Aircraft Systems
A device used to redirect engine thrust forward to assist with deceleration after landing.
Quick answer: A device used to redirect engine thrust forward to assist with deceleration after landing.
This term page is part of the Protermify Aviation glossary and is published as static HTML for fast indexing and clear language coverage.
A device used to redirect engine thrust forward to assist with deceleration after landing.
bộ đảo chiều lực đẩy matters because it supports clear communication in Aircraft Systems 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.
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Questions and answers
In this glossary, bộ đảo chiều lực đẩy refers to: A device used to redirect engine thrust forward to assist with deceleration after landing.
In aviation communication, this term appears in contexts such as: "Sau khi tiếp đất, lập tức sử dụng bộ đảo chiều lực đẩy để giảm quãng đường hãm trên đường băng ướt."
bộ đảo chiều lực đẩy matters because it supports clear communication in Aircraft Systems 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.
bộ đảo chiều lực đẩy is mainly used by Pilots, Air Traffic Controllers, and Cabin Crew.
In this glossary, bộ đảo chiều lực đẩy is grouped under Aircraft Systems. Related pages in this category explain adjacent procedures, commands and operational concepts.
This definition is sourced from ICAO Doc 9432, FAA PCG and published by Protermify Aviation as a static aviation reference page.
A device used to redirect engine thrust forward to assist with deceleration after landing.
After touchdown, deploy thrust reverser immediately to reduce landing roll on the wet runway.
bộ đảo chiều lực đẩy
Sau khi tiếp đất, lập tức sử dụng bộ đảo chiều lực đẩy để giảm quãng đường hãm trên đường băng ướt.
English reference definition
ICAO Doc 9432, FAA PCG
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