Superior O-360 SERIES, IO-360 SERIES, Vantage Engine O-360 SERIES, Vantage Engine IO-360 SERIES Overhaul Manual

O-360 & IO-360 SERIES ENGINES
OVERHAUL MANUAL
Manual P/N SVOHM01 Revision A, March 2005
www.superiorairparts.com
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© March 2005 Superior Air Parts Inc.
Overhaul Manual
O-360 and IO-360 Series Engines
Manual Number SVOHM01
Revision History
Revision
Letter
A 08/31/04 Initial Release All
Effective
Date
Description
Pages
Revised
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O-360 and IO-360 Series Engines
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O-360 and IO-360 Series Engines
SAFETY ADVISORY
WARNING: BEFORE MATERIALS CALLED OUT IN THIS PUBLICATION ARE USED, KNOW THE
HANDLING, STORAGE AND DISPOSAL PRECAUTIONS RECOMMENDED BY THE MANUFACTURER OR SUPPLIER. FAILURE TO COMPLY WITH THE MANUFACTURERS' OR SUPPLIERS’ RECOMMENDATION CAN RESULT IN PERSONAL INJURY.
The user must know the manufacturer or supplier information and keep to the procedures, recommendations, warnings and cautions set forth for the use, handling, storage, and disposal of materials. The WARNINGS used in this manual inform the user about dangerous materials or equipment that can cause injury; they do not replace the manufacturer's instructions.
This Safety Advisory has all the warnings included in this manual.
WARNING: OPERATION OF A DEFECTIVE ENGINE WITHOUT A PRELIMINARY EXAMINATION CAN
CAUSE FURTHER DAMAGE TO A DISABLED COMPONENT AND POSSIBLE INJURY TO PERSONNEL. MAKE SURE THOROUGH INSPECTION AND TROUBLESHOOTING PROCEDURES ARE ACCOMPLISHED. THIS WILL HELP TO PREVENT INJURIES TO PERSONNEL AND/OR DAMAGE TO THE EQUIPMENT.
WARNING: FUEL IS TOXIC AND FLAMMABLE. DO NOT BREATHE VAPORS. USE INA A WELL
VENTILATED AREA FREE FROM SPARKS, FLAME, OR HOT SURFACES.AVOID EYE AND SKIN CONTACT. PUT ON SPLASH GOGGLES, SOLVENT-RESISTANT GLOVES, AND OTHER PROTECTIVE GEAR. IN CASE OF EYE CONTACT, FLUSH WITH WATER FOR 15 MINUTES AND SEEK MEDICAL ATTENTION. IN CASE OF SKIN CONTACT, WASH WITH SOAP AND WATER.
WARNING: HOT OIL MAY CAUSE BURNS TO EYES AND SKIN. PUT ON SPLASH GOGGLES AND
INSULATED GLOVES, AND OTHER PROTECTIVE GEAR. IN CASE OF EYE CONTACT, FLUSH WITH WATER FOR 15 MINUTES AND SEEK MEDICAL ATTENTION. IN CASE OF SKIN CONTACT, WASH WITH SOAP AND WATER.
WARNING: ENGINE OIL IS HAZARDOUS AND MAY CAUSE INJURY TO SKIN AND EYES. PUT ON
PERSONNEL PROTECTIVE GEAR.
WARNING: USE THE CORRECT PERSONAL PROTECTION. HEATED PARTS WILL CAUSE BURNS. WARNING: WHEN YOU USE COMPRESSED AIR TO CLEAN OR DRY PARTS, MAKE SURE THAT
THE PRESSURE IS NOT MORE THAN 30 PSI. DO NOT DIRECT THE AIRSTREAM AT PERSONNEL OR LIGHT OBJECTS. PUT ON GOGGLES OR A FACE SHIELD TO PROTECT YOUR EYES. IF YOU GET AN EYE INJURY, GET MEDICAL ATTENTION.
WARNING: LUBRICANTS ARE TOXIC AND FLAMMABLE. DO NOT BREATHE VAPORS. BEFORE
YOU USE, READ THE MATERIAL SAFETY DATA SHEET (MSDS) FROM THE MANUFACTURER OR SUPPLIER. USE IN A WELL VENTILATED AREA FREE FROM SPARKS. WEAR PROTECTIVE GEAR. IN CASE OF EYE CONTACT, FLUSH WITH WATER FOR 15 MINUTES AND SEEK MEDICAL ATTENTION. IN CASE OF SKIN CONTACT, WASH WITH SOAP AND WATER.
