
Sources of Inadvertent Stalls Becoming Spins:
- Inadequate rudder application in steep climbs
- False concept of airspeed when on base to final due to tailwind
- Having aircraft in "reverse command" area in then pattern
Full Answer
Why do Planes spin when they stall?
Many types of airplanes spin only if the pilot simultaneously yaws and stalls the airplane (intentionally or unintentionally). Under these circumstances, one wing stalls, or stalls more deeply than the other. The wing that stalls first drops, increasing its angle of attack and deepening the stall.
What is the aerodynamics of a spin in aviation?
Aerodynamics: All that is required is sufficient yaw rate while an aircraft is stalled In a spin, one or both wings are in a stalled condition, if both are stalled one wing will be in a deeper stall condition than the other The wing that stalls first will drop, increasing its angle of attack and deepening the stall.
What happens to the wings during a spin?
In a normal spin, the wing on the inside of the turn stalls while the outside wing remains flying. It is possible for both wings to stall, but the angle of attack of each wing, and consequently its lift and drag, are different.
Why do airplanes spin on their noses?
The nose sinking should cause the airspeed to increase, thereby making a flat spin impossible. The airplane is designed to avoid this dangerous condition, and all the pilot has to do is get out of the way and allow the plane to recover. But what if the pilot has ignored the proper loading of the plane?

What two things must occur for an airplane to spin?
For an airplane to actually spin, as opposed to spiral, two elements must be present - yaw and an excessive angle of attack that results in a stall. If either one of these elements is missing, the airplane won't spin.
Can a plane recover from a spin?
The recovery procedure from a spin requires using rudder to stop the rotation, then elevator to reduce angle of attack to stop the stall, then pulling out of the dive without exceeding the maximum permitted airspeed (VNE) or maximum G loading.
In what flight condition must an aircraft be placed in order to spin?
stalledIn order for an airplane to enter a spin, the airplane's wings must be stalled first. Then, an airplane begins to spin when one wing is "less" stalled than the other wing.
How do you stop a plane from spinning?
0:242:01How to Get Out of a Spin | 60 Second Flight Training - YouTubeYouTubeStart of suggested clipEnd of suggested clipYou can add power on the inboard engine to help stop the rotation. The next step is to bring yourMoreYou can add power on the inboard engine to help stop the rotation. The next step is to bring your ailerons to neutral.
How do you fix an aircraft spin?
2:006:44Spin Recovery Training in a Cessna 172 - YouTubeYouTubeStart of suggested clipEnd of suggested clipNext a ailerons neutral using ailerons to correct for a spindle just make it worse. And you wantMoreNext a ailerons neutral using ailerons to correct for a spindle just make it worse. And you want your wings to be at the same angle of attack. Then r rudder opposite the direction of the spin.
What are the 3 phases of a spin?
There are four phases of a spin: entry, incipient, developed, and recovery.
What three things must occur before recovering from a spin?
To recover from a spin, you must ensure power is off, oppose the yaw, and unstall the wings. First note yaw direction and apply full opposite rudder, and then move the control column forward to unstall the wings by decreasing the angle of attack.
What are the 4 phases of flight?
It flies because of four forces. These same four forces help an airplane fly. The four forces are lift, thrust, drag, and weight. As a Frisbee flies through the air, lift holds it up.
Can a 737 recover from a flat spin?
With it's wings swept back it tends to enter a flat spin, from my training and studies, a flat spin is unrecoverable. However, FSX Boeing 737 has a hard time recovering from the stall warning.
Can an F14 recover from a flat spin?
The F14 in a flat spin was considered unrecoverable, and none of the supposed "magical" recovery techniques that you may have heard were actually proven. Things like sweeping the wings were probably never tried in an actual spinning aircraft.
How do you recover from a stall spin?
Stall recovery is simple. You recover by adding forward elevator pressure, or at least relaxing the back elevator pressure to decrease, or lower, the angle of attack below the critical point. There's no need to panic—your airplane will respond to all of your control inputs.
Can a jet go into a flat spin?
Yes, a fighter jet can get into a flat spin at a high angle of attack. Fighter jets can get into flat spins due to faulty weight and balance before flight or disturbance in CG. More than 30 F-14 fighter jets crashed due to spin.
What causes a spin aviation?
