# Eagle Ivex IO-360 - Type: Engine model (FAA registry) - Registry code: 24600 - Manufacturer (registry): EAGLE IVEX - Model: IO-360 - Engine type: 4 cycle - Power: 180 hp - Installed in: 12 registered aircraft - Page: https://openairdocs.org/engine/eagle-ivex-io-360 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. None matched. ## Registered aircraft (12) - [N14VR](https://openairdocs.org/aircraft/N14VR): [Hugonnard-Roche Vincent Paul Marie](https://openairdocs.org/faa-owner/HUGONNARD-ROCHE%20VINCENT%20PAUL%20MARIE), [Miami Beach, FL](https://openairdocs.org/faa-place/FL/Miami%20Beach), built 2008, S/N 724-320-57 - [N223AC](https://openairdocs.org/aircraft/N223AC): [Skinner Robert A](https://openairdocs.org/faa-owner/SKINNER%20ROBERT%20A), [Fayetteville, GA](https://openairdocs.org/faa-place/GA/Fayetteville), built 2011, S/N 73060 - [N22AE](https://openairdocs.org/aircraft/N22AE): [Stegmaier David J](https://openairdocs.org/faa-owner/STEGMAIER%20DAVID%20J), [Rosemount, MN](https://openairdocs.org/faa-place/MN/Rosemount), built 2011, S/N 82804 - [N315TB](https://openairdocs.org/aircraft/N315TB): [Burns Daniel F](https://openairdocs.org/faa-owner/BURNS%20DANIEL%20F), [Hermiston, OR](https://openairdocs.org/faa-place/OR/Hermiston), built 2010, S/N 70582 - [N323AT](https://openairdocs.org/aircraft/N323AT): [Heart Of Georgia Skies LLC](https://openairdocs.org/faa-owner/HEART%20OF%20GEORGIA%20SKIES%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2013, S/N 714555 - [N359TG](https://openairdocs.org/aircraft/N359TG): [Martin Darwin G](https://openairdocs.org/faa-owner/MARTIN%20DARWIN%20G), [Carson City, NV](https://openairdocs.org/faa-place/NV/Carson%20City), built 2006, S/N 444 - [N383Z](https://openairdocs.org/aircraft/N383Z): [Tucson, AZ](https://openairdocs.org/faa-place/AZ/Tucson), built 2010, S/N 72815, Registration pending - [N4693A](https://openairdocs.org/aircraft/N4693A): [Pralle Douglas Dwight](https://openairdocs.org/faa-owner/PRALLE%20DOUGLAS%20DWIGHT), [Hampton, IA](https://openairdocs.org/faa-place/IA/Hampton), built 2015, S/N M-II-1626 - [N488EF](https://openairdocs.org/aircraft/N488EF): [Farry Eric V](https://openairdocs.org/faa-owner/FARRY%20ERIC%20V), [Creswell, OR](https://openairdocs.org/faa-place/OR/Creswell), built 2026, S/N 91054 - [N515WB](https://openairdocs.org/aircraft/N515WB): [Calvert Wilson D Jr](https://openairdocs.org/faa-owner/CALVERT%20WILSON%20D%20JR), [Anacortes, WA](https://openairdocs.org/faa-place/WA/Anacortes), built 2021, S/N 74803 - [N569Q](https://openairdocs.org/aircraft/N569Q): [Jtq Aviation LLC](https://openairdocs.org/faa-owner/JTQ%20AVIATION%20LLC), [Peyton, CO](https://openairdocs.org/faa-place/CO/Peyton), built 