WARNING: USE THE CORRECT PERSONAL PROTECTION. POLISHING WILL CAUSE LOOSE
PARTICLES THAT CAN GET IN YOUR EYES.
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WARNING: PUT ON SAFETY GOGGLES WHEN INSTALLING OR REMOVING SAFETY WIRE. WARNING: USE THE CORRECT PERSONAL PROTECTION EQUIPMENT TO AVOID INJURY.
ENSURE AREA IS FREE OF MOVABLE OBJECTS THAT COULD IMPACT BY PROPELLER AIR BLAST.
WARNING: ADHESIVE SEALANT IS TOXIC AND FLAMMABLE. DO NOT BREATHE VAPORS.
AVOID EYE AND SKIN CONTACT. USE PROTECTIVE GEAR. IN CASE OF EYE CONTACT, FLUSH WITH WATER FOR 15 MINUTES AND SEEK MEDICAL ATTENTION. IN CASE OF SKIN CONTACT, WASH WITH SOAP AND WATER.
WARNING: SOLVENT IS TOXIC. USE IN WELL-VENTILATED AREA. PREVENT EYE AND SKIN
CONTACT AND DO NOT BREATHE VAPORS. IN CASE OF EYE CONTACT, FLUSH WITH WATER FOR 15 MINUTES AND SEEK MEDICAL ATTENTION. IN CASE OF SKIN CONTACT, WASH WITH SOAP AND WATER.
WARNING: DO NOT INSTALL THE IGNITION HARNESS “B” NUTS ON THE SPARK PLUGS UNTIL
THE PROPELLER INSTALLATION IS COMPLETED. FAILURE TO COMPLY COULD RESULT IN BODILY INJURY WHEN THE PROPELLER IS ROTATED DURING INSTALLATION.
WARNING: IF ONE SURFACE IS POLISHED TO UNDERSIZE, ALL CORRESPONDING SURFACES
MUST BE POLISHED TO THE SAME SIZE.
WARNING: PLACE A SUITABLE STAND UNDER THE AIRCRAFT TAILCONE IF NEEDED BEFORE
REMOVING THE ENGINE. THE LOSS OF WEIGHT MAY CAUSE THE AIRCRAFT TAIL TO DROP.
WARNING: DO NOT DAMAGE THE NITRIDED SURFACES OF THE CRANKSHAFT. WARNING: USE CORRECT PERSONAL PROTECTION. SOME CHEMICAL SOLUTIONS CAN CAUSE
EYE, SKIN, AND LUNG DAMAGE. FOLLOW THE MANUFACTURER’S INSTRUCTIONS FOR EACH STRIPPING SOLUTION.
WARNING: USE THE CORRECT PERSONAL PROTECTION. USE OF A HAMMER CAN CAUSE
LOOSE PARTICLES THAT CAN GET IN YOUR EYES.
WARNING: DO NOT ROTATE ENGINE OR CRANKSHAFT BEFORE REMOVAL OF TIMING
LOCATOR PINS.
WARNING: TO PREVENT THE POSSIBILITY OF SERIOUS BODILY INJURY OR DEATH, BEFORE
MOVING THE PROPELLER DO THE FOLLOWING:
VERIFY ALL SPARK PLUG LEADS ARE DISCONNECTED.
VERIFY MAGNETO SWITCHES ARE CONNECTED TO MAGNETOS AND THAT THEY ARE IN THE “OFF” POSITION AND “P” LEADS ARE GROUNDED.
THROTTLE POSITION “CLOSED.”
MIXTURE CONTROL “IDLE-CUT OFF.”
SET BRAKES AND BLOCK AIRCRAFT WHEELS. ENSURE THAT AIRCRAFT TIE DOWNS ARE INSTALLED AND VERIFY THAT THE CABIN DOOR LATCH IS OPEN.
DO NOT STAND WITHIN THE ARC OF THE PROPELLER BLADES WHILE TURNING THE PROPELLER.
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Section
Chapter
General Information
Sub-Section
Revision History i Safety Advisory iii Table of Contents v List of Figures ix List of Tables xi
Overhaul Manual
O-360 and IO-360 Series Engines
TABLE OF CONTENTS
Page Number
01 00 00 Introduction
02 00 00 Description and Operation
04 00 00 Airworthiness Limitations
72 00 03 Testing and Fault Isolation
About This Manual 1 Related Publications 1 Obtaining Service Information 1 Abbreviations 1 Consumable Materials List 3
General Description 1 Continued Airworthiness 1 Model Designations 1 Engine Components General Description 3 Specifications 3 Features and Operating Mechanisms 16
Mandatory Replacement Time 1 Mandatory Inspection Intervals 1 Other Mandatory Intervals or Procedures 1 Distribution of Changes to Airworthiness 1
General 1 Troubleshooting 1
04 Special Procedures
Prior to Break-In Start-Up Break-In Ground Run Break-In Flight Operation
© March 2005 Superior Air Parts Inc.
