS TO BE PERFORMED. NOTICED THE SMALL 
- [SDR NX4R000011](https://openairdocs.org/sdr/NX4R000011), Apr 20, 2011: ATTACH FITTING. BROKEN. DURING TAKEOFF, THE PILOT RETRACTED THE LANDING GEAR. THE GEAR "UNSAFE LIGHT" REMAINED ILLUMINATED. ALSO THE ATC TOWER CONTROLLER ADVISED THE CREW THAT THEIR NL
- [SDR 2011FA0000054](https://openairdocs.org/sdr/2011FA0000054), Jan 28, 2011: SHAFT. FAILED. MAG SHAFT COMPLETELY SEPARATED FROM THE MAG AS THE SHAFT EXITED THE MAG. CAUSING INOPERATIVE SYS, LOSS OF 1/2 ENGINE IGNITION AND ASSOCIATED WARNING LIGHTS IN T
- [SDR 2010FA0001258](https://openairdocs.org/sdr/2010FA0001258), Dec 20, 2010: DISTRIBUTOR BLK. MELTED. DURING A 500 HOUR INSP, COMPLIANCE OF M/N 6314 MAGNETOS, LT MAGNETO SHOWED SIGNS OF EXTREAM HIGH HEAT INTERNALLY. SB SB3-08A ADDRESSES PROBLEM CAUSED BY "SOFT" 
- [SDR 2010FA0001132](https://openairdocs.org/sdr/2010FA0001132), Aug 21, 2010: SPRING. BROKEN. ON LANDING TAILSPRING BROKE. ACFT GROUND LOOPED CAUSING SUBSTANTIAL DAMAGE TO AIRCRAFT. INVESTIGATION OF BROKEN TAILSPRING REVEALED 2 EXISTING LOW CYCLE FATIGUE
- [SDR ZB0R20100002](https://openairdocs.org/sdr/ZB0R20100002), May 31, 2010: MASTER SWITCH. BURNED. ((ZB0R)) PILOT REPORTED BURNING SMELL AND FAILURE OF AVIONICS BUSS NR 2 ON RUN-UP. ACFT REPORTED TO MX. TROUBLESHOOTING REVEALED AVIONICS MASTER SWITCH RT SIDE 
- [SDR 2010FA0000425](https://openairdocs.org/sdr/2010FA0000425), Apr 19, 2010: GUIDE. BROKEN. (HE8S) PILOT`S SEAT HARNESS GUIDE BROKE AT SHOULDER HARNESS MOUNT TUBE. SUGGEST MAKING THIS PART WITH MORE DURABLE MATERIAL OR HAVING A REINFORCEMENT AT AREA OF
- [SDR 2010FA0000228](https://openairdocs.org/sdr/2010FA0000228), Mar 12, 2010: MOUNT. BROKEN. HAVE HAD MULTIPLE PROBLEMS WITH THE MOUNTING KIT FOR THE ALTERNATOR THROUGH STC SA334SW. A NEW ALTERNATOR WAS INSTALLED ON 9/8/2006. AFTER 64 FLIGHT HOURS, THE 
- [SDR 2010FA0000196](https://openairdocs.org/sdr/2010FA0000196), Mar 3, 2010: SOLENOID. STICKS. BURNED ODOR OF ELECTRICAL COMPONENTS AFTER ENGINE START UP. SELECTED ACFT MASTER SWITCH OFF AND SHUTDOWN ENGINE. INSP REVEALED STARTER MOTOR HAD OVERHEATED. FUR
- [SDR 2010FA0000045](https://openairdocs.org/sdr/2010FA0000045), Jan 15, 2010: TRACK. BROKEN. PN 1513055-1 CAM TRACK ASSY BROKE UPON GEAR RETRACTION. NOSE GEAR THEN WOULD NOT RETRACT PROPERLY OR EXTEND AND LOCK PROPERLY. PUMP MOTOR C/B CONTINUED TO TRIP 
- [SDR 2009FA0000986](https://openairdocs.org/sdr/2009FA0000986), Nov 20, 2009: SHAFT. FRACTURED. ROTOR SHAFT FRACTURED AT THE BOTTOM OF THE RUBBING BROOK SLOT. (K)
- [SDR 2009FA0000873](https://openairdocs.org/sdr/2009FA0000873), Oct 22, 2009: NUT. CRACKED. WHEN REMOVING PROPELLER FOR RESEAL, FOUND 2 MOUNTING NUTS CRACKED. THE PROP HAS 93.5 HRS SINCE INSTALLATION. THE PROPELLER PREVIOUSLY HAD THE BLADES REPLACED DU
- [SDR 2009FA0000921](https://openairdocs.org/sdr/2009FA0000921), Aug 14, 2009: SCREEN. CRACKED. REPAIR STATION IS HOLDER OF STC SA03674AT FOR THE INSTALATION OF R-134 COOLANT AIR CONDITIONER SYS IN THIS ACFT. IAW THIS STC INSTALLATION, A CONDENSER HOUSING 