2012, S/N 72769 - [N988GH](https://openairdocs.org/aircraft/N988GH): [John Bell Consulting LLC](https://openairdocs.org/faa-owner/JOHN%20BELL%20CONSULTING%20LLC), [Baytown, TX](https://openairdocs.org/faa-place/TX/Baytown), built 2012, S/N 73170 ## 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 WPR15LA262](https://openairdocs.org/ntsb/WPR15LA262), Sep 21, 2015: Graves Bryon S Vans RV-7A (N507RV), Byron, CA, substantial damage. Probable cause: Improper overhaul of the right magneto, which eliminated system redundancy, and resulted in a loss of engine power when the left magneto failed during aerobatic flight maneuvers. ## 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. - [Accident 20150920021419A](https://openairdocs.org/incident/20150920021419A), Sep 20, 2015: Graves Bryon S VANS RV-7A (N507RV), Byron, CA, Substantial damage. Aircraft was flying from Byron, CA. (C83) and approx.3 miles northeast of airport, pilot encountered engine RPM sputter, pilot performed ignition switching… ## Service difficulty reports (86, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2023FA0000622](https://openairdocs.org/sdr/2023FA0000622), Oct 20, 2023: CYLINDER. CRACKED. PILOT REPORTED LOSS OF ENGINE POWER. BEGAN TO RUN ROUGH. MADE A PRECAUTIONARY NORMAL LANDING. MECHANIC REMOVED COWLING AND FOUND A CRACKED NR 4 CYLINDER. LB STA - [SDR 2021FA0000407](https://openairdocs.org/sdr/2021FA0000407), Dec 16, 2021: NONE. LOOSE. DURING R/H AILERON BELLCRANK CABLES DISCONNECTION FOR CLEANING / INSPECTION / LUBE, FOUND BELLCRANK ASSY P/N 47350-2 CONSTITUTED OF PIVOT BALL BEARING HOUSING P - [SDR 4RPA201307010001](https://openairdocs.org/sdr/4RPA201307010001), Jun 28, 2013: PUMP. FAILED. LEFT ENGINE FUEL FLOW DROPPED FROM 25 GALLONS AN HOUR AT TOP OF CLIMB TO 7 GALLONS AN HOUR AT ALL POWER SETTINGS. ELECTRIC FUEL PUMP SWITCH ALSO FAILED. PILOT U - [SDR 2012FA0000727](https://openairdocs.org/sdr/2012FA0000727), Oct 25, 2012: POWER SUPPLY. FAILED. LEFT STROBE INOPERATIVE. TESTED FLASH TUBE WITH ANOTHER POWER SUPPLY - FUNCTION CHECK OK. PULLED THE POWER SUPPLY AND OPENED - EVIDENCE OF CAPACITOR EXPLOSION A - [SDR 2012FA0000517](https://openairdocs.org/sdr/2012FA0000517), Jul 9, 2012: COWL DOOR. DEPARTED. DURING DESCENT THROUGH 7,000 FT, TOP COWL ASSEMBLY DEPARTED THE ACFT AND STRUCK THE LEFT WINDSCREEN CAUSING A LARGE HOLE. FURTHER INSPECTION REVEALED THAT THE R - [SDR 2012FA0000343](https://openairdocs.org/sdr/2012FA0000343), May 29, 2012: CASE. CRACKED. DURRING PRE FLIGHT FOUND OIL ON COWLING. INVESTIGATION FOUND A CRACK IN THE RT FWD TOP OF THE ENGINE CASE. - [SDR 2011FA0000544](https://openairdocs.org/sdr/2011FA0000544), Aug 22, 2011: BOLT. LOOSE. WHILE COMPLYING WITH AD 