What is Устройство задней кромки крыла?
In this glossary, Устройство задней кромки крыла refers to: A movable aerodynamic surface located on the trailing edge of an aircraft wing, such as a flap, extended to increase lift and control at low speeds, especially during takeoff and landing.
How is Устройство задней кромки крыла used in aviation?
In aviation communication, this term appears in contexts such as: "Перед посадкой подтвердите выпуск всех устройств задней кромки крыла и сохраняйте конфигурацию до скорости руления."
Why does Устройство задней кромки крыла matter in aviation?
Устройство задней кромки крыла matters because it supports clear communication in Flight Phase contexts for Pilots, Air Traffic Controllers, and Cabin Crew. It also connects to aviation training and exam language such as ICAO Level 4, ICAO Level 5, ICAO Level 6, and EASA FCL.055.
Who uses Устройство задней кромки крыла?
Устройство задней кромки крыла is mainly used by Pilots, Air Traffic Controllers, and Cabin Crew.
What category does Устройство задней кромки крыла belong to?
In this glossary, Устройство задней кромки крыла is grouped under Flight Phase. Related pages in this category explain adjacent procedures, commands and operational concepts.
Where does this definition come from?
This definition is sourced from ICAO Doc 9432, FAA PCG and published by Protermify Aviation as a static aviation reference page.