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are inhibited.
GX_11_029
FUEL XFER ON
Indicates that the left to right
transfer system is in the MANUAL
mode of operation.
AFT FUEL XFER OFF
Indicates aft fuel transfer has been
inhibited.
WING FUEL XFER OFF
Indicates that transfer of fuel from
left to right, and from right to left
has been selected off.
L (R) ENG SOV CLSD
Indicates that left or right fuel
shutoff valve is closed.
L (R) AUX PUMP OFF
Indicates that the left or right
auxiliary pump has been
inhibited.
FUEL XFER ON
Indicates that the right to left
transfer system is in the
MANUAL mode of operation.
AFT FUEL XFER ON
Indicates aft fuel transfer is in
progress under manual control.
XFEED VALVE OPEN
Indicates that the crossfeed
shutoff valve is open.
APU FUEL SOV CLSD
Indicates that APU fuel shutoff
valve is closed.
FUEL RECIRC ON
Indicates that the FRTT valves are
opened when commanded by flight
crew. Prior to -9 FMQGC.
FUEL RECIRC OFF
Indicates that the FRTT valves
are closed when commanded
by flight crew. -9 FMQGC and
later.
For Training Purposes Only
Sept 04
11-45
P I LOT T R A I N I N G GU I D E
FUEL SYSTEM
EMS CIRCUIT PROTECTION
BRT
CIRCUIT BREAKER SYSTEM
STAT SYS BUS
PREV
PAGE
NEXT
PAGE
CNTL TEST
BUS
EMER
CONT
CB - FUEL SYSTEM 1/6
XFER SOV C
XFER SOV O
XFER SOV C
XFER SOV O
AFT TANK L PUMP
AFT TANK L SOV C
DC ESS
DC ESS
BATT
BATT
AC 2
DC 1
IN
IN
IN
IN
IN
IN
2/6
AFT TANK L SOV O
AFT TANK R PUMP
AFT TANK R SOV C
AFT TANK R SOV O
APU FIRE SOV
FUEL COMPUTR CH A
DC 1
AC 3
DC 2
DC 2
DC EMER
BATT
IN
IN
IN
IN
IN
IN
X
X
X
X
DCPC
R AFT PRI PUMP
R AUX PUMP
R CTR XFER PUMP
L ENG FUEL SOV
L FWD PRI PUMP
L FUEL RECIRC VLV
AC 4
BATT
AC 4
DC EMER
AC 2
DC 1
CB - FUEL SYSTEM
CB - FUEL SYSTEM 4/6
X
X
X
DCPC
X
X
IN
IN
IN
IN
IN
IN
5/6
R ENG FUEL SOV
R/D MOTOR VALVES
R/D PANEL COCKPIT
R/D PANEL EXT
R FWD PRI PUMP
R FUEL RECIRC VLV
DC EMER
APU BATT
APU BATT
APU BATT
AC 3
DC 2
CB - FUEL SYSTEM
IN
IN
IN
IN
IN
IN
NOTE: The fuel recirculation protection is not active, TBD by flight test.
FUEL COMPUTR CH B
FUEL R/D CH A
FUEL R/D CH B
L AFT PRI PUMP
L AUX PUMP
L CTR XFER PUMP
DC ESS
APU BATT
APU BATT
AC 1
DC ESS
AC 1
6/6
R/D SOL VALVES
X FEED SOV C
XFEED SOV O
APU BATT
BATT
BATT
X ASCA
ASCA
ASCA
IN
IN
IN
CB - FUEL SYSTEM 3/6 CB - FUEL SYSTEM
IN
IN
IN
IN
IN
IN
GX_11_030
M
CIRCUIT BREAKER - SYSTEM 1/2
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
DCPC
X
X
ASCA
ASCA
ASCA
P I LOT T R A I N I N G GU I D E
FUEL SYSTEM
11-46 For Training Purposes Only
Sept 04
PAGE INTENTIONALLY LEFT BLANK
For Training Purposes Only
Sept 04
Appx-i
P I LOT T R A I N I N G GU I D E
GLOBAL 5000 DIFFERENCES
APPENDIX 1
Appendix 1: Global 5000 Differences TABLE OF CONTENTS
Page
Introduction ............................................................................................................................ 1
Airplane Dimension Schematic ........................................................................................ 2
Dimensions and General Data ......................................................................................... 3
Steering Radii................................................................................................................... 5
Steering Radii Schematic........................................................................................... 5
Aural and Visual Warning Messages – Differences ......................................................... 6
Smoke Detection.............................................................................................................. 8
Avionics and Cockpit Display Ventilation ....................................................................... 10
　
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