# Continental TSIO-360-FB - Type: Engine model (FAA registry) - Registry code: 17292 - Manufacturer (registry): CONT MOTOR - Model: TSIO-360-FB - Engine type: Reciprocating - Power: 200 hp - Data sheet: [TCDS E9CE](https://openairdocs.org/tcds/E9CE) (OpenAirDocs) - Holder: Continental Aerospace Technologies, Inc. - Installed in: 29 registered aircraft - Page: https://openairdocs.org/engine/continental-tsio-360-fb 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 (29) - [N109KB](https://openairdocs.org/aircraft/N109KB): [Wings Aviation Inc](https://openairdocs.org/faa-owner/WINGS%20AVIATION%20INC), [Valparaiso, IN](https://openairdocs.org/faa-place/IN/Valparaiso), built 1978, S/N 28R7803043 - [N142MS](https://openairdocs.org/aircraft/N142MS): [Plane Fun Inc Tr Trustee](https://openairdocs.org/faa-owner/PLANE%20FUN%20INC%20TR%20TRUSTEE), [Snellville, GA](https://openairdocs.org/faa-place/GA/Snellville), S/N 28R-8331017 - [N17SG](https://openairdocs.org/aircraft/N17SG): [Helisur USA LLC](https://openairdocs.org/faa-owner/HELISUR%20USA%20LLC), [Pembroke Pines, FL](https://openairdocs.org/faa-place/FL/Pembroke%20Pines), built 1982, S/N 28R-8231060 - [N207HV](https://openairdocs.org/aircraft/N207HV): [Euroaviation Inc Trustee](https://openairdocs.org/faa-owner/EUROAVIATION%20INC%20TRUSTEE), Kematen, built 1978, S/N 28R7803303 - [N211DC](https://openairdocs.org/aircraft/N211DC): [N211dc LLC](https://openairdocs.org/faa-owner/N211DC%20LLC), [Los Angeles, CA](https://openairdocs.org/faa-place/CA/Los%20Angeles), built 1979, S/N 28-7921037 - [N2148X](https://openairdocs.org/aircraft/N2148X): [Mckinley John Perry](https://openairdocs.org/faa-owner/MCKINLEY%20JOHN%20PERRY), [Amarillo, TX](https://openairdocs.org/faa-place/TX/Amarillo), built 1979, S/N 28R-7931129 - [N2158V](https://openairdocs.org/aircraft/N2158V): [De Sousa Jorge Norberto Freitas](https://openairdocs.org/faa-owner/DE%20SOUSA%20JORGE%20NORBERTO%20FREITAS), [Cape Coral, FL](https://openairdocs.org/faa-place/FL/Cape%20Coral), built 1978, S/N 28R-7803151 - [N2230Q](https://openairdocs.org/aircraft/N2230Q): [Schmidt John J](https://openairdocs.org/faa-owner/SCHMIDT%20JOHN%20J), [Pueblo West, CO](https://openairdocs.org/faa-place/CO/Pueblo%20West), built 1979, S/N 28R-7931072 - [N277MH](https://openairdocs.org/aircraft/N277MH): [Euroaviation Inc Trustee](https://openairdocs.org/faa-owner/EUROAVIATION%20INC%20TRUSTEE), Kematen, built 1982, S/N 28R8231035 - [N2879W](https://openairdocs.org/aircraft/N2879W): [Evenson Paul S](https://openairdocs.org/faa-owner/EVENSON%20PAUL%20S), [Grant, MN](https://openairdocs.org/faa-place/MN/Grant), built 1979, S/N 28R-7931239 - [N29FZ](https://openairdocs.org/aircraft/N29FZ): [Trn Aviation