SAE ARP 1084 : 2013

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

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