The drift-down rate after an engine failure at altitude is a critical factor in aviation safety, especially for single-engine aircraft. This rate determines how quickly the aircraft loses altitude due to the loss of power from the failed engine.
Several factors influence the drift-down rate, including the aircraft’s weight, airspeed, and the angle of attack. The formula used to calculate the drift-down rate is based on these variables:
W = Weight of the aircraft
S = Wing area
(theta) = Angle of attack
V = Airspeed
What is the drift-down rate in aviation?
How do I calculate the drift-down rate?
Why is the drift-down rate important for aviation?
What factors affect the drift-down rate?
Can I use this calculator for multi-engine aircraft?
How does altitude affect the drift-down rate?
What should I do if my aircraft experiences a sudden engine failure?
Results are for informational purposes only and do not constitute professional advice.
