Pilot Institute

NOVEMBER 23, 2024

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. Some aircraft can enter flat spins even if their center of gravity is in the normal range.

Center of Gravity 98

Center of Gravity Weight-Shift-Control Aileron Rudder 98

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

Vintage Aviation News

FEBRUARY 19, 2025

(Wright State University) The original configuration of the Bell Model 68 was an open cockpit all-metal monoplane with fixed landing gear that was powered by two Armstrong Siddeley Viper turbojet engines with thrust deflectors located at the aircraft’s center of gravity.

Thrust 94

Thrust Center of Gravity Descent Cockpit 94

Pilot Institute

NOVEMBER 1, 2024

Remember that wings, propeller blades, and tail surfaces are airfoil-shaped. Additional Dangers of Ice Accumulation Icing also makes your aircraft heavier and can even change the position of the center of gravity. Many aircraft have heated leading edges on the wings, tail, and propellers.

Pitot Tube 52

Pitot Tube Drag Lift Airfoil 52

Pilot Institute

MARCH 26, 2024

This tendency is due to their high center of gravity and heavy engine over the nose wheel. As with any landing, it’s vital to have a stabilized approach. If you’re not stabilized at 200 feet AGL, go around. Make sure not to pull back too hard, or you could cause a tail strike.

NOTAMs 52

NOTAMs Runway Approach Descent 52

Pilot Institute

FEBRUARY 20, 2025

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. Lateral stability depends on the aircrafts design. This shifts the ailerons Center of Gravity (C.G.)

Aileron 90

Aileron Weight-Shift-Control Rudder Longitudinal Axis 90

Vintage Aviation News

DECEMBER 14, 2024

It was certainly a most unusual aircraft, distinguished by its forward swept wing and canard horizontal stabilizers. One of the biggest challenges for the X-29 was the unusual center of gravity, which was affected by the rear-mounting of the forward-swept wings and made the X-29 inherently unstable.

Horizontal Stabilizer 96

Horizontal Stabilizer Center of Gravity Tail Drag 96