# Continental IO-360-C

- Type: Engine model (FAA registry)
- Registry code: 17147
- Manufacturer (registry): CONT MOTOR
- Model: IO-360-C
- Engine type: Reciprocating
- Power: 210 hp
- Data sheet: [TCDS E1CE](https://openairdocs.org/tcds/E1CE) (OpenAirDocs)
- Holder: Continental Aerospace Technologies, Inc.
- Installed in: 14 registered aircraft
- Page: https://openairdocs.org/engine/continental-io-360-c

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 2023-05-16](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 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 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 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 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 70-14-07](https://openairdocs.org/ad/70-14-07): Fuel Injection Pump · Continental Motors IO-360-A, IO-360-C, IO-360-D and 25 more. Effective Nov 22, 1974
- [AD 74-18-07](https://openairdocs.org/ad/74-18-07): Cylinder · Continental Motors IO-360-A, IO-360-C, IO-360-D and 3 more. Effective Aug 28, 1974

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

## 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 CE-02-09](https://openairdocs.org/saib/CE-02-09): . Issued Dec 28, 2001

## Registered aircraft (14)

- [N14MR](https://openairdocs.org/aircraft/N14MR): [Marlin Aviation Flying Service LLC](https://openairdocs.org/faa-owner/MARLIN%20AVIATION%20FLYING%20SERVICE%20LLC), [West Palm Beach, FL](https://openairdocs.org/faa-place/FL/West%20Palm%20Beach), built 1972, S/N 33701459
- [N175TT](https://openairdocs.org/aircraft/N175TT): [Farrell Dolliver T](https://openairdocs.org/faa-owner/FARRELL%20DOLLIVER%20T), [Sterling, AK](https://openairdocs.org/faa-place/AK/Sterling), built 1958, S/N 55193
- [N254WT](https://openairdocs.org/aircraft/N254WT): [Clik Services LLC](https://openairdocs.org/faa-owner/CLIK%20SERVICES%20LLC), [Forestdale, MA](https://openairdocs.org/faa-place/MA/Forestdale), built 1968, S/N 337-0921
- [N337FT](https://openairdocs.org/aircraft/N337FT): [Mclenaghan Alvin N](https://openairdocs.org/faa-owner/MCLENAGHAN%20ALVIN%20N), [Phoenix, AZ](https://openairdocs.org/faa-place/AZ/Phoenix), built 1966, S/N 3370384
- [N337RC](https://openairdocs.org/aircraft/N337RC): [N337rc Corp Trustee](https://openairdocs.org/faa-owner/N337RC%20CORP%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1968, S/N 337-1014
- [N337WZ](https://openairdocs.org/aircraft/N337WZ): [Air Data Solutions LLC](https://openairdocs.org/faa-owner/AIR%20DATA%20SOLUTIONS%20LLC), [Natchitoches, LA](https://openairdocs.org/faa-place/LA/Natchitoches), built 1971, S/N 33701397
- [N3812K](https://openairdocs.org/aircraft/N3812K): [Cook Steven A](https://openairdocs.org/faa-owner/COOK%20STEVEN%20A), [Vineland, NJ](https://openairdocs.org/faa-place/NJ/Vineland), built 1948, S/N 3501
- [N446SN](https://openairdocs.org/aircraft/N446SN): [Warren Dennis](https://openairdocs.org/faa-owner/WARREN%20DENNIS), [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas), built 1966, S/N 337-0454
- [N5456S](https://openairdocs.org/aircraft/N5456S): [Wood Charles G Trustee](https://openairdocs.org/faa-owner/WOOD%20CHARLES%20G%20TRUSTEE), [Amarillo, TX](https://openairdocs.org/faa-place/TX/Amarillo), built 1967, S/N 337-0556
- [N706DV](https://openairdocs.org/aircraft/N706DV): [Schile David V](https://openairdocs.org/faa-owner/SCHILE%20DAVID%20V), [Bonney Lake, WA](https://openairdocs.org/faa-place/WA/Bonney%20Lake), built 2006, S/N 99R
- [N765ES](https://openairdocs.org/aircraft/N765ES): [Wetzig Rodney L Trustee](https://openairdocs.org/faa-owner/WETZIG%20RODNEY%20L%20TRUSTEE), [San Angelo, TX](https://openairdocs.org/faa-place/TX/San%20Angelo), built 2009, S/N ES-207
- [N789GA](https://openairdocs.org/aircraft/N789GA): [Proctor John](https://openairdocs.org/faa-owner/PROCTOR%20JOHN), [Rosebud, TX](https://openairdocs.org/faa-place/TX/Rosebud), S/N 2346
- [N903KK](https://openairdocs.org/aircraft/N903KK): [Hanger Nine Point Five LLC](https://openairdocs.org/faa-owner/HANGER%20NINE%20POINT%20FIVE%20LLC), [Aztec, NM](https://openairdocs.org/faa-place/NM/Aztec), built 1970, S/N 33701263
- [N905KK](https://openairdocs.org/aircraft/N905KK): [Rdc Air LLC](https://openairdocs.org/faa-owner/RDC%20AIR%20LLC), [Lithia, FL](https://openairdocs.org/faa-place/FL/Lithia), built 1970, S/N 33701348

