Flight Training Central

SEPTEMBER 9, 2024

Airplane performance can be defined as the capability of an airplane to operate effectively while serving a specific purpose. The result of an alteration in airflow patterns increasing induced drag about the wings of an airplane. Determine the approximate landing ground roll distance. a higher-than-normal angle of attack.

Density Altitude 105

Density Altitude Knot Ground Effect True Airspeed 105

Pilot Institute

DECEMBER 12, 2024

” The answers come from a clever little setup on your airplane: a metal tube sticking into the airstream and a tiny hole on the fuselage. It helps measure how fast the airplane is going by measuring the air pressure. The other important part of the system is a tiny hole on the side of the airplane, called a static port.

Pitot Tube 98

Pitot Tube Altimeter Descent Airplanes 98

Pilot Institute

NOVEMBER 16, 2024

If you’re aiming to get comfortable with managing both airspeed and altitude in flight, you’ll need to understand the difference between indicated airspeed (IAS) and true airspeed (TAS). Key Takeaways Airspeed and altitude are directly linked to each other throughout different phases of your flight.

True Airspeed 52

True Airspeed Indicated Airspeed Altimeter Lift 52

Pilot Institute

FEBRUARY 1, 2025

This section is also needed when youre calculating your true airspeed, which you need to know to plan your flight. If youre in the aircraft, set the altimeter to 29.92 If you dont have access to an altimeter, you can manually calculate the pressure altitude. Thats your true airspeed. Subtract it from 29.92.

Groundspeed 52

Groundspeed True Airspeed Density Altitude Knot 52

Pilot Institute

MAY 4, 2024

Your aircraft will fly at a faster true airspeed at higher density altitudes. The local altimeter setting is 29.65, the temperature is 25°C, and we have a 9-knot headwind. Subtract the altimeter setting from 29.92, multiply it by 1,000, and add that to the field elevation. Start by calculating the pressure altitude.

Weight-Shift-Control 52

Weight-Shift-Control Runway Approach Density Altitude 52