Pilot Institute

MAY 4, 2024

Your aircraft will fly at a faster true airspeed at higher density altitudes. Any substantial changes to speed and descent rate will destabilize the landing. The drag allows for a steeper descent, which is particularly helpful when avoiding obstacles. Power controls the rate of descent, and pitch controls airspeed.

Weight-Shift-Control 52

Weight-Shift-Control Runway Density Altitude Approach 52

Plane and Pilot

SEPTEMBER 20, 2024

“A few seconds later the airplane data showed a maneuver consistent with an aileron roll followed by a rapid descent about 1,000 feet before regaining its prior altitude and track above the highway.” I did my first aileron roll in an RV-4. Airspeed reached 248 kias, well over the never exceed VNE of 200 kias.

True Airspeed 87

True Airspeed Indicated Airspeed Horizontal Stabilizer Aileron 87

Plane and Pilot

SEPTEMBER 20, 2024

“A few seconds later the airplane data showed a maneuver consistent with an aileron roll followed by a rapid descent about 1,000 feet before regaining its prior altitude and track above the highway.” I did my first aileron roll in an RV-4. Airspeed reached 248 kias, well over the never exceed VNE of 200 kias.

True Airspeed 85

True Airspeed Indicated Airspeed Horizontal Stabilizer Aileron 85