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General| Compression Ratio | 8.5:1 |
|---|---|
| Ignition | Dual Magneto |
| Cooling System | Air-cooled |
| Redline | 2700 RPM |
| Displacement | 360 cubic inches (5.9 L) |
| Bore | 5.125 inches (130.2 mm) |
| Stroke | 4.375 inches (111.1 mm) |
| Max Power | 180 hp (134 kW) at 2700 RPM |
| Fuel Type | Avgas 100LL |
| Weight | 270 lbs (122 kg) |
| Oil Capacity | 8 quarts (7.6 liters) |
| Type | Horizontally opposed, four-cylinder, four-stroke, air-cooled, direct-drive, fuel-injected aircraft engine |
General description of engine parts and their function.
Details on cylinders, crankcase, crankshaft, connecting rods, and pistons.
Information on cooling, induction, lubrication, and ignition systems.
Model application table and counterweight details.
Detailed specifications for various O-360, HO-360, IO-360 series.
Specifications for engine accessories and weight data.
Physical dimensions for different engine models.
Basic principles for engine operation and care.
Step-by-step guide for starting the engine.
Procedures for ground running, warm-up, and checks.
Guidelines for operating the engine during flight.
Procedures for adjusting fuel-air mixture.
Use and operation of the carburetor heat system.
Essential checks before each flight.
Details for 25, 50, and 100-hour inspections.
Procedures for longer interval inspections.
Procedures for ignition and electrical components.
Maintenance tasks for fuel lines, filters, and carburetors.
Procedures for oil system components.
Tasks related to engine cylinders and mounts.
Procedures for drive belts and turbocharger controls.
Diagnosing and fixing common engine issues.
Diagnosing and fixing turbocharger problems.
Data on horsepower reduction at altitude.
Conversion between speed units.
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