## 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 FTW68D0114](https://openairdocs.org/ntsb/FTW68D0114), Jul 14, 1967: Cessna 337B (N5456S), Carrizo Sprgs, TX, substantial damage

## FAA accident and incident reports (3)

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 20250216004049I](https://openairdocs.org/incident/20250216004049I), Feb 16, 2025: Cessna 337F (N14MR), Palm Beach, FL, Minor damage. At 1951Z [privacy data omitted] C337 was given taxi instructions to taxi RWY28R via e, l cross RWY14/32. [privacy data omitted] Taxied on the access Road…
- [Incident 20180925019229I](https://openairdocs.org/incident/20180925019229I), Sep 25, 2018: Bloodworth Tommy LANCAIR ES (N765ES), West Point, VA, Minor damage. A/c practicing missed approach lost power while attempting a go around. Aircraft touched down with 300 feet of runway left. Aircraft ran off the end of the…
- [Incident 20160618009599I](https://openairdocs.org/incident/20160618009599I), Jun 18, 2016: Allegre Gary A STARDUSTER TOO SA300 (N789GA), Hermiston, OR, Minor damage. After refueling in hood river, OR (4S2), pilot took off and was enroute to TX in tandem seat, open air cockpit, amateur-built bi-plane, when engine began to…

## Service difficulty reports (49)

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

- [SDR 2026FA0000662](https://openairdocs.org/sdr/2026FA0000662), Aug 23, 2026: POINTS. DEFECTIVE. THE ENGINE INTERMITTENTLY RAN ROUGH ON THE RIGHT MAG CHECK AND WOULD OCCASIONALLY COMPLETELY CUT OUT BUT THE EGT'S DIDN'T POINT TO ANY PARTICULAR CYLINDER. THE 
- [SDR 2023FA0000107](https://openairdocs.org/sdr/2023FA0000107), Mar 3, 2023: CONTACTOR. DEFECTIVE. TACHOMETER BREAKER POINTS ARE FAILING PREMATURELY DUE TO DEFECTIVE MATERIALS OR PROCESSES. POINTS ARE FAILING WITHIN 5-10 HOURS WHICH CAUSES ERRATIC TACHOMETER 
- [SDR 2014FA0000265](https://openairdocs.org/sdr/2014FA0000265), Apr 25, 2014: ALTERNATOR. FAILED. FRONT ENGINE CHARGING SYSTEM, INTERMITTENT, THEN CONSTANT ALTERNATOR INOPERATIVE LIGHT. CHECKED CHARGING SYSTEM IAW MM. FOUND THREE BOLTS THAT HOLD THE ALTERNAT
- [SDR CA110720008](https://openairdocs.org/sdr/CA110720008), Jul 14, 2011: CLEVIS PIN. BROKEN. THE PILOT REPORTED THAT HIS UNDERCARRIAGE WARNING LIGHT FOR THE LT MAIN GEAR DID NOT GIVE A SAFE INDICATION WHEN THE GEAR WAS SELECTED DOWN. (GREEN INDICATIOR L
- [SDR CA100805001](https://openairdocs.org/sdr/CA100805001), Jun 4, 2010: CRANKCASE. CRACKED. DURING A ROUTINE INSP, DISCOVERED A 2.5" CRACK IN THE ENGINE CASE RUNNING FWD FROM NR 5 C4L BASE TO THE FRONT BEARING AREA. THE CRANK WAS ALLOWING ENGINE OIL SE