- [SDR 2009FA0000922](https://openairdocs.org/sdr/2009FA0000922), Aug 14, 2009: SCREEN. CRACKED. REPAIR STATION IS HOLDER OF STC SA03674AT FOR THE INSTALATION OF R-134 COOLANT AIR CONDITIONER SYS IN THIS ACFT. IAW THIS STC INSTALLATION, A CONDENSER HOUSING 
- [SDR 2009FA0000510](https://openairdocs.org/sdr/2009FA0000510), Jun 9, 2009: AIR FILTER. DEFECTIVE. UPON RECEIVING INSP OF NEW MFG AIR FILTERS PN P107336 IT WAS FOUND THAT 3 OUT OF 4 NEW FILTERS HAD A DEFECTIVE SEALING SURFACE CAUSING THE SEALING/MATING SURFAC
- [SDR 2009FA0000449](https://openairdocs.org/sdr/2009FA0000449), May 12, 2009: CONTROL CABLE. BROKEN. AN INSP OF RT WING FLAP CABLE REVEALED BROKEN STRANDS WHERE THE CABLE THIMBLE AND SHACKLE TO THE FLAP BELLCRANK INSIDE THE WING. THERE IS INSUFFICIENT CLEARANCE
- [SDR 2009FA0000396](https://openairdocs.org/sdr/2009FA0000396), May 11, 2009: PLUNGER. DAMAGED. PLUNGER P/N 210332 INSPECTED IAW SB 33571C AND FAILED.
- [SDR 2008FA0000841](https://openairdocs.org/sdr/2008FA0000841), Nov 24, 2008: LATCH. DISENGAGED. AT 10500 FT IN CRUISE FLIGHT, GOT AN AUDIBLE "DING" ON THE G1000 WARNING AND THEN A LIGHT SAYING THAT A DOOR WAS OPEN. BACK DOOR HAD COME OPEN IN FLIGHT. THE DO
- [SDR 2008FA0000880](https://openairdocs.org/sdr/2008FA0000880), Nov 22, 2008: SENSOR. DEFECTIVE. SENSOR PRODUCED A FALSE HIGH OIL PRESSURE INDICATION DURING ACFT APPROACH TO AIRPORT. PROBABLE CAUSE WAS INTERNAL FAILURE, RECOMMENDATIONS TO PREVENT RECURRENCE
- [SDR 2010FA0000758](https://openairdocs.org/sdr/2010FA0000758), Nov 7, 2008: WIRE. CHAFED. (NU7R) PILOT REPORTED AVIONICS INTERMITTENT TO COME ON WITH AVIONICS SWITCH. MFG DWG PAGE 24-50-01, PAGE 1 SHOWS AVIONICS RELAY NR 1 WITH WIRE CSVA661-14 LEAVIN
- [SDR CA081009009](https://openairdocs.org/sdr/CA081009009), Sep 27, 2008: WIRE. BROKEN. (CAN) A+ TERMINAL MELTED OFF ALTERNATOR AND LOOSE. PROBLEM CAUSED BY BROKEN TERMINAL ON A+ WIRE GOING TO ALTERNATOR. WIRE WAS ORIGINALLY VERY TIGHT CAUSING THE 
- [SDR 2008FA0000661](https://openairdocs.org/sdr/2008FA0000661), Sep 17, 2008: CASTING. BROKEN. CUSTOMER ATTEMPTED TO START ENGINE. WHILE CRANKING ENGINE, CUSTOMER REPORTED A LOUD "CLUNK" AND THE PROPELLER STOPPED ROTATING. INVESTIGATED PROBLEM AND FOUND T
- [SDR 2008FA0000505](https://openairdocs.org/sdr/2008FA0000505), Jul 22, 2008: CONNECTOR. DAMAGED. ON JUNE 28TH, 2008, DURING CLIMB OUT, PASSING THROUGH 4000 FEET THE ENGINE SUDDENLY WENT INTO AN OVER SPEED CONDITION OF OVER 3100 RPM. THE AIRCRAFT REMAINED UN
- [SDR 2008FA0000278](https://openairdocs.org/sdr/2008FA0000278), Apr 15, 2008: VALVE. LOOSE. THE ALTERNATE AIR VALVE IS VIBRATING AND CAUSING FRETTING BETWEEN THE INLET RING, PN D41-7166-20-31 AND FLANGE, PN D41-7166-20-33. THE "DUST" IS BEING INGESTED 
