SAE ARP 5672 : 2016

Table of Contents

1. SCOPE
2. RELATED DOCUMENTS
3. BACKGROUND
4. P-STATIC PROTECTION DESIGN AND COMPLIANCE
5. DEFINE AIRCRAFT CONFIGURATION, OPERATING
    CONDITIONS AND MATERIALS
6. ESTABLISH THE AIRCRAFT P-STATIC CHARGING ENVIRONMENT
7. DESIGN AIRCRAFT P-STATIC PROTECTION
8. VERIFY P-STATIC PROTECTION EFFECTIVENESS
9. IMPLEMENT CORRECTIVE MEASURES
10. MAINTENANCE

Abstract

Gives information and guidance concerning an acceptable means, but not the only means, of compliance with Parts 23, 25, 27, and 29 (23.867, 25.899, 27.610, and 29.610) of the Federal Aviation Regulations (FAR) and European Aviation Safety Agency (EASA), applicable to aircraft for protection against the adverse effects of precipitations static.

General Product Information

Published
Document Type	Standard
Status	Current
Publisher	SAE International
Pages
ISBN
Committee	AE-2