SAE ARP5818A

1. SCOPE
2. REFERENCES
3. AIRCRAFT REFUELING VEHICLE SYSTEM COMPONENTS
    AND SYSTEMS SELECTION AND UTILIZATION
4. DESIGN CRITERIA
5. ACCEPTANCE CRITERIA
6. AIRCRAFT REFUELING VEHICLE DESIGN
7. AIRCRAFT REFUELING SYSTEM
8. ELECTRICAL SYSTEM EQUIPMENT
9. IDENTIFICATIONS AND MARKINGS
10. LABELING
11. MANLIFT PLATFORMS, LADDERS AND HANDRAILS
12. INTERLOCK SYSTEM
13. DEADMAN CONTROL
14. EMERGENCY SHUTDOWN
15. PNEUMATIC SYSTEM
16. ELECTRICAL SYSTEM
17. HYDRAULIC SYSTEM
18. STATIC BONDING
19. SAMPLING POINTS
20. AIRCRAFT REFUELING VEHICLE LIGHTS
21. FIRE EXTINGUISHERS
22. WHEEL CHOCKS AND HOLDER
23. HOSES
24. FINISHING AND PAINTING
25. LETTERING AND LABELING
26. AIRCRAFT REFUELING VEHICLE CERTIFICATES AND
    TESTS DOCUMENTATION
27. AIRCRAFT REFUELING VEHICLE OPERATORS,
    MAINTENANCE, AND ILLUSTRATED PARTS MANUALS
28. NOTES
APPENDIX A

Acts as a guideline for the design and operation of Aviation Aircraft Refueling Vehicles and for the materials, components, and systems used thereon.

This document is a guideline for the design and operation of Aviation Aircraft Refueling Vehicles and for the materials, components, and systems used thereon. The criteria set forth herein are the minimum recommendations for all types of aircraft refueling vehicles, including tanker vehicles, hydrant service vehicles, towable hydrant carts, fixed refueling cabinets, and any other type of aircraft refueling vehicles used at airports for aircraft refueling operations with nominal operating fuel pressures and flow rates as specified within this document.