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AUTO-UPDATE CANCEL
To cancel the auto-update function.
UPDATE CANCEL...................................................................................................... SELECT (1)
The REQ SEND function associated to the applicable arrival airport, