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Time is displayed in
hours, minutes, and
seconds (HH:MMss)
DATE is displayed as
Day/Month/Year.
Mode annunciator
Indicates the present
mode of operation.
DT -- date
GPS -- GPS synchro--
nization enabled
INT -- internal time/
date operation (GPS
disabled).
LT -- local time
NOTE
ET time corresponds to
airplane flight time and
starts when the airplane
takes off and stops at
touch down. ET can
only be reset on ground.
Effectivity:
Airplanes 15016 and subsequent.
ET SEL
Used to select the
elapsed time function
when the chronometer
function is active.
Also used to decrease the
data in one digit
increments during
manual setting of the
clock.
MODE
Used to select the mode of
operation (DT, GPS, INT, LT)
and also used in conjunction
with ET SEL and ET RST
buttons to set UTC time, date,
and local time.
Vol. 1 12--60--8
FLIGHT INSTRUMENTS
Standby Instruments and Clocks REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
D. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
Integrated
Standby
Instrument
INT STBY
INST BATTERY
2
N10
Standby
Instruments
CLOCK 1
BUS
N11
and Clocks
Clocks
(PILOTS) MAIN
BATTERY
6
B7
CLOCK 2
DIRECT BUS
B8
(COPILOTS) DC BUS 2 2 H5
Vol. 1 13--00--1
FUEL SYSTEM
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
CHAPTER 13 --- FUEL SYSTEM
Page
TABLE OF CONTENTS 13--00
Table of Contents 13--00--1
INTRODUCTION 13--10
Introduction 13--10--1
FUEL STORAGE 13--20
Fuel Storage 13--20--1
Collector Tanks 13--20--1
Venting 13--20--1
FUEL MANAGEMENT 13--30
Fuel Management 13--30--1
Fuel Transfer 13--30--1
Fuel Crossflow 13--30--1
System Circuit Breakers 13--30--5
FUEL DISTRIBUTION 13--40
Fuel Distribution 13--40--1
System Circuit Breakers 13--40--7
REFUELING AND DEFUELING 13--50
Refueling and Defueling 13--50--1
Control Panel 13--50--3
System Circuit Breakers 13--50--6
FUEL QUANTITY GAUGING 13--60
Fuel Quantity Gauging 13--60--1
Magnetic Level Indicators 13--60--7
System Circuit Breakers 13--60--10
LIST OF ILLUSTRATIONS
INTRODUCTION
Figure 13--10--1 Fuel System -- General 13--10--2
FUEL STORAGE
Figure 13--20--1 Storage and Vent System 13--20--2
FUEL MANAGEMENT
Figure 13--30--1 Fuel Transfer and Crossflow System 13--30--2
Vol. 1 13--00--2
FUEL SYSTEM
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Figure 13--30--2 Fuel -- EICAS -- Synoptic Page 13--30--3
Figure 13--30--3 Fuel System -- EICAS Indications 13--30--4
FUEL DISTRIBUTION
Figure 13--40--1 Fuel Distribution Schematic 13--40--2
Figure 13--40--2 Fuel Distribution -- ENG and APU Control Panels 13--40--3
Figure 13--40--3 Fuel Synoptic Page -- Distribution 13--40--4
Figure 13--40--4 Fuel System EICAS Indications -- Sheet 1 13--40--5
Figure 13--40--4 Fuel System EICAS Indications -- Sheet 2 13--40--6
REFUELING AND DEFUELING
Figure 13--50--1 Refuel/Defuel Components 13--50--2
Figure 13--50--2 Refuel/ Defuel Control Panel -- Sheet 1 13--50--4
Figure 13--50--2 Refuel/ Defuel Control Panel -- Sheet 2 13--50--5
FUEL QUANTITY GAUGING
Figure 13--60--1 Fuel Quantity System -- Schematic 13--60--2
Figure 13--60--2 Fuel System Synoptic Page -- Gauging 13--60--3
Figure 13--60--3 Fuel System Gauging EICAS Indications -- Primary Page 13--60--4
Figure 13--60--4 Fuel System Gauging EICAS Indications -- Status Page 13--60--5
Figure 13--60--5 Fuel System -- Menu Page 13--60--6
Figure 13--60--6 Magnetic Level Indicators 13--60--8
Figure 13--60--7 Pitch and Roll Inclinometers 13--60--9
Vol. 1 13--10--1
FUEL SYSTEM
Introduction REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
1. INTRODUCTION
The fuel system consists of three integral tanks within the wing box structure. Ejectors and
electrical boost pumps supply fuel to each engine. An independent system provides fuel to
the auxiliary power unit (APU). The fuel system also provides facilities for pressure
refueling/defueling and gravity refueling/defueling. Power and gravity crossflow systems
allow fuel transfer between wing tanks.
A fuel quantity gauging computer (FQGC) automatically controls refueling, powered fuel
　
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