# Continental TSIO-360-EB

- Type: Engine model (FAA registry)
- Registry code: 17288
- Manufacturer (registry): CONT MOTOR
- Model: TSIO-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: 13 registered aircraft
- Page: https://openairdocs.org/engine/continental-tsio-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 2023-17-04](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 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
- [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 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 (13)

- [N109WE](https://openairdocs.org/aircraft/N109WE): [Space Coast Aircraft Co](https://openairdocs.org/faa-owner/SPACE%20COAST%20AIRCRAFT%20CO), [Merritt Island, FL](https://openairdocs.org/faa-place/FL/Merritt%20Island), built 1978, S/N 347870405
- [N234TG](https://openairdocs.org/aircraft/N234TG): [Avionicos Corp](https://openairdocs.org/faa-owner/AVIONICOS%20CORP), [Sarasota, FL](https://openairdocs.org/faa-place/FL/Sarasota), S/N 34-8070234
- [N23JC](https://openairdocs.org/aircraft/N23JC): [Jet & Rotor Aviation LLC](https://openairdocs.org/faa-owner/JET%20%26%20ROTOR%20AVIATION%20LLC), [Sacramento, CA](https://openairdocs.org/faa-place/CA/Sacramento), built 1980, S/N 348070121
- [N2610](https://openairdocs.org/aircraft/N2610): [Avionicos Corp](https://openairdocs.org/faa-owner/AVIONICOS%20CORP), [Nokomis, FL](https://openairdocs.org/faa-place/FL/Nokomis), built 1977, S/N 34-7770428
- [N331V](https://openairdocs.org/aircraft/N331V): [Raptor Airmotive LLC](https://openairdocs.org/faa-owner/RAPTOR%20AIRMOTIVE%20LLC), [Poplar Grove, IL](https://openairdocs.org/faa-place/IL/Poplar%20Grove), built 1978, S/N 347870340
- [N4387F](https://openairdocs.org/aircraft/N4387F): [Valiair Lc Trustee](https://openairdocs.org/faa-owner/VALIAIR%20LC%20TRUSTEE), [Casper, WY](https://openairdocs.org/faa-place/WY/Casper), built 1978, S/N 34-7670336
- [N50ZM](https://openairdocs.org/aircraft/N50ZM): [American Air Academy Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIR%20ACADEMY%20INC), [Merritt Island, FL](https://openairdocs.org/faa-place/FL/Merritt%20Island), built 1980, S/N 348070168
- [N6557C](https://openairdocs.org/aircraft/N6557C): [Fox Kilo Aviation Corp](https://openairdocs.org/faa-owner/FOX%20KILO%20AVIATION%20CORP), [Pompano Beach, FL](https://openairdocs.org/faa-place/FL/Pompano%20Beach), built 1976, S/N 347670184, Non-citizen corporation, flight hours not reported
- [N6945F](https://openairdocs.org/aircraft/N6945F): [Euroaviation Inc Trustee](https://openairdocs.org/faa-owner/EUROAVIATION%20INC%20TRUSTEE), Kematen, built 1977, S/N 34-7770049
- [N826VG](https://openairdocs.org/aircraft/N826VG): [A Bit Extra LLC](https://openairdocs.org/faa-owner/A%20BIT%20EXTRA%20LLC), [River Ridge, LA](https://openairdocs.org/faa-place/LA/River%20Ridge), built 1975, S/N 34-7570218
- [N8303U](https://openairdocs.org/aircraft/N8303U): [International Air Service Inc Owner Trustee](https://openairdocs.org/faa-owner/INTERNATIONAL%20AIR%20SERVICE%20INC%20OWNER%20TRUSTEE), [Carson City, NV](https://openairdocs.org/faa-place/NV/Carson%20City), built 1980, S/N 348170048
