Standard

NS-EN 4832:2018

Oct 2018 Published

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Language English

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Abstract

This specification establishes the requirements for ring locked fitting assemblies according to EN 4833 and EN 4836, for use in aircraft systems at nominal operating pressure of 35 000 kPa (5 080 psi) maximum and temperature range of −54 °C to +135 °C (−65 °F to +275 °F).

Document information

Standard from SN
Published: 1 October 2018
Edition: 2018-07
Version: 1
Document type: NAT
ISBN:

ICS 49.080
National Committee ASD-STAN

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Adopted from: EN 4832:2018 , 0

NS-EN 4832:2018

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Abstract

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