Your Pilot InterviewATPL EASA

Piston induction, mixture, injection and icing

Understand piston induction, mixture, injection and icing through causal explanations, a worked case and an interactive laboratory.

Meter fuel to the changing inducted air mass

Explain how a carburettor meters fuel and predict how changing air density alters the mixture at unchanged fuel delivery.

Mechanism and relationships

A float-type carburettor uses pressure differences in a venturi to meter fuel into airflow. Air accelerates through the restriction, reducing static pressure; fuel is drawn from the bowl into the low-pressure region. Mixture control changes fuel delivery relative to air. At higher altitude the same inducted volume contains less air mass, so a system without full compensation may deliver an increasingly rich mixture. Fuel injection meters and distributes fuel without the same carburettor venturi arrangement.

Reason through the evidence

Stoichiometric mixture denotes a chemically balanced air–fuel ratio, but the best-power and best-economy operating mixtures differ and depend on the engine and limitations. Rich fuel can support cooling under approved conditions; this does not make every rich setting safer, because excess fuel can reduce power and cause other problems. Exhaust-gas temperature and cylinder-head temperature measure different thermal states and respond differently to mixture changes. Use the engine’s approved leaning and power procedures rather than a universal graph setting.

Apply the explanation to a different case

Assume a synthetic metering system initially admits 14.7 units of air mass for each unit of fuel. If air mass falls to 80% while fuel remains unchanged, the ratio becomes 11.76:1. The charge is richer relative to the original chemical reference because the fuel fraction rose. If a compensating system also reduces fuel to 80%, the original ratio is retained. These two outcomes explain why altitude alone does not identify the actual mixture without knowing the metering architecture. They do not select an approved best-power, economy or cooling mixture for a particular engine.

Keep this distinction clear

A fuel-injection manifold or distribution system may have a different response to a failed pump or blocked injector than a shared carburettor. Uniform total fuel flow cannot guarantee equal delivery to every cylinder. The architecture and cylinder indications are needed to explain that distinction.

Explain why carburettor ice can form above freezing

Combine venturi cooling and fuel evaporation to explain internal carburettor icing when outside air is above freezing.

Mechanism and relationships

Fuel evaporation absorbs heat and the venturi pressure change lowers local air temperature. These effects can cool the carburettor throat below freezing even when outside air temperature is above 0°C. Moisture can then freeze on the throat or throttle, restricting airflow and changing mixture. Reduced engine power can lower temperature and pressure conditions further. The risk therefore cannot be assessed from outside temperature alone.

Reason through the evidence

Carburettor heat admits air heated through a designed path. Warmer induction air is less dense, so its selection can initially reduce power and alter mixture even when ice is absent. Melting ice can produce a transient rough response according to system and conditions. Fuel-injected engines avoid the same fuel-evaporation location but can still experience other induction icing mechanisms. Supercharging and turbocharging increase induction pressure but also heat the charge, so intercooling and boost control affect the resulting mass flow and engine limits.

Apply the explanation to a different case

A venturi changes local pressure while fuel evaporation absorbs latent heat, so the coldest internal region need not track the temperature displayed outside the aircraft. A partly closed throttle also creates a local restriction and changes the icing location. Introducing warm alternate air can alter pressure recovery and mixture as well as temperature. The apparent power change after heat selection must therefore be interpreted according to the actual system and procedure. The principle generalises to all induction systems: trace the air path and the local physical conditions rather than infer internal temperature from outside air alone.

Keep this distinction clear

An intercooler removes part of the heat added during boost compression before the charge enters the engine. At a given pressure, a lower absolute temperature increases charge density in the ideal gas relationship. Pressure improvement and temperature management must therefore be considered together when reasoning about boosted airflow.

Can you explain and apply the mechanism?

Four original questions. Work from the stated facts, then compare your reasoning with the explanation.

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Learning overview