- [SDR 2008FA0000234](https://openairdocs.org/sdr/2008FA0000234), Mar 7, 2008: VALVE. BROKEN. THE ENG AUTOMATIC ALTERNATE INDUCTION AIR VALVE THAT IS PARTIALLY LOCATED INSIDE THE CYLINDRICAL PAPER INDUCTION AIR FILTER CAME APART AND SOME OF ITS PART (2 I
- [SDR 2008FA0000254](https://openairdocs.org/sdr/2008FA0000254), Mar 5, 2008: SERVO. DAMAGED. WHILE PERFORMING A 100 HR INSP, THE TECH DISCOVERED FINE METAL PARTICLES COVERING THE THROAT AND VALVE OF THE FUEL INJECTION SERVO (2576568-1, SN 70B10709). THE
- [SDR 2008FA0000238](https://openairdocs.org/sdr/2008FA0000238), Feb 27, 2008: BUSHING. INCORRECT. STATIC SYSTEM FAILED LEAK CHECK DURING 2 YEAR STATIC SYS IFR CERTIFICATION, LEAKS WERE CAUSED BY REDUCED BUSHING FAILING TO SEAL STATIC LINE SUMP. (ON BOTH SIDE
- [SDR 2007FA0000711](https://openairdocs.org/sdr/2007FA0000711), Jul 10, 2007: RESISTOR. DAMAGED. MFG FABRICATED AN IN-LINE RESISTOR FROM THE ALTERNATOR TO THE VOLTAGE REGULATOR. THE RESISTOR WAS LOCATED APPROXIMATELY 2 INCHES FROM AUX TERMINAL ON ALTERNATOR
- [SDR 2007FA0000554](https://openairdocs.org/sdr/2007FA0000554), Jun 28, 2007: ANTENNA. DISCONNECTED. WHILE IN CRUISE FLIGHT THE NR 1 GPS STOPPED RECEIVING A SIGNAL. AFTER LANDING, REMOVED THE MFD AND FOUND THE GLUE HOLDING THE VELCRO TO THE GPS ANTENNA HAD COME
- [SDR 2007FA0000533](https://openairdocs.org/sdr/2007FA0000533), Jun 22, 2007: STRUT. CRACKED. NOSE LANDING GEAR STRUT HAS A CRACK AT THE TOP. THE STRUT COMES UP TO A Y FOR MOUNT. AT THE YOKE OF THE Y IS A WELDED REINFORCEMENT, AND THE CRACK IS AT THE TOP
- [SDR AW42007F00000](https://openairdocs.org/sdr/AW42007F00000), Jun 8, 2007: NUT. LOOSE. DURING THE PERFORMANCE OF A 100 HOUR INSPECTION, SLIGHT MOVEMENT OF THE HORIZONTAL STABILIZER WAS NOTED RELATIVE TO THE RT SIDE OF THE FUSELAGE. INVESTIGATION F
- [SDR 2007FA0000571](https://openairdocs.org/sdr/2007FA0000571), May 31, 2007: BRACKET. FAILED. THE PILOT STATED NOSE GEAR COLLAPSED ON LANDING. AFTER AIRCRAFT REMOVED FROM RUNWAY AND PUT ON JACKS. THE NOSE GEAR WOULD NOT EXTEND OR RETRACT. THE GEAR WAS EX
- [SDR 2007FA0000577](https://openairdocs.org/sdr/2007FA0000577), May 12, 2007: DOWNLOCK. BROKEN. THE LOWER LATCH HOOK WAS BROKEN OFF ALLOWING THE NOSE GEAR TO COLLAPSE. (K)
- [SDR 2007FA0000349](https://openairdocs.org/sdr/2007FA0000349), Apr 1, 2007: SPAR. LOOSE. DURING AN ANNUAL INSPECTION, THE RT FLAP IB HINGE/CONTROL BRACKET WAS FOUND TO BE LOOSE. FURTHER INSPECTION REVEALED THAT THE FLAP SPAR WAS CRACKED AT THE UPPER
- [SDR 2007FA0000112](https://openairdocs.org/sdr/2007FA0000112), Jan 8, 2007: AIR FILTER. TWISTED. DURING REMOVAL OF THE AIR FILTER THE CENTER WIRE MESH SCREEN WAS FOUND TWISTED AND BENT. SOME OF THE WELDS WERE BROKEN. SCREEN DEFORMATION CAN LEAD TO UNFILTERE
- [SDR 2006FA0001020](https://openairdocs.org/sdr/2006FA0001020), Oct 18, 2006: LINE. CHAFED. FUEL LINE CHAFED, LINE REPLACED.
- [SDR 2006FA0000561](https://openairdocs.org/sdr/2006FA0000561), May 31, 2006: ATTACH BRACKET. CRACKED. ENGINE MOUNT ATTACHMENT BRACKET WITH CRACKS AT THE 12 AND 6 O`CLOCK POSITION. CRACKS ON IB AND OB SIDES OF THE AN960-616 WASHER. NORMAL FLIGHT CONDITIONS UNDER 
