Instrument Flight Rules Practice Exam 2025 – Complete Test Prep

Question: 1 / 400

What is the expected change in pitch and thrust required when a headwind shifts to a constant tailwind?

PITCH ATTITUDE: increases; REQUIRED THRUST: increased, then reduced.

PITCH ATTITUDE: decreases; REQUIRED THRUST: increased, then reduced.

When a headwind shifts to a constant tailwind, the aircraft experiences a notable change in performance characteristics, particularly in pitch attitude and thrust requirements. A headwind is essentially opposition to the aircraft’s forward motion, requiring a certain amount of thrust to maintain a steady climb or cruise. When this headwind shifts to a tailwind, the aircraft is pushed forward more easily due to the airflow now working in the direction of travel.

Initially, the required thrust will increase because the aircraft is in the process of transitioning from a headwind scenario to a tailwind scenario. This increase in thrust helps maintain the desired airspeed as the aircraft adjusts to the change. As the aircraft stabilizes with the tailwind, the thrust can be reduced because the lift-to-drag ratio improves, and less power is required to maintain level flight or a climb.

In terms of pitch attitude, because the aircraft is effectively moving faster with the tailwind, the natural aerodynamic response promotes a decrease in required pitch attitude to maintain level flight. Therefore, in this context, as the aircraft transitions to a tailwind, it experiences a decrease in pitch attitude while requiring increased thrust initially, followed by a reduction in thrust as it settles into the new flight conditions.

This reasoning aligns with the

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PITCH ATTITUDE: remains the same; REQUIRED THRUST: consistently increased.

PITCH ATTITUDE: decreases; REQUIRED THRUST: only increased.

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