Aircraft Systems

Triebwerksdruckverhältnis

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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Quick answer

Ratio of total pressure at the engine exhaust to that at the engine inlet, used as a primary engine thrust indicator.

Why it matters

Triebwerksdruckverhältnis 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.

Editorial context

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Questions and answers

Questions and answers

What is Triebwerksdruckverhältnis?

In this glossary, Triebwerksdruckverhältnis refers to: Ratio of total pressure at the engine exhaust to that at the engine inlet, used as a primary engine thrust indicator.

How is Triebwerksdruckverhältnis used in aviation?

In aviation communication, this term appears in contexts such as: "Das Triebwerksdruckverhältnis ist unter dem Normalwert, bitte auf Schub- oder Sensorprobleme prüfen."

Why does Triebwerksdruckverhältnis matter in aviation?

Triebwerksdruckverhältnis 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.

Who uses Triebwerksdruckverhältnis?

Triebwerksdruckverhältnis is mainly used by Pilots, Air Traffic Controllers, and Cabin Crew.

What category does Triebwerksdruckverhältnis belong to?

In this glossary, Triebwerksdruckverhältnis is grouped under Aircraft Systems. 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.

Definition

Ratio of total pressure at the engine exhaust to that at the engine inlet, used as a primary engine thrust indicator.

Operational example

Engine pressure ratio is below normal limits, recommend checking for possible thrust or sensor issues.

Localized term

Triebwerksdruckverhältnis

Localized example

Das Triebwerksdruckverhältnis ist unter dem Normalwert, bitte auf Schub- oder Sensorprobleme prüfen.

Definition language

English reference definition

Source

ICAO Doc 9432, FAA PCG

Category

Aircraft Systems

Exam relevance

  • ICAO Level 4
  • ICAO Level 5
  • ICAO Level 6
  • EASA FCL.055

Target audience

  • Pilots
  • Air Traffic Controllers
  • Cabin Crew

Related terms

Use the related links below to continue through connected aviation terminology.

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