# Continental TSIO-360-F

- Type: Engine model (FAA registry)
- Registry code: 17291
- Manufacturer (registry): CONT MOTOR
- Model: TSIO-360-F
- Engine type: Reciprocating
- Power: 200 hp
- Data sheet: [TCDS E9CE](https://openairdocs.org/tcds/E9CE) (OpenAirDocs)
- Holder: Continental Aerospace Technologies, Inc.
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/continental-tsio-360-f

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 2023-09-09](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 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 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 2000-23-21](https://openairdocs.org/ad/2000-23-21): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 164 more. Effective Dec 12, 2000
- [AD 98-19-02](https://openairdocs.org/ad/98-19-02): Piston Pins · Continental Motors IO-360-A, IO-360-AB, IO-360-C and 31 more. Effective Nov 9, 1998
- [AD 97-26-17](https://openairdocs.org/ad/97-26-17): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 90 more. Effective Jan 23, 1998
- [AD 95-21-15](https://openairdocs.org/ad/95-21-15): Aviation Gasoline · Continental Motors A-65-8, C85-12F, C85-12FJ and 77 more. Effective Nov 28, 1995
- [AD 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 88-03-06](https://openairdocs.org/ad/88-03-06): Oil Filter · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 155 more. Effective Apr 15, 1988
- [AD 81-13-10 R1](https://openairdocs.org/ad/81-13-10-R1): Oil Pressure · Continental Motors IO-360-A, IO-360-AB, IO-360-C and 28 more. Effective Nov 20, 1981
- [AD 81-16-05](https://openairdocs.org/ad/81-16-05): Magnetos · Lycoming Engines AEIO-320-E1B, AEIO-320-E2B, AEIO-360-B1G6 and 234 more. Effective Aug 6, 1981

Historical (superseded or no longer in force):

- [AD 2022-04-04](https://openairdocs.org/ad/2022-04-04) (historical): 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 Mar 29, 2022
- [AD 2009-24-52](https://openairdocs.org/ad/2009-24-52) (historical): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 192 more
- [AD 2009-24-51](https://openairdocs.org/ad/2009-24-51) (historical): Hydraulic lifters · Teledyne Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 156 more
- [AD 2002-13-04](https://openairdocs.org/ad/2002-13-04) (historical): Magneto impulse coupling stop pin · Teledyne Continental Motors C-125-1, C-125-2, C145-2 and 48 more. Effective Jul 12, 2002
- [AD 2000-08-51](https://openairdocs.org/ad/2000-08-51) (historical): Crankshaft · Teledyne Continental Motors IO-360-A, IO-360-AB, IO-360-B and 158 more
- [AD 94-14-12](https://openairdocs.org/ad/94-14-12) (historical): Octane Aviation Gasoline · Teledyne Continental Motors A-65-8, C85-12, E185-11 and 68 more

## Information bulletins (advisory) (5)

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

## Registered aircraft

None registered with this engine model now.

## NTSB investigations (1)

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 CEN14WA363](https://openairdocs.org/ntsb/CEN14WA363), Jul 12, 2014: Piper PA 28R-201T (N717ND), Urtaca, France, destroyed, 3 fatal

## 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 19830831052009I](https://openairdocs.org/incident/19830831052009I), Aug 31, 1983: Piper PA28R201T (N9239C), Wheeling, IL, Minor damage. Landed gear up. Had automatic gear override engaged per club policy. Club policy to use auto gear in the future.

