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Configuration | Horizontally opposed |
---|---|
Number of Cylinders | 4 |
Firing Order | 1-3-2-4 |
Cooling System | Air-cooled |
Oil System | Wet sump |
Displacement | 361 cubic inches (5.9 liters) |
Bore | 5.125 in (130.2 mm) |
Stroke | 4.375 inches (111.1 mm) |
Weight | 258 lbs (117 kg) |
Fuel Type | Avgas 100LL |
Compression Ratio | 8.5:1 |
Technical data for various O-360, HO-360, IO-360, etc. engine models.
Fundamental guidelines for engine operation, economy, and longevity.
Recommended steps for starting engines with different fuel systems.
Procedures for ground checks, takeoff, climb, and in-flight operation.
Guidance on leaning mixture and managing cylinder head temperatures.
Data on fuel pressure, oil, engine conditions, and performance curves.
Instructions for properly shutting down the engine.
Importance of regular checks for safety and durability.
Essential pre-flight checks for engine safety and readiness.
Procedures for ignition harness, wiring, and magneto timing.
Common engine problems, their probable causes, and recommended remedies.
Common turbocharger issues, causes, and solutions.