General Break-In Procedures 1 Special Tools and Equipment 1 Break-In Procedures 1
Post Break-In Procedures 2
1 1 1
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Chapter
TABLE OF CONTENTS (cont’d)
Page Number
Section
Sub-Section
05 Engine Removal
06 Engine Disassembly
07 Cleaning
Degreasing Decarbonizing Scratch and Corrosion Removal Accessory Mounts Fuel Injector and Primer Nozzles Screens and Filters Accessories
General 1 Removal 1 Preservation 1
General 1 Disassembly Materials 1 Parts for Discard 1 Special Tools and Equipment 1 General Disassembly Procedures 2 Disassembly 2
General 1 Tools and Materials 1 Cleaning Instructions 1
Preservation and Corrosion Prevention 4
1 2 2 2 3 3 3
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Section
Chapter
72 00 08 Inspection and Check
Sub-Section
General 1 Materials and Tools 1 General Inspection Procedures 2 General Non-Destructive Testing 2 Accessory Housing 3 Crankcase Assembly 3 Cylinder Head 6 Cylinder Head Dimensional Inspections 6 Cylinder Barrel Inspections 6 Cylinder Barrel Dimensional Inspections 7 Cylinder Assembly Inspection 7 Piston Inspections 7 Piston Dimensional Inspections 7 Valve Rockers 11 Pushrod Inspection 11 Valve Springs Inspection 11 Crankshaft 13 Crankshaft Counterbore Face Inspection 13 Camshaft Inspection 14 Connecting Rods Inspection 14
Overhaul Manual
O-360 and IO-360 Series Engines
TABLE OF CONTENTS (cont’d)
Page Number
09 Engine Assembly
10 Engine Installation
© March 2005 Superior Air Parts Inc.
General 1 Fits, Clearances and Torque Values 1 Materials Required for Assembly 1 Special Tools and Equipment 1 Engine Assembly 2 Engine Accessory Assembly Installation 46 Storage After Assembly 58
General 1 Preparing Engine for Service 1 Installation of Engine 1
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General Information
Section
Chapter
72 00 11 Fits and Clearances
Sub-Section
General 1 Service Limits 1
Overhaul Manual
O-360 and IO-360 Series Engines
TABLE OF CONTENTS (cont’d)
Page Number
12 Preservation and Storage
13 Repair
Repair 1 – Threaded Area Repair and Stud Replacement Repair 2 – Nick and Scratch Repair Repair 3 – Crankshaft or Crankpin Repair Repair 4 – Painted Parts Repair 5 – Crankshaft Oil Seal Surface Repair 6 – Cylinder Interior Surface Repair 7 – Cylinder Head Cooling Fins Repair 8 – Valve, Valve Seat, and Valve Guide Repair 9 – Spark Plug Threaded Insert Repair 10 – Rocker Bushing Replacement Repair 11 – Connecting Rod Bushing Replacement
14 Testing
Appendix A Assembly In Process Quality Inspections
General 1 Temporary Storage 2 Indefinite Storage 3 Returning an Engine to Service After Storage 3
General 1 Repair Procedures 1
General 1 Special Tools and Equipment 1 Engine Installation and Testing Procedures 1 Engine Storage After Testing 1
5 7
9 11 13 15 17 19 27 29 31
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O-360 and IO-360 Series Engines
LIST OF FIGURES
Figure
02-00-00.1 Engine Model Number Designation 02 00 00 1 02-00-00.2 O-360 Engine Front View 6 02-00-00.3 O-360 Engine Left Side View 7 02-00-00.4 O-360 Engine Top View 8 02-00-00.5 O-360 Engine Rear View 9 02-00-00.6 IO-360 Engine Front View 10 02-00-00.7 IO-360 Engine Left Side View 11 02-00-00.8 IO-360 Engine Top View 12
02-00-00.9 IO-360 Engine Rear View 13 02-00-00.10 Ignition Wiring Diagram 14 02-00-00.11 Oil System Schematic 15
72-00-08.1 Reserved 08 -
72-00-08.2 Accessory Housing 4
72-00-08.3 Crankcase Bearing and Flange Surfaces 5
72-00-08.4 Cylinder Assembly 8
72-00-08.5 Piston Assembly 9
72-00-08.6 Piston Rings and Lands 10
72-00-08.7 Valve Train 12
72-00-08.8 Camshaft Assembly 15
Chapter
Section
Page
Sub-Section
72-00-09.1 Crankcase Bearing Retention Dowel 09 4
72-00-09.2 Crankshaft Bearing and Oil Pressure Relief Valve 5
72-00-09.3 Crankshaft Assembly 6
72-00-09.4 Crankshaft Thrust and Slinger Clearance 7
72-00-09.5 Crankcase Assembly 8
72-00-09.6 Connecting Rod and Piston Assembly 12
72-00-09.7 Connecting Rod Installation 13
72-00-09.8 Camshaft Assembly 14
72-00-09.9 Main Bearing Reference Marks 15 72-00-09.10 Main Bearing Installation 16 72-00-09.11 Crankcase Attaching Hardware 17 72-00-09.12 Crankcase Attaching Hardware (cont’d.) 18 72-00-09.13 Sealant Compound and Silk Thread Application 19 72-00-09.14 Crankcase Halves Assembly 20
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LIST OF FIGURES (cont’d.)
