What is the maximum glide distance after engine failure at cruising altitude?

The maximum glide distance after engine failure at cruising altitude for the CRJ 900 is indeed 60 nautical miles. This figure is based on the aircraft's aerodynamic design and performance characteristics, which allow it to maintain a specific glide ratio. The glide ratio is influenced by various factors including altitude, weight, and environmental conditions, but at a standard cruising altitude, the CRJ 900 is capable of achieving this notable glide range.

Understanding this figure is essential for pilots to make informed decisions during emergency situations, ensuring they can reach a suitable landing area after an engine failure. In flight training, this information is emphasized to help pilots appreciate the dynamics of controlled descents and optimize their response in emergency scenarios.