Aerospace series - Heat-shrinkable moulded shapes - Part 103: Fluoroelastomeric, temperature range -55 °C to 200 °C - Product standard; German and English version EN 4840-103:2023

Standard [CURRENT]

DIN EN 4840-103:2024-05

Aerospace series - Heat-shrinkable moulded shapes - Part 103: Fluoroelastomeric, temperature range -55 °C to 200 °C - Product standard; German and English version EN 4840-103:2023

German title
Luft- und Raumfahrt - Wärmeschrumpfende Formteile - Teil 103: Fluorelastomer, Temperaturbereich -55 °C bis 200 °C - Produktnorm; Deutsche und Englische Fassung EN 4840-103:2023
Publication date
2024-05
Original language
German, English
Pages
26

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Publication date
2024-05
Original language
German, English
Pages
26
DOI
https://dx.doi.org/10.31030/3508331

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Overview

Committee NA 131-04-08 AA "Installationskomponenten" ("Installation components") at DIN is responsible for this standard. This document specifies the required characteristics for fluoroelastomeric, heat-shrinkable boots for use in aircraft electrical systems at operating temperatures between - 55 °C and 200 °C. The moulded shapes can be supplied with a pre-coated adhesive. Refer to the manufacturers/suppliers for options. A guide to adhesive compatibility is given in Annex A. These moulded shapes are normally supplied in the styles and dimensions given in EN 4840-002. The colour is normally black. Styles and dimensions other than those specifically listed in EN 4840-002 can be available as custom items. These items are considered to comply with this document if they comply with the property requirements listed in Table 1 with the exception of dimensions. The EN 4840-103 standard has been prepared by the standardization organization ASD-STAN of the AeroSpace and Defence Industries Association of Europe (ASD) with the participation of German experts at DIN Standards Committee Aerospace (NL). The responsible German standardization committee is Working Committee NA 131-04-08 AA "Installationskomponenten" ("Installation components") at DIN Standards Committee Aerospace (NL).

Content

ICS

49.060

DOI

https://dx.doi.org/10.31030/3508331

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