Figure
72-00-09.15 Cylinder Valve Train and Spring Assembly 72 00 09 22 72-00-09.16 Piston Assembly to Connecting Rod 23 72-00-09.17 Cylinder Assembly and Head Oil Drain Line 25 72-00-09.18 Piston Assembly with Ring Compressor Tool 26 72-00-09.19 Cylinder Base Nuts Sequence of Tightening 27 72-00-09.20 Idler Gear and Tachometer Shaft Assemblies 30 72-00-09.21 Idler Gear and Tachometer Shaft Assemblies (cont’d.) 31 72-00-09.22 Accessory Drive Gear Arrangement 32 72-00-09.23 Accessory Housing 35 72-00-09.24 Oil Pump Assembly 36 72-00-09.25 Accessory Housing Gasket Trimming 37 72-00-09.26 Inner Cylinder Cooling Baffle 39 72-00-09.27 Oil Sump and Induction System 40 72-00-09.28 Oil Level Gage 41 72-00-09.29 Induction System 42 72-00-09.30 Intake Tube Assembly 43 72-00-09.31 Vacuum Pump Drive 45 72-00-09.32 Fuel Pump 47 72-00-09.33 Propeller Governor Adapter 49 72-00-09.34 Propeller Governor Oil Line 50 72-00-09.35 Oil Filter Assembly 51 72-00-09.36 Fuel Priming System 53 72-00-09.37 Carburetor Installation 54 72-00-09.38 Fuel Injection Servo Installation 55 72-00-09.39 Fuel Injection Manifold Installation 56 72-00-09.40 Magneto and Adapter Installation 59 72-00-09.41 Starter Ring Gear Alignment 60 72-00-09.43 Alternator Installation 61
Chapter
Section
Page
Sub-Section
72-00-13.1 Cylinder Interior Resurface Crosshatch 15 16
72-00-13.2 Cooling Fin Removal Maximum 18
72-00-13.3 Valve Seat Dimensions 23
72-00-13.4 Valve Guide Dimensions 24
72-00-13.5 Valve to Seat Fit Acceptable Criteria 25
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O-360 and IO-360 Series Engines
LIST OF TABLES
Table
Section
Chapter
01-00-00.1 Abbreviations 01 00 00 2
01-00-00.2 Consumable Materials 3
02-00-00.1 Manufacturer’s General Specifications 02 00 00 3
02-00-00.2 Accessory Drive Specifications 4
02-00-00.3 Manufacturer’s Physical Specifications 4
02-00-00.4 Engine Accessories 4
02-00-00.5 Illustrated Views of the Engine 5
72-00-03.1 Special Tools and Equipment 72 00 03 1
72-00-03.2 Abnormal Operating Procedures 1
72-00-03.3 Engine Will Not Start 2
72-00-03.4 Rough Idling 2
72-00-03.5 Engine Not Able To Develop Full Power 2
72-00-03.6 Rough Engine Operation 3
72-00-03.7 Low Power & Engine Runs Rough 3
72-00-03.8 Low Oil Pressure On Engine Gage 3
72-00-03.9 High Oil Temperature 4 72-00-03.10 Excessive Oil Consumption 4
Page
Sub-Section
72-00-05.1 Equipment and Materials List 05 1
72-00-06.1 Disassembly Materials 06 1
72-00-06.2 Discard Parts 1
72-00-06.3 Special Tools and Equipment 3
72-00-07.1 Equipment Required for Cleaning 07 1
72-00-07.2 Materials Required for Cleaning 1
72-00-08.1 Inspection Materials 08 1
72-00-08.2 Special Tools and Equipment 1
72-00-09.1 Assembly Materials 09 1
72-00-09.2 Special Tools and Equipment 2
72-00-10.1 Equipment and Materials List 10 1
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O-360 and IO-360 Series Engines
LIST OF TABLES (cont’d)
Table
Section
Chapter
72-00-11.1 Dimensional Limits 72 00 11 1
72-00-11.2 Torque Limits 3
72-00-11.3 Backlash and End Clearance Limits 4
72-00-11.4 Valve Spring Dimensional Limits 4
72-00-11.5 Crush Type Gasket Tightening Angles 4
72-00-12.1 Storage Materials 14 1
72-00-13.1 List of Repairs 13 2
72-00-13.2 List of Materials 2
72-00-13.3 List of Equipment 3
72-00-13.4 List of Repair Codes 3
72-00-13.5 Reserved -
72-00-13.6 Consumable Materials for Paint Procedures 11
72-00-13.7 Exhaust Valve Seat Standard and Oversize Dimensions 20
72-00-13.8 Intake Valve Seat Standard and Oversize Dimensions 20
72-00-13.9 Exhaust Valve Guide Standard and Oversize Dimensions 21 72-00-13.10 Intake Valve Guide Standard and Oversize Dimensions 21
Page
