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Note : Certain actions will not disappear after execution
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.31.15 P 2 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I -~ A318 ┃I INDICATIINDICATIONSGONYE/WDS ┃SEQ 001 1 ┃F REV 32 ┃
┃ ~ ~ o ~L'~ A319 ┃ ┃ ┃ ┃
┃ LI,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
INDEPENDENT
FAILURE
(AMBER OR RED)
f_/_/+
,~J 5
ACTION LINE
(BLUE)
OVERFLOW SYMBOL
(GREEN)
Name of the
system affected
by a failure~
Displayed here
in case of
overflow of the
left part
(amber or red)
If there are too many ECAM messages for the amount of space available in the lower part
of the F_/WD, a green arrow appears at the bottom of the display, pointing down to show
that the information has overflowed off the screen. The pilot can scroll down to view
additional messages by pushing the CLR pushbutton on the ECAM control panel (on the
pedestal, just below the lower ECAM DU).
PRIMARY
FAILURE
(AMBER OR RED)
~.. F/O 3
~. CHECK
ACTION LINE
(BLUE)
SECONDARY FAILURES
(AMBER)
The ECAM DU displays a primary failure as a boxed title.
It identifies a secondary failure by putting a star in front of the title of the affected system
Note : The OU displays the overflow symbol, if primary or secondary failures overflow. In
case of ELEC EMER CONFIG, the secondary failures are inhibited.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━┳━━━━━━━━━┓
┃I ~-~ A318 ┃INDICATING/RECORDING SYSTEMS ┃1.31.15 P 3 ┃
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual4(26)
