Aircraft Systems
A sensor in an engine or gearbox that detects metallic particles, indicating wear or damage to internal components.
Quick answer: A sensor in an engine or gearbox that detects metallic particles, indicating wear or damage to internal components.
This term page is part of the Protermify Aviation glossary and is published as static HTML for fast indexing and clear language coverage.
A sensor in an engine or gearbox that detects metallic particles, indicating wear or damage to internal components.
Spanndetektor 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, Spanndetektor refers to: A sensor in an engine or gearbox that detects metallic particles, indicating wear or damage to internal components.
In aviation communication, this term appears in contexts such as: "Wartung, Spanndetektor am rechten Triebwerk zeigt Metallpartikel, bitte genaue Überprüfung nach Abschaltung."
Spanndetektor 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.
Spanndetektor is mainly used by Pilots, Air Traffic Controllers, and Cabin Crew.
In this glossary, Spanndetektor 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 sensor in an engine or gearbox that detects metallic particles, indicating wear or damage to internal components.
Maintenance, chip detector on right engine indicates metal particles, requesting detailed inspection after shutdown.
Spanndetektor
Wartung, Spanndetektor am rechten Triebwerk zeigt Metallpartikel, bitte genaue Überprüfung nach Abschaltung.
English reference definition
ICAO Doc 9432, FAA PCG
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