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TM 5-4320-313-14
1-10. LOCATION AND DESCRIPTION OF MAJOR COMPONENTS.
a. Rear and Left Side. (Refer to figure 1-2).
(1) Pump. The pump is engine driven and pumps fuel from a container to aircraft.
(2) Frame Assembly. The frame assembly is used to support and transport the pumping assembly.
(3) Crank Assembly. The crank assembly is used in starting the engine.
(4) Ground Cable. The ground cable is used to ground the pump assembly during operation.
Figure 1-2. Pumping Assembly, Rear and Left Side.
1-4
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