- [SDR 2006FA0000134](https://openairdocs.org/sdr/2006FA0000134), Jan 31, 2006: ATTACH BRACKET. BROKEN. THE AC EXPERIENCED A HARD LANDING. DURING THE LANDING THE 2 TOP ENGINE MOUNT ATTACH BRACKETS FAILED BEHIND THE FIREWALL, ALLOWING THE TOP HALF OF THE FIREWALL T
- [SDR 10943282](https://openairdocs.org/sdr/10943282), Jan 20, 2006: FRAME. CRACKED. FOUND CRACK APPROXIMATELY .3750 INCH IN LENGTH ON RT FRAME 20 WING ATTACH POINT.
- [SDR 2005FA0001483](https://openairdocs.org/sdr/2005FA0001483), Oct 5, 2005: HINGE. FAILED. UPON INSTALLATION OF A NEW AFT CABIN DOOR SUPPORT STRUT, THE DOOR WAS CLOSED, AND THE AFT CABIN DOOR HINGE FAILED. UPON FURTHER INSPECTION, THE DOOR HINGE WAS F
- [SDR 2005FA0001311](https://openairdocs.org/sdr/2005FA0001311), Sep 9, 2005: ENGINE. STOPPED. DURING CRUISE CLIMB, PILOT REPORTED BOTH ENGINES QUIT RUNNING AND DEVERTED. DURING DECENT ENGINES CAME BACK TO LIFE. SUMPED 1 PINT EACH FROM FRONT, BACK FUEL ST

All 86: https://openairdocs.org/engine/lycoming-i0-360-series/reports.md

## STCs that may be installed (OpenAirDocs) (55, first 50)

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. Lists IO-360-B1C
- [STC SE00825WI](https://openairdocs.org/stc/SE00825WI): Installation of Specialty Products Spin-on oil filter on Lycoming Engines. B & C Specialty Products Inc. Lists IO-360-A1A
- [STC SE04349CH](https://openairdocs.org/stc/SE04349CH): Installation of SureFly electronic ignition. SureFly Partners Ltd. Lists IO-360-A1A
- [STC SE01954SE](https://openairdocs.org/stc/SE01954SE): Installation of engine crankcase seal. Ly-Con Rebuilding Company. Lists IO-360-A1A
- [STC SE02352CH](https://openairdocs.org/stc/SE02352CH): Installation of Challenger cleanable oil filter assembly. Challenger Aviation Products Inc. Lists IO-360-A1A
- [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. Lists IO-360-A1A
- [STC SE2389CE](https://openairdocs.org/stc/SE2389CE): Installation of B&C Speciality Products lightweight (10.2) pounds) engine starter, part number BC-315-100-1 (12 volts) or part number BC-315-100-3 (24 volts). B & C Specialty Products Inc. Lists IO-360-A1A
- [STC SE03232CH](https://openairdocs.org/stc/SE03232CH): Installation of Engine Preheat Kit p/n TA2925-1 for 115 volt application. Hartzell Propeller Inc. Lists IO-360-A1A
- [STC SE32WE](https://openairdocs.org/stc/SE32WE): Installation of Turbocharger P/N 600573-00 (formerly RJ 0326, RJ 0326-1), 600576-00(formerly RJ 0326-2) and600577000 (formerly RJ 0329). TALCO Aviation. Lists IO-360-A1A
- [STC SE90WE](https://openairdocs.org/stc/SE90WE): Installation of Roto-Master (Rajay) Turbochargers Model 3AT6EE10J2 (325E10-1) P/N 600573-00 (RJ0331-1). TALCO Aviation. Lists IO-360-A1D6D
- [STC SE04577CH](https://openairdocs.org/stc/SE04577CH): Install an electronic engine ignition system. Electroair Acquisition Corp. Lists IO-360-A1A