11-07-13 LT AND RT ELEVATOR SPAR, IT WAS NOTED THAT THE HORIZONTAL STAB WAS LOOSE AT BOTH THE FRONT AND REAR MOUNTING POINTS. MOVEMENT W - [SDR 2011FA0000373](https://openairdocs.org/sdr/2011FA0000373), Jun 9, 2011: FILTER ELEMENT. SPLIT. DURING ROUTINE INSPECTION, AIR FILTER WAS FOUND SPLIT OPEN AT THE SEAM. IT IS A CYLINDRICAL SHAPE AND IT WRAPS AROUND A METAL SCREEN. THE SPLIT AREA COMPRISED S - [SDR 2011FA0000334](https://openairdocs.org/sdr/2011FA0000334), May 18, 2011: SPAR. CORRODED. DURING REPAIR OF LT WING THE AFT SPAR ATTACH FITTING WAS REMOVED. SEVERE CORROSION WAS FOUND UNDER THE FITTING. PROBABLE CAUSE IS TRAPPED MOISTURE, LACK OF PREV - [SDR NX4R000013](https://openairdocs.org/sdr/NX4R000013), Apr 28, 2011: MOUNT. CRACKED. DURING ROUNTINE MX, THE TECH WAS PERFORMING A PRELIMINARY/HIDDEN DAMAGE INSP OF THE AREA SURROUNDING THE AREA WHERE WORK WAS TO BE PERFORMED. NOTICED THE SMALL - [SDR NX4R000011](https://openairdocs.org/sdr/NX4R000011), Apr 20, 2011: ATTACH FITTING. BROKEN. DURING TAKEOFF, THE PILOT RETRACTED THE LANDING GEAR. THE GEAR "UNSAFE LIGHT" REMAINED ILLUMINATED. ALSO THE ATC TOWER CONTROLLER ADVISED THE CREW THAT THEIR NL - [SDR 2011FA0000054](https://openairdocs.org/sdr/2011FA0000054), Jan 28, 2011: SHAFT. FAILED. MAG SHAFT COMPLETELY SEPARATED FROM THE MAG AS THE SHAFT EXITED THE MAG. CAUSING INOPERATIVE SYS, LOSS OF 1/2 ENGINE IGNITION AND ASSOCIATED WARNING LIGHTS IN T - [SDR 2010FA0001258](https://openairdocs.org/sdr/2010FA0001258), Dec 20, 2010: DISTRIBUTOR BLK. MELTED. DURING A 500 HOUR INSP, COMPLIANCE OF M/N 6314 MAGNETOS, LT MAGNETO SHOWED SIGNS OF EXTREAM HIGH HEAT INTERNALLY. SB SB3-08A ADDRESSES PROBLEM CAUSED BY "SOFT" - [SDR 2010FA0001132](https://openairdocs.org/sdr/2010FA0001132), Aug 21, 2010: SPRING. BROKEN. ON LANDING TAILSPRING BROKE. ACFT GROUND LOOPED CAUSING SUBSTANTIAL DAMAGE TO AIRCRAFT. INVESTIGATION OF BROKEN TAILSPRING REVEALED 2 EXISTING LOW CYCLE FATIGUE - [SDR ZB0R20100002](https://openairdocs.org/sdr/ZB0R20100002), May 31, 2010: MASTER SWITCH. BURNED. ((ZB0R)) PILOT REPORTED BURNING SMELL AND FAILURE OF AVIONICS BUSS NR 2 ON RUN-UP. ACFT REPORTED TO MX. TROUBLESHOOTING REVEALED AVIONICS MASTER SWITCH RT SIDE - [SDR 2010FA0000425](https://openairdocs.org/sdr/2010FA0000425), Apr 19, 2010: GUIDE. BROKEN. (HE8S) PILOT`S SEAT HARNESS GUIDE BROKE AT SHOULDER HARNESS MOUNT TUBE. SUGGEST MAKING THIS PART WITH MORE DURABLE MATERIAL OR HAVING A REINFORCEMENT AT AREA OF - [SDR 2010FA0000228](https://openairdocs.org/sdr/2010FA0000228), Mar 12, 2010: MOUNT. BROKEN. HAVE HAD MULTIPLE PROBLEMS WITH THE MOUNTING KIT FOR THE ALTERNATOR THROUGH STC SA334SW. A NEW ALTERNATOR WAS INSTALLED ON 9/8/2006. AFTER 64 FLIGHT HOURS, THE - [SDR 2010FA0000196](https://openairdocs.org/sdr/2010FA0000196), Mar 3, 2010: SOLENOID. STICKS. BURNED ODOR OF ELECTRICAL COMPONENTS AFTER ENGINE START UP. SELECTED ACFT MASTER SWITCH OFF AND SHUTDOWN ENGINE. INSP REVEALED STARTER MOTOR HAD OVERHEATED. FUR - [SDR 2010FA0000045](https://openairdocs.org/sdr/2010FA0000045), Jan 15, 2010: TRACK. BROKEN. PN 1513055-1 CAM TRACK ASSY BROKE UPON GEAR RETRACTION. NOSE GEAR THEN WOULD NOT RETRACT PROPERLY OR EXTEND AND LOCK PROPERLY. PUMP MOTOR C/B CONTINUED TO TRIP - [SDR 2009FA0000986](https://openairdocs.org/sdr/2009FA0000986), Nov 20, 2009: SHAFT. FRACTURED. ROTOR SHAFT FRACTURED AT THE BOTTOM OF THE RUBBING BROOK SLOT. (K) - [SDR 2009FA0000873](https://openairdocs.org/sdr/2009FA0000873), Oct 22, 2009: NUT. CRACKED. WHEN REMOVING PROPELLER FOR RESEAL, FOUND 2 MOUNTING NUTS CRACKED. THE PROP HAS 93.5 HRS SINCE INSTALLATION. THE PROPELLER PREVIOUSLY HAD THE BLADES REPLACED DU - [SDR 2009FA0000921](https://openairdocs.org/sdr/2009FA0000921), Aug 14, 2009: SCREEN. CRACKED. REPAIR STATION IS HOLDER OF STC SA03674AT FOR THE INSTALATION OF R-134 COOLANT AIR CONDITIONER SYS IN THIS ACFT. IAW THIS STC INSTALLATION, A CONDENSER HOUSING - [SDR 2009FA0000922](https://openairdocs.org/sdr/2009FA0000922), Aug 14, 2009: SCREEN. CRACKED. REPAIR STATION IS HOLDER OF STC SA03674AT FOR THE INSTALATION OF R-134 COOLANT AIR CONDITIONER SYS IN THIS ACFT. IAW THIS STC INSTALLATION, A CONDENSER HOUSING - [SDR 2009FA0000510](https://openairdocs.org/sdr/2009FA0000510), Jun 9, 2009: AIR FILTER. DEFECTIVE. UPON RECEIVING INSP OF NEW MFG AIR FILTERS PN P107336 IT WAS FOUND THAT 3 OUT OF 4 NEW FILTERS HAD A DEFECTIVE SEALING SURFACE CAUSING THE SEALING/MATING SURFAC - [SDR 2009FA0000449](https://openairdocs.org/sdr/2009FA0000449), May 12, 2009: CONTROL CABLE. BROKEN. AN INSP OF RT WING FLAP CABLE REVEALED BROKEN STRANDS WHERE THE CABLE THIMBLE AND SHACKLE TO THE FLAP BELLCRANK INSIDE THE WING. THERE IS INSUFFICIENT CLEARANCE - [SDR 2009FA0000396](https://openairdocs.org/sdr/2009FA0000396), May 11, 2009: PLUNGER. DAMAGED. PLUNGER P/N 210332 INSPECTED IAW SB 33571C AND FAILED. - [SDR 2008FA0000841](https://openairdocs.org/sdr/2008FA0000841), Nov 24, 2008: LATCH. DISENGAGED. AT 10500 FT IN CRUISE FLIGHT, GOT AN AUDIBLE "DING" ON THE G1000 WARNING AND THEN A LIGHT SAYING THAT A DOOR WAS OPEN. BACK DOOR HAD COME OPEN IN FLIGHT. THE DO - [SDR 2008FA0000880](https://openairdocs.org/sdr/2008FA0000880), Nov 22, 2008: SENSOR. DEFECTIVE. SENSOR PRODUCED A FALSE HIGH OIL PRESSURE INDICATION DURING ACFT APPROACH TO AIRPORT. PROBABLE CAUSE WAS INTERNAL FAILURE, RECOMMENDATIONS TO PREVENT RECURRENCE - [SDR 2010FA0000758](https://openairdocs.org/sdr/2010FA0000758), Nov 