LLC](https://openairdocs.org/faa-owner/TRN%20AVIATION%20LLC), [Mcallen, TX](https://openairdocs.org/faa-place/TX/Mcallen), built 1977, S/N 28R7703052 - [N321CN](https://openairdocs.org/aircraft/N321CN): [International Air Services Inc Trustee](https://openairdocs.org/faa-owner/INTERNATIONAL%20AIR%20SERVICES%20INC%20TRUSTEE), [Carson City, NV](https://openairdocs.org/faa-place/NV/Carson%20City), built 1978, S/N 28R7803166 - [N35636](https://openairdocs.org/aircraft/N35636): [Carreno Miriam](https://openairdocs.org/faa-owner/CARRENO%20MIRIAM), [Portland, OR](https://openairdocs.org/faa-place/OR/Portland), built 1979, S/N 28R-8031036 - [N41GF](https://openairdocs.org/aircraft/N41GF): [Mesmer Refrigeration Inc](https://openairdocs.org/faa-owner/MESMER%20REFRIGERATION%20INC), [Buffalo, NY](https://openairdocs.org/faa-place/NY/Buffalo), built 1977, S/N 28R-7703083 - [N425K](https://openairdocs.org/aircraft/N425K): [Plane Fun Inc Tr Trustee](https://openairdocs.org/faa-owner/PLANE%20FUN%20INC%20TR%20TRUSTEE), [Snellville, GA](https://openairdocs.org/faa-place/GA/Snellville), built 1979, S/N 28R7931243 - [N540AG](https://openairdocs.org/aircraft/N540AG): [Aircraft Guaranty Corp Trustee](https://openairdocs.org/faa-owner/AIRCRAFT%20GUARANTY%20CORP%20TRUSTEE), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City), built 1984, S/N 28R8431025 - [N577EA](https://openairdocs.org/aircraft/N577EA): [Qualitair LLC Trustee](https://openairdocs.org/faa-owner/QUALITAIR%20LLC%20TRUSTEE), Michelstadt, built 1979, S/N 28R7931157 - [N579GZ](https://openairdocs.org/aircraft/N579GZ): [Euroaviation Inc Trustee](https://openairdocs.org/faa-owner/EUROAVIATION%20INC%20TRUSTEE), Kematen, built 1978, S/N 28R7803212 - [N642CF](https://openairdocs.org/aircraft/N642CF): [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 28R8031155 - [N687TJ](https://openairdocs.org/aircraft/N687TJ): [Mirarchi Joseph F](https://openairdocs.org/faa-owner/MIRARCHI%20JOSEPH%20F), [New Braunfels, TX](https://openairdocs.org/faa-place/TX/New%20Braunfels), built 1977, S/N 28R7703235 - [N81053](https://openairdocs.org/aircraft/N81053): [Wernimont Thomas R](https://openairdocs.org/faa-owner/WERNIMONT%20THOMAS%20R), [Spring Valley, WI](https://openairdocs.org/faa-place/WI/Spring%20Valley), S/N 28R-8031010 - [N8238X](https://openairdocs.org/aircraft/N8238X): [International Air Services Inc Owner Trustee](https://openairdocs.org/faa-owner/INTERNATIONAL%20AIR%20SERVICES%20INC%20OWNER%20TRUSTEE), [Carson City, NV](https://openairdocs.org/faa-place/NV/Carson%20City), built 1982, S/N 28R8231059 - [N832JA](https://openairdocs.org/aircraft/N832JA): [Moore Jimmy L](https://openairdocs.org/faa-owner/MOORE%20JIMMY%20L), [Beach City, TX](https://openairdocs.org/faa-place/TX/Beach%20City), built 1979, S/N 28R7931187 - [N8406T](https://openairdocs.org/aircraft/N8406T): [Cook