The FAA defines a spin as “an aggravated stall that results in an airplane descending in a helical, or corkscrew path.” Since your high wing generates more lift than the low wing, it rolls your aircraft into the spin. And at the same time, your low wing produces more drag, because it’s at a higher angle-of-attack.
What are the 4 phases of a spin?
There are four phases of a spin: entry, incipient, developed, and recovery.
Can you spin a Cessna 172?
The later model 172s will spin, and are approved, but they just don’t spin as nicely as the old ones.
Can you spin a Piper Warrior?
The Warrior had to meet basic requirements, including spin recovery, in order to be Part 23 certified. It may just be that Piper didn’t choose to spend the time and money to go through the entire protocol of testing necessary to get the Warrior FAA approved for intentional spins. Defiantly possible.
Is spin training required?
Spin Training Is Rarely Required Of all pilot certificates issued in the United States, only an initial CFI certificate requires spin training. Because of this, unless flying aerobatic aircraft or holding a CFI certificate, hundreds pilots have never performed a spin.
Can a Cirrus recover from a spin?
Normally a single-engine airplane has to be spun as part of the certification process. The Cirrus wasn’ t. That is the only way a pilot can recover from a spin in a Cirrus. The stall characteristics of the airplane are not bad when compared with some other airplanes but they aren’t real good, either.
What is the difference between a spin and a spiral dive?
The difference between a spin and spiral dive is that a spin is a stalled condition and a spiral dive is an accerated condition. A spin is where you are stalled, then one wing gets more stalled than the rotation starts from that, the speed is low and stable.
What is the function of pitching down?
Next is pitch down. Well pitching down, what is the function of this? We’re once again attempting to try to break the airplane out of a stalled condition. If the airplane isn’t stalled, then we’re not in a spin, we’re just simply in a steep spiraling turn, but it’s not a spin condition. So, pitching down is ideally there to, once again, try to break the stall or reduce our angle of attack.
What is spin in airplanes?
A spin is simply an uncontrolled condition of flight for an airplane where in which it is also stalled. That seems sort of simple, so let’s break that down a little bit more and talk a little bit about some of the different elements of a spin. To start with, the first main element of a spin is that we have to be stalled.
Why do we need power idle?
What does that mean? It means that it’s going to continue on this cycle indefinitely unless we break it. Adding power at this point, is only going to make that spinning happen faster, meaning it’s going to tighten the spin even more aggressively. So, we want power idle so that it’s not aggravated any further. Additionally, this is valuable because once we break the stalled condition, generally we’re now at a fairly low pitch attitude. If we have a lot of power and they’re at low pitch attitude, we’re going to gain airspeed very quickly and then we have potentially some issues as we pull out of this dive, that we could exceed g-force limitations or exceed airspeed limitations. So easiest to remember power idle, this will prevent any of that from occurring.
How to stop auto yaw?
Once again, in the example that we had previously, we were spinning to the right so ideally, we want to stop that auto yaw by applying left rudder. In a spin condition, our rudder is not a stalled airfoil, it’s still able to produce a force, in which case pushing the left rudder in that example would ideally reduce or entirely stop the auto yaw to the right.
What is the first element of a spin?
To start with, the first main element of a spin is that we have to be stalled. So, we need the airplane to be in a stalled condition. The second piece is what is known as an incipient phase. The third is a fully developed spin and the fourth is the recovery.
Which side of an airplane has more drag?
Additionally, the right wing of the airplane has more drag than the left wing . What does that mean?
Which aileron will go down?
Well first, let’s think about the movement of the ailerons. As we move the yoke to the left, we know the left aileron will go up, the right aileron will go down, ideally then that means that the right aileron would have a greater angle of attack.
What Causes a Flat Spin?
The type of spin a plane enters depends on what happened when the condition started and how the aircraft was loaded. Weight and balance plays a pivotal role in stalls and spins.
What is flat spin training?
Stall and Spin Training. A flat spin is a dangerous flight condition that can be impossible to recover from. Thankfully, it’s not likely to happen on any routine flight. It occurs when the plane has no forward airspeed as it spins towards the ground around its vertical axis.
Why do pilots use the acronym "PARE"?
The FAA teaches the acronym “PARE” to help pilots remember how to recover from a spin and spin recovery technique.
