曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

panel. The CDLS is not electrically-supplied, and is inoperative.
CKPT DOOR CONT
panel .................................................................................................................CHECK
This panel is located on the overhead panel. It is used to identify the faulty CDLS item,
and to verify the
status of the pressure sensors and the three electrical latches (referred to as strikes).
�� If one or more electrical latches (strikes) are faulty:
The cockpit door is not intrusion-proof if two or more electrical latches are faulty.
The system may be recovered by performing the following steps:
Cockpit
door..................................................................................................................................
.OPEN
COCKPIT DOOR
sw......................................................................................................SET to UNLOCK
After 10 s:
COCKPIT DOOR
sw..........................................................................................................SET to NORM
�� If two pressure sensors are faulty:
Automatic latch release is not available, in case of cockpit decompression.
�� If no LED on the CKPT DOOR CONT panel is on:
The CDLS control unit is faulty, therefore, the cockpit door might unlock
automatically. If it does not,
consider using the mechanical override system to unlock the door.
ABN-25
2/2
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
Intentionally left blank
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , , , , ,
, , , , ,
ABN-25
1/2
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , , , , ,
, , , ,
COCKPIT DOOR FAULT
This procedure should be applied, if the Cockpit Door Locking System (CDLS) fails.
This failure is indicated
when the FAULT light on the center pedestal’s COCKPIT DOOR panel comes on.
In the case of a DC BUS 2 fault, no FAULT indication appears on the center
pedestal’s COCKPIT DOOR
panel. The CDLS is not electrically-supplied, and is inoperative.
CKPT DOOR CONT
panel .................................................................................................................CHECK
This panel is located on the overhead panel. It is used to identify the faulty CDLS item,
and to verify the
status of the pressure sensors and the three electrical latches (referred to as strikes).
�� If one or more electrical latches (strikes) are faulty:
The cockpit door is not intrusion-proof if two or more electrical latches are faulty.
The system may be recovered by performing the following steps:
Cockpit
door..................................................................................................................................
.OPEN
COCKPIT DOOR
sw......................................................................................................SET to UNLOCK
After 10 s:
COCKPIT DOOR
sw..........................................................................................................SET to NORM
�� If two pressure sensors are faulty:
Automatic latch release is not available, in case of cockpit decompression.
�� If no LED on the CKPT DOOR CONT panel is on:
The CDLS control unit is faulty, therefore, the cockpit door might unlock
automatically. If it does not,
consider using the mechanical override system to unlock the door.
ABN-25
2/2
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
Intentionally left blank
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , , , , ,
, , , ,
ABN-25
1/2
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , , , , ,
, , MSN,,,
COCKPIT DOOR FAULT
This procedure should be applied, if the Cockpit Door Locking System (CDLS) fails.
This failure is indicated
when the FAULT light on the center pedestal’s COCKPIT DOOR panel comes on.
In the case of a DC BUS 2 fault, no FAULT indication appears on the center
pedestal’s COCKPIT DOOR
panel. The CDLS is not electrically-supplied, and is inoperative.
CKPT DOOR CONT
panel .................................................................................................................CHECK
This panel is located on the overhead panel. It is used to identify the faulty CDLS item,
and to verify the
status of the pressure sensors and the three electrical latches (referred to as strikes).
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A318/A319/A320/A321 QRH快速檢查單QUICK REFERENCE HAND BOOK3(5)