Private Pilot Ground Course Lesson 6: Aircraft Stability Explained

Private Pilot Ground Course Lesson 6: Aircraft Stability Explained

Why Does an Airplane Want to Return to Straight-and-Level Flight?

Have you ever been flying along, hit a little turbulence, and noticed that the airplane seems to want to settle itself back down?

That isn't an accident. It is aircraft stability, and understanding it can make you a much better pilot.

In Lesson 5, we talked about how the pilot controls the airplane using the elevator, ailerons, and rudder. Now we're going to build on that and look at what the airplane itself does after it has been disturbed.

Aircraft stability can sound like one of those subjects you only memorize long enough to pass the FAA written exam. It shouldn't be. Once you start flight training, understanding stability will help explain why your trainer behaves the way it does and why new pilots have a tendency to overcontrol the airplane.

Quick answer: Aircraft stability is the airplane's tendency to correct for a disturbance and return toward its original flight condition. Most common training airplanes are intentionally designed to be stable because a stable airplane is generally easier to control.

What Is Aircraft Stability?

Imagine that you're flying straight and level and turbulence suddenly pushes the nose upward.

What happens next?

A stable airplane has a natural tendency to work its way back toward the condition it was in before the disturbance. The pilot may still need to make corrections, but the airplane isn't fighting you every second of the flight.

This is one reason airplanes such as the Cessna 172 and Piper Cherokee make good trainers. They are designed to be relatively forgiving.

But there is more than one kind of stability. For the private pilot written exam, and for understanding what you actually feel in the airplane, you need to know the difference between static stability and dynamic stability.

Static Stability: What Does the Airplane Do First?

Static stability describes the airplane's initial reaction after it has been disturbed.

Suppose you raise the nose five degrees and then relax the control pressure. There are three possibilities:

Type What the Airplane Initially Does
Positive static stability Tends to move back toward its original position
Neutral static stability Tends to remain in the new position
Negative static stability Tends to continue moving farther away from the original position

For most normal training airplanes, positive static stability is what we want.

If turbulence raises the nose, the airplane has a tendency to bring the nose back down. If the airplane is disturbed in roll or yaw, the design of the aircraft also provides stabilizing tendencies around those axes.

That doesn't mean you can take your hands off the controls and ignore the airplane. It simply means the airplane's design is helping you instead of constantly working against you.

Dynamic Stability: What Happens After That?

Static stability tells us what happens first. Dynamic stability tells us what happens over time.

Let's use the same example. The nose gets pushed upward. Positive static stability causes it to start moving back down. But it probably won't stop at exactly the original attitude. It may move slightly below it, then back above it, then below it again. Those movements are called oscillations.

With positive dynamic stability, each oscillation becomes smaller until the airplane settles back toward equilibrium.

With neutral dynamic stability, the oscillations continue at roughly the same size. With negative dynamic stability, the oscillations become progressively larger.

For the type of flying most student pilots are doing, positive dynamic stability is desirable because the airplane tends to settle down instead of becoming progressively harder to control.

Why Student Pilots Tend to Overcontrol

This is where stability stops being a written-test definition and starts becoming useful in the cockpit.

A new student feels the nose move and immediately makes a correction. Then the airplane starts responding, but the student doesn't wait long enough to see what that correction actually did. So another correction goes in. Then another.

Pretty soon the student and the airplane are taking turns correcting each other.

One of the hardest things for a new pilot to learn is that small control inputs are usually better than large ones. Make the correction, give the airplane time to respond, and then decide whether another correction is necessary.

Understanding stability helps you trust the airplane a little more instead of chasing every tiny movement of the nose or wings.

Stability Around the Three Axes

Remember the three aircraft axes from Lesson 5? Aircraft stability works around those same axes.

Type of Stability Movement Axis
Longitudinal stability Pitch Lateral axis
Lateral stability Roll Longitudinal axis
Directional stability Yaw Vertical axis

Those names can be confusing at first. The easiest way to remember them is to focus on the movement: longitudinal stability deals with pitch, lateral stability deals with roll, and directional stability deals with yaw.