How do ailerons work?
Ailerons work by changing the angle of attack at the plane’s wingtips. In the middle of a spin, any use of the ailerons will make the spin worse. Remember, a spin occurs when one wing is more severely stalled than the other. Ailerons will make it even more stalled.
What does it mean when an airplane spins?
A spin occurs when the aircraft is stalled, but one wing is more severely stalled than the other. To understand precisely what this means, you’ll need to understand a few basic terms and some aerodynamics.
How does a flat spin work?
To get a flat spin’s look and feel, power is used to flatten out the aircraft’s flight attitude during a normal upright spin. Even still, the forces that are put on the airframe, engine, and pilot are extreme during such a maneuver.
How to recover from a stall?
The only way to recover from a stall is to reduce the angle of attack, and that is done by moving the control column forward. In a spin, this can seem a very unnatural thing to do since the aircraft’s nose is often pointed down. But it’s the only way to get out of the situation.
How do airplanes spin?
Many types of airplanes spin only if the pilot simultaneously yaws and stalls the airplane (intentionally or unintentionally). Under these circumstances, one wing stalls, or stalls more deeply than the other. The wing that stalls first drops, increasing its angle of attack and deepening the stall. At least one wing must be stalled for a spin to occur. The other wing rises, decreasing its angle of attack, and the aircraft yaws towards the more deeply stalled wing. The difference in lift between the two wings causes the aircraft to roll, and the difference in drag causes the aircraft to continue yawing.
What is spin in flight?
In flight dynamics a spin is a special category of stall resulting in autorotation (uncommanded roll) about the aircraft's longitudinal axis and a shallow, rotating, downward path approximately centred on a vertical axis. Spins can be entered intentionally or unintentionally, from any flight attitude if the aircraft has sufficient yaw while at the stall point. In a normal spin, the wing on the inside of the turn stalls while the outside wing remains flying. It is possible for both wings to stall, but the angle of attack of each wing, and consequently its lift and drag, are different.
What are the different types of spins?
Spins can be classified using the following descriptors: 1 Incipient – With the inside wing stalled more deeply than the advancing wing, both the roll and yaw motions dominate. 2 Developed – The aircraft's rotation rate, airspeed, and vertical speed are stabilized. One wing is stalled more deeply than the other as the aircraft spins downward along a corkscrew path. 3 Recovery – With appropriate control inputs, the yaw rotation is slowed or stopped and the aircraft nose attitude is lowered, thus decreasing the wing's angle of attack and breaking the stall. Airspeed increases quickly in a nose low attitude and the aircraft is no longer in a spin. The controls respond conventionally and the airplane can be returned to normal flight.
What can lead to an unintentional spin?
One common scenario that can lead to an unintentional spin is a skidding uncoordinated turn toward the runway during the landing sequence. A pilot who is overshooting the turn to final approach may be tempted to apply more rudder to increase the rate of turn.
How many phases of spin are there in an aircraft?
In aircraft that are capable of recovering from a spin, the spin has four phases. Some aircraft are difficult or impossible to recover from a spin, especially a flat spin. At low altitude, spin recovery may also be impossible before impacting terrain, making low and slow aircraft especially vulnerable to spin-related accidents.
How does a spiral dive differ from a spin dive?
A spin differs from a spiral dive in which neither wing is stalled and which is characterized by a low angle of attack and high airspeed. A spiral dive is not a type of spin because neither wing is stalled. In a spiral dive, the aircraft responds conventionally to the pilot's inputs to the flight controls and recovery from a spiral dive requires a different set of actions from those required to recover from a spin.
What causes an aircraft to yaw?
The other wing rises, decreasing its angle of attack, and the aircraft yaws towards the more deeply stalled wing. The difference in lift between the two wings causes the aircraft to roll, and the difference in drag causes the aircraft to continue yawing.
What happens if you uncorrect a spin?
If uncorrected, an incipient spin degrades into a fully developed spin composed of a near-vertical helical flight path -- as if the plane is descending an invisible spiral stair. Such a spin can cost an aircraft hundreds of feet with every turn.
What is a spin in an air show?
Typically, you'll see the prop-driven plane soar upward in a steep ascension, only to stall out and fall into a dramatic spin.
What is stall and spin?
