Aerotime

APRIL 3, 2025

The 56 aircraft that participated in the 1914 competition presented a wide range of aviation innovations, ranging from assisted starting mechanisms, automatic carburetors, basic stabilization systems, and many other innovations that purported to benefit aviation safety.

Weight-Shift-Control 298

Weight-Shift-Control Cockpit Pilot Stability 298

Pilot Institute

JUNE 4, 2025

A tailless aircraft is a fixed-wing airplane without a horizontal stabilizing surface. With this type of aircraft, the functions of longitudinal stability and control are incorporated into the main wing. A tailless aircraft may still have a fuselage and a vertical tail (fin and rudder). How does the tail do this? Lets find out.

Tail 52

Tail Airplanes Weight-Shift-Control Drag 52

Plane and Pilot

MAY 3, 2025

To some extent this was carried out with the Cherokee, though the key design elementuse of a stabilator in place of a conventional elevator and fixed horizontal stabilizeris likely the influence of John Thorp. Thorp joined the Piper design team during the Cherokees development; his own Sky Scooter used a stabilator.

Approach 73

Approach Airplanes Stability Weight-Shift-Control 73

Pilot Institute

FEBRUARY 20, 2025

Adverse yaw is a side effect of aileron use, countered by rudder input. What Is Aircraft Stability? Stability is the aircrafts tendency to maintain its attitude or orientation. This means that they have to be effective enough to counter the aircrafts inherent lateral stability. This is where the rudder comes in.

Aileron 90

Aileron Weight-Shift-Control Rudder Longitudinal Axis 90

Pilot Institute

NOVEMBER 23, 2024

PARE: Power idle, Ailerons neutral, Rudder opposite, Elevator forward. An aft center of gravity increases flat spin risk. A flat spin happens when the center of gravity shifts too far aft (toward the tail), and the aircraft’s rotation becomes more horizontal. Rudder: Full opposite input to the spin direction.

Center of Gravity 98

Center of Gravity Weight-Shift-Control Aileron Rudder 98

Pilot Institute

APRIL 12, 2025

The aircraft pivots about its center of gravity. Rudder The rudder is the panel on the vertical part of the aircrafts tail. This is where the rudder comes in. If you press the left pedal, the rudder turns to the left. Oncoming airflow hits the protruding rudder and deflects to the left ( action ).

Lift 52

Lift Torque Thrust Aileron 52

Pilot Institute

NOVEMBER 11, 2024

How an aircraft handles Dutch roll depends on its dynamic stability. The aircraft’s design influences its dynamic stability. To understand the aircraft’s response to a disturbance, you need to understand aerodynamic stability. There are two main types of stability: Static and Dynamic stability.

Stability 52

Stability Center of Gravity Aileron Rudder 52