- [SDR CA100127014](https://openairdocs.org/sdr/CA100127014), Jan 4, 2010: SPAR. CRACKED. (CAN) ON INSP OF WING AD 78-09-05 WAS ACCOMPLISHED AND THE LT WING FWD SPAR AFT WEB WAS FOUND CRACKED.
- [SDR CA080910001](https://openairdocs.org/sdr/CA080910001), Sep 3, 2008: INTAKE DUCT. CRACKED. (CAN) DURING A ROUTINE PATROL FLIGHT THE PILOT EXPERIENCED A VIBRATION IN THE AREA OF THE REAR ENGINE. HE ELECTED TO RETURN TO THE AIRPORT AND MADE AN UNSCHEDUL
- [SDR CA060131003](https://openairdocs.org/sdr/CA060131003), Jan 20, 2006: CABLE. BENT. AIRCRAFT WAS IN CRUISE FLT WHEN THE PILOT ATTEMPTED TO CHANGE LT FUEL SELECTOR FOR FORWARD ENGINE TO A DIFFERENT TANK. WHEN SELECTED THE KNOB STOPPED AT THE 1/2
- [SDR CA050724002](https://openairdocs.org/sdr/CA050724002), Jul 22, 2005: CRANKCASE. CRACKED. AFTER LANDING FROM A ROUTINE COMPANY FLIGHT, THE MAINTENANCE ENGINEER NOTED MORE THAN NORMAL OIL ON THE LT REAR COWLING. UPON FURTHER INVESTIGATION, A 3 INCH CR
- [SDR CA041020011](https://openairdocs.org/sdr/CA041020011), Oct 19, 2004: BOLT. MISSING. (CAN) WHILE TAXING TO PARK, THE LEFT WHEEL STARTED TO SMOKE AND THE AIRCRAFT STARTED TO SHAKE. AFTER APPLYING BRAKES EVERYTHING WENT BACK TO NORMAL. UPON INSPEC
- [SDR KRCX0101AA](https://openairdocs.org/sdr/KRCX0101AA), Aug 27, 2004: COUNTERWEIGHT. DISPLACED. ON ANNUAL INSPECTION SAW FINE ALUMINUM POWDER ON ONE BLADE SHANK ON REAR PROP. FOUND SPINNER HAD A LARGE BLISTER CAUSED BY PRESSURE FROM WITHIN. WHEN WE REMOVED
- [SDR CA040730005](https://openairdocs.org/sdr/CA040730005), May 23, 2004: CRANKCASE. CRACKED. (CAN) ENGINE OIL LEAK DETECTED ON REAR ENGINE SUCTION INSPECTED FOUND 1.5 INCH LONG CRACK IN CASE BETWEEN NR 3 AND NR 5 CYLINDER. NO OTHER REPORTED DAMAGE. ENGI
- [SDR CA040225011](https://openairdocs.org/sdr/CA040225011), Feb 24, 2004: CONTROL CABLE. FRAYED. (CAN) FLAP CABLES REMOVED FOR INSPECTION DUE TO SERVICE DIFFICULTY ALERT AL-2003-05. LT AND RT OUTBOARD FLAP CABLES FOUND TO BE FREYED AT THE INBOARD BELLCRANK,
- [SDR CA040225014](https://openairdocs.org/sdr/CA040225014), Feb 24, 2004: CONTROL CABLE. FRAYED. (CAN) FLAP CABLES REMOVED FOR INSPECTION, REFERENCE SD ALERT AL-2003-05 IB FLAP CABLE, RT SIDE, PART NR 1460100-7 FRAYED APPROX 50 PERCENT AT IB BELLCRANK. 1 IN
- [SDR CA040106007](https://openairdocs.org/sdr/CA040106007), Nov 21, 2003: MAGNETO. DAMAGED. (CAN) FRONT ENGINE WOULD NOT RUN WHEN LT SETTING WAS SELECTED DURING GROUND RUN UP. IT WAS LATER DISCOVERED THAT THE LT MAGNETO NOISE SUPRESSOR WAS ALSO DEFECTI