Stalls and Spins. As we covered earlier, an aircraft's flight is a careful balance of thrust, drag, weight and lift. Should lift decrease and drag increase suddenly, such as when an aircraft's angle of attack surpasses that for maximum lift, a stall occurs. The airframe shakes and the plane falls, at least for a few feet.
How does a pilot correct a stall?
The airframe shakes and the plane falls, at least for a few feet. In most cases the pilot merely corrects for the stall by lowering the plane's angle of attack. However, an improperly corrected stall can result in a secondary stall, or degrade into a spin.
Is a plane level or level?
In other words, the plane is mostly level as it falls in an extremely dangerous spin. Spin recovery techniques vary depending on the design of a given aircraft and where its center of gravity is situated.
Do pilots take passengers for a spin?
Most pilots aren't looking to take their passengers for a spin though. They're too busy manning the flight instruments we'll talk about next.
Why do airplanes yaw?
The other wing will rise, decreasing its angle of attack, and the aircraft will yaw toward the more deeply-stalled wing. The difference in lift between the two wings causes the aircraft to roll, and the difference in drag causes the aircraft to yaw.
Why do you need to hold the rudder after the rotation stops?
You want to stabilize the aircraft's directional control. Holding the rudder after the rotation stops could induce a spin in the opposite direction. Roll wings level. Level wins ensures you are not climbing in a turn. Climbing in a turn decreases vertical lift, and causes unnecessary load factors.
What happens when both wings are stalled?
In a spin, one or both wings are in a stalled condition, if both are stalled one wing will be in a deeper stall condition than the other. The wing that stalls first will drop, increasing its angle of attack and deepening the stall. Both wings must be stalled for a spin to occur.
How long does the spin phase last?
This phase may last for as little as a quarter turn or up to several turns depending upon the airplane and the type of spin
What is the entry phase of a pilot?
In the entry phase, the pilot intentionally or accidentally provides the necessary elements for the spin
How many steps are required for spin recovery?
In the absence of the manufacturer’s recommended spin recovery procedures and techniques, use the six-step spin recovery procedure in Figure 5-17
What is auto rotation?
Auto-rotation occurs from an asymmetrical stall (think skid) There is an abrupt loss of control when leaving the stall and entering the spin.
How a spin occurs?
At least one wing should stall for creating a normal spin condition. The inner wing loses lift and begins to stall while the outer wing supports the lift at the same moment. This movement raises the outer wing, and the aircraft began to roll towards the wing stalled at first. The difference of lift coefficient between two wings causes aircraft to roll uncontrollably, and the difference of drag causes aircraft to yaw continuously.
What is the spin recovery technique?
FAA recommends a spin recovery technique known as PARE. This method is created for pilots to recall easily during a flat spin condition.
First Off, What Exactly Is A Spin?
Before we jump into the spin recovery steps, let's take a quick look at what's happening in a spin. The FAA defines a spin as "an aggravated stall that results in an airplane descending in a helical, or corkscrew path."
So How Do You Recover With "PARE"?
Spin recovery is pretty simple: break the stall on both your wings. When you do, your plane with fly itself out of the spin. And that's where the "PARE" acronym comes into play.
Finish Your Spin Recovery
Once you've completed these 4 steps, your plane will fly itself out of the spin. When it does, bring your rudder to neutral, and raise the nose, and slowly add power to get as you get back to level flight.
Watch A Spin From The Air
Want to try a spin? Grab an instructor and a spin-approved airplane. It's a great experience, no matter how much flying time you have.
How to bring stall speed to boil?
All it takes to bring the stall/spin mix to a boil is for the pilot to let the nose slide slowly up during the turn. Between the skid and the turn, the airplane's stall speed has already gone up a few knots. The flaps have added still more drag, and if the flaps are extended fully, they are creating far more drag than lift. So, when the nose comes up a few degrees, the airplane is eager to shed still more speed.
How to train for spin?
In spin training, as it's too often given, students slow the airplane to stall speed in a nose-high, wings-level attitude. Then they stomp the rudder to the floor - and the ride begins. After a few turns the instructor tells the student to reduce power to idle, reverse the rudder (apply rudder opposite the spin's direction), ease the stick forward to break the stall, and fly out of the resulting dive.
