Aerodynamics

Load Factor

Definition

The ratio of total lift to aircraft weight, expressed in G units. In straight and level flight, load factor is 1G. In a 60-degree banked turn, load factor is 2G. Exceeding structural limits causes overstress.

Why Load Factor Matters for Pilots

Understanding Load Factor is critical for passing the FAA Private Pilot Knowledge Test and performing safely in flight. Aerodynamics questions make up a significant portion of both written exams and oral checkrides. Pilots who grasp concepts like Load Factor can make better decisions during all phases of flight, from takeoff to landing.

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Exam Tip

This concept is commonly tested in aerodynamics-related questions on FAA and EASA exams. Make sure you can explain Load Factor in your own words for the oral exam. Practice applying this concept to real-world scenarios, not just memorizing the definition.

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