- [SDR CA031001010](https://openairdocs.org/sdr/CA031001010), Sep 23, 2003: CONTROL CABLE. DAMAGED. (CAN) A SPECIAL INSPECTION WAS INITIATED TO COMPLY WITH REMOVAL AND INSPECTION OF FLAP CONTROL CABLES THAT ARE CONNECTED TO THE INBOARD FLAP BELLCRANK. CABLE PN
- [SDR AUS20030364](https://openairdocs.org/sdr/AUS20030364), Mar 26, 2003: SEAT TRACK. CRACKED. (AUS) SEAT TRACK CRACKED AT REAR SEAT STOP. ON REMOVAL ANOTHER CRACK WAS FOUND AT THE SEAT REMOVAL CUTOUT.
- [SDR AUS20030365](https://openairdocs.org/sdr/AUS20030365), Mar 26, 2003: SEAT TRACK. CRACKED. (AUS) SEAT TRACK CRACKED IN TWO PLACES. ON REMOVAL OF THE SEAT TRACK ANOTHER CRACK WAS FOUND AT THE CUTOUT FOR THE REMOVAL OF THESECOND ROW OF SEATS.
- [SDR AUS20030264](https://openairdocs.org/sdr/AUS20030264), Mar 3, 2003: CONTROL CABLE. CORRODED. (AUS) FLAP CONTROL CABLES PN 14601007 AND PNO 14601008 CORRODED AND FRAYED.
- [SDR CA021125010](https://openairdocs.org/sdr/CA021125010), Nov 21, 2002: BRACKET. CRACKED. (CAN) CRACK FOUND ON BOTH INBOARD RUDDER TORQUE TUBE MOUNTING BRACKETS. THE CRACK BEGAN AT THE AFT END OF THE BRACKET, EXTENDING FORWARD APPROXIMATELY 3-4 INCHE
- [SDR CA021004007](https://openairdocs.org/sdr/CA021004007), Sep 15, 2002: DOWNLOCK SWITCH. BROKEN. (CAN) ONE WIRE THAT ATTACHES TO THE LT MLG DOWNLOCK SWITCH FRACTURED CAUSING NO 'GREEN' DOWN GEAR LIGHT TO ILLUMINATE AFTER GEAR WAS SELECTED DOWN. THE WIRES TH
- [SDR 20010605CW019](https://openairdocs.org/sdr/20010605CW019), May 11, 2001: SWITCH. DEFECTIVE. INVESTIGATION SUBSEQUENT GEAR UP LANDING, FINDS WIRES TO THROTTLE MICRO SWITCH FOR GEAR WARNING SYSTEM INCORRECTLY CONNECTED. SWITCH FUNCTION INOPERATIVE. WHEN 
- [SDR WI3](https://openairdocs.org/sdr/WI3), Apr 27, 2001: GEAR. WORN. ACCESSORY DRIVE GEAR TEETH WORN AWAY 317 HOURS SINCE FACTORY REBUILD OF ENGINE. DRIVEN GEAR WAS NOT WORN.
- [SDR WI2](https://openairdocs.org/sdr/WI2), Apr 22, 2001: GEAR. WORN. ACCESSORY DRIVE GEAR TEETH WORN AWAY 104 HOURS SINCE INSTALLATION. GEAR HAD BEEN INSTALLED DUE TO FAILURE OF PREVIOUS GEAR FOR THE SAME REASON. DRIVEN GEAR WAS 
- [SDR 20000808SH028](https://openairdocs.org/sdr/20000808SH028), Jul 20, 2000: BRACE. LOOSE. DURING INSPECTION, P/N 1455017-1 AND P/N 1455017-2 BRACE ASSYS WERE FOUND CHAFING ON THE PN 629671A2 OIL SUMP. THE P/N 1555001-1 MUFFLER CAN MOVE FWD AND AFT DU
- [SDR 20000808SH029](https://openairdocs.org/sdr/20000808SH029), Jul 20, 2000: BRACE. CHAFED. DURING INSPECTION, P/N 1455017-1 AND P/N 1455017-2 BRACE ASSYS WERE FOUND CHAFING ON THE PN 629671A2 OIL SUMP. THE P/N 1555001-1 MUFFLER CAN MOVE FWD AND AFT DU
