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
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.
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
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
ix
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
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:
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
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
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
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