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TABLE OF CONTENTS
DESCRIPTION
General
Fuel Specifications
Fuel System Synoptic Page
AC Boost Pumps DC Auxiliary Pumps Center Transfer Pumps
Fuel Control Panel
Fuel Tanks
Service Points
Vent System
Vent System Schematic
Transfer System
Center Transfer Wing Transfer Auto Wing Transfer Manual Wing Transfer Crossfeed
Engine Feed System Engine Feed System Indication APU Fuel Feed Fuel Quantity and Indication Flight Management Display Refuel/Defuel System
Refuel/Defuel Panel
Normal Fuel Loading
Gravity Refueling
Pressure Refueling
Manual Refueling
Suction Defueling
Pressure Defueling
Fault Reporting
Error Messages
INHIBIT
FULL
LOAD ERROR
TABLE OF CONTENTS
CHAPTER 12
Page
12.00.1
12.10.1 12.10.2 12.10.3 12.10.3 12.10.3 12.10.4 12.10.4 12.10.5 12.10.5 12.10.6 12.10.6 12.10.7 12.10.7 12.10.7 12.10.8 12.10.8 12.10.8
12.10.11
12.10.11
12.10.13
12.10.14
12.10.15
12.10.16 12.10.17 12.10.18 12.10.18 12.10.18 12.10.19 12.10.19 12.10.19 12.10.19 12.10.19 12.10.20 12.10.20 12.10.20
Rev 3, Apr 25, 2005 Flight Crew Operating Manual Volume 2
TABLE OF CONTENTS
Page
DESCRIPTION
IMBAL 12.10.20
REPEATER 12.10.20
FAILED 12.10.20
FMQGC . FAILURE 12.10.20
Refueling Distribution 12.10.21
Refuel/Defuel Schematic 12.10.22
Fuel Re-Circulation System 12.10.23
Fuel Filters, Quantity and Temperature Readouts 12.10.25
Fuel Pump Displays 12.10.26
Fuel Shutoff Displays 12.10.27
Fuel Synoptic Page Symbols 12.10.28
EICAS Philosophy 12.10.28
Fuel Management Quantity Gauging System (FMQGS) 12.10.28
FMQGC Schematic 12.10.29
EICAS Messages 12.10.30
EMS CIRCUIT PROTECTION
CB . Fuel System 12.20.1
Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
GENERAL
Fuel is contained in a wet wing box structure, which is sealed to form three main separate wing tanks (left wing, right wing and center wing). The tanks are vented to atmosphere and slightly pressurized by an air scoop located on the lower surface of each wing. A scavenge pump purges fuel from the vent lines and a climb vent, located in each main wing tank, provides ventilation when the airplane is in a nose up attitude.
Each engine is supplied with fuel from its respective feed tank which contains two alternating current or AC primary pumps and one Direct Current (DC) back up boost pump. The transfer system maintains the feed tanks full during all attitudes and provides automatic transfer of fuel from the center tank to the main wing tanks.
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