Tail will tilt up
An airplanes Tail is called a Stabeliser. It is there to to stabilise the aircraft in the conditions that the Ailerons (Wings) cannot handle. The Stabilisor has 6different parts: - Elevator 1 - Elevator 1 yaw trim (Powered by jackscrew) - Elevator 2 - Elevator 2 yay trim (Powered by jackscrew) - Stabeliser - Vertical turner yaw
Wings, slats, flaps, fuel tanks, rudder, elevator, landing gear, cockpit, fuselage, tail fin
An elevator on a airplane are tabs on the tail that control its up and down motion in the air
The elevator is used to control the airplane's pitch (up, and down angle of the nose). The elevator is located on the horizontal tail fins.
airplanes
The plane follows the arc of the elevator and moves up when the elevators are up.
The elevator are the control surfaces on an airplane that make the aircraft pitch nose UP or DOWN and causes the airplane to rise or descend. The Elevator are usually on the tail of the aircraft and are mounted on the horizontal tail surfaces. However, some aircraft have this control forward of the main wings.
The wolf whimpers and lowers its body/tail. It then walks away with its tail behind its legs. ~chibikokomon@gmail.com
Most airplanes have fixed tail surfaces known as either a horizontal stabilizer or vertical stabilizer. The horizontal stabilizer has an attached moveable surface called an elevator while the vertical stabilizer has an attached moveable surface called a rudder. On certain airplane models, such as the Piper Cherokee or Cessna Cardinal, the entire horizontal tail is a one-piece surface that rotates and performs the function of both the horizontal stabilizer and elevator. Combining the words stabilizer and elevator, this type of control is known as a stabilator. Elevators, stabilators, and rudders, generally have another small moveable control piece on the trailing edge known as a trim tab. Most trim tabs can be adjusted by the pilot in flight to cause the control surface, to which it is attached, to stay slightly deflected in a particular direction, relieving the pilot of having to apply control forces during stabilized flight. Some trim tabs, such as rudder trim tabs on many small airplanes, must be adjusted on the ground and cannot be adjusted in flight. Some airplane designs do not require any stabilizers or control surfaces on the tail. The canard design places a horizontal stabilizer and elevator, or a stabilator, near the front of the airplane and vertical stabilizers and rudders on the tips of the main wing. The main wing is located near the rear of the airplane. The canard design is more efficient in flight than a conventional airplane design, since both the wing and horizontal stabilizer produce lift in flight. In a conventional airplane design, with stabilizers on the tail, the horizontal stabilizer produces a downward force during flight to provide stability, reducing the overall efficiency.
On almost all airplanes that have a control wheel, moving it forward and backward moves the elevator on the tail, which controls pitch (nose up or down), and turning it from side to side moves the ailerons on the wings, which makes the plane bank right or left.
that is needed to help the plane to balanceActually the planes 'TAIL' is called an elevator and an ELEVATOR is used for lift off and landing . It controls the way a plane goes up and down.By Samantha DudleyFirst Maori Female InternationalPilot
An elevator is mounted on the back edge of the horizontal stabilizer on each side of the fin in the tail. They move up and down together. When the pilot pulls the stick backward, the elevators go up. Pushing the stick forward causes the elevators to go down. Raised elevators push down on the tail and cause the nose to pitch up. This makes the wings fly at a higher angle of attack which generates more lift and more drag. Centering the stick returns the elevators to neutral and stops the change of pitch. Many aircraft use a stabilator — a moveable horizontal stabilizer — in place of an elevator. Some aircraft, such as an MD-80, use a control tab within the elevator surface to aerodynamically backdrive the main surface into position. The direction of travel of the control tab will thus be in a direction opposite to the main control surface. It is for this reason that an MD-80 tail looks like it has a 'split' elevator system.