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To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AIR CONDITIONING / PRESSURIZATION / VENTILATION
A318/A319/A320/A321 FLEET PRO-ABN-21 P 16/78
FCOM 19 AUG 10
AIR PACK 1(2) REGUL FAULT (Cont'd)
STATUS
INOP SYS
PACK 1(2) REGUL (1)
HOT AIR (2)
(1) (In case of By Pass Valve or RAM Air Inlet failure)
(2) (In case of Flow Control Valve in backup mode)
AIR PACK 1(2) REGUL FAULT
Applicable to:
L2 Pack primary channel, or pack primary and secondary channels fault.
Crew awareness.
Note: Following an internal Pack Controller 1(2) failure, the “AIR PACK 1(2) REGUL FAULT”
ECAM warning may be spuriously triggered. During flight, pack regulation is not affected.
The warning can be cleared. On ground, pack performance may be degraded. As such,
a Pack Controller 1(2) reset may be attempted via circuit breaker PACK TEMP CTL SYS
2/1/115 VAC/2HH (PACK TEMP CTL SYS 2/2/115 VAC/22HH), located in the Y18 (Y20)
position of the rear panel 122 VU.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AIR CONDITIONING / PRESSURIZATION / VENTILATION
A318/A319/A320/A321 FLEET PRO-ABN-21 P 17/78
FCOM 19 AUG 10
AIR PACK 1(2) REGUL FAULT (Cont'd)
L12
STATUS
�� If the primary channel fails:
The pack air inlet flap fully opens; pack flow is fixed at the
previous setting.
�� If the primary and secondary channels fail:
PACK 1(2) AT FIXED TEMP
The pack outlet temperature is controlled by the pack anti-ice
valve and is stabilized to a temperature between 5 °C (41 °F)
and 30 °C (86 °F) within a maximum of 6 min.
The pack outlet temperature is controlled by the pack anti-ice
valve and is stabilized to a temperature between 5 °C (41 °F)
and 30 °C (86 °F) within a maximum of 6 min.
INOP SYS
PACK 1(2) REGUL
AIR PACK 1(2) REGUL FAULT
Applicable to:
L2 Pack primary channel, or pack primary and secondary channels fault.
Crew awareness.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AIR CONDITIONING / PRESSURIZATION / VENTILATION
A318/A319/A320/A321 FLEET PRO-ABN-21 P 18/78
FCOM 19 AUG 10
AIR PACK 1(2) REGUL FAULT (Cont'd)
L12
STATUS
�� If the primary channel fails:
The pack air inlet flap fully opens; pack flow is fixed at the
previous setting.
�� If the primary and secondary channels fail:
PACK 1(2) AT FIXED TEMP
The pack outlet temperature is controlled by the pack anti-ice
valve and is stabilized to a temperature between 5 °C (41 °F)
and 30 °C (86 °F) within a maximum of 6 min.
The pack outlet temperature is controlled by the pack anti-ice
valve and is stabilized to a temperature between 5 °C (41 °F)
and 30 °C (86 °F) within a maximum of 6 min.
INOP SYS
PACK 1(2) REGUL
AIR PACK 1(2) REGUL FAULT
Applicable to:
L2 Pack primary channel, or pack primary and secondary channels fault.
Crew awareness.
L2 The temperature regulation performance is degraded.
Crew awareness.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AIR CONDITIONING / PRESSURIZATION / VENTILATION
A318/A319/A320/A321 FLEET PRO-ABN-21 P 19/78
FCOM 19 AUG 10
AIR PACK 1(2) REGUL FAULT (Cont'd)
L12
STATUS
�� If the primary channel fails:
The pack air inlet flap fully opens; pack flow is fixed at the
previous setting.
�� If the primary and secondary channels fail:
PACK 1(2) AT FIXED TEMP
The pack outlet temperature is controlled by the pack anti-ice
valve and is stabilized to a temperature between 5 °C (41 °F)
and 30 °C (86 °F) within a maximum of 6 min.
The pack outlet temperature is controlled by the pack anti-ice
valve and is stabilized to a temperature between 5 °C (41 °F)
and 30 °C (86 °F) within a maximum of 6 min.
INOP SYS
PACK 1(2) REGUL
STATUS
INOP SYS
PACK 1(2) REGUL (1)
HOT AIR (2)
(1) (In case of By Pass Valve or RAM Air Inlet failure)
(2) (In case of Flow Control Valve in backup mode)
AIR PACK 1(2) REGUL FAULT
Applicable to:
,
L2 The temperature regulation performance is degraded.
Crew awareness.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
　
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