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SAE ARP 1084 : 2013

SAE ARP 1084 : 2013

EXTERNAL HYDRAULIC LEAKAGE FOR IN-SERVICE COMPONENTS

SAE International

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Table of Contents

FOREWORD
1. SCOPE
2. REFERENCES
3. LEAKAGE - GENERAL
4. NOTES

Abstract

Specifies guidelines for allowable leakage for in-service aircraft hydraulic components at a nominal 100 degrees F (38 degrees C) temperature and to outline the procedure for measuring such leakage.

General Product Information

Document Type Standard
Status Current
Publisher SAE International
Committee A-6A1

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