- [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. Lists IO-360-A1A
- [STC SE8628SW](https://openairdocs.org/stc/SE8628SW): Installation of oil nozzles for lubrication of cam and filters. Cygnet Aerospace Corp. Lists IO-360-A1A
- [STC SE09445SC](https://openairdocs.org/stc/SE09445SC): Installation of fuel injector nozzles. General Aviation Modifications Inc
- [STC SE1339SW](https://openairdocs.org/stc/SE1339SW): Modify pistons to Drawings 11007 and 11015; piston rings. Continental Motors, Inc. Lists IO-360-A1A
- [STC SE4408SW](https://openairdocs.org/stc/SE4408SW): Miscellaneous engine cylinder replacement parts. Continental Motors, Inc
- [STC SE7508SW](https://openairdocs.org/stc/SE7508SW): Installation of any or all parts listed on Airmotive Engineering Drawing List No. 852-1, Rev. 1, dated 10/4/88, or later, FAA approved revision. Continental Motors, Inc
- [STC SE7661SW](https://openairdocs.org/stc/SE7661SW): Installation of parts listed on Airmotive Drawing No. 8810-3. Continental Motors, Inc
- [STC SE8776SW](https://openairdocs.org/stc/SE8776SW): Installation of coated cylinders and piston rings. Continental Motors, Inc
- [STC SE00218NY](https://openairdocs.org/stc/SE00218NY): Replacement of Lycoming starter with SKY-TEC 12 volt starter installed. Hartzell Engine Technologies, LLC
- [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. Lists IO-360-A1A
- [STC SE00357NY](https://openairdocs.org/stc/SE00357NY): Replacement of Lycoming starter with SKY-TEC 24-volt starter installed. Hartzell Engine Technologies, LLC
- [STC SE2901NM](https://openairdocs.org/stc/SE2901NM): Lycoming valve cover gasket. Real Gaskets Tennessee. Lists IO-360-A1A
- [STC SE2902NM](https://openairdocs.org/stc/SE2902NM): Lycoming valve cover gasket. Real Gaskets Tennessee. Lists IO-360-A1A
- [STC SE5203NM](https://openairdocs.org/stc/SE5203NM): Installation of turbocharger and induction air intercooler. Fly In Vacations. Lists IO-360-C1D6
- [STC SE7582SW](https://openairdocs.org/stc/SE7582SW): Grinding of high compression NITRIDED Cylinders to .010 oversize, as an alternative to chrome plating or rebarreling, and the installation of SL10207 P10 Piston, SL74241 P10 Top and second compression ring, and SL 73857 P10 oil control ring. Superior Air Parts, Inc. Lists IO-360-A1A
- [STC SE02409AK](https://openairdocs.org/stc/SE02409AK): Installation of the Superior Air Parts Cold Air Induction System (CAIS). Wattum Aircraft Services. Lists IO-360-A1A
- [STC SE02555AT](https://openairdocs.org/stc/SE02555AT): Consolidated Fuel Systems 201F series fuel pump assembly on various Textron Lycoming engine models. Kelly Aerospace Energy Systems LLC. Lists IO-360-A1B
- [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. Lists IO-360-A1A
- [STC SE916GL](https://openairdocs.org/stc/SE916GL): Replacement of Bendix S4LN-20, -21, -1209, or -1227 model magnetos with Slick model 4250 and 4251 magnetos. Champion Aerospace LLC. Lists IO-360-A1B