- [N977SF](https://openairdocs.org/aircraft/N977SF): [Aerospace Trust Management LLC Trustee](https://openairdocs.org/faa-owner/AEROSPACE%20TRUST%20MANAGEMENT%20LLC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1979, S/N 347970169
- [N9996](https://openairdocs.org/aircraft/N9996): [Qualitair LLC](https://openairdocs.org/faa-owner/QUALITAIR%20LLC), Michelstadt, built 1977, S/N 347770163

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports (2)

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 20210725016049I](https://openairdocs.org/incident/20210725016049I), Jul 25, 2021: Piper PA-34-200T (N109WE), Merritt Island, FL, Minor damage. Ramp personnel discovered and reported damaged propeller tips on right engine of N109WE on 7/25/2021. Operator advised FSDO of damage on 7/26/2021. The FAA pmi…
- [Incident 20090826018619I](https://openairdocs.org/incident/20090826018619I), Aug 26, 2009: Piper PA34200T (N449S), Goodyear, AZ, Minor damage. Aircraft was flying on flight training flight and had just landed on rwy 3 at Goodyear airport. The aircraft landed and rolled out with little braking action…

## Service difficulty reports (76, newest 50)

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

- [SDR AYKA20240403108](https://openairdocs.org/sdr/AYKA20240403108), Apr 3, 2024: RETAINER. CRACKED. ROCKER ARM SHAFT RETAINER CONTINENTAL P/N # 631996. FOUND CRACKED RETAINERS DURING ANNUAL INSPECTION WHILE PERFORMING VISUAL INSPECTION. ORDER REPLACEMENTS. OLD
- [SDR 2024FA0000277](https://openairdocs.org/sdr/2024FA0000277), Apr 2, 2024: RETAINER. CRACKED. ROCKER SHAFT RETAINERS CRACKED. X 8 4 ON LEFT ENGINE AND 4 ON RIGHT ENGINE.
- [SDR 2022FA0000485](https://openairdocs.org/sdr/2022FA0000485), Aug 1, 2022: BOLT. USED. LEFT LANDING GEAR SCISSOR LINK CENTER BOLT FAILED DURING TAXI
- [SDR CA190521033](https://openairdocs.org/sdr/CA190521033), May 17, 2019: COTTER PIN. BROKEN. (CAN) DURING ROUTINE MAINTENANCE A PIECE OF METAL WAS FOUND IN THE L/H ENGINE OIL SUMP SCREEN. FURTHER INVESTIGATION FOUND THAT THE COTTER PIN INSTALLED INTO TH
- [SDR CA190405018](https://openairdocs.org/sdr/CA190405018), Apr 5, 2019: SEAL. INADEQUATE. (CAN) RH WINDSHIELD LOWER OUTBOARD CORNER WAS NOT SEALED SUFFICIENTLY AND CAUSED MOISTURE TO ENTER STRUCTURE. THE STEEL BRACKET BELOW THIS CORNER HAD ACCUMULATE
- [SDR APCA2016072600001](https://openairdocs.org/sdr/APCA2016072600001), Jul 26, 2016: STUD. BROKEN. CYLINDER NR 6 HAD BROKEN BOTH EXHAUST ROCKER SHAFT STUDS. HAPPENED ON SAME CYLINDER APPROXIMATELY 200 HOURS AGO ON A FACTORY CYLINDER WITH 1000 HOURS. PUSH ROD 
- [SDR CA140822003](https://openairdocs.org/sdr/CA140822003), Aug 7, 2014: CRANKSHAFT. CRACKED. (CAN) DURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED ON THE ENGINE CRANKSHAFT FLANGE, WHERE THE PROPELLER MOUNTS. THE CRACK WAS VERY SEVERE AS VERY TINY PI
- [SDR CA121214007](https://openairdocs.org/sdr/CA121214007), Dec 14, 2012: TRUNNION. CRACKED. (CAN) DURING ANNUAL INSPECTION, THE ENGINEER VISUALLY INSPECTING THE MAIN LANDING GEAR NOTICED A CRACK MIGRATING OUT OF THE LOWER BOLT HOLE OF LT FWD MLG ATTACH