## Service difficulty reports (28)

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

- [SDR 2012FA0000228](https://openairdocs.org/sdr/2012FA0000228), Mar 2, 2012: SPARK PLUG. DAMAGED. PILOT REPORTED ENGINE BEGAN RUNNING ROUGH AT 11,000 FT. DESCENDED TO 5,000 FT AND ENGINE OPERATED CORRECTLY. RETURNED TO AIRPORT, LANDED WITHOUT FURTHER INCIDEN
- [SDR CA090303006](https://openairdocs.org/sdr/CA090303006), Mar 2, 2009: MAIN BEARING. FAILED. (CAN) LARGE PIECE OF FERROUS MATERIAL FOUND IN OIL PICKUP SCREEN DURING ROUTINE INSP, PIECE IDENTIFIED AS PORTION OF CTR MAIN BRG. ENGINE REMOVED FROM ACFT, DIS
- [SDR CA090220005](https://openairdocs.org/sdr/CA090220005), Feb 13, 2009: PLUG. MISSING. ON APPROACH TO YBL, THE PILOT DETECTED BURNING OIL AND SAW SMOKE, THE PILOT LANDED THE AIRCRAFT AND NOTICED A LARGE AMOUNT OF OIL ON THE BELLY OF THE AIRCRAFT A
- [SDR NTB2008F00000](https://openairdocs.org/sdr/NTB2008F00000), Aug 8, 2008: IMPULSE COUPLING. BROKEN. IMPULSE COUPLING SPRING BROKEN. EVIDENCE OF PRE-EXISTING CRACK AND CORROSION. VERY LOW TIME IN SERVICE. MAG TO ENGINE TIMING LOST. BOTH MAGS EXPERIENCED THE SAM
- [SDR NTB2008F00001](https://openairdocs.org/sdr/NTB2008F00001), Aug 8, 2008: SPRING. BROKEN. IMPULSE COUPLING SPRING BROKEN. EVIDENCE OF PRE-EXISTING CRACK AND CORROSION. VERY LOW TIME IS SERVICE. MAG TO ENGINE TIMING LOST. BOTH MAGS EXPERIENCED THE SAM
- [SDR CA070919001](https://openairdocs.org/sdr/CA070919001), Sep 17, 2007: TUBE. BROKEN. (CAN) FUEL DISCHARGE TUBE BROKE, ENGINE LOST POWER. SUSPECT MID-TUBE CLIP P/N: 626477-2 MAY HAVE FAILED FIRST. (TC NR 20070919001)
- [SDR CA070502008](https://openairdocs.org/sdr/CA070502008), Apr 27, 2007: CONTROL CABLE. DAMAGED. (CAN) MIXTURE CONTROL WAS FOUND TO BE STIFF BY MAINT ON AN ENGINE START FOR TAXI TO HANGER. CABLE WAS REMOVED. THE CABLE ROUTING POSITIONS THE CABLE LESS THAN (
- [SDR CA070118003](https://openairdocs.org/sdr/CA070118003), Jan 10, 2007: PUMP. FAULTY. (CAN) ENGINE DRIVEN FUEL PUMP OUTPUT IS LOW AT RATED RPM 2600. (TC NR 20070118003)
- [SDR 2004FA0000845](https://openairdocs.org/sdr/2004FA0000845), Oct 18, 2004: SHAFT. MISMANUFACTURED. DURING 100 HOUR INSP AT 1V5, LT CONTROL COLUMN, P/N 62834-02, WAS REMOVED FOR REPLACEMENT DUE TO EXCESS PLAY. UPON REMOVAL, CONTROL COLUMN SHAFT, P/N 62716-02, 
- [SDR 2004FA0000846](https://openairdocs.org/sdr/2004FA0000846), Oct 18, 2004: SHAFT. MISMANUFACTURED. DURING 100 HR INSP AT 1V5, LT CONTOL COLUMN UNIVERSAL,P/N 62834-02, WAS REMOVED FOR REPLACEMENT DUE TO EXCESS PLAY. CONTROL COLUMN SHAFT, P/N 62716-02, WAS FOUN
- [SDR AUS20030626](https://openairdocs.org/sdr/AUS20030626), Jun 20, 2003: STUD. CRACKED. (AUS) MAIN LANDING GEAR SIDE BRACE STUD CONTAINED LONGITUDINAL MPI INDICATIONS. FOUND DURING INSPECTION IAW AD/PA28/91 AMDT1.
- [SDR AUS20030367](https://openairdocs.org/sdr/AUS20030367), Mar 25, 2003: LINK. FAILED. (AUS) NOSE LANDING GEAR DRAG LINK ASSEMBLY SHEARED IN AREA LOCATEDFORWARD OF THE RH ATTACHMENT POINT.
- [SDR AUS20020155](https://openairdocs.org/sdr/AUS20020155), Mar 1, 2002: CAPACITOR. FAULTY. (AUS) LH MAGNETO CAPACITOR WIRE INTERMITTENT CONTACT.
- [SDR AUS20020156](https://openairdocs.org/sdr/AUS20020156), Feb 5, 2002: CAPACITOR. FAULTY. (AUS) RH MAGNETO CAPACITOR WIRE INTERMITTENT CONTACT.