- [SDR 20000802SH020](https://openairdocs.org/sdr/20000802SH020), Jul 10, 2000: VALVE. LEAKING. AIRCRAFT REAR ENGINE WAS FOUND TO HAVE OIL LEAK WHICH WS TRACED TO FAILED SEAL IN P/N B51000AH300, OIL SUMP DRAIN VALVE. POSSIBLY CAUSED BY HIGH HEAT RADIATION 
- [SDR WI1](https://openairdocs.org/sdr/WI1), Jul 1, 2000: GEAR. WORN. ACCESSORY DRIVE GEAR TEETH WORN AWAY 120 HOURS SINCE FACTORY REBUILD.
- [SDR CA000320012](https://openairdocs.org/sdr/CA000320012), Mar 10, 2000: COUPLING. DISINTEGRATED. (CAN) DURING SCHEDULED MAINTENANCE, METAL CONTAMINATION WAS FOUND IN THE OIL FILTER. FURTHER INVESTIGATION REVEALED PARTS OF THE ALTERNATOR DRIVE BUSHINGS IN TH
- [SDR AU990416](https://openairdocs.org/sdr/AU990416), Apr 29, 1999: BEARING. MISSING. (AUS) NOSE LANDING GEAR OLEO STRUT BEARING MISSING. SUSPECT BEARING HAD BEEN LEFT OUT AT THE LAST INSPECTION WHEN NEW SEALS HAD BEEN FITTED.
- [SDR CA990330017](https://openairdocs.org/sdr/CA990330017), Feb 11, 1999: PISTON. CRACKED. (CAN) IN CRUISE, THE ENGINE BEGAN TO RUN ROUGH. ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED. POST-FLIGHT INSPECTION FOUND A CYLINDER PISTON CRACKED.
- [SDR CA981216002](https://openairdocs.org/sdr/CA981216002), Dec 5, 1998: DRIVE. BROKEN. (CAN) THE REAR ENGINE HAD AN UNCOMMANDED SHUTDOWN IN-FLIGHT. THE AIRCRAFT LANDED WITH ONLY THE FRONT ENGINE OPERATING. INVESTIGATION FOUND THE ENGINE OIL PUMP D
- [SDR 98ZZZX4523](https://openairdocs.org/sdr/98ZZZX4523), Nov 1, 1998: LINE. CLOGGED. PERFORMED FUEL LEAK CHECK AND NOTICED FUEL WAS NOT OVERFLOWING FROM INDICATION ELBOW FUEL DRAIN LINE. REMOVED INDUCTION ELBOW FUEL DRAIN LINE. REMOVED INDUCTION
- [SDR CA980603016](https://openairdocs.org/sdr/CA980603016), May 25, 1998: DOOR. STIFF. (CAN) WHEN GEAR SELECTED UP A GEAR UNSAFE LIGHT ILLUMINATED. RIGHT GEAR DOOR FOUND TIGHT INTERFERRING WITH UP TRAVEL. DOOR RE-RIGGED.
- [SDR CA980608002](https://openairdocs.org/sdr/CA980608002), May 22, 1998: JOINT. FAILED. (CAN) DURING FLIGHT, THE THROTTLE CONTROL BECAME DETACHED FROM THE THROTTLE CONTROL ARM CAUSING THE ENGINE TO DEVELOP FULL POWER. ENGINE SHUT DOWN. SINGLE ENGIN
- [SDR AU980255](https://openairdocs.org/sdr/AU980255), Feb 23, 1998: STUD. SHEARED. (AUS) CRANKCASE LOWER THOUGH BOLT LOCATED BETWEEN NR 4 AND NR 5 CYLINDERS SHEARED OFF AT THE THREAD.
- [SDR 98ZZZX829](https://openairdocs.org/sdr/98ZZZX829), Jan 31, 1998: BREAKER ASSY. FAILED. THE FAILURE OF THE RT MAG ON THE REAR ENGINE WAS NOTICED DURING A PRE-TAKEOFF MAG CHECK.
