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Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
12-01-09 FUEL INDICATION AND CONTROL (Cont)
FUEL QUANTITY GAGING
DESCRIPTION
Fuel quantities are displayed in lbs or kg on the EICAS and FUEL synoptic displays.
COMPONENTS AND OPERATION FUEL COMPUTER
The dual-channel fuel system automatically calculates the quantity of fuel in the wing tanks. Each channel receives signals from the fuel system and aircraft attitude information from the AHRS. The computer uses the information to calculate the fuel weight in each tank.
CONTROLS AND INDICATION
DESCRIPTION
The FUEL control panel provides control and system indications for the fuel system. The panel controls the boost pumps and provides manual control and indications of the gravity and powered crossflow system.
Fuel system information is presented on the EICAS and FUEL synoptic pages. Fuel temperature is displayed in degrees celsius and quantity is displayed in pounds or kilograms.
The refuel/defuel control panel controls all of the refueling and defueling operations. It tests the integrity of the components of the fuel system and displays individual fuel tank quantities.
FUEL CONTROL PANEL
L (R) PUMP, GRAVITY XFLOW, and XFER are selected on the FUEL control panel.
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
12-01-10 CONTROLS AND INDICATION (Cont)
FUEL DISPLAY
The fuel display synoptic page presents digital indications of fuel flow and quantity.
Fuel flow is indicated in either pounds per hour (PPH) or in kilograms per hour (KPH). Magenta dashes will be displayed
if the input value is invalid.
Fuel tank quantity for the left and right fuel tanks are presented in pounds or kilograms.
URE READOUTS
e readout indicates the temperature of the fuel in the right wing. Green readouts indicate temperatures F), while a WING FUEL TEMP LOW(C) CAS message indicates -38.2 ° C (-36.7 ° F) or below.
DICATIONS
the amount of fuel used since the counter was reset. The reset is carried out automatically on powerup a dashes indicate the input data is invalid.
a FUEL IMBALANCE (C) CAS message will illuminate if the following conditions exist:13 kg) or more with a total fuel weight of more than 13 700 lb (6214 kg)43 kg) or more with a total fuel weight between 13 700 (6214 kg) and 10 000 lb (4536 kg)04 kg) or more with a total fuel weight between 10 000 lb (4536 kg) and 4700 lb (2132 kg)72 kg) or more with a total fuel weight of less than 4700 lb (2132 kg)
NG TANKS
May 06/2005 Flight Crew Operating Manual Volume 2 REV 2 CSP 100-6
12-01-11
FUEL
CONTROLS AND INDICATION (Cont) FUEL SYNOPTIC PAGE
The EICAS synoptic page displays a pictorial view of the system operation.
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UP UP
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
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