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side behind the pilot’s seat) in the flight compartment. The panel will display all lights for a period
of three seconds when the panel is powered up.
Each engine may be replenished individually if:
· The engine has been shut down for a minimum of 15 minutes.
· The engine to be replenished is not already full.
· One of the other engines or APU is not currently being replenished.
POWER PLANT
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
18−10−7
ENGINE OIL SYSTEM (CONT'D)
Oil Replenishment Panel
GF1810_013
SYSTEM ON
Selecting the POWER switch to ON does
the following:
The SYSTEM ON lamp will come on.
A three second lamp test will be carried
out on all annunciators.
Provides power to all switches on the oil
replenishment panel.
TANK LO
The reservoir TANK
LO legend comes
on to indicate that
the reservoir is low
in quantity.
VLV OPEN RH (left engine similar)
Selecting the switch will illuminate the VLV
OPEN switch legend indicating valve operation.
Oil will be pumped from the reservoir (through
the valve) to the engine until full is achieved.
The VLV OPEN and LO OIL switch legends
will go out when the correct level is reached.
PUMP ON
Selecting the PUMP ON switch does the
following:
The reservoir pump will operate and the
PUMP ON lamp will come on to indicate
operation. The legend will remain on until
the correct level of the system to be
topped up is achieved.
LO OIL LH ENG (right engine similar)
The LO OIL comes on to indicate that the
engine is low in oil quantity and will remain
on until the engine oil tank is replenished.
OIL REPLENISHMENT
POWER
RESERVOIR LH ENG APU RH ENG
SYSTEM
ON
TANK
LO
PUMP
ON
LO
OIL
VLV
OPEN
LO
OIL
VLV
OPEN
LO
OIL
VLV
OPEN
Oil is to be added to the engine(s) when an OIL LO QTY message is displayed on EICAS and
when
LO
OIL is displayed on the oil replenishment panel with the replenishment system
powered.
POWER PLANT
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
18−10−8
ENGINE OIL SYSTEM (CONT'D)
Oil Replenishment Schematic
GF1810_015
O
OIL REPLENISHMENT
POWER
RESERVOIR LH ENG APU RH ENG
SYSTEM
ON
TANK
LO
PUMP
ON
LO
OIL
VLV
OPEN
LO
OIL
VLV
OPEN
LO
OIL
VLV
OPEN
AIRFRAMEMOUNTED
AIRFRAMEMOUNTED
Operation
The following procedural steps outlined are to be used only as a guide to replenish the engine oil
system. The Airplane Maintenance Manual takes precedence over all servicing procedures.
· Select the “POWER” switch on the oil replenishment panel, “SYSTEM ON” legend on.
· Confirm that the “LO OIL” lamp on the oil replenishment panel corresponds to the condition
indicated on EICAS “L−R OIL LO QTY” caution message.
· Select the switch labeled “LH or RH ENG” on the oil replenishment panel.
· Confirm that the “PUMP ON” (below reservoir label) and “VLV OPEN” (below the engine to
be filled) legends are displayed on the oil replenishment panel.
· Monitor the oil level on EICAS for both the engine and reservoir (example: if approximately 1
US quart is added to the engine, the oil replenishment tank level should have reduced by the
same amount).
· When the engine reaches maximum level confirm that the “PUMP ON” legend on the oil
replenishment panel goes out (indicating pump stops). Also confirm that the “VLV OPEN”
legend on the oil replenishment panel goes out (indicating valve closed).
POWER PLANT
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
18−10−9
ENGINE FUEL SYSTEM
The fuel system provides engine fuel for combustion, HP compressor Variable Stator Vanes (VSV)
actuation and engine oil cooling.
The main components that are contained in the fuel system are as follows:
· Fuel Pump Unit − The fuel pump unit contains both the LP and HP pumps. Fuel supplied from
the airplane fuel system passes through the (centrifugal type) LP pump, is pressurized and is
delivered to the Fuel Cooled Oil Cooler (FCOC).
· LP Filter − Fuel from the FCOC enters the LP fuel filter, where any debris is trapped before
　
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