The typical glide ratio of an Airbus A320 (and similar modern jet airliners) in a clean configuration (engines idle, landing gear up, flaps up) is approximately 17:1 to 18:1.
This means that from an altitude of 1 mile (or 1 kilometer), the aircraft can glide about 17 to 18 miles (or kilometers) horizontally in still air.
Important Context and Nuances:
- Speed for Best Glide: This ratio is achieved at a specific speed, which for the A320 is around 210–220 knots Indicated Airspeed (IAS). This is the speed pilots aim for during a complete loss of engine thrust (a “dead-stick” scenario).
- Configuration is Critical: The glide ratio degrades significantly if the aircraft is not clean:
- Landing Gear Down: Creates massive drag, severely reducing the glide distance.
- Flaps/Slats Extended: Also increases drag and reduces the ratio.
- Real-World Factors: The actual glide distance in a real emergency is affected by:
- Wind: A headwind reduces distance over the ground; a tailwind increases it.
- Altitude: Higher altitude provides more potential energy and more time to select a landing site, but the ratio remains roughly constant.
- Aircraft Weight: Heavier weight requires a higher optimum glide speed but does not significantly change the glide ratio in jet aircraft.
- Pilot Technique: Precise speed management is crucial to achieve the best performance.
Comparison and “Miracle on the Hudson” Reference: