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A forward-opening hinge door separates the cockpit from the passenger
comportment. It has an electric-locking latch, controlled by pilots. In normal
conditions, when the door is closed, it remains locked. Upon cockpit entry
request, the flight crew can authorize entry by unlocking the door, which remains
closed until it is pushed open.
When the flight crew does not respond to request for entry , the door can be
unlocked by the cabin crew, by entering a two to seven digit code (programmed
by the airline) on the keypad, installed on the lateral side of the Forward
Attendant Panel (FAP).
The door is bulletproof and fully compliant with rapid decompression requirements.
A mechanical override enables the pilots to open the door from the cockpit side.
Refer to COCKPIT DOOR OPERATION
TR1 A318/A319/A320/A321 FLEET CCOM Page 6 of 12
CABIN CREW OPERATING MANUAL
EVACUATION DEVICES
COCKPIT EMERGENCY EXITS
05.020
OCT 27/07
COCKPIT DOOR
ESCAPE PANEL
SPY HOLE
LOCKING
LATCHES
MECHANICAL
OVERRIDE
QUICK RELEASE
PINS
NOC 05020 00053 0001
DOOR HANDLE
Note:
TR1 A318/A319/A320/A321 FLEET CCOM Page 7 of 12
CABIN CREW OPERATING MANUAL
EVACUATION DEVICES
COCKPIT EMERGENCY EXITS
05.020
OCT 27/07
1. The escape panel enables the flight crew to evacuate the cockpit, in
case of an emergency, when the door is jammed or stuck. This panel
can only be removed from the cockpit side by pulling the quick release
pin towards the centre of the flap, and kicking the panel open.
2. In case of an electrical supply failure, the door is automatically
unlocked, but remains closed.
3. If installed and in the event that one locking latch strike fails, or in case
of a total CDLS failure, a deadbolt is located at the level of the center
latch area of the cockpit door. This deadbolt bolts the door from the
cockpit side.
4. In case of rapid decompression in the cockpit, the door is automatically
unlocked.
In case of a rapid decompression in the cabin, venting from the cockpit
to the cabin is ensured via existing gaps between the cockpit and the
cabin, and with additional grids installed in the ceiling panels .
KEYPAD LOCATION AND OPERATION
The keypad is located at the lateral side of the Forward Attendant Panel (FAP)
and is used by the cabin crew to request pilots to open the door.
KEYPAD
1 2
#
3 4
5 6
7 8
9 0
*
1
2
NOC 05020 00054 0001
TR1 A318/A319/A320/A321 FLEET CCOM Page 8 of 12
CABIN CREW OPERATING MANUAL
EVACUATION DEVICES
COCKPIT EMERGENCY EXITS
05.020
OCT 27/07
1 LOCKED/UNLOCKED DOOR INDICATOR
GREEN light ON : The door has been unlocked either by a flight
crew action, or automatically (during 5 seconds)
when no flight crew action is performed during the
delay following an emergency access request. The
door can be pushed open.
GREEN light flashes: An emergency request to enter the cockpit has
been made ; the buzzer will sound continuously in
the cockpit, but no action has yet been taken by
the flight crew.
RED light ON : The flight crew has denied access, and the door
remains locked.
2 DIGITAL KEYPAD
The keypad is used to sound the buzzer in the cockpit for one to nine
seconds (three seconds by default), by entering a zero to seven-digit code,
as programmed by the airline, followed by the ’#’ key.
It is also used to enter the two to seven-digit emergency code, followed by
the ’#’ key, when the flight crew does not respond.
COCKPIT DOOR CONTROL PANEL
LOCATION
A
A
NOC 05020 00055 0001
TR1 A318/A319/A320/A321 FLEET CCOM Page 9 of 12
CABIN CREW OPERATING MANUAL
EVACUATION DEVICES
COCKPIT EMERGENCY EXITS
05.020
OCT 27/07
The secure cockpit door is controlled by a toggle switch, located on the central
pedestal.
CONTROL PANEL
1
2
NOC 05020 00056 0001
1 COCKPIT DOOR toggle switch
UNLOCK position : This position is used to enable the cabin
crewmember to open the door. The switch must
be pulled and maintained in the unlock position
until the door is pushed open.
NORM position : All latches are locked, and EMERGENCY access
is possible for the cabin crew.
LOCK position : Once the button has been moved to this position,
the door is locked; emergency access, the buzzer,
and the keypad are inhibited for a preselected
time (5 to 20 minutes).
Note:
1. If the LOCK position has not been used by the pilot, for at least 5
to 20 minutes, the cabin crew is able to request an emergency
　
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