Sub-Section
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Overhaul Manual
O-360 and IO-360 Series Engines
INTRODUCTION
About This Manual
The purpose of this Overhaul Manual is to provide the necessary instructions for major repair and replacement of Superior Vantage O-360 and IO-360 series engines. Maintenance information may be found in the Maintenance Manual, SVMM01.
The information in this publication is based on data available at the time of publication and is updated, supplemented, and automatically amended by Service Bulletins and Publication Revisions that are issued by Superior Air Parts Inc.
This manual is divided into separate sections relating to the general and specific overhaul instructions required for the engine. These general and specific instructions are generally organized and numbered per the recommendations of the General Aviation Manufacturers Association (GAMA). In this way, information may be located in a conventional manner to aid in both accuracy and timeliness.
Page numbering is organized within each section. The section number (e.g., 72-00-01) is displayed in the right hand section of the footer on each page. The page number is displayed in the center of the footer on each page.
Superior Air Parts has made clear and accurate information available for those who maintain, own and repair the Vantage O-360 and IO-360 Series Engines. Superior Air Parts values your input regarding revisions and additional information for our manuals. Please forward your comments and input to:
Superior Air Parts Attn: Engineering Department 621 South Royal Lane Suite 100 Coppell, Texas 75019
Related Publications
The following are related engine and accessory publications.
O & IO-360 Installation and Operation Manual, SVIOM01 O & IO-360 Maintenance Manual, SVMM01 O & O-360 Illustrated Parts Catalog, SVIPC01 Unison Master Service Manual, F-1100 Unison Autolite Manual, L-1710A Precision RSA-5 Service Manual, 15-338 Precision MA-4-5 Manual, MSAHBK-1 Champion Aerospace Service Manual, AV-6R Kelly Aerospace Service Manual, OE-A2
Obtaining Service Information
All Vantage Series Engine manuals and service information may be downloaded at: www.superiorairparts.com
All Vantage Series Engine manuals and service information may be purchased by contacting:
Superior Air Parts 621 South Royal Lane, Suite 100 Coppell, Texas 75019
or call: 972-829-4600 Accessory Information may be obtained at:
www.championaerospace.com www.unisonindustries.com www.skytecair.com www.precisionairmotive.com www.aeroaccessories.com www.kellyaerospace.com
Abbreviations
A list of abbreviations used in this manual is shown in Table 01-00-00.1 below.
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Introduction
Overhaul Manual
O-360 and IO-360 Series Engines
Table 01-00-00.1 • Abbreviations
Abbreviation Definition
AMS Aerospace Material Standard Assy Assembly BTC / BTDC Before Top Center / Before Top Dead Center CHT Cylinder Head Temperature DIA Diameter F Fahrenheit Fig. Figure Ft-Lb Foot-Pounds IAW In Accordance With I.D. Inside Diameter In-Lb Inch-Pounds Lb Pounds No. Number NPT National Pipe Thread O.D. Outside Diameter Oz. Ounce P/N Part Number Prop Propeller PSI Pounds per Square Inch RPM Revolutio ns Per Minute SAE Society of Automotive Engineers TIR Total Indicator Reading UNF Unified National Fine ° Degree
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Introduction
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O-360 and IO-360 Series Engines
Consumable Materials List
Refer to Table 01-00-00.2 below for consumable materials used during repair of the Vantage O­360 and IO-360 series engines.
