Advanced ATC
Artificially higher temperature entered in FMS to calculate reduced-thrust take-off setting (flex) within performance limits.
Quick answer: Artificially higher temperature entered in FMS to calculate reduced-thrust take-off setting (flex) within performance limits.
This term page is part of the Protermify Aviation glossary and is published as static HTML for fast indexing and clear language coverage.
Artificially higher temperature entered in FMS to calculate reduced-thrust take-off setting (flex) within performance limits.
フレックス想定温度 matters because it supports clear communication in Advanced ATC 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.
This page is rendered as static HTML from source-backed terminology data so search engines and AI systems can parse the content without client-side code.
Questions and answers
In this glossary, フレックス想定温度 refers to: Artificially higher temperature entered in FMS to calculate reduced-thrust take-off setting (flex) within performance limits.
In aviation communication, this term appears in contexts such as: "滑走路14の離陸性能余裕確認のため、フレックス想定温度58度を入力してフレックススラストを計算。"
フレックス想定温度 matters because it supports clear communication in Advanced ATC 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.
フレックス想定温度 is mainly used by Pilots, Air Traffic Controllers, and Cabin Crew.
In this glossary, フレックス想定温度 is grouped under Advanced ATC. 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.
Artificially higher temperature entered in FMS to calculate reduced-thrust take-off setting (flex) within performance limits.
Enter flexible assumed temperature five eight Celsius to compute flex thrust and verify take-off performance margin on runway one four.
フレックス想定温度
滑走路14の離陸性能余裕確認のため、フレックス想定温度58度を入力してフレックススラストを計算。
English reference definition
ICAO Doc 9432, FAA PCG
Use the related links below to continue through connected aviation terminology.
