SAE ARP 4028 : 2014

SAE ARP 4028 : 2014

AIRCRAFT/ENGINE FUEL PUMP TWO PHASE (SLUGGING FLOW) INLET PERFORMANCE TEST AND EVALUATION

SAE International

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Table of Contents

FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS/CONSIDERATIONS
4. TECHNICAL REQUIREMENTS
5. DETAILED REQUIREMENTS
6. TEST DATA
7. TEST PROCEDURE

Abstract

Pertains to all engine or airframe mounted fuel pumps and controls when required by the applicable specification.

General Product Information

Document Type Standard
Status Current
Publisher SAE International
Committee AE-5B

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