- [SDR CA970812010](https://openairdocs.org/sdr/CA970812010), Jul 23, 1997: TUBE. BROKEN. (CAN) DURING ANNUAL INSPECTION, IT WAS FOUND THAT A REAR ENGINE MOUNT WAS BROKEN. LOWER RIGHT HAND TUBE 1.5 INCHES BELOW THE WEB. CRACKED THROUGH THE ENTIRE DIA
- [SDR 97ZZZX2578](https://openairdocs.org/sdr/97ZZZX2578), May 1, 1997: CRANKCASE. CRACKED. THIRTY HOURS AFTER REPAIR AND OVERHAUL OF ENGINE, CRANKCASE WAS FOUND TO HAVE A CRACK ON UPPER AREA ABOVE NR 2 CYLINDER (NOT A STUD HOLE CRACK) EXTENDING 1 INCH
- [SDR AU970555](https://openairdocs.org/sdr/AU970555), Apr 25, 1997: SWITCH. FAULTY. (AUS) LH MAIN LANDING GEAR DOWN LIMIT MICROSWITCH LEVER BROKEN OFF
- [SDR AU970441](https://openairdocs.org/sdr/AU970441), Apr 7, 1997: CYLINDER. CRACKED. (AUS) NO4 CYLINDER CRACKED IN AREA BEHIND ROCKER COVERS - OIL LEAK
- [SDR AU970442](https://openairdocs.org/sdr/AU970442), Apr 7, 1997: BOLT. BROKEN. (AUS) ENGINE CRANKCASE THROUGH BOLTS (2OFF) SHEARED - TWO OPPOSITE SIDE THROUGH BOLTS LOOSE
- [SDR 97ZZZX960](https://openairdocs.org/sdr/97ZZZX960), Feb 11, 1997: CRANKCASE. CRACKED. FACTORY REMANUFACTURED ENGINE: OPENED CRATE TO INSTALL ENGINE. FOUND CRACK IN CRANKCASE REAR NR 2 TOP CYLINDER BASE STUD. CRACK APPROXIMATELY .6250 INCH LONG. Z
- [SDR 97ZZZX792](https://openairdocs.org/sdr/97ZZZX792), Oct 29, 1996: HOSE. WRONG PART. AEROQUIP FC 300-04 HOSE MEETING SAE 100R5-23 WAS FOUND INSTALLED IN REAR ENGINE FUEL SYSTEM. THIS HOSE IS INDUSTRIAL AIR BRAKE HOSE AND THE END FITTINGS MAY NOT
- [SDR CA960819201](https://openairdocs.org/sdr/CA960819201), Aug 7, 1996: PUSHROD. SHEARED. (CAN) PILOT REPORTED BACKFIRE DURING GROUND RUN-UP. INVESTIGATION FOUND REAR ENGINE #3 CYLINDER EXHAUST PUSHROD SNAPPED APPROXIMATELY 1" FROM THE TIP. RETAINER 
- [SDR AU960895](https://openairdocs.org/sdr/AU960895), Jun 3, 1996: SHAFT. FRACTURED. (AUS) LH MAGNETO BREAKER POINT DRIVE SHAFT FRACTURED IN AREA OF CAM SLOT
- [SDR AU960738](https://openairdocs.org/sdr/AU960738), May 23, 1996: HUB. ILLEGAL REPAIR. (AUS) PROPELLER LEAKING OIL - INVESTIGATION FOUND THAT THE PROPELLER HUB HAD BEEN ILLEGALY REPAIRED/MODIFIED BY MACHINING IN THEPRELOAD PLATE AREA - SUSPECT HUB
- [SDR 96ZZZX2765](https://openairdocs.org/sdr/96ZZZX2765), May 4, 1996: PISTON PIN. FAILED. IT APPEARS THE PISTON PIN BROKE AND THE PISTON HIT THE CRANKSHAFT COUNTERWEIGHT WHICH BROKE A LARGE HOLE IN THE TOP OF THE CRANKCASE. THE AIRCRAFT WAS ON A CROS
- [SDR 96ZZZX1711](https://openairdocs.org/sdr/96ZZZX1711), Mar 14, 1996: VALVE. FAILED. ON TAKEOFF, ENGINE BEGAN TO VIBRATE (AT FULL POWER SETTINGS). RETURNED TO AIRPORT. UPON INSPECTION, FOUND NR 4 INTAKE VALVE BROKEN IN HALF ON FACE AREA. NR 4 PI