Table 01-00-00.2 • Consumable Materials
Material Source
Acetone or Methyl Ethyl Ketone (MEK) Commercially Available Assembly Grease – Lubriplate No. 105 Commercially Available Cleaning Solvent Comm ercially Available Copper Based Anti-seize, Fel-ProTM C5-A Commercially Available Fuelube Isopropyl alcohol Commercially Available LoctiteTM 271, P/N 27183 Commercially Available LoctiteTM No. 2 Gasket Sealant P/N 30514 Commercially Available Lubricating Oil, SAE 10 Commercially Available Lubricating Oil, SAE 50 Commercially Available Mineral Oil (MIL-L-6082), SAE 50 weight Commercially Available PermatexTM, P/N 27100 Commercially Available PliobondTM #20 Commercially Available Pre-Lube Mixture – approx. 15% pre-lubricant
(STPTM brand or equivalent) plus 85% SAE 50 straight weight mineral oil
Preservative oil mix (MIL-C-6529, type 1 plus MIL-L-6082)
RTVTM 102 Silicon Sealant General Electric Safety Wire (0.032) Type 304 Stainless Steel,
P/N MS20995 C32 Safety Wire (0.041) Type 304 Stainless Steel,
P/N MS20995 C41 SilasticTM 140 Sealant Commercially Available Silk thread, size 00 (100% Silk) Commercially Available STPTM High Viscosity Oil Treatment Commercially Available TitesealTM No. 2 Gasket and Joint Compound
P/N T2-01 Phthalate resin-type enamel AMS3125C or
equivalent MIL-E-7729 Randolph Black (#303) Toluene or equivalent AMS3180 (or equivalent
Federal Spec TT-T-548) Zinc Chromate Primer Commercially Available
TM
NOTE:
Equivalent substitutes may be used.
Ohio Industrial Lubricants
Locally Prepared Mixture
Locally Prepared Mixture
Commercially Available
Commercially Available
Commercially Available
Commercially Available
Commercially Available
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Introduction
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O-360 and IO-360 Series Engines
DESCRIPTION AND OPERATION
General Description
Superior Vantage Engines are four-cylinder, horizontally opposed, air-cooled, direct drive powerplants incorporating a wet sump, bottom mounted induction, bottom exhaust with either carbureted or port injected fuel systems. Provisions exist for both front and rear mounted accessories. All engine components will be referenced as they are installed in the airframe. Therefore, the “front” of the engine is the propeller end and the “rear” of the engine is the accessory mounting drive area. The oil sump is on the “bottom” of the engine and the cylinder shroud tubes are on the “top”. The terms “left” and “right” are defined as being viewed from the rear of the engine looking toward the front. Cylinder numbering is from the front to the rear with odd numbered cylinders on the right side of the engine. The direction of crankshaft rotation is clockwise as viewed from the rear of the engine looking forward unless otherwise specified. Accessory drive rotation direction is
defined as viewed from the rear of the engine looking forward.
Continued Airworthiness
Vantage Engines discussed in this document must be installed and operated in accordance with the limitations, conditions and operating procedures described in the Installation and Operation Manual (SVIOM01). They must also be maintained in accordance with this manual and the applicable Overhaul Manual (SVOHM01) and other Instructions for Continued Airworthiness. The engine’s time between overhaul (TBO) period is initially defined as 1000 hours. A TBO extension program is in process.
Model Designations
The model number designation is defined in a way that the digits of the model number can easily identify the basic configuration of the engine as described in Figure 02-00-00.1.
Figure 02-00-00.1 • Engine Model Number Designation
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Description and Operation
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O-360 and IO-360 Series Engines
Fuel System Type
IO Denotes Port Fuel Injection System and “opposed cylinder” arrangement. O Denotes a carbureted system and “opposed cylinder” arrangement.
