Tagged: engine out acceleration altitude
The “Engine Out Acceleration Altitude” is an important concept in aviation, especially when planning and executing takeoff procedures. This altitude refers to the specific flight altitude at which an aircraft experiencing an engine failure during takeoff should reduce the rate of climb and transition to more level flight to increase speed. The main goal of this maneuver is to reach a safe level of speed that will allow the aircraft to remain stable and controllable even with one engine inoperative. The Engine Out Acceleration Altitude is determined depending on various factors such as aircraft type, weather conditions, weight of the aircraft and specific aerodynamic properties. Maintaining this specified altitude is critical to flight safety as it provides pilots with clear guidelines on how to act in the event of an engine failure during the critical takeoff phase. This scenario is intensively trained both in pilot training and in flight simulators in order to be as well prepared as possible in a real emergency.
Werbung / Advertisements In this article I would like to explain to you the often confusing entries for Thrust Reduction, Thrust Acceleration and Engien Out Acceleration in the MCDU. These often lead to quite...