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

Plane and Pilot

SEPTEMBER 20, 2024

Alongside a nearby highway, some recognizable bits of airplane, the vertical stabilizer and rudder, a horizontal stabilizer and elevator, fell separately to Earth. Airspeed reached 248 kias, well over the never exceed VNE of 200 kias. The vertical descent rate reached the data-recording limit of 9,999 feet per minute.

True Airspeed 89

True Airspeed Indicated Airspeed Horizontal Stabilizer Aileron 89

Plane and Pilot

SEPTEMBER 20, 2024

Alongside a nearby highway, some recognizable bits of airplane, the vertical stabilizer and rudder, a horizontal stabilizer and elevator, fell separately to Earth. Airspeed reached 248 kias, well over the never exceed VNE of 200 kias. The vertical descent rate reached the data-recording limit of 9,999 feet per minute.

True Airspeed 88

True Airspeed Indicated Airspeed Horizontal Stabilizer Aileron 88

AV Web

AUGUST 28, 2024

Powered by a single Pratt & Whitney Canada PT6A-52 turboprop engine, the M700 Fury has a maximum cruise speed of 301 knots true airspeed (ktas), with a range of 1,149 nautical miles. At normal cruise (292 ktas), range is 1,424 nm. The Fury comes with the certified FIKI system and Garmin Autoland.

True Airspeed 52

True Airspeed Descent Knot Stability 52

Air Facts

MAY 10, 2024

Perhaps just prior to the start of descent could be the optimum time–certainly completed no later than commencement of approach. Particular attention to true airspeed vs. turn radius. Recall that we must remain at or above MDA until we are in a normal position to perform a normal rate of descent to landing.

Approach 97

Approach AGL Descent Runway 97

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. This gives you a safe buffer on the stall speed and plenty of time to stabilize. Power controls the rate of descent, and pitch controls airspeed.

Weight-Shift-Control 52

Weight-Shift-Control Runway Approach Density Altitude 52