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A
P U
APU AUTO
SHUTDOWN 5
‐ In case of oil low press,
automatic shutdown is
delayed by 15.5 s
‐ In case of oil low press, the
automatic shutdown is delayed
by :
• 15.5 s if the oil temp < -4 °C
• 0.05 s if oil temp
> -4 °C
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 7/14
FCOM 19 AUG 10
Continued from previous page
SYSTEM LGCIU 1
OUTPUT
LGCIU 2
OUTPUT A/C IN FLT A/C ON GRND
SERVICE
INTERPHONE 6 6 Inhibited(6)Available(7)
PUBLIC
ADDRESS
13
13
P.A. increased level(6)P.A. low level(7)
ADIRU and
AVIONICS
ground warning
13
13
External horn and
light inhibited(6)
External horn and
light not inhibited(7)
FLT
INTERPHONE 9 Communication with
ground mechanic inhibited
Communication with
ground mechanic available
COCKPIT
CALL LIGHT 9 Inhibited Not inhibited
ACARS 7 Available Available
CVR
137
13
Runs(6)Runs :(7)
during ‐ the first 5 min following
energization
‐ with one engine running
Stops :(7)
5 min after second engine
shutdown
COMMUN
I C
A T
I O
N S
CVR 5
• ERASE function inhibited
• No low frequency signal
in the loudspeakers if test
performed
• ERASE function not inhibited
• Low frequency signal in the
loudspeakers if test performed
DC generation 5 APU start on batteries
only, is delayed by 45 s
No APU start delay
E L when on batteries only
E C GALLEY supply 5 Main galley not supplied when
APU GEN only is supplying
Main galley supplied when
APU GEN only is supplying
E
I S EIS 5 Display test inhibited when
ANN LT TEST is selected Display test not inhibited
F I
R E APU 5 No APU fire automatic
extinguishing
Automatic extinguishing
not inhibited
F
L T
• For SFCC 1(2) :
Slats alpha/speed lock
function active
• For SFCC 1(2) :
Slats alpha/speed lock function
active if speed > 60 kt
C
T L
SFCC 1(2) 5 (5)
• For SFCC(2) :
No flaps movement inhibition
if the cargo door is opened
• For SFCC (2) :
Flaps movement inhibition if
cargo door is opened
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 8/14
FCOM 19 AUG 10
Continued from previous page
SYSTEM LGCIU 1
OUTPUT
LGCIU 2
OUTPUT A/C IN FLT A/C ON GRND
F
L T
Runs (6)Runs :(7)
• during the first 5 min following
energization
• with one engine running
I N
S T
• DFDR
• QAR
(if installed)
137
13
Stops :(7)
5 min after second engine shut
down
F U
E L FQI 5 FQI uses flight attitude
correction due to wing bending
FQI uses ground
attitude correction
BLUE and
GREEN pumps
13
Blue or green pump "FAULT"
light not inhibited when
related pump is stopped(6)
Blue or green pump
"FAULT" light inhibited when
related pump is stopped(7)
BLUE pump 7 Runs when electrical
power is available
Runs when at least
one engine is running
BLUE and
YELLOW pumps
13
Blue or yellow pump "FAULT"
light not inhibited when
related pump is stopped(6)
Blue or yellow pump
"FAULT" light inhibited when
related pump is stopped(8)
H
Y D
PTU 7 PTU runs if green/yellow
diff. press > 500 PSI
PTU runs if green/yellow diff.
press > 500 PSI and
• both MASTER LEVERS are at
OFF or
• both MASTER LEVERS are at
ON or
• nose wheel steering is not in
towing position with parking
brake released.
PTU is inhibited during the use of
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 :
　
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