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not be performed. This is to avoid possible nose landing gear damage upon green
hydraulic pressurization.
To dispatch the aircraft in such a case,Refer to 99 Duref Cible MEL.
Applicable to: ,
NWS DISC................................................................................................................CHECK AS REQD
In case of pushback (conventional or towbarless), the nosewheel steering selector bypass pin must
be in the tow position. The ECAM NWS DISC memo indicates this to the flight crew.
CAUTION If NWS DISC is not displayed on the ECAM, but the ground crew confirms that the
steering selector bypass pin is in the towing position, then the pushback must not be
performed. This is to avoid possible nose landing gear damage upon green hydraulic
pressurization.
To dispatch the aircraft in such a case,Refer to 99 Duref Cible MEL.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES
- BEFORE PUSHBACK OR START
A330/A340 FLEET PRO-NOR-SOP-07 P 3/4
FCOM 19 AUG 10
Applicable to: ALL
WINDOWS and DOORS............................................................................................CHECK CLOSED
Check that the cockpit windows ‐ closed and locked (flush, no red)
‐ Check, on the ECAM lower display, that all the aircraft doors are closed
‐ When required by local airworthiness authorities, check that the cockpit door is closed and locked
(no cockpit door open/fault indication).
If entry is requested, identify the person requesting entry before unlocking the door. With the
cockpit door selector on NORM, the cockpit door is closed and locked. If entry is requested from
the cabin, and if no further action is performed by the pilot, the cabin crew will be able to unlock
the door by using the emergency access procedure. Except for crew entry/exit, the cockpit door
should remain closed until engine shutdown.
Note: Starting one engine with a door not closed will result in pack valve closure.
Applicable to: ALL
BEACON sw.................................................................................................................................... ON
Applicable to: ALL
THR lever .................................................................................................................................... IDLE
CAUTION The engines will start, regardless of the thrust lever position. If the thrust lever are
not at IDLE, then the thrust will rapidly increase to the corresponding thrust lever
position, causing a hazardous situation.
Applicable to: ALL
PRK BRK handle ACCU PRESS...............................................................................................CHECK
The ACCU PRESS indicator must be in the green band.
PRK BRK handle................................................................................................................... AS RQRD
If no pushback is required, check that the PRK BRK handle ‐ is ON, and check the BRAKES
PRESS indicator.
CAUTION If, during engine start with the parking brake on, the aircraft starts to move due to a
parking brake failure, immediately release the PRK BRK handle to restore braking
by pedals.
‐ If pushback is required, set the PRK BRK handle to OFF.
CAUTION Do not use brakes during pushback, unless required due to an emergency.
After pushback is completed, set the PRK BRK handle to ON, and inform the ground crew to allow
the towbar to be disconnected.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES
- BEFORE PUSHBACK OR START
A330/A340 FLEET PRO-NOR-SOP-07 P 4/4
FCOM 19 AUG 10
Applicable to: ALL
BEFORE START CHECKLIST below the line....................................................................COMPLETE
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - ENGINE START
A330/A340 FLEET PRO-NOR-SOP-08 P 1/6
FCOM 19 AUG 10
AUTOMATIC ENGINE START
Applicable to:
If, during the start of a cold soak engine (at around -20 °C) the ground crew reports a fuel leak from
the engine drain mast, run the engine at idle for 5 min. If the leak disappears during these 5 min,
the aircraft can be dispatched without maintenance action. If the leak is still present after 5 min,
maintenance action may be required before the flight.
ENG MODE selector ..........................................................................................................IGN START
The lower ECAM displays the ENGINE SD page.
START ENGINE 1 and 2................................................................................................... ANNOUNCE
　
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