- [SDR 2012FA0000133](https://openairdocs.org/sdr/2012FA0000133), Feb 24, 2012: TRUNNION. WORN. DURING AN INSPECTION OF THE MLG, THE GEAR TRUNNION MOUNTING PLATES BOLTS WERE FOUND TO BE WITHIN TORQUE LIMITS, BUT LOOSE IN THE PLATES AND SPARS, REMOVED PLATE
- [SDR 2012FA0000134](https://openairdocs.org/sdr/2012FA0000134), Feb 24, 2012: TRUNNION. WORN. DURING AN INSPECTION OF THE MLG, TRUNNION MOUNTING PLATES BOLTS FOUND TO BE WITHIN TORQUE LIMITS, BUT LOOSE IN THE PLATES AND SPARS, REMOVED PLATES AND FOUND MO
- [SDR 2012FA0000089](https://openairdocs.org/sdr/2012FA0000089), Feb 1, 2012: SEAL. FROZEN. DEPARTED AND CLIMBED THROUGH MODERATE TO HEAVY PARTICIPATION FOR 10-15 MINUTES, LEVELED OFF AT 9,000 FT WHICH WAS AN ALTITUDE THAT WAS BELOW FREEZING. SET AUTOP
- [SDR CA110719006](https://openairdocs.org/sdr/CA110719006), Jul 19, 2011: MAGNETO. DEPARTED. DURING ENGINE THE PRE-FLIGHT RUN UP THE PILOTS NOTICED RT ENGINE ROUGHNESS AND LT MAGNETO DROP WAS EXCESSIVE. ACFT RETURNED TO CHOCKS AND FLIGHT WAS CANCELLED. 
- [SDR 2011FA0000402](https://openairdocs.org/sdr/2011FA0000402), Jun 7, 2011: ADAPTER. SLIPPED. THE STARTER ADAPTER WAS SENT IN FOR REPAIR, UPON DISASSEMBLY, OUR FINDINGS, THE STARTER ADAPTER WAS SLIPPING DUE TO EXCESSIVE STARTER ENGAGEMENT WHICH OVERHEATE
- [SDR 2011F00018](https://openairdocs.org/sdr/2011F00018), Jan 16, 2011: CYLINDER. FAILED. PILOT NOTED REDUCTION IN MANIFOLD PRESSURE AND OIL PRESSURE ON LT ENGINE. PILOT REDUCED POWER TO IDLE AND REQUESTED LANDING AT NEAREST AIRPORT. POST LANDING INS
- [SDR FFKA139](https://openairdocs.org/sdr/FFKA139), Jul 6, 2009: STUD. SHEARED. PILOT REPORTED-ENG ROUGHNESS, WAS NOTICED ON THE LT ENGINE, TURNED ON THE AUXILIARY FUEL PUMP AND ENGINE BEGAN TO RUN BETTER BUT UNABLE TO MATCH MANIFOLD TO RT 
- [SDR FFKA138](https://openairdocs.org/sdr/FFKA138), May 11, 2009: OIL COOLER. LEAKING. IN CRUISE FLIGHT PILOT NOTICED LOW OIL PRESSURE LIGHT ILLUMINATED AND THE LEFT ENGINE OIL PRESSURE GAUGE DROPPING TO ZERO. PILOT PERFORMED ENGINE SHUTDOWN AND L
- [SDR FFK2008F00002](https://openairdocs.org/sdr/FFK2008F00002), Sep 2, 2008: CAM. WORN. PILOT REPORTED A "POPPING" SOUND COMING FROM THE LT ENGINE, AFTER INVESTIGATION MAINT FOUND THAT THE LT ENGINE LT MAGNETO CAM FOLLOWER EXCESSIVELY WORN. REPLACE
- [SDR CA080317004](https://openairdocs.org/sdr/CA080317004), Feb 14, 2008: GEAR. FAILED. (CAN) LOW OIL PRESSURE LIGHT CAME ON IMMEDIATELY AFTER TAKEOFF. PWR WAS BROUGHT BACK AND AC RETURNED FOR SAFE LANDING. ENGINE WAS SHUTDOWN OFF RUNWAY, PROP FEAT
- [SDR FFKA118](https://openairdocs.org/sdr/FFKA118), May 17, 2007: CRANKSHAFT. CRACKED. PILOT REPORTED AN OIL LEAK COMING FROM THE LEFT (NR 1) ENGINE AFTER FINISHING THEIR FLIGHT FOR THE DAY. MAINTENANCE INVESTIGATED THE OIL LEAK AND FOUND THE CRAN
- [SDR 2007FA0000277](https://openairdocs.org/sdr/2007FA0000277), Mar 22, 2007: CRANKSHAFT. FAILED. CRANKSHAFT FAILED NDI SB MSB96-10. (K)
- [SDR FFKA1020112](https://openairdocs.org/sdr/FFKA1020112), Oct 19, 2006: ADAPTER. BROKEN. FUEL FITTING ADAPTER P/N 630119 BROKE IN HALF CAUSING A LOSS OF POWER.
