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the cargo door hand pump and for
40 s after its use.
I C
E
CAPT, (F/O),
(STBY) probes
and CAPT, (F/O)
windows heating
4,
(2)
((8))
4,
(2)
((8))
• CAPT, (F/O), ((STBY)) pitots
and CAPT, (F/O) windows :
high heating level applied
• All other probes and windows
are heated(6)
• With engines stopped: no
heating(8)
• With at least one engine
running :
• CAPT, (F/O), ((STBY)) pitots
and CAPT, (F/O) windows are
heated at low level(8)
RA
I N
WING ANTI ICE 3 1
Wing anti ice valves
open when the WING
ANTI ICE pb is at ON(6)
Wing anti ice valves open
for 30 s when the WING
ANTI ICE pb is at ON(8)
RAIN
REPELLENT
13
13
Not inhibited(6) Inhibited if engines are stopped(7)
P R
O T DRAIN MAST(10) 9 High heating level is applied Low heating level is applied
L/G SAFETY
VALVE 6 Safety valve closes if
L A aircraft speed > 260 kt Safety valve opened
ND
I N
G
L/G control 10 10 Retraction not inhibited(9)Retraction inhibited(9)
G
E A
R
TIRE PRESS �� 5 "TYRE LO PRESS" warning
threshold set to its flight level
"TYRE LO PRESS" warning
threshold set to its ground level
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
LANDING GEAR
GEARS AND DOORS - INTERACTIONS BETWEEN
LANDING GEAR AND AIRCRAFT SYSTEMS
A318/A319/A320/A321 FLEET DSC-32-10-30 P 5/14
FCOM 19 AUG 10
Continued from previous page
SYSTEM LGCIU 1
OUTPUT
LGCIU 2
OUTPUT A/C IN FLT A/C ON GRND
STAND BY ALTI 5 VIBRATION function active Vibration function inhibited
ATC 1(2) 3 (1) ATC 1(2) available
in AUTO mode ATC 1(2) inhibited in AUTO mode
N
A V
I G
A T
I O
N
ADIRU 1(10) 7 No external horn when ADIRU
supplied from batteries only External horn not inhibited
POW
E R
13
(1)
(3)
On ENG 1(2) :(6)
‐ Reverse inhibited
‐ No automatic start abort
‐ FADEC always supplied
‐ FLEX not available
‐ If installed, BUMP not
selectable
On ENG 1(2) :(8)
‐ Reverse available
‐ Automatic start abort available
‐ 5 min after eng-shut down
FADEC 1(2) no more supplied
‐ FLEX available
‐ If installed, BUMP selectable
P L
A
N T
FADEC 1(2)
138
(1)
(3)
(8)
Modulated idle and approach
idle are available(6)
Modulated idle only available(7)
(1)When either LGCIU indicates flight
(2)When both LGCIU indicate ground
(3)When either LGCIU indicates ground
(4)When both LGCIU indicate flight
(5) Valid from MSN 44.
(6)When either output indicates flight
(7)When all outputs indicate ground
(8)When both outputs indicate ground
(9) One valid output is sufficient
(10) Valid from MSN 22
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
LANDING GEAR
GEARS AND DOORS - INTERACTIONS BETWEEN
LANDING GEAR AND AIRCRAFT SYSTEMS
A318/A319/A320/A321 FLEET DSC-32-10-30 P 6/14
FCOM 19 AUG 10
PROXIMITY DETECTORS ON SHOCK ABSORBERS
Applicable to:
,
,
MSN,,,,
SYSTEM LGCIU 1
OUTPUT
LGCIU 2
OUTPUT A/C IN FLT A/C ON GRND
STROBE lts 5 On when AUTO selected Off when AUTO selected
LOGO lts 5 Off when flaps retracted On
AIRSTAIRS
(if installed) 3 1 Control inhibited(1)Control not inhibited(2)
CARGO DOOR(5) 5 normal control not available normal control available
G
E N
E R
A L
WATER FILLING 5 Preselect water
servicing inhibited
Preselect water
servicing available
AVNCS COOLING 5 5
• Skin temp. < 35 °C : The
system is in closed conf.(1)
• Skin temp. > 35 °C : The
system is in intermediate
conf.(1)
• Skin temp. < 5 °C : The system
is in closed conf.(2)
• Skin temp. > 5 °C : The system
is in open conf.(2)
GRND COOLING
(if installed)
13
13
Inhibited(1)Not inhibited(2)
A
I R
FWD CARGO
VENT 5 Extract fan stopped
when ◂P > 1 PSI Extract fan on
CAB PRESS 5 5
‐ Climb mode active(4)‐ Prepressurization active before
TO (3)
Depressurization ‐ active after
LDG (3)
COND
PACK 1(2) TEMP
CONTROL
3
(1) Pack air inlet flaps opened. Pack air inlet flap fully
closed at TO and LDG
　
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