7, 2008: WIRE. CHAFED. (NU7R) PILOT REPORTED AVIONICS INTERMITTENT TO COME ON WITH AVIONICS SWITCH. MFG DWG PAGE 24-50-01, PAGE 1 SHOWS AVIONICS RELAY NR 1 WITH WIRE CSVA661-14 LEAVIN - [SDR CA081009009](https://openairdocs.org/sdr/CA081009009), Sep 27, 2008: WIRE. BROKEN. (CAN) A+ TERMINAL MELTED OFF ALTERNATOR AND LOOSE. PROBLEM CAUSED BY BROKEN TERMINAL ON A+ WIRE GOING TO ALTERNATOR. WIRE WAS ORIGINALLY VERY TIGHT CAUSING THE - [SDR 2008FA0000661](https://openairdocs.org/sdr/2008FA0000661), Sep 17, 2008: CASTING. BROKEN. CUSTOMER ATTEMPTED TO START ENGINE. WHILE CRANKING ENGINE, CUSTOMER REPORTED A LOUD "CLUNK" AND THE PROPELLER STOPPED ROTATING. INVESTIGATED PROBLEM AND FOUND T - [SDR 2008FA0000505](https://openairdocs.org/sdr/2008FA0000505), Jul 22, 2008: CONNECTOR. DAMAGED. ON JUNE 28TH, 2008, DURING CLIMB OUT, PASSING THROUGH 4000 FEET THE ENGINE SUDDENLY WENT INTO AN OVER SPEED CONDITION OF OVER 3100 RPM. THE AIRCRAFT REMAINED UN - [SDR 2008FA0000278](https://openairdocs.org/sdr/2008FA0000278), Apr 15, 2008: VALVE. LOOSE. THE ALTERNATE AIR VALVE IS VIBRATING AND CAUSING FRETTING BETWEEN THE INLET RING, PN D41-7166-20-31 AND FLANGE, PN D41-7166-20-33. THE "DUST" IS BEING INGESTED - [SDR 2008FA0000234](https://openairdocs.org/sdr/2008FA0000234), Mar 7, 2008: VALVE. BROKEN. THE ENG AUTOMATIC ALTERNATE INDUCTION AIR VALVE THAT IS PARTIALLY LOCATED INSIDE THE CYLINDRICAL PAPER INDUCTION AIR FILTER CAME APART AND SOME OF ITS PART (2 I - [SDR 2008FA0000254](https://openairdocs.org/sdr/2008FA0000254), Mar 5, 2008: SERVO. DAMAGED. WHILE PERFORMING A 100 HR INSP, THE TECH DISCOVERED FINE METAL PARTICLES COVERING THE THROAT AND VALVE OF THE FUEL INJECTION SERVO (2576568-1, SN 70B10709). THE - [SDR 2008FA0000238](https://openairdocs.org/sdr/2008FA0000238), Feb 27, 2008: BUSHING. INCORRECT. STATIC SYSTEM FAILED LEAK CHECK DURING 2 YEAR STATIC SYS IFR CERTIFICATION, LEAKS WERE CAUSED BY REDUCED BUSHING FAILING TO SEAL STATIC LINE SUMP. (ON BOTH SIDE - [SDR 2007FA0000711](https://openairdocs.org/sdr/2007FA0000711), Jul 10, 2007: RESISTOR. DAMAGED. MFG FABRICATED AN IN-LINE RESISTOR FROM THE ALTERNATOR TO THE VOLTAGE REGULATOR. THE RESISTOR WAS LOCATED APPROXIMATELY 2 INCHES FROM AUX TERMINAL ON ALTERNATOR - [SDR 2007FA0000554](https://openairdocs.org/sdr/2007FA0000554), Jun 28, 2007: ANTENNA. DISCONNECTED. WHILE IN CRUISE FLIGHT THE NR 1 GPS STOPPED RECEIVING A SIGNAL. AFTER LANDING, REMOVED THE MFD AND FOUND THE GLUE HOLDING THE VELCRO TO THE GPS ANTENNA HAD COME - [SDR 2007FA0000533](https://openairdocs.org/sdr/2007FA0000533), Jun 22, 2007: STRUT. CRACKED. NOSE LANDING GEAR STRUT HAS A CRACK AT THE TOP. THE STRUT COMES UP TO A Y FOR MOUNT. AT THE YOKE OF THE Y IS