- [SDR CA050913008](https://openairdocs.org/sdr/CA050913008), Sep 1, 2005: O-RING. WORN. (CAN) PILOT REPORTED THAT LANDING GEAR FAILED TO RETRACT. AIRCRAFT PLACED ON JACKS, LANDING GEAR SWUNG, FOUND NOSE GEAR ACTUATOR FAILED TO COMPLETELY RETRACT. R
- [SDR CA050505003](https://openairdocs.org/sdr/CA050505003), Apr 25, 2005: WHEEL. CRACKED. (CAN) ON LANDING PILOT REPORTED A NOISE FROM THE LT MAIN LANDING GEAR. INSPECTION FOUND THE INNER WHEEL HALF CRACKED AT THE BASE OF THE WHEEL FLANGE FOR APPROX 
- [SDR CA050414009](https://openairdocs.org/sdr/CA050414009), Apr 14, 2005: BEARING. CHIPPED. (CAN) HUB P/N D2201-18, CHIPPED IN TWO PLACES AND TOOL MARK ALL IN A 1 INCH AREA ON INSTALLATION SEAL LIP. FORK P/N WORN BEYOND MAXIMUN/M LIMITS T/2 BEARINGS P/
- [SDR CA050401008](https://openairdocs.org/sdr/CA050401008), Mar 24, 2005: ALTERNATOR. FAILED. (CAN) ALTERNATOR FAILURE, SEPARATION OF DRIVE GEAR DUE TO SHEARED ROTOR SHAFT. METAL CONTAMINATION OF ENGINE.
- [SDR 2004FA0000874](https://openairdocs.org/sdr/2004FA0000874), Oct 6, 2004: IMPULSE COUPLING. MISSING. WHILE PERFORMING AD 96-12-07, THE MECHANIC NOTICED THAT THE STOP PIN FOR THE IMPULSE COUPLING WAS MISSING. INSPECTED THE ACCESSORY SECTION AND FOUND THE PIN WED
- [SDR CA040830002](https://openairdocs.org/sdr/CA040830002), Aug 26, 2004: NUT. FAILED. (CAN) DISCOVERED RT FWD TRUNION FITTING ATTACH BOLT ANCHOR NUT NOT RETAINING TORQUE DURING INSPECTION OF LANDING GEAR. LANDING GEAR REMOVED TO FACILITATE ANCHOR
- [SDR CA030324004](https://openairdocs.org/sdr/CA030324004), Mar 17, 2003: MOUNT. CRACKED. (CAN) LOWER PORTION OF MOUNT ASSEMBLY TUBULAR STRUCTURE CRACKED, MOUNT MUST BE REMOVED TO FURTHER EVALUATEI.E. STRIP AND NDT INSPECTION BEFORE REPAIR STATUS CAN
- [SDR AYQ2004F00000](https://openairdocs.org/sdr/AYQ2004F00000), Jan 23, 2003: IMPULSE COUPLING. INOPERATIVE. DEAD MAGNETO ON RUN UP. FOUND MAGNETO ROTATED IN ITS CLAMPS, TIMING WAY OFF. REMOVED MAG AND FOUND IMPULSE COUPLING MISSING CORNER OF PAWL PLATE.
- [SDR 2002FA0001153](https://openairdocs.org/sdr/2002FA0001153), Aug 22, 2002: DRIVE SHAFT. FAILED. RT ENGINE LOST OIL PRESSURE AFTER TAKEOFF DISASSEMBLY REVEALED BROKEN OIL PUMP DRIVE SHAFT/GEAR. SHAFT IS THE WEAK LINK.
