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FUEL SYSTEM
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TM-55-2840-254-23-1 Engine Gas Turbine Model T55-L-712 Manual
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FUEL SYSTEM (Cont)

TM 55-2840-254-23
IN-LINE FUEL FILTER. Mounts on bracket on right side of compressor housing. Contains re-
E
placeable filter element. Also contains a popout indicator button. Button will
pop out if filter element is close to being bypassed because of clogging.
FLOW DIVIDER. Mounts at 6-o'clock positon on combustor section. Contains one common in-
F
put and five separate outputs. One output port contains a check valve. The other
four output ports consist of two primary and two secondary ports. Designed so
primary and secondary ports allow fuel to flow at different predetermined input
pressures.
G
STARTING FUEL SOLENOID VALVE. Mounts on bracket on left side of compressor housing.
Normally closed and will not let fuel flow through it. Designed to open on
electrical signal allowing fuel to flow through it.
H START FUEL NOZZLES. Mount at 6 - and 9-o'clock position near aft end of combustor section.
Provide means of feeding starting fuel into combustion chamber where it is
ignited by spark from igniter plug.
1-29

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