A WELDED REINFORCEMENT, AND THE CRACK IS AT THE TOP - [SDR AW42007F00000](https://openairdocs.org/sdr/AW42007F00000), Jun 8, 2007: NUT. LOOSE. DURING THE PERFORMANCE OF A 100 HOUR INSPECTION, SLIGHT MOVEMENT OF THE HORIZONTAL STABILIZER WAS NOTED RELATIVE TO THE RT SIDE OF THE FUSELAGE. INVESTIGATION F - [SDR 2007FA0000571](https://openairdocs.org/sdr/2007FA0000571), May 31, 2007: BRACKET. FAILED. THE PILOT STATED NOSE GEAR COLLAPSED ON LANDING. AFTER AIRCRAFT REMOVED FROM RUNWAY AND PUT ON JACKS. THE NOSE GEAR WOULD NOT EXTEND OR RETRACT. THE GEAR WAS EX - [SDR 2007FA0000577](https://openairdocs.org/sdr/2007FA0000577), May 12, 2007: DOWNLOCK. BROKEN. THE LOWER LATCH HOOK WAS BROKEN OFF ALLOWING THE NOSE GEAR TO COLLAPSE. (K) - [SDR 2007FA0000349](https://openairdocs.org/sdr/2007FA0000349), Apr 1, 2007: SPAR. LOOSE. DURING AN ANNUAL INSPECTION, THE RT FLAP IB HINGE/CONTROL BRACKET WAS FOUND TO BE LOOSE. FURTHER INSPECTION REVEALED THAT THE FLAP SPAR WAS CRACKED AT THE UPPER - [SDR 2007FA0000112](https://openairdocs.org/sdr/2007FA0000112), Jan 8, 2007: AIR FILTER. TWISTED. DURING REMOVAL OF THE AIR FILTER THE CENTER WIRE MESH SCREEN WAS FOUND TWISTED AND BENT. SOME OF THE WELDS WERE BROKEN. SCREEN DEFORMATION CAN LEAD TO UNFILTERE - [SDR 2006FA0001020](https://openairdocs.org/sdr/2006FA0001020), Oct 18, 2006: LINE. CHAFED. FUEL LINE CHAFED, LINE REPLACED. - [SDR 2006FA0000561](https://openairdocs.org/sdr/2006FA0000561), May 31, 2006: ATTACH BRACKET. CRACKED. ENGINE MOUNT ATTACHMENT BRACKET WITH CRACKS AT THE 12 AND 6 O`CLOCK POSITION. CRACKS ON IB AND OB SIDES OF THE AN960-616 WASHER. NORMAL FLIGHT CONDITIONS UNDER - [SDR 2006FA0000134](https://openairdocs.org/sdr/2006FA0000134), Jan 31, 2006: ATTACH BRACKET. BROKEN. THE AC EXPERIENCED A HARD LANDING. DURING THE LANDING THE 2 TOP ENGINE MOUNT ATTACH BRACKETS FAILED BEHIND THE FIREWALL, ALLOWING THE TOP HALF OF THE FIREWALL T - [SDR 10943282](https://openairdocs.org/sdr/10943282), Jan 20, 2006: FRAME. CRACKED. FOUND CRACK APPROXIMATELY .3750 INCH IN LENGTH ON RT FRAME 20 WING ATTACH POINT. - [SDR 2005FA0001483](https://openairdocs.org/sdr/2005FA0001483), Oct 5, 2005: HINGE. FAILED. UPON INSTALLATION OF A NEW AFT CABIN DOOR SUPPORT STRUT, THE DOOR WAS CLOSED, AND THE AFT CABIN DOOR HINGE FAILED. UPON FURTHER INSPECTION, THE DOOR HINGE WAS F - [SDR 2005FA0001311](https://openairdocs.org/sdr/2005FA0001311), Sep 9, 2005: ENGINE. STOPPED. DURING CRUISE CLIMB, PILOT REPORTED BOTH ENGINES QUIT RUNNING AND DEVERTED. DURING DECENT ENGINES CAME BACK TO LIFE. SUMPED 1 PINT EACH FROM FRONT, BACK FUEL ST All 86: https://openairdocs.org/engine/eagle-ivex-io-360/reports.md --- 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.