- [SDR 2002FA0000953](https://openairdocs.org/sdr/2002FA0000953), Jul 24, 2002: RETAINER. CRACKED. DURING AN ANNUAL INSPECTION, ONE ROCKER BOX COVER ON THE LEFT ENGINE WAS REMOVED IN THE PROCESS OF REPLACING PUSHROD TUBE SEALS. DISCOVERED ONE ROCKER SHAFT RET
- [SDR CA020725006](https://openairdocs.org/sdr/CA020725006), Jul 7, 2002: BEARING. BROKEN. (CAN) ON A TRAINING FLIGHT IN CRUISE PILOTS OBSERVED LOW OIL PRESSURE LIGHT ILLUMINATION ON THE LT ENGINE AND NO OIL PRESSURE ON THE GAUGE. THE PROPELLER FEATHE
- [SDR CA020521005](https://openairdocs.org/sdr/CA020521005), May 13, 2002: CYLINDER. CRACKED. (CAN) STEEL BARREL CRACKED AROUND CIRCUMFERENCE JUST BELOW HEAD ATTACH AREA. 90 PERCENT.
- [SDR 2002FA0000310](https://openairdocs.org/sdr/2002FA0000310), Feb 22, 2002: MASTER SWITCH. BROKEN. THE MASTER SWITCH IS DIVIDED INTO TWO SWITCHES A THAT ARE COUPLED TOGETHER WITH A PLASTIC TAB. THE HALF OF THE SWITCH THAT CONTROLS THE ALTERNATOR FIELDS IS HID
- [SDR CTU2002F00003](https://openairdocs.org/sdr/CTU2002F00003), Feb 22, 2002: MASTER SWITCH. BROKEN. THE MASTER SWITCH IS DIVIDED INTO TWO SWITCHES THAT ARE COUPLED TOGETHER WITH A PLASTIC TAB. THE HALF OF THE SWITCH THAT CONTROLS THE ALTERNATOR FIELDS IS HIDDE
- [SDR 2004FA0000626](https://openairdocs.org/sdr/2004FA0000626), Jan 16, 2002: CRANKCASE. CRACKED. THE TURBOCHARGER ATTACHES TO THE ENGINE RT CRANKCASE, THROUGH A 21 INCH MOUNTING BRACKET, WHICH ATTACHES TO THE RT AFT ENGINE MOUNT. DURING A ROUTINE 100 HR INS
- [SDR 2004FA0000627](https://openairdocs.org/sdr/2004FA0000627), Jan 16, 2002: CRANKCASE. CRACKED. THE TURBOCHARGER ATTACHES TO THE ENGINE RT CRANKCASE, THROUGH A 21 INCH MOUNTING BRACKET, WHICH ATTACHES TO THE RT AFT ENGINE MOUNT. DURING A ROUTINE 100 HR INS
- [SDR 2002FA0000154](https://openairdocs.org/sdr/2002FA0000154), Dec 31, 2001: CYLINDER HEAD. SEPARATED. DURING LEVEL FLIGHT THE LEFT ENGINE STARTED RUNNING VERY ROUGH. ENGINE FEATHERED AND AIRCRAFT RETURNED TO AIRPORT. ENGINE UNCOWLED AND NR 5 CYLINDER HEAD WAS FO
- [SDR EEJ2001F00001](https://openairdocs.org/sdr/EEJ2001F00001), Oct 12, 2001: CHANNEL. CRACKED. NOSE WHEEL STEERING CHANNEL CRACKED AT RIGHT REAR WELD. MADE POPPING NOISE WHILE TAXING. DUE TO STEERING AIRCRAFT ON GROUND, NOSE WHEEL STEERING (WHERE BALL GOE
- [SDR CA010322002](https://openairdocs.org/sdr/CA010322002), Feb 8, 2001: LINER. DESTROYED. (CAN) WHILE CONDUCTING A GENERAL WALK AROUND FOR A PRE-PURCHASE, THE INBOARD PRESSURE PLATE SIDE OF THE BRAKE CALIPERS, THE BRAKE LINERS WERE TOTALLY DESTROYED,
- [SDR 20010305CW012](https://openairdocs.org/sdr/20010305CW012), Jan 25, 2001: ADAPTER. FAILED. 90 DEGREE TACH DRIVE ADAPTER PUT ON AIRCRAFT. WHEN ADAPTER FAILS, THERE IS NO RPM INDICATION TO TACH. PROBLEM, APPARENTLY VIBRATION INDUCED. SOME PROVISIONS SHO
- [SDR 20010222CW002](https://openairdocs.org/sdr/20010222CW002), Jan 23, 2001: COUPLER. FAILED. RT ALTERNATOR FAILED IN FLIGHT AT NIGHT. ALTERNATOR FAILURE CAUSED BY DRIVE COUPLER FAILURE.