- [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. Lists IO-360-B1A
- [STC SE459GL](https://openairdocs.org/stc/SE459GL): Incorporation of a fuel flow transducer. Shadin Company Inc. Lists IO-360-A1A
- [STC SE01930NY](https://openairdocs.org/stc/SE01930NY): Installation of Casper Labs 90 degree oil filter housing adapter. Casper Labs Inc. Lists IO-360-A1A
- [STC SE2741NM](https://openairdocs.org/stc/SE2741NM): Installation of high compressoin pistonsd, connecting rods, bearings and associated hardware. Firewall Forward Inc. Lists IO-360-A1B6
- [STC SE1779NM](https://openairdocs.org/stc/SE1779NM): Installation of Precise Flight, Inc. Standby Vacuum System SVS III. Precise Flight Inc. Lists IO-360-A1A
- [STC SE5743NM](https://openairdocs.org/stc/SE5743NM): Intallation of adapter for externally mounted oil filter. Aviation Development Corporation. Lists IO-360-A1A
- [STC SE4082NM](https://openairdocs.org/stc/SE4082NM): Installation of turbocharger. General Aviation Modifications, Inc. Lists IO-360-A1B6
- [STC SE00889LA](https://openairdocs.org/stc/SE00889LA): Installation of Nickson's cylinder barrels on Lycoming reciprocating engine models. Nickson's Machine Shop Inc. Lists IO-360-A1A
- [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
- [STC SE01643AT](https://openairdocs.org/stc/SE01643AT): Installation of a Roto-Master turbocharger P/N 600573-00, Roto-Master scavenge pump, AC diaphragm fuel pump, and TCM fixed wastegate. M-20 Oil Separators LLC. Lists IO-360-A1A
- [STC SE00350SE](https://openairdocs.org/stc/SE00350SE): Installation of sump mounted chip detector. Aviation Development Corporation. Lists IO-360-A1A
- [STC SE8023SW](https://openairdocs.org/stc/SE8023SW): Installation and usage of AEROSHELL. Shell Development Co
- [STC SE4757NM](https://openairdocs.org/stc/SE4757NM): Installation of Rotomaster turbo- charger, scavenge pump, diaphragm fuel pump, fuel injectors, fixed wastegate, and an ACD intercooler. Aircraft Design Inc. Lists IO-360-A1B6D
- [STC SE5898SW](https://openairdocs.org/stc/SE5898SW): Installation of turbosupercharger. FliteCraft Turbo. Lists IO-360-A1B6D
- [STC SE739NE](https://openairdocs.org/stc/SE739NE): Installation of 'Auto-Vac-4' primary vacuum system. Raymond Ives. Lists IO-360-B1E
- [STC SE2389SE](https://openairdocs.org/stc/SE2389SE): Installation of B & C Specialty Products. Bainbridge William C III
- [STC SE474NE](https://openairdocs.org/stc/SE474NE): Installation of 'Auto-Vac-2' auxiliary vacuum system. Raymond Ives. Lists IO-360-A1B6
- [STC SE2261SO](https://openairdocs.org/stc/SE2261SO): Installation of IO-360-C1C fuel nozzles, injector fuel lines and adjust fuel pressure. Gator Aerial Enterprises. Lists IO-360-C1F
- [STC SE452NE](https://openairdocs.org/stc/SE452NE): Installation and usage of 'Mobil AV 1' aviation oil. Mobil Research & Development Corp

All 55: https://openairdocs.org/engine/lycoming-i0-360-series/stcs.md

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