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Applicable to: ,
MSN ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - ENGINE START
Intentionally left blank
A330/A340 FLEET PRO-NOR-SOP-08 P 6/6
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - AFTER START
A330/A340 FLEET PRO-NOR-SOP-09 P 1/4
FCOM 19 AUG 10
AFTER START
Applicable to:
ENG START selector ................................................................................................................. NORM
Turning the ENG START selector to NORM indicates the end ‐ of the start sequence. AFTER
START actions may be performed.
‐ ON the ECAM's lower display, the WHEEL SD page replaces the ENG SD page.
Note: If the ENG START selector is not switched to NORM, the ENG SD page is automatically
replaced by the WHEEL SD page 15 s after second engine start.
Leaving the ENG START selector at the START/IGN position would ‐ prevent continuous relight
selection on ground (would be supplied at lift-off). The selector must be cycled to recover normal
control of ignition.
‐ 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. A longer warm-up time (up to about 10 min) may result in a lower peak EGT
value during takeoff.
Applicable to: ,
ENG START selector ................................................................................................................. NORM
‐ Turning the ENG START selector to NORM indicates the end of the start sequence. AFTER
START actions may be performed.
‐ ON the ECAM's lower display, the WHEEL SD page replaces the ENG SD page.
Note: If the ENG START selector is not switched to NORM, the ENG SD page is automatically
replaced by the WHEEL SD page 15 s after second engine start.
‐ Leaving the ENG START selector at the START/IGN position would prevent continuous relight
selection on ground (would be supplied at lift-off). The selector must be cycled to recover normal
control of ignition.
‐ After start, to avoid thermal shock, the engine should be operated at idle, or near idle for at least:
• 5 min when engines are cold, or
• 3 min when engines are warm after a stop of 1.5 h or less
prior to advancing the thrust lever to high power. Taxi time at idle may be included in the warm-up
period.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - AFTER START
A330/A340 FLEET PRO-NOR-SOP-09 P 2/4
FCOM 19 AUG 10
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.
Applicable to:
ENG ANTI ICE........................................................................................................................ ASRQRD
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 for more than 30 min, 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 approximately 70 % of N1 for 30 s at intervals not greater than 30 min.
In addition, this engine acceleration should also be performed just before take-off, with particular
attention to engine parameters to ensure normal engine operation.
If ground surface or environment do not permit to accelerate the engine to 70 % N1, then power
setting and dwell line should be as high as practical.
When operating in conditions of freezing rain, freezing drizzle, freezing fog or heavy snow, ice
shedding may be enhanced, by additional runups at intervals, to not exceed 10 min, advancing
throttles to 70 % N1 momentarily (no hold time).
Applicable to: ,
ENG ANTI ICE........................................................................................................................ ASRQRD
Note: Icing conditions may be expected when the OAT (on ground and for takeoff), or the TAT (in
　
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