Left-turning tendencies and ground effect
8 min readLesson 16 of 59
By the end of this lesson you'll be able to:
- Name the four left-turning tendencies
- Explain when P-factor is strongest
- Describe ground effect and how it affects takeoff and landing
Why the airplane wants to go left
In airplanes with a propeller that turns clockwise (as seen from the cockpit), four effects make the nose want to go left, especially at high power and low airspeed, like on takeoff and climb. You counter them with right rudder.
- Torque. The engine spins the propeller clockwise, so the airplane wants to roll the opposite way, to the left (Newton's third law).
- Spiraling slipstream. The propeller's slipstream corkscrews around the fuselage and hits the left side of the vertical tail, yawing the nose left.
- P-factor (asymmetric propeller loading). At a high angle of attack, the descending blade on the right side takes a bigger "bite" of air than the ascending blade on the left, so the right side makes more thrust and yaws the nose left. It's strongest at high power and high angle of attack, like a climb.
- Gyroscopic precession. The spinning propeller acts like a gyroscope. When you pitch the nose (for example, raising the tail on a tailwheel takeoff), the force shows up 90° ahead in the direction of rotation, producing a yaw.
Ground effect
When the airplane is within about one wingspan of the ground, the ground interferes with the wingtip vortices and the downwash. That reduces induced drag and lets the wing make the same lift at a lower angle of attack. The effect is strongest very close to the surface.
- On landing, ground effect makes the airplane float, especially if you're too fast. Fly the right approach speed.
- On takeoff, an airplane can lift off in ground effect at a speed too slow to climb out of it. As it rises above ground effect, induced drag increases and it can settle back down. Soft-field takeoffs use ground effect on purpose, but you must accelerate to a safe climb speed before climbing out of it.
Key takeaways
- Four left-turning tendencies: torque, spiraling slipstream, P-factor, gyroscopic precession. Counter with right rudder.
- P-factor is strongest at high power and high AoA.
- Ground effect (within about one wingspan) reduces induced drag: floating on landing, early liftoff on takeoff.
What the examiner may ask
Practice answering out loud before you open each answer.
Why does the airplane yaw left on takeoff?
Torque, spiraling slipstream, P-factor and gyroscopic precession, strongest at high power and low airspeed.
How does ground effect affect a landing?
It reduces induced drag, so the airplane floats, especially if you're fast.
Why can't you climb out of ground effect too slowly?
As you leave ground effect, induced drag increases, and the airplane may settle back or stall if it's below a safe climb speed.
Common mistakes
- Not adding enough right rudder on takeoff and climb.
- Landing fast and fighting the float instead of slowing on approach.
- Climbing out of ground effect before reaching a safe climb speed on soft-field takeoffs.
Read it in the FAA sources
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Lesson check
Get every question right to complete the lesson. Take your time; wrong answers explain why.
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