## STCs that may be installed (OpenAirDocs) (30)

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 IO-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 SE1429SW](https://openairdocs.org/stc/SE1429SW): Installation of piston rings for chrome plated cylinders and cast iron valve guides. Continental Motors, Inc
- [STC SE3330NM](https://openairdocs.org/stc/SE3330NM): Continental valve cover gasket. Real Gaskets Tennessee
- [STC SE909SO](https://openairdocs.org/stc/SE909SO): Installation of fuel line filters into the individual fuel injector lines in accordance with Beryl D Shannon Aviation Specialties, Inc. Installations Instructions BI 2510, approved September 17, 1976, or later FAA approved revision. D'Shannon Products Ltd
- [STC SE09846SC](https://openairdocs.org/stc/SE09846SC): Installation of S539800M30 starter adapter springs. Aircraft Specialties Services Inc
- [STC SE822GL](https://openairdocs.org/stc/SE822GL): Installation of a Shadin Co. fuel flow transducer. Shadin Avionics
- [STC SE01559SE](https://openairdocs.org/stc/SE01559SE): Modify the existing fuel induction system to install the Continental ES tuned induction system. Merlyn Sales 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 SE09513SC](https://openairdocs.org/stc/SE09513SC): Installation and usage of Exxon 20W50 Multigrade aircraft engine oil conforming to Exxon Oil Formulation WS-3013. Exxon Company USA. Lists IO-360 Series
- [STC SE09401SC](https://openairdocs.org/stc/SE09401SC): Installation of modified fuel injector nozzles. General Aviation Modifications, Inc
- [STC SE00577NY](https://openairdocs.org/stc/SE00577NY): Installation of Canadian Aero Mfg. (C.A.M.) Oil Coolers. Canadian Aero Manufacturing. Lists IO-360 Series
- [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 SE8023SW](https://openairdocs.org/stc/SE8023SW): Installation and usage of AEROSHELL. Shell Development Co. Lists IO-360 Series
- [STC SE414NE](https://openairdocs.org/stc/SE414NE): Installation of Auto-Vac-2 instrument 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 IO-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 IO-360 Series
- [STC SE244NE](https://openairdocs.org/stc/SE244NE): Installation of Mattituck plasma flame sprayed cylinder barrels in Teledyne reciprocating engines. Mattituck Airbase, Inc. Lists IO-360 Series
- [STC SE1445SO](https://openairdocs.org/stc/SE1445SO): Use of Aero-blend oil additive in Teledyne (non turbocharged) aircraft engines. ProTec. Lists IO-360 Series
- [STC SE99WE](https://openairdocs.org/stc/SE99WE): Installation of Equa-Flo fuel/air induction system. Circle Machine Company
- [STC SE234GL](https://openairdocs.org/stc/SE234GL): Installation of a steel pin in Continental fuel pump, P/N 638157. Approved Aircraft Accessories, Inc
- [STC SE12GL](https://openairdocs.org/stc/SE12GL): Installation of oil filler cap. Ray Whyte Electric Products Co
- [STC SE44WE](https://openairdocs.org/stc/SE44WE): Use of Kling Aviation Oil, Specifications KL-100, KL-200 and KL-300 in Continental and Lycoming engines. Kling Oil Company

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