Continuous ignition is NOT automatically provided for which of the following conditions?

Continuous ignition is a system designed to enhance engine reliability and to prevent engine stalls by automatically supplying ignition to the engine when certain conditions arise. The main purpose is to ensure the engines can maintain operation during situations that may disrupt normal combustion.

In the context of the question, continuous ignition is crucial in various scenarios like applying maximum thrust during takeoff or dealing with engine anomalies such as surges or stalls, where the risk of combustion interruption is greater. This ensures that the engines remain lit and operative under conditions where engine performance is under duress.

The selection of thrust during takeoff—whether FLEX or TOGA—activates continuous ignition to safeguard against potential engine failure during this critical phase. Similarly, if the flaps are positioned to a setting other than 0 in flight, it indicates a specific flight configuration that might create unique aerodynamic conditions, prompting the ignition system to engage continuously.

However, during turbulent air encounters, while the risk of engine performance being affected exists, the activation of continuous ignition is not automatic since it's primarily designed for conditions that more directly jeopardize engine stability, like surges or stalls. Hence, turbulent air alone does not trigger continuous ignition, making this scenario the correct answer to the question. It underscores a key aspect of the aircraft's