- [SDR 20010301CW007](https://openairdocs.org/sdr/20010301CW007), Jan 23, 2001: COUPLER. FAILED. LT ALTERNATOR FAILED IN FLIGHT AT NIGHT. ALTERNATOR FAILURE CAUSE: DRIVE COUPLER FAILURE.
- [SDR 20010305CW011](https://openairdocs.org/sdr/20010305CW011), Jan 23, 2001: ADAPTER. FAILED. 90 DEGREE TACH DRIVE ADAPTER PUT ON AIRCRAFT. WHEN ADAPTER FAILS, THERE IS NO RPM INDICATION TO TACH. PROBLEM APPARENTLY VIBRATION INDUCED. SOME PROVISION SHOUL
- [SDR CA001212018](https://openairdocs.org/sdr/CA001212018), Nov 24, 2000: NUT. CRACKED. (CAN) THREE NUTS USED TO ATTACH THE LOWER END OF THE MAIN WING LONGERON TO THE INTERIOR LONGERON WERE FOUND CRACKED.ACCORDING TO A PIPER REP FOR API, THE SAME T
- [SDR 2002FA0000131](https://openairdocs.org/sdr/2002FA0000131), Aug 28, 2000: PUSHROD. CRACKED. ON ANNUAL INSPECTION OF THE LEFT ENGINE THREE PUSHRODS WERE NOTED TO BE CRACKED ALONG WHAT LOOKS LIKE THEIR ENTIRE LENGTHS. THE THREE DEFECTIVE PUSHRODS WERE RE
- [SDR 20000821SH001](https://openairdocs.org/sdr/20000821SH001), Aug 8, 2000: SEAL. WORN. 372 HOURS TOTAL TIME SINCE NEW. RETAINER SPRINGS FELL OFF OF SEAL AND INTO THE OIL SYSTEM. NO DAMAGE CAUSED. THEY WERE CAUGHT IN OIL SCREEN. UPON REMOVAL OF VAL
- [SDR 20000515SH009](https://openairdocs.org/sdr/20000515SH009), Apr 20, 2000: GEAR. MISMANUFACTURED. NEW OIL PUMP DRIVEN GEAR DOES NOT HAVE THE CHAMFER ON THE INSIDE OF THE TWO DRIVE SLOTS. THIS IS A MFG''S DEFECT. WHEN THE DRIVE IMPELLER NR 653814 IS INSTALLED
- [SDR CA000301041](https://openairdocs.org/sdr/CA000301041), Feb 17, 2000: FUEL CELL. CONTAMINATED. (CAN) WATER AND ICE IN FUEL SYSTEM.
- [SDR CA990303003](https://openairdocs.org/sdr/CA990303003), Feb 19, 1999: HUB. CORRODED. (CAN) INSPECTION FOUND CORROSION ON THE HUB TO ENGINE MOUNTING FLANGE. THE BEARING RACES WERE ALSO DENTED BY THE BALLBEARINGS. THE HUB WAS OVERHAULED AND THE BE

All 76: https://openairdocs.org/engine/continental-tsio-360-eb/reports.md

## 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 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 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 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 SE09401SC](https://openairdocs.org/stc/SE09401SC): Installation of modified fuel injector nozzles. General Aviation Modifications, Inc
- [STC SE00350SE](https://openairdocs.org/stc/SE00350SE): Installation of sump mounted chip detector. Aviation Development Corporation
- [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 TSIO-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 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

---
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.