Neal L](https://openairdocs.org/faa-owner/COOK%20NEAL%20L), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), built 1981, S/N 28R-8131161 - [N842TS](https://openairdocs.org/aircraft/N842TS): [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 1997, S/N 28R-7703180 - [N871MS](https://openairdocs.org/aircraft/N871MS): [Lackey Christopher Donald](https://openairdocs.org/faa-owner/LACKEY%20CHRISTOPHER%20DONALD), [Helotes, TX](https://openairdocs.org/faa-place/TX/Helotes), built 1981, S/N 28R-8131167 - [N972QJ](https://openairdocs.org/aircraft/N972QJ): [Invictus Health LLC](https://openairdocs.org/faa-owner/INVICTUS%20HEALTH%20LLC), [Yorktown, VA](https://openairdocs.org/faa-place/VA/Yorktown), built 1978, S/N 28R7803366 - [N987DC](https://openairdocs.org/aircraft/N987DC): [Lewis Michael](https://openairdocs.org/faa-owner/LEWIS%20MICHAEL), [Anaheim, CA](https://openairdocs.org/faa-place/CA/Anaheim), built 1980, S/N 28R8031103 - [N9FS](https://openairdocs.org/aircraft/N9FS): [Eagle Ey5 LLC](https://openairdocs.org/faa-owner/EAGLE%20EY5%20LLC), [Ashland, MO](https://openairdocs.org/faa-place/MO/Ashland), built 1977, S/N 28R7703378 ## 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 CEN13WA307](https://openairdocs.org/ntsb/CEN13WA307), May 29, 2013: Piper PA-28RT-201T (N68XM), Tallard, France, destroyed, 1 fatal ## FAA accident and incident reports None matched to aircraft with this engine model. ## Service difficulty reports (49) As reported by operators and repair stations, by the model named in the report. - [SDR 2015FA0000189](https://openairdocs.org/sdr/2015FA0000189), May 11, 2015: CABLE. WORN. COWL FLAP CABLE RUBBING ON EXHAUST ON LT SIDE OF ENGINE. RUBBED THROUGH THE OUTER COVER AND HALF THROUGH THE INNER CORE. THIS ACFT HAS HAD A REPLACEMENT COWL IN - [SDR 2015FA0000190](https://openairdocs.org/sdr/2015FA0000190), May 11, 2015: HOUSING. WORN. REPLACED COWL FLAP CABLE, PN LSM-SCD-032-1 DUE TO WORN SPOT NEAR CONNECTION TO COWL. COWL HAS BEEN REPLACE IAW STC SA03470AT. ACFT HAD TO MAKE AN UNSCHEDULED ST - [SDR 2013FA0000438](https://openairdocs.org/sdr/2013FA0000438), Jul 19, 2013: SWITCH. SHORTED. ACFT DEPARTED, DURING INITIAL CLIMB, EXPERIENCED A LOSS OF POWER AT APPROX 1000 FT AGL. PILOT SWITCHED FUEL TANKS, CYCLED FUEL PUMP, AND MAGNETOS IN AN ATTEMPT - [SDR CA130412007](https://openairdocs.org/sdr/CA130412007), Apr 12, 2013: HUB. DAMAGED. (CAN) UPON DISASEMBLY OF THE PROPELLER THE PRELOAD SHELVES SHOWED EVIDENCE OF PREVIOUS SEVERE PROPELLER IMPACT DAMAGE. ACCORDING TO PROPELLER MANUAL 202A THERE - [SDR CA120607009](https://openairdocs.org/sdr/CA120607009), Jun 5, 2012: COUPLING. FAILED. (CAN) ELECTRICAL FAILURE REPORTED. INSPECTED CHARGING SYS AND FOUND ALTERNATOR DRIVE COUPLING FAILED. - [SDR