- [SDR AU000534](https://openairdocs.org/sdr/AU000534), Jul 10, 2000: STUD. CRACKED. (AUS) LEFT AND RIGHT MAIN LANDING GEAR SIDE BRACE STUDS CRACKED. FOUND DURING MAGNETIC PARTICLE INSPECTION IAW AD/PA28/91. (X)
- [SDR CA000530031](https://openairdocs.org/sdr/CA000530031), May 1, 2000: TRUNNION. CRACKED. (CAN) DURING A 50-HOUR INSPECTION OF THE LANDING GEAR, THE NOSE GEAR TRUNNION WAS FOUND CRACKED AT SHIMMY DAMPENER ATTACHMENT POINT. POSSIBLE CAUSE - OVERSTEER.
- [SDR AU000342](https://openairdocs.org/sdr/AU000342), Apr 7, 2000: FUEL TANK. LEAKING. (AUS) FUEL TANK LEAKING. INSPECTION FOUND FAULTY SEALANT. FOUND FOLLOWING COMPLIANCE WITH AD/GEN/80.
- [SDR 99ZZZX1076](https://openairdocs.org/sdr/99ZZZX1076), Mar 5, 1999: BYPASS PIPE. NOT INSTALLED. A TURBO HEAT BLANKET WAS INSTALLED ON 1-28-99. SUBMITTER STATED DURING THE INSTALLATION OF THE TURBO HEAT BLANKET, THE MECHANIC FAILED TO REINSTALL THE EXHAUST 
- [SDR CA990318049](https://openairdocs.org/sdr/CA990318049), Feb 18, 1999: FLYWEIGHT. LOOSE. (CAN) PILOT REPORTED ROUGH RUNNING ENGINE ON RUN-UP. INSPECTION FOUND RIGHT HAND MAGNETO DEAD. DURING REMOVAL OF THE MAGNETO, THE IMPULSE COUPLING FLYWEIGHT FEL
- [SDR CA980430038](https://openairdocs.org/sdr/CA980430038), Apr 14, 1998: TUBE ASSY. CRACKED. (CAN) TUBE CRACKED UNDER CLAMP. NOT VISIBLE WITH CLAMP ON. REPLACED.
- [SDR CA980331021](https://openairdocs.org/sdr/CA980331021), Mar 9, 1998: CABLE. STIFF. (CAN) BOTH PROP AND MIXTURE CONTROL CABLES VERY STIFF. AREA BEHIND TURBO BADLY CORRODED. CABLES REPLACED.
- [SDR AU970577](https://openairdocs.org/sdr/AU970577), Jun 2, 1997: ELT. FAULTY. (AUS) ELT FAULTY - `G' SWITCH UNSERVICEABLE - BATTERIES OF EUROPEAN ORIGIN FITTED - BATTERY INSULATORS WORN - EVIDENCE OF MOISTURE INGRESS
- [SDR AU970450](https://openairdocs.org/sdr/AU970450), Apr 18, 1997: CABLE. STUCK. (AUS) MIXTURE CONTROL CABLE STUCK - CABLE RUNS ADJACENT TO TURBOCHARGER - THROTTLE CABLE AND PROPELLER CONTROL CABLES ALSO RUN ADJACENT TO THE TURBOCHARGER
- [SDR 97ZZZX1589](https://openairdocs.org/sdr/97ZZZX1589), Mar 21, 1997: CYLINDER. HEAD SEPARATED. DURING ANNUAL INSPECTION, FOUND NR 2 CYLINDER HEAD SEPARATING FROM BARREL. THE HEAD WAS TURNED COUNTERCLOCKWISE 4 DEGREES AND WAS .0625 INCH FARTHER FROM FIRST 
- [SDR AU970140](https://openairdocs.org/sdr/AU970140), Jan 27, 1997: ACTUATOR. FAILED. (AUS) NOSE LANDING GEAR HYDRAULIC ACTUATOR FAILED AT FUSELAGE ATTACHMENT POINT
- [SDR 97ZZZX3739](https://openairdocs.org/sdr/97ZZZX3739), Dec 31, 1996: STUD. FAILED. AS A RESULT OF AN ACCIDENT, FOLLOW-UP INVESTIGATION REVEALED THE ENGINE LOST POWER DUE TO FAILURE OF THE ROCKER ARM SHAFT HOLD-DOWN STUDS ON NR 2 CYLINDER. AD 9
- [SDR 96ZZZX5470](https://openairdocs.org/sdr/96ZZZX5470), Sep 10, 1996: LOCK TAB. FAILED. CYLINDERS WERE SENT OUT FOR CHROMING AND OVERHAUL. CYLINDERS WERE RECEIVED BACK READY TO INSTALL. NEW SUPERIOR AIR PARTS ROCKER ARM SHAFT BOLT LOCK TABS WERE IN
- [SDR 95ZZZX5104](https://openairdocs.org/sdr/95ZZZX5104), Aug 1, 1995: PISTON PIN. BROKEN. NR 2 CYLINDER PISTON PIN FAILED AT MIDSECTION (BROKEN IN HALF). SUBSEQUENT FAILURE OF NR 2 PISTON AND METAL CONTAMINATED SUPERIOR AIR PARTS SUPPLIED PISTON PIN 

