Aircraft Systems
Ratio of total pressure at the engine exhaust to that at the engine inlet, used as a primary engine thrust indicator.
Quick answer: Ratio of total pressure at the engine exhaust to that at the engine inlet, used as a primary engine thrust indicator.
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Ratio of total pressure at the engine exhaust to that at the engine inlet, used as a primary engine thrust indicator.
อัตราส่วนแรงดันเครื่องยนต์ 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, อัตราส่วนแรงดันเครื่องยนต์ refers to: Ratio of total pressure at the engine exhaust to that at the engine inlet, used as a primary engine thrust indicator.
In aviation communication, this term appears in contexts such as: "อัตราส่วนแรงดันเครื่องยนต์ต่ำกว่าปกติ แนะนำให้ตรวจสอบแรงขับหรือเซ็นเซอร์"
อัตราส่วนแรงดันเครื่องยนต์ 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.
อัตราส่วนแรงดันเครื่องยนต์ is mainly used by Pilots, Air Traffic Controllers, and Cabin Crew.
In this glossary, อัตราส่วนแรงดันเครื่องยนต์ 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.
Ratio of total pressure at the engine exhaust to that at the engine inlet, used as a primary engine thrust indicator.
Engine pressure ratio is below normal limits, recommend checking for possible thrust or sensor issues.
อัตราส่วนแรงดันเครื่องยนต์
อัตราส่วนแรงดันเครื่องยนต์ต่ำกว่าปกติ แนะนำให้ตรวจสอบแรงขับหรือเซ็นเซอร์
English reference definition
ICAO Doc 9432, FAA PCG
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