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TM 10-4320-351-14
Section III. OPERATION UNDER USUAL CONDITIONS
2.4 SYSTEM ASSEMBLY AND PREPARATION FOR USE.
CAUTION
The fuel transfer pump may be damaged by running dry longer than two minutes.
If running of the engine is desired, uncouple the engine from the fuel transfer
pump.
Figure 2-3 illustrates a typical setup, showing the operational relationship of the pump-engine module and the accessory
module to overall system. The illustration is not drawn to scale. It is similar to the layout diagram displayed on the
accessory module and is provided as a visual reference only. Actual emplacement may require a slightly different
configuration due to terrain or mission constraints.
WARNING
Death or personal injury may result from the explosion of fuel fumes exposed to an
open flame or spark, or to static discharge. Do not permit smoking, any open
flame, or spark producing equipment within 50 feet (15 m) of the pumping
assembly. Ensure all equipments are well grounded prior to commencing any
operation or maintenance task. Always ensure the ground connection from the
aircraft is complete prior to beginning any fueling operation.
CAUTION
All couplings have caps that must be removed before a connection is made.
Ensure the cap remains in place until just before connection to prevent
contamination of the fueling system by foreign materials. Once the caps are
removed, couple adjacent caps to reduce the probability of foreign materials
contaminating the aircraft fuel.
a. Inspect the pumping assembly for damage that may have occurred during transport and ensure that the
received assemblies are complete.
NOTE
Steps "b", "c" and "d" apply if the pump-engine module must be repositioned. If
the module position is satisfactory proceed to step "e".
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