What are the elements that make an airplane spin?
For an airplane to actually spin, as opposed to spiral, two elements must be present - yaw and an excessive angle of attack that results in a stall. If either one of these elements is missing, the airplane won't spin. If a pilot stalls an airplane when the slip/skid ball is centered, the airplane simply stalls. If the ball is off center but the speed (angle of attack) is above stall for the given situation, the airplane just slips or skids.
Why does the drag skyrocket when a pilot crosses control?
With the flaps down, its drag has increased. Also remember, when a pilot cross-controls an airplane its drag skyrockets because it's flying sideways through the air. Even if the nose stays at the same pitch angle, the increased drag scrubs off a few knots of airspeed and the airplane decelerates.
Why is it important to know how to handle everything an airplane is capable of throwing at them?
But the training to prevent stall/spin accidents has to include more than just the traditional yank-and-stomp entries and recoveries. If it doesn't, the training doesn't mirror real life and won't do much good .
Why is spin training not necessary?
Traditional spin training is not the answer to preventing stall/spin accidents. It's a fact that even if pilots were taught how to recover from a fully developed spin, it would prevent few, if any, stall/spin accidents. This is because in most stall/spin accidents, the airplane is too low to allow the spin to fully develop. Usually, the airplane is still in the early transition phase, barely past the first turn, when it hits the ground.
How to speed up a stall/spin accident?
They try to speed up the turn by using excess inside rudder (the rudder pedal on the inside of the turn) to help drag the nose around. Most of the time, they don't even realize they're doing it. They want the nose to go to the left, so they step on the left rudder to "help it along."

Overview
Aircraft design
For safety, all certificated, single-engine fixed-wing aircraft, including certificated gliders, must meet specified criteria regarding stall and spin behavior. Complying designs typically have a wing with greater angle of attack at the wing root than at the wing tip, so that the wing root stalls first, reducing the severity of the wing drop at the stall and possibly also allowing the ailerons to remain somewhat effective until the stall migrates outward toward the wing tip. One method of tailorin…
How a spin occurs
Many types of airplanes spin only if the pilot simultaneously yaws and stalls the airplane (intentionally or unintentionally). Under these circumstances, one wing stalls, or stalls more deeply than the other. The wing that stalls first drops, increasing its angle of attack and deepening the stall. At least one wing must be stalled for a spin to occur. The other wing rises, decreasing its angle of attack, …
Phases
In aircraft that are capable of recovering from a spin, the spin has four phases. Some aircraft are difficult or impossible to recover from a spin, especially a flat spin. At low altitude, spin recovery may also be impossible before impacting terrain, making low and slow aircraft especially vulnerable to spin-related accidents.
• Entry – The airplane is stalled by exceeding the wing's critical angle of attack, while allowing the …
Modes
The U.S. National Aeronautics and Space Administration (NASA) has defined four different modes of spinning. These four modes are defined by the angle of attack of the airflow on the wing.
During the 1970s NASA used its spin tunnel at the Langley Research Center to investigate the spinning characteristics of single-engine general aviation airplane designs. A 1/11-scale model was used with nine different tail designs.
History
In aviation's early days, spins were poorly understood and often fatal. Proper recovery procedures were unknown, and a pilot's instinct to pull back on the stick served only to make a spin worse. Because of this, the spin earned a reputation as an unpredictable danger that might snatch an aviator's life at any time, and against which there was no defense. In early aviation, individual pilots explored spins by performing ad-hoc experiments (often accidentally), and aerodynamicis…
Entry and recovery
Some aircraft cannot be recovered from a spin using only their own flight control surfaces and must not be allowed to enter a spin under any circumstances. If an aircraft has not been certified for spin recovery, it should be assumed that spins are not recoverable and are unsafe in that aircraft. Important safety equipment, such as stall/spin recovery parachutes, which generally are not installed on production aircraft, are used during testing and certification of aircraft for spins …
Center of gravity
The characteristics of an airplane with respect to spinning are significantly influenced by the position of the center of gravity. In general terms, the further forward the center of gravity the less readily the airplane will spin, and the more readily it can recover from a spin. Conversely, the further aft the center of gravity the more readily the airplane will spin, and the less readily it can recover from a spin. In any airplane, the forward and aft limits on center of gravity are carefully d…