Cylinder Type
360 Parallel valve cylinder, 361 cubic inches.
Model Suffix
1st Digit Crankshaft & Propeller Type A Fixed-Pitch, Thin-wall front main
B Constant-Speed, Thin-wall front main D Constant-Speed, Heavy-wall front main
E Fixed-Pitch, Solid front main
2nd Digit Crankcase & Engine Mount Type
3rd Digit Accessory Package
4th Digit Power Rating: Piston Compression Ratio
Denotes detail engine configuration
C Fixed-Pitch, Heavy-wall front main
1 #1 Dynafocal Mount 2 #2 Dynafocal Mount 3 Conical Mount
Fuel System Ignition System
Carbureted (O-360) Fuel Injected (IO-360)
A Unison Magnetos Precision Carburetor Precision Fuel Injection
1* - ­ 2 8.5:1 180
* For Future Use
Cylinder Type 360 CR HP
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Description and Operation
Overhaul Manual
O-360 and IO-360 Series Engines
Engine Components General Description
The O-360 and IO-360 series engines are air­cooled, four cylinder, horizontally opposed, direct drive engines. See Table 02-00-00.1 for Manufacturer’s General Specifications.
The complete engine includes the following components and assemblies:
Crankcase Assembly Crankshaft Assembly Camshaft Assembly Valve Train Assembly Cylinder Assemblies Connecting Rod Assemblies Oil Sump Assembly Intercylinder Baffles Starter Lubrication System (Includes Oil Filter) Accessory Drive Ignition System (Includes Spark Plugs) Fuel System Starter Support Assembly Oil Gage Induction System Accessories
NOTE: Complete engine does not include outer cylinder baffles, propeller governor, and airframe to engine control cables, attaching hardware, hose clamps, vacuum pump, exhaust system, or fittings. Fuel pump is included, unless otherwise specified, on carbureted engines. Alternator may be included, if specified.
Specifications
The manufacturer’s physical specifications are listed in Table 02-00-00.2 and are applicable to the O-360 and IO-360 series engines. Accessory Drive Specifications are provided in Table 02-00-00.2 and is also applicable for both O-360 and IO-360 models. Table 02-00-00.3 lists Physical Specifications for the engines and Accessories are provided in Table 02-00-00.4. The Model Specification Data (MSD) provides more specific information by engine type and is available from Superior Air Parts, Inc.
Illustrated views of the O-360 and IO-360 engines identifying key components and sub­assemblies are provided in Figures 02-00-00.1 thru 02-00-00.9 of this section and are listed Table 02-00-00.5 for convenience. Figure 02­00-00.10 illustrates the engine wiring diagram and Figure 02-00-00.11 illustrates the oil system schematic.
Table 02-00-00.1 • Manufacturer’s General Specifications
Model O-360 and IO-360 Rated Power Hp 180 Rated Speed, RPM RPM 2700 Bore, inches In 5.125 Stroke, inches In 4.375 Displacement cubic inches In Compression Ratio 8.5:1 Firing Order 1-3-2-4 Spark timing °BTDC 25 Propeller drive ratio 1:1 Propeller drive rotation
(viewed from rear)
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3
361.0
Clockwise
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Overhaul Manual
O-360 and IO-360 Series Engines
Table 02-00-00.2 • Accessory Drive Specifications
Accessory
Starter 16.556:1 Counter-Clockwise Alternator (not included) 3.250:1 Clockwise Tachometer 0.500:1 Clockwise Magneto 1.000:1 Clockwise Vacuum Pump (not included) 1.300:1 Counter-Clockwise Propeller Governor (not included) 0.866:1 Clockwise Fuel Pump (if furnished) 0.500:1 Plunger Operated
Table 02-00-00.3 • Manufacturer’s Physical Specifications
Model
O-360-Axxx 24.6 33.4 32.8 288 O-360-Bxxx 24.6 33.4 32.8 291 O-360-Cxxx 24.6 33.4 32.8 291 O-360-Dxxx 24.6 33.4 32.8 294 O-360-Exxx 24.6 33.4 32.8 295 IO-360-Axxx 24.0 33.4 32.8 290 IO-360-Bxxx 24.0 33.4 32.8 293 IO-360-Cxxx 24.0 33.4 32.8 IO-360-Dxxx 24.0 33.4 32.8 296 IO-360-Exxx 24.0 33.4 32.8 297
Height
(In)
Table 02-00-00.4 • Approved Engine Accessories
Drive Ratio
Width
(In)
Direction of
Rotation
Length
(In)
Weight
(Lb)
293
Model
O-360
IO-360
© March 2005 Superior Air Parts Inc.
Left
Magneto
Unison
4371
Unison
4371
Right
Magneto
Unison
4371
Unison
4371
Fuel
System
Precision
MA-4-5
Precision
RSA-5
Fuel Pump
(if furnished)
Aero Acc.
