ATPL Performance: Descent and Glide Performance

032-01-05Pablo Asensio Martínez2026-04-012 min

Forces in Descent

In a steady descent, the Component of Weight acting forward aids the Thrust (if any) to balance Drag. In a glide (idle thrust), the forward component of weight balances the Drag completely.

$ \text{Thrust} + \text{Weight Component} = \text{Drag} $

Gliding

For an engine failure scenario, maximizing the glide distance is critical.

Glide Angle ($\gamma$)

The glide angle depends purely on the Lift-to-Drag Ratio (L/D). $ \tan \gamma = \frac{\text{Drag}}{\text{Lift}} = \frac{1}{L/D} $

  • Minimum Glide Angle (Max Distance): Occurs at the speed for Maximum L/D ($V_{MD}$).
  • Mass Effect: Mass does NOT affect the glide angle or distance in a steady glide.
    • A heavier aircraft glides at the same angle but at a higher speed (due to $L=W$ requirement). It reaches the ground sooner, but touches down at the same distance point as a lighter aircraft.

Drift Down

If a multi-engine aircraft loses an engine at high altitude, it may not be able to maintain that altitude (Thrust Available < Thrust Required). It must descend to a lower altitude where it can maintain level flight. This procedure is called Drift Down.

  • Drift Down Speed: Usually Green Dot or $V_{MD}$ to minimize the rate of descent.
  • Net Ceiling: The altitude the aircraft can maintain with one engine inoperative, minus a safety margin (measure of obstacle clearance).

Factors Affecting Descent

Wind

  • Range: Headwind reduces ground distance covered (steepers the descent path relative to ground). Tailwind increases ground distance.
    • Max Glide Distance Strategy: Increase speed in headwind (fly slightly faster than $V_{MD}$), decrease speed in tailwind? No, usually fly $V_{MD}$ but be aware of the ground path change.
  • Rate of Descent: Wind has no effect on the vertical rate of descent (time to descend), only on the ground path.

Configuration

  • Flaps/Gear: Increase Drag significantly, degrading the L/D ratio. Result: Steeper descent angle and increased Rate of Descent. Used to lose altitude quickly without gaining speed.