Aerospace series — Hydraulic tubing joints and fittings — Planar flexure test

This document specifies a planar flexure test procedure for reconnectable and permanent hydraulic tube joints and fittings. This procedure is intended for conducting flexure tests on fittings with high-strength hydraulic tubes made of corrosion-resisting steel, titanium and aluminium for use on commercial and military aircraft.

Série aérospatiale — Joints et raccords des tuyauteries hydrauliques — Essai de flexion plane

General Information

Status
Published
Publication Date
18-Jun-2025
Current Stage
6060 - International Standard published
Start Date
19-Jun-2025
Due Date
21-Nov-2025
Completion Date
19-Jun-2025
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ISO 9538:2025 - Aerospace series — Hydraulic tubing joints and fittings — Planar flexure test Released:19. 06. 2025
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International
Standard
ISO 9538
Third edition
Aerospace series — Hydraulic
2025-06
tubing joints and fittings — Planar
flexure test
Série aérospatiale — Joints et raccords des tuyauteries
hydrauliques — Essai de flexion plane
Reference number
© ISO 2025
All rights reserved. Unless otherwise specified, or required in the context of its implementation, no part of this publication may
be reproduced or utilized otherwise in any form or by any means, electronic or mechanical, including photocopying, or posting on
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or ISO’s member body in the country of the requester.
ISO copyright office
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Phone: +41 22 749 01 11
Email: copyright@iso.org
Website: www.iso.org
Published in Switzerland
ii
Contents Page
Foreword .iv
Introduction .v
1 Scope . 1
2 Normative references . 1
3 Terms and definitions . 1
4 Device for flexure test . 1
5 Flexure test specimens . 3
6 Stress determination . 3
7 Procedure . 4
7.1 Instrumentation and strain gauges .4
7.2 Frequency .5
7.2.1 Test frequency .5
7.2.2 Natural frequency of the specimens .5
7.2.3 Verification of the natural frequency . .5
7.3 Bending stress calibration of test specimen .5
7.4 Test .5
8 Requirements . 5
Bibliography . 7

iii
Foreword
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of ISO document should be noted. This document was drafted in accordance with the editorial rules of the
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rights in respect thereof. As of the date of publication of this document, ISO had not received notice of (a)
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This document was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles, Subcommittee
SC 10, Aerospace fluid systems and components.
This third edition cancels and replaces the second edition (ISO 9538:2017), which has been technically
revised.
The main changes are as follows:
— Clause 4 and Clause 7 were updated.
Any feedback or questions on this document should be directed to the user’
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