AF15472
Aero Acc.
AF15473
4
Starter
SkyTec
149-12LS
SkyTec
149-12LS
Spark Plug
Harness
Unison M4001
Unison M4001
Alternator
(if furnished)
Kelly Aerospace
ALY8520LS
Kelly Aerospace
ALY8520LS
02-00-00
Description and Operation
Overhaul Manual
O-360 and IO-360 Series Engines
Table 02-00-00.5 • Illustrated Views of the Engine
Engine View Figure Number Location
O-360 Engine Front View Figure 02-00-00.2 p. 7 O-360 Engine Left Side View Figure 02-00-00.3 p. 8 O-360 Engine Top View Figure 02-00-00.4 p. 9 O-360 Engine Rear View Figure 02-00-00.5 p. 10 IO-360 Engine Front View Figure 02-00-00.6 p. 11 IO-360 Engine Left Side View Figure 02-00-00.7 p. 12 IO-360 Engine Top View Figure 02-00-00.8 p. 13 IO-360 Engine Rear View Figure 02-00-00.9 p. 14 Ignition Wiring Diagram Figure 02-00-00.10 p. 15 Oil System Schematic Figure 02-00-00.11 p. 16
© March 2005 Superior Air Parts Inc.
5
02-00-00
Description and Operation
Overhaul Manual
O-360 and IO-360 Series Engines
SPARK P LUG
SPARK PLUG
CHT PROBE LOCATION (TYPICAL EACH HEAD)
ALTERNATOR & BELT NOT
PROVIDED WITH ENGINE
THROTTLE LEVER
FUEL LINE
CARBURETOR
Figure 02-00-00.2 • O-360 Engine Front View
STARTER
PRIMING
SYSTEM
© March 2005 Superior Air Parts Inc.
6
02-00-00
Description and Operation
Overhaul Manual
O-360 and IO-360 Series Engines
CYLINDER
CRANKCASE
ASSEMBLY
ASSEMBLY
ACCESSORY
HOUSING
STARTER SUPPORT
ASSEMBLY
PRIMING
SYSTEM
STARTER
INDUCTION
SYSTEM
SPARK P L U G
OIL SUMP
ASSEMBLY
CARBURETOR
MIXTURE
LEVER
OIL FILTER
FUEL
PUMP
FUEL LINE
HARNESS
MAGNETO
Figure 02-00-00.3 • O-360 Engine Side View
© March 2005 Superior Air Parts Inc.
7
02-00-00
Description and Operation
Overhaul Manual
O-360 and IO-360 Series Engines
INTER-CYLINDER BAFFLE
SPARK P L U G
MAGNETO
OIL FILTER
Figure 02-00-00.4 • O-360 Engine Top View
8
© March 2005 Superior Air Parts Inc.
MAGNETO
02-00-00
Description and Operation
Overhaul Manual
O-360 and IO-360 Series Engines
Figure 02-00-00.5 • O-360 Engine Rear View
© March 2005 Superior Air Parts Inc.
9
02-00-00
Description and Operation
Overhaul Manual
O-360 and IO-360 Series Engines
FUEL INJECTION
MANIFOLD
CHT PROBE LOCATION (TYP ICAL EAC H H EAD)
NOT PROVIDED WITH ENGINE
SPARK PLUG
ALTERNATOR & BELT
STARTER
SPARK PLUG
FUEL
INJECTOR
Figure 02-00-00.6 • IO-360 Engine Front View
© March 2005 Superior Air Parts Inc.
FUEL INJECTION
SERVO
10
02-00-00
Description and Operation
Overhaul Manual
O-360 and IO-360 Series Engines
STARTER SUPPORT
ASSEMBLY
CRANKCASE
ASSEMBLY
STARTER
SPARK PLUG
OIL SUMP
CYLINDER
ASSEMBLY
FUEL INJECTION
MANIFOLD
ACCESSORY
FUEL INJECTION
SERVO
HOUSING
FUEL LINE
OIL FILTER
WIRING
HARNESS
MAGNETO
FUEL PUMP
Figure 02-00-00.7 • IO-360 Engine Left Side View
© March 2005 Superior Air Parts Inc.
11
02-00-00
Description and Operation
Overhaul Manual
O-360 and IO-360 Series Engines
FUEL INJECTION
MANIFOLD
FUEL INJ ECTIOR
Figure 02-00-00.8 • IO-360 Engine Top View
© March 2005 Superior Air Parts Inc.
12
02-00-00
Description and Operation
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