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A318/A319/A320/A321 FLEET PRO-NOR-SOP-09 P 1/4
FCOM 19 AUG 10
AFTER START
Applicable to:
, ,
MSN
ENG MODE selector....................................................................................................................NORM
Turning the ENG MODE selector to NORM indicates the end of the start sequence. AFTER START
actions may be performed.
On ECAM lower display the WHEEL SD page replaces the ENG SD page.
Leaving the ENG MODE selector at the START/IGN position would prevent continuous relight
selection on the ground (would be supplied at lift off). In addition, the ENG SD page would remain
displayed. The selector must be cycled to recover normal control of ignition and to display WHEEL
SD page.
After start, to avoid thermal shock, the pilot should operate the engine at idle or near idle for at
least 2 min before advancing the thrust lever to high power. Taxi time at idle may be included in the
warm-up period.
The last engine started must run for at least 2 min before takeoff initiation, to ensure that takeoff is
not initiated before the center tank pumps test is finished, since takeoff on center tank is prohibited.
Applicable to: MSN
4566,,,
ENG MODE selector....................................................................................................................NORM
Turning the ENG MODE selector to NORM indicates the end of the start sequence. AFTER START
actions may be performed.
On ECAM lower display the WHEEL SD page replaces the ENG SD page.
Leaving the ENG MODE selector at the START/IGN position would prevent continuous relight
selection on the ground (would be supplied at lift off). In addition, the ENG SD page would remain
displayed. The selector must be cycled to recover normal control of ignition and to display WHEEL
SD page.
After a shutdown period greater than 2 h, to avoid thermal shock, the pilot should operate the engine
at idle or near idle for at least 5 min before advancing the thrust lever to high power. Taxi time at idle
may be included in the warm-up period.
The last engine started must run for at least 2 min before takeoff initiation, to ensure that takeoff is
not initiated before the center tank pumps test is finished, since takeoff on center tank is prohibited.
Applicable to: ALL
APU BLEED pb-sw..........................................................................................................................OFF
‐ Turn APU BLEED pb-sw off just after engine start to avoid ingestion of engine exhaust gases.
‐ APU BLEED valve closes, ENG BLEED valves open.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - AFTER START
A318/A319/A320/A321 FLEET PRO-NOR-SOP-09 P 2/4
FCOM 19 AUG 10
Applicable to: MSN
4566,,,
ENG 1 ANTI ICE pb-sw and ENG 2 ANTI ICE pb-sw...........................................................AS RQRD
Note: Icing conditions may be expected when the OAT (on ground and for takeoff), or the TAT (in
flight), is 10 °C or below, and there is visible moisture in the air (such as clouds, fog with
low visibility, rain, snow, sleet, ice crystals), or when standing water, slush, ice or snow is
present on the taxiways or runway.
During ground operation, when in icing conditions and the OAT is plus 3 °C or less, or if significant
engine vibration occurs, the following procedure should be applied for ice shedding :
CAUTION If, during thrust increase, the aircraft starts to move, immediately retard the thrust
levers to IDLE.
If ground surface conditions and the environment permit, the flight crew should accelerate the
engines to minimum 50 % of N1 at intervals not greater than 15 min. There is no requirement to
maintain the high trust settings.
In addition, this engine acceleration should also be performed just before take-off, with particular
attention to engine parameters to ensure normal engine operation.
Note: When performing the static run–up, the 61-74 % N1 range should be avoided.
If ENG ANTI ICE is selected ON and the valve(s) do not open (FAULT light(s) remain on), increase
the N2 of the associated engine by about 5 %.
When the valves are open, retard the thrust lever(s) to idle.
If ENG ANTI ICE is switched on, the IGNITION memo appears on the ECAM because continuous
ignition is automatically selected.
Applicable to:
, ,
MSN
ENG 1 ANTI ICE pb-sw and ENG 2 ANTI ICE pb-sw...........................................................AS RQRD
Note: Icing conditions may be expected when the OAT (on ground and for takeoff), or the TAT (in
flight), is 10 °C or below, and there is visible moisture in the air (such as clouds, fog with
　
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