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TM 10-4930-240-13
2-15. ASSEMBLY AND PREPARATION FOR USE - cont.
(17) Connect 3 in. x 10 ft. discharge hose (23) between refueling manifold assembly (14) and 3-inch
manifold (19).
(18) Connect 2 in. x 10 ft. discharge hose (24) between refueling manifold assembly (14) and pressure
reducing assembly (25).
(19) Connect 2 in. x 10 ft. suction hose (26) to pressure reducing assembly (25).
(20) Connect wye (27) (2 in. M x 2 in. M x 2 in. F) to 2 in. x 10 ft. suction hose (26).
(21) Connect water detection kit adapter assembly (28) to filter separator (22).
(22) Connect valve section (29) to water detection kit adapter assembly (28).
(23) Connect 3 in. female x 2 in male reducer (30) to valve section (29).
(24) Connect 2 in. x 10 ft. discharge hose (31) between reducer (30) and wye (27).
(25) Connect 2 in. x 10 ft. discharge hose (32) and wye (33) (2 in. M x 2 in. M x 2 in. F) to wye (27).
(26) Connect three 2 in. x 50 ft. discharge hoses (34, 35, and 36) to wye (33).
(27) Connect three 2 in. x 50 ft. discharge hoses (37, 38, and 39) to wye (33).
(28) Connect D1 nozzle (40) or CCR nozzle (41) to 2 in. x 50 ft. discharge hose (39).
(29) Connect D1 nozzle (40) or CCR nozzle (41) to 2 in, x 50 ft. discharge hose (36).
j. Refueling Point Ground Rod Installation. Refer to figure 2-17. Before the AFARE can be placed In
operation, it must be properly grounded Install ground rods at both refueling points. Rods must be
installed within 6 feet of each refueling point to provide enough slack In grounding cable to connect
nozzles to aircraft adapters.
WARNINGS
Use care to prevent injury when driving ground rod into the soil. Wear gloves to
protect your hands. Do not hold ground rod above the stop collar.
Do NOT operate the fuel system until it has been properly grounded. Flow fuel
can generate static charges within the fuel hoses. A static discharge could
ignite the fuel or cause an explosion of fuel vapor.
(1) Place ground rod (1) in vertical position.
2-46
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