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.
Written and reviewed by

Pablo Asensio

Aeronautical engineer. Passed the thirteen EASA ATPL(A) theoretical knowledge exams studying from these very notes. Writes and reviews each topic against the Part-FCL Learning Objectives.