Longitudinal Stability: Keeping Pitch Under Control

Longitudinal stability is the airplane's stability in pitch.

In many conventional training airplanes, the center of gravity is located ahead of the aerodynamic center, and the horizontal tail provides the balancing aerodynamic force needed to keep the airplane in equilibrium.

The location of the center of gravity is extremely important. An aft CG generally reduces longitudinal stability. If the CG moves too far aft, the airplane can become more difficult to recover from a stall or spin.

A forward CG generally provides greater stability, but too much forward CG also creates problems. It increases the tail force required, adds drag, and can eventually reduce the elevator authority available for rotation or landing flare.

That is why weight and balance isn't paperwork you do just to satisfy a regulation. Where the weight is located actually changes the way the airplane flies.

Lateral Stability: Helping Keep the Wings Level

Lateral stability deals with roll around the airplane's longitudinal axis.

Aircraft designers use several features to improve lateral stability. One of the easiest to recognize is dihedral.

Dihedral means the wings angle slightly upward from the fuselage toward the wingtips. If the airplane is disturbed and begins to roll, the resulting sideslip and wing geometry can create a restoring tendency that helps roll the airplane back toward level flight.

Wing position, sweep, keel effect, and weight distribution can also contribute to lateral stability depending on the aircraft design.

Directional Stability: Keeping the Nose Pointed Straight

Directional stability deals with yaw.

The big player here is the vertical stabilizer. Think of the feathers on the back of an arrow or the tail of a weather vane. When the airplane yaws away from the relative wind, airflow against the vertical tail helps create a restoring tendency that points the airplane back toward the relative wind.

That doesn't eliminate the need for rudder. You still have to control adverse yaw, coordinate turns, compensate for left-turning tendencies, and use the rudder correctly during takeoff and landing.

Where Does Trim Fit Into All of This?

Trim is one of the best tools a student pilot has, and many new pilots don't use it enough.

When you change airspeed, power, or configuration, the control pressure required to hold the airplane where you want it can change. Instead of constantly pulling or pushing on the yoke, you can use trim to relieve that control pressure.

A good habit is: Pitch. Power. Trim.

Put the airplane where you want it, establish the correct power and airspeed, and then trim away the remaining control pressure. The goal is not to fly the airplane with the trim wheel. The goal is to use trim after establishing the desired condition so you aren't constantly fighting the controls.

Why Aircraft Stability Matters in Real Flying

  • Training airplanes are generally forgiving.
  • Small control inputs usually work better than large ones.
  • An aft CG can make an airplane less stable.
  • Proper trim can dramatically reduce your workload.
  • The airplane may oscillate slightly after a disturbance before settling.
  • You need to give the airplane time to respond instead of immediately making another correction.

The better you understand what the airplane is naturally trying to do, the easier it becomes to work with the airplane instead of fighting it.

The Bottom Line

Aircraft stability is the airplane's tendency to respond to disturbances in a predictable way.

Static stability describes the airplane's initial response. Dynamic stability describes what happens over time. And the airplane must be stable around all three axes: pitch, roll, and yaw.

If Lesson 5 was about how you tell the airplane what to do, Lesson 6 is about what the airplane does after you tell it—or after turbulence tells it for you.

Learn it for the written exam, but don't forget it after the test. Understanding stability will make the concepts your instructor teaches in the airplane make a lot more sense.

Continue Your Private Pilot Training

Lesson 6 is part of the complete Red Yeti Aviation Private Pilot Ground Course series.

You can watch the full Aircraft Stability lesson for free through Free Pilot Training, or continue through the structured Red Yeti Aviation Private Pilot Ground Course with video lessons, reading assignments, quizzes, practice tests, and the instructor endorsement required when you're ready for the FAA knowledge test.

WATCH LESSON 6 → VIEW THE PRIVATE PILOT GROUND COURSE →

Back to blog