## STCs that may be installed (OpenAirDocs) (29)

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 TSIO-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 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 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 SE3330NM](https://openairdocs.org/stc/SE3330NM): Continental valve cover gasket. Real Gaskets Tennessee
- [STC SE09846SC](https://openairdocs.org/stc/SE09846SC): Installation of S539800M30 starter adapter springs. Aircraft Specialties Services Inc
- [STC SE624GL](https://openairdocs.org/stc/SE624GL): Incorporation of a fuel flow transducer. Shadin Avionics
- [STC SE1760NM](https://openairdocs.org/stc/SE1760NM): Installation of a pressurized magneto system for Bendix models S6RN-25 and S6LN-25. Sky Services 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 SE3701NM](https://openairdocs.org/stc/SE3701NM): Installation of an intercooler in engine Air induction duct downstream of turbocharger per engine portion. STC SA3700NM is required as part of this installation. Airmotive Industries, Inc
- [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 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 SE4731NM](https://openairdocs.org/stc/SE4731NM): Replace fixed wastegate with a turbocharger differential pressure control system. Merlyn Products Inc
- [STC SE740NE](https://openairdocs.org/stc/SE740NE): Installation of Auto-Vac-4 primary 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 TSIO-360 Series
- [STC SA3701NM](https://openairdocs.org/stc/SA3701NM): Installation of an intercooler in engine air induction duct downstream of the turbocharger. Airflow Systems
- [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 TSIO-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 TSIO-360 Series
- [STC SE102NM](https://openairdocs.org/stc/SE102NM): Installation of magneto pressurization kit. Kim Davidson Avn Inc
- [STC SE235GL](https://openairdocs.org/stc/SE235GL): Installation of a steel pin in Continental fuel pump P/N 634263(TSIO-360-A, -B), 639508 (TSIO-360-C, -D, -E, -F), and 639508(LTSIO-360-E). Approved Aircraft Accessories, Inc

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