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Figure 2-27. Gravity Feed Fuel Flow
Table 2-3. - Fuel Sump Drain Locations

Operator Manual For RC-12x Aircraft
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TM 1-1510-262-10
NOTE
Both STANDBY PUMP switches will be OFF during crossfeed operation.
The engine-driven primary (HIGH PRESSURE) fuel pump is limited to 10 hours of operation,
throughout its TBO period, without standby fuel pump or engine-driven boost pump fuel pres-
sure.
Diagram shows typical fuel crossfeed situation with left wing fuel system supplying both en-
gines (All BOOST and STANDBY PUMPS operable). For selection of right wing fuel for cross-
feed reverse CROSSFEED switch position. Either coniguration will supply either engine during
single-engine operation Fuel will not cross transfer between tank systems.
Figure 2-28. Crossfeed Fuel Flow
2-42


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