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┃FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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CREW INTERFACE WITH FMGC
CAPT EFIS CONTROL PANEL
FCU
F/O EFIS CONTROL PANEL
CCM ALL
MCDUI
THRUST LEVERS
MCDU3
OPTIONAL
MCDU2
CCM ALL
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┃ ┃ ┃1.22.10 P 6 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ aw aw ,, ~e~ A319 ┃l AUTO FGENERAL ┃SEQ 001 1 ┃I REV 23 ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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┃I -~ A318 ┃AUTO FLIGHT ┃1.22.10 P 7 ┃
┃ .*,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃ GENERAL ┃SEQ 001 ┃REV 28 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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The FMGS has three modes of operation :
- dual mode (the normal mode)
- independent mode. Each FMGC being controlled by its associated MCDU
- single mode (using one FMGC only)
DUAL MODE
This is the normal mode. The two FMGCs are synchronized : each performs its own
computations and exchanges data with the other through a crosstalk bus.
One FMGC is the master, the other the slave, so that some data in the slave FMGC comes
from the master. All data inserted into any MCDU is transferred to both FMGCs and to all
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AIRBUS A320 Flight Crew Operating Manual1(142)
