Piston Engine Fuel Properties and Management

021-10-02Pablo Asensio Martínez2026-03-242 min

Aviation Fuel Properties

  • Octane Rating: Indicates the fuel's resistance to detonation.
    • Higher Octane: Higher resistance to detonation (burns slower/smoother).
    • Lower Octane: Lower resistance.
    • Usage: Usually safe to use a higher grade than recommended (e.g., using 100LL instead of 80/87), but strictly forbidden to use a lower grade.
  • Contamination: Water is the most common contaminant.
    • Can accumulate from condensation (empty tanks overnight) or leaks.
    • Prevention: Fill tanks overnight to minimize air space for condensation.
    • Check: Drain fuel sumps before the first flight of the day to remove water/sediment.

Abnormal Combustion

Detonation ("Engine Knock")

  • Definition: Spontaneous explosion of the fuel/air mixture inside the cylinder (instead of a smooth burn).
  • Effects:
    • Exerts excessive force/shock load on piston and cylinder head.
    • Increased noise ("knocking") and vibration.
    • High Cylinder Head Temperature (CHT).
    • Loss of power.
    • Engine damage (piston/ring failure) if severe.
  • Causes:
    • Too low octane fuel.
    • High Manifold Pressure (MAP) with Low RPM.
    • High Cylinder Head Temperature.
    • Too lean mixture.
  • Corrective Actions:
    • Reduce Manifold Pressure (Retard Throttle).
    • Enrich Mixture (Fuel cools the cylinder).
    • Increase Airspeed (Improve cooling).

Pre-Ignition

  • Definition: The mixture is ignited prematurely (before the spark plug fires) by a hot spot in the cylinder (e.g., carbon deposit, glowing spark plug tip).
  • Effects:
    • Rough running.
    • Power loss.
    • Further overheating.
    • Can cause the engine to continue running after ignition is switched off (Dieseling).
  • Difference from Detonation: Detonation is an explosion after ignition; Pre-ignition is an ignition before the spark.

Vapour Lock

  • Definition: Fuel vaporizes in the feed lines, creating bubbles that block the flow of liquid fuel.
  • Cause: High fuel temperatures, low pressure, or high altitude.
  • Prevention: Booster pumps (low-pressure pumps) in the tanks pressurize the fuel lines to suppress vaporization.
Written and reviewed by

Pablo Asensio

Aeronautical engineer. Passed the thirteen EASA ATPL(A) theoretical knowledge exams studying from these very notes. Writes and reviews each topic against the Part-FCL Learning Objectives.