CA111107008](https://openairdocs.org/sdr/CA111107008), Nov 2, 2011: FAIRING. DAMAGED. (CAN) VERTICAL FIN AFT TIP FAIRING FOUND CONTACTING RUDDER TOP SURFACE DURING GROUND HANDLING AND PRE-FLIGHT INSPECTION. FAIRING REMOVED AND FOUND MOUNTING HARD - [SDR CA110906002](https://openairdocs.org/sdr/CA110906002), Sep 6, 2011: FORK. DAMAGED. (CAN) UPON DISASSEMBLY AND VISUAL INSP OF THIS PROPELLER, WE FOUND 1 EA, A-2202 BEARING TO BE DENTED BEYOND REPAIR, THE HUB PRELOAD SHELVES TO BE DAMAGED FROM P - [SDR 2011FA0000406](https://openairdocs.org/sdr/2011FA0000406), Apr 21, 2011: SEAL. FAILED. OVERHAULED AND INSTALLED CYLINDERS, PN EC641370CN IAW SERVICE INFO AND MFG SERVICE INFORMATION. DURING THE OVERHAUL INTAKE VALVE SEALS PN 646678 WERE INSTALLED - [SDR 2011FA0000407](https://openairdocs.org/sdr/2011FA0000407), Apr 21, 2011: SEAL. FAILED. OVERHAULED AND INSTALLED CYLINDERS, PN EC641370CN IAW SERVICE INFO AND MFG SERVICE INFORMATION. DURING THE OVERHAUL INTAKE VALVE SEALS PN 646678 WERE INSTALLED - [SDR 2011FA0000408](https://openairdocs.org/sdr/2011FA0000408), Apr 21, 2011: SEAL. FAILED. OVERHAULED AND INSTALLED CYLINDERS, PN EC641370CN IAW SERVICE INFO AND MFG SERVICE INFORMATION. DURING THE OVERHAUL INTAKE VALVE SEALS PN 646678 WERE INSTALLED - [SDR 2011FA0000409](https://openairdocs.org/sdr/2011FA0000409), Apr 21, 2011: SEAL. FAILED. OVERHAULED AND INSTALLED CYLINDERS, PN EC641370CN IAW SERVICE INFO AND MFG SERVICE INFORMATION. DURING THE OVERHAUL INTAKE VALVE SEALS PN 646678 WERE INSTALLED - [SDR 2011FA0000410](https://openairdocs.org/sdr/2011FA0000410), Mar 21, 2011: SEAL. FAILED. OVERHAULED AND INSTALLED CYLINDERS, PN EC641370CN IAW SERVICE INFO AND MFG SERVICE INFORMATION. DURING THE OVERHAUL INTAKE VALVE SEALS PN 646678 WERE INSTALLED - [SDR 2011FA0000411](https://openairdocs.org/sdr/2011FA0000411), Mar 21, 2011: SEAL. FAILED. OVERHAULED AND INSTALLED CYLINDERS, PN EC641370CN IAW SERVICE INFO AND MFG SERVICE INFORMATION. DURING THE OVERHAUL INTAKE VALVE SEALS PN 646678 WERE INSTALLED - [SDR CA110215006](https://openairdocs.org/sdr/CA110215006), Feb 10, 2011: TUBE. LOOSE. DURING THE ANNUAL INSP OF THE ACFT, THE STABILATOR BALANCE WEIGHT TUBE WAS FOUND TO BE LOOSE. THERE ARE 2 ATTACH BOLTS. THE FWD ATTACH BOLT WAS LOOSE AND WAS RE - [SDR 2011FA0000168](https://openairdocs.org/sdr/2011FA0000168), Feb 3, 2011: LINK. CRACKED. CRACK DISCOVERED IN FWD FACING RADIUS OF NOSE GEAR RETRACTION CYLINDER AND DOWN LOCK ATTACHMENT TANG DURING ANNUAL INSP. REPLACED ENTIRE NOSE GEAR LINK AND BRAC - [SDR CA090520002](https://openairdocs.org/sdr/CA090520002), May 1, 2009: PACKING. MISMANUFACTURED. (CAN) ENGINE WAS REMOVED DUE TO LOW OIL PRESSURE IN FLIGHT. UPON INSP IT WAS FOUND THAT THE NYLON PACKING INSIDE THE FRONT MAIN BEARING SHELLS WERE TOO SHORT. T - [SDR CA090326013](https://openairdocs.org/sdr/CA090326013), Mar 26, 2009: DIMMER. OVERHEATED. (CAN) PILOT OBSERVED SMOKE AND ODOR COMING FROM INSTRUMENT PANEL IN THE AREA OF ELECTRICAL SWITCHES, ELECTRICAL SYS WAS SWITCHED OFF AND ACFT LANDED SUCCESSFULL - [SDR CA090112008](https://openairdocs.org/sdr/CA090112008), Oct 31, 2008: GASKET. LEAKING. (CAN) ENGINE INSPECTED FOR OIL LEAK AT REAR ACCESSORY SECTION, FOUND OIL COMING FROM RIGHT MAGNETO ATTACH GASKET. MAGNETO REMOVED, GASKET AND ENGINE MATING SURF - [SDR 2008FA0000243](https://openairdocs.org/sdr/2008FA0000243), Apr 10, 2008: TURBOCHARGER. FOD. TURBOCHARGER COMPRESSOR DAMAGED BY FOD INGESTED THROUGH THE ALTERNATE AIR DOOR. THIS DOOR IS ON TOP OF THE AIR FILTER BOX ALLOWING ANY OBJECT THROWN UP BY THE N - [SDR UQM2005F00000](https://openairdocs.org/sdr/UQM2005F00000), Dec 8, 2004: CRANKSHAFT. BROKEN. AFTER INSTALLING REBUILT MAGS, TEST RAN AND WAS KNOCKING. REMOVED NR 1 CYLINDER AND FOUND CRANKSHAFT BROKEN AT THE JOURNAL. I FEEL THE CRANK MAY BE BROKEN IN AN - [SDR UQM2005F00001](https://openairdocs.org/sdr/UQM2005F00001), Nov 18, 2004: MAGNETO. FAILED. PILOT WAS FLYING AT 7000 FT AND LOST POWER. ENGINE WENT TO IDLE. MADE A SAFE LANDING. AFTER COMING TO A STOP THE ENGINE WS NOT RUNNING. FOUND THE MAGS BOTH LT A - [SDR UQM2005F00002](https://openairdocs.org/sdr/UQM2005F00002), Nov 18, 2004: MAGNETO. FAILED. PILOT WAS FLYING AT 7000 FT AND LOST POWER. HE SAID ENGINE WENT TO IDLE. HE MADE A SAFE LANDING. AFTER COMING TO A STOP THE ENGINE WAS NOT RUNNING. FOUND THE MA - [SDR CA041013007](https://openairdocs.org/sdr/CA041013007), Sep 16, 2004: FITTING. CRACKED. (CAN) BRASS OUTLET ANGLE FITTING ON FUEL PUMP CRACKED CAUSING FUEL TO LEAK OUT IN FLIGHT. - [SDR 2004FA0000339](https://openairdocs.org/sdr/2004FA0000339), Mar 23, 2004: HOUSING. CRACKED. REMOVED TURBO FOR OTHER WORK, INSPECTED HOUSING PN 600510-04 AND FOUND IT TO BE CRACKED AS SHOWN IN AD 82-27-03 FIGURE 2, AD 82-27-03 DOES NOT APPLY TO THIS HOU - [SDR 2003FA0000939](https://openairdocs.org/sdr/2003FA0000939), Sep 17, 2003: ATTACH FITTING. CRACKED. COMPONENT WAS CRACKED IN THREE PLACES, THIS IS IN THE DRIVE ATTACHMENT BASE. (JUST FORWARD OF THE ATTACHMENT PLATE), ON THE WEB THAT SECURES THE ALTERNATOR. OWN - [SDR 920DM](https://openairdocs.org/sdr/920DM), Aug 12, 2002: VALVE GUIDE. BROKEN. CYLINDER WAS REMOVED FOR LEAKING EXHAUST VALVE BY CUSTOMER. UPON DISASSEMBLY AND REMOVAL OF LOWER VALVE SPRING RETAINER, THE GUIDE WAS FOUND TO BE IN TWO PIECES - [SDR 2002FA0000217](https://openairdocs.org/sdr/2002FA0000217), Feb 15, 2002: LINE. WORN. ENGINE LOST OIL PRESSURE IN CRUISE FLIGHT. THE PILOT MADE AN UNSCHEDULED LANDING. INVESTIGATION REVEALED THAT THE OIL FILLER CAP HAD COME OFF AND THE ENGINE LOS - [SDR 2001FA0000376](https://openairdocs.org/sdr/2001FA0000376), Oct 2, 2001: ISOLATOR. BURNED OUT. IN CRUISE FLIGHT NOTICED THE AMP GAUGE WAS SHOWING THE ALTERNATOR PUTTING OUT OVER 45 TO 50 AMPS. DME DROPPED OF LINE, LOST THE TRANSPONDER SIGNAL. VFR CONDITIO - [SDR CA010627054](https://openairdocs.org/sdr/CA010627054), Jun 8, 2001: TRUNNION. CRACKED. (CAN) WHILE INSPECTING SHIMMEY DAMPENER AS PART OF 100 HOUR INSPECTION. IT WAS DISCOVERED THAT THE NLG TRUNNION ASSEMBLY WAS CRACKED AT SHIMMEY DAMPENE R ATTACH - [SDR 20000425SH039](https://openairdocs.org/sdr/20000425SH039), Apr 3, 2000: DRIVE GEAR. BROKEN. PILOT WAS IN-FLIGHT WHEN ENGINE FAILED. PILOT PERFORMED EMERGENCY PROCEDURES AND RETURNED TO AIRPORT. INSPECTION REVEALED THE GOVERNOR DRIVE GEAR HAD FAILED. GO - [SDR 99ZZZX956](https://openairdocs.org/sdr/99ZZZX956), Feb 3, 1999: RETAINER. CRACKED. UPON COMPLETION OF CSB 98-1A, FOUND THAT NR 2 CYLINDER EXHAUST ROCKER SHAFT RETAINER WAS CRACKED. SUBMITTER SUGGESTED A POSSIBLE CAUSE IS OVERTORQUING OF ROCKER - [SDR 98ZZZX4047](https://openairdocs.org/sdr/98ZZZX4047), Sep 18, 1998: STUD. SEPARATED. NR 3 CYLINDER ROCKER ARM CAME LOOSE, STUDS PULLED OUT OF CYLINDER. TACHOMETER: 540. - [SDR 98ZZZX998](https://openairdocs.org/sdr/98ZZZX998), Feb 23, 1998: COUPLING. FAILED. ALTERNATOR FAILED WHEN GEAR WAS RETRACTED. GEAR LOWERED AND RETURNED TO FIELD. PILOT REPORTED ALTERNATOR CHANGED ABOUT 10 HOURS AGO AND REGULATOR CHANGED ABOUT - [SDR 97ZZZX574](https://openairdocs.org/sdr/97ZZZX574), Jan 14, 1997: INJECT PUMP. PIN DETACHED. UPON REACHING AN ALT OF 4500 FEET, THE PILOT LEANED THE MIXTURE CONT. AT THE POINT OF ENG ROUGHNESS, HE ATTEMPTED TO ENRICHEN THE MIXTURE. THE MIXTURE WOULD NOT - [SDR 96ZZZX5448](https://openairdocs.org/sdr/96ZZZX5448), Oct 8, 1996: CRANKSHAFT. BROKEN. ENGINE LOST POWER IN-FLIGHT. ACFT ABLE TO LAND AND TAXIED IN UNDER ITS OWN POWER. ENG INSP REVEALED PROP COULD BE MOVED 15 TO 20 DEGREES WITHOUT RESISTANCE. WIT - [SDR 96ZZZX4383](https://openairdocs.org/sdr/96ZZZX4383), Aug 1, 1996: STUD. STRETCH. ENGINE WAS BEING REPAIRED FOR SEVERAL BROKEN CYLINDERS, BASE STUDS, AND LOOSE NUTS. MECHANIC RECEIVED 36 BRAND NEW STUDS FROM THREE DIFFERENT VENDORS IN TCM PAC - [SDR 96ZZZX3207](https://openairdocs.org/sdr/96ZZZX3207), May 29, 1996: FILL TUBE. RUSTY. THE INSIDE OF THE OIL FILLER TUBE AND OIL CAP WERE RUSTED TO THE POINT OF FLAKES OF RUST BEING KNOCKED OFF OF THE SURFACE AND FALLING INTO THE CRANKCASE. SUBMIT - [SDR 96ZZZX3072](https://openairdocs.org/sdr/96ZZZX3072), May 28, 1996: COIL. WIRE BROKEN. INSTALLED NEW MAGNETO, WAS INOPERATIVE. TROUBLESHOOTING REVEALED THE COIL WIRE WAS BROKEN AT THE TERMINAL END. (INSULATION WAS STILL INTACT). SUBMITTER STATED C - [SDR 96ZZZX3074](https://openairdocs.org/sdr/96ZZZX3074), May 28, 1996: CONDENSER. FAILED. INVESTIGATION FOR MAG PROBLEM FOUND CONDENSER HAD NO CONTINUITY. - [SDR 96ZZZX3075](https://openairdocs.org/sdr/96ZZZX3075), May 28, 1996: CONDENSER. WIRE BROKEN. RT MAG INOPERATIVE. INSTALLED NEW MAG, SN 1069532DR. THIS NEW MAG WAS INOPERATIVE. TROUBLESHOOTING BOTH MAGS REVEALED ORIGINAL MAG HAD BAD CONSENSER AND THE NEW - [SDR 96ZZZX3073](https://openairdocs.org/sdr/96ZZZX3073), May 26, 1996: MAGNETO. FAILED. MAGNETO FAILED. DID NOT TROUBLESHOOT MAG DUE TO IT BEING UNDER WARRANTY. - [SDR MCA12BMV](https://openairdocs.org/sdr/MCA12BMV), Oct 27, 1995: VALVE. LEAKING. FUEL MANIFOLD VALVE FOUND LEAKING AROUND VALVE DIAPHRAGM. REASON FOR LEAK UNKNOWN. ENGINE AND COMPONENTS REBUILT BY TCM 5-12-95. (X) - [SDR 95ZZZX6417](https://openairdocs.org/sdr/95ZZZX6417), Oct 18, 1995: ROCKER SHAFT. WORN. DURING ROUTINE OIL CHANGE, OIL FILTER WAS FOUND CONTAMINATED WITH FERROUS MATERIAL. OIL ANALYSIS DETERMINED MATERIAL TO BE CASE HARDENED STEEL. UPON INSPECTION, - [SDR 95ZZZX5949](https://openairdocs.org/sdr/95ZZZX5949), Sep 29, 1995: HOUSING. CRACKED. DURING COMPLIANCE WITH AD 82-27-03 AND AFTER REMOVING THE EXHAUST HOUSING OF THE TURBOCHARGER, A CRACK, APPROXIMATELY .75 INCH LONG, WAS NOTED IN THE WEB AREA N - [SDR 96ZZZX936](https://openairdocs.org/sdr/96ZZZX936), Sep 25, 1995: RETAINER. CRACKED. DURING C/W CONTINENTAL SB CSB95-4, FOUND 2 ROCKER SHAFT RETAINERS CRACKED THROUGH THE BOLT HOLE. - [SDR 95ZZZX5765](https://openairdocs.org/sdr/95ZZZX5765), Aug 14, 1995: GASKET. FAILED. REPLACED ROCKER BOX COVER GASKETS WITH NEW SUPERIOR SILICON GASKET. USED ALL NORMAL PROCEDURES FOR INSTALLATION. COVERS CAME OFF IN-FLIGHT CAUSING ENGINE OIL LO - [SDR 95ZZZX3244](https://openairdocs.org/sdr/95ZZZX3244), Jun 13, 1995: IDLE SHAFT. WORN. OIL PUMP WOULD LOSE PRIME AND HAVE NO OIL PRESSURE AFTER START-UP. OIL PUMP IDLE SHAFT EXTREMELY WORN AND BOTH GEARS WORN. WORE THE PUMP HOUSING CAUSING AN OIL - [SDR 95ZZZX1601](https://openairdocs.org/sdr/95ZZZX1601), Mar 21, 1995: CONNECT ROD. FAILED. THIS ENGINE, CONVERTED FROM A TSIO-360-GB, HAD NR 3 AND NR 4 CONNECTING RODS FAIL AT THE SAME TIME KNOCKING A HOLE IN THE UPPER CASE AREA OF ABOUT 8 INCHES DIAM - [SDR 95ZZZX764](https://openairdocs.org/sdr/95ZZZX764), Jan 1, 1995: ADAPTER. FAILED. STARTER ADAPTER FAILED. FOUND SPRING, PN 539800, BROKE AT LOCATION OF LOCK SCREW, PN 633845. ## STCs that may be installed (OpenAirDocs) (26) 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 SE2146NM](https://openairdocs.org/stc/SE2146NM): Conversion of the Continental TSIO-360-FB engine (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 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 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 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 --- 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.