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TM 10-4930-240-13
1-8. GLOSSARY.
Term
Description
Interchangeable.................................
Two or more like parts with the same function and
features that can be exchanged one for the other without
changing parts or selecting size to obtain correct fit.
Plenum..............................................
Collection point for exhaust gases.
SECTION II. EQUIPMENT DESCRIPTION AND DATA
1-9. EQUIPMENT CHARACTERISTICS, CAPABILITIES AND FEATURES.
a.
Characteristics.
(1) Turbine powered pump provides a maximum pumping capacity of 200 gallons per minute (GPM).
Turbine powered pump draws fuel from system hoses.
(2) Maximum fuel storage capacity of 1,500 gallons.
(3) Easily transportable. Hoses, nozzles and coupling components are stowed in hose carriers.
(4) Quick disconnect cam-lock couplings on all components allow rapid system assembly and
disassembly.
(5) System can be configured to meet varying mission and site requirements.
(6) Major operating assemblies are skid mounted to aid movement in arctic conditions.
(5) No external electrical power source required.
b.
Capabilities and Features.
(1) System operating range: -60°F to + 95°F (-51°C to + 35°C).
(1) Two aircraft refueling points. Each point independently controlled by a refueling nozzle 50 GPM
minimum fuel flow.
(2) Hand operated valves control fuel flow through the system.
(4) 1,500 gallon fuel storage capacity provided by three 500 gallon collapsible fuel drums. Drums can
be transported by truck or aircraft. Fuel drums can be adapted for ground handling.
(5) Turbine powered, 200 GPM pump operates off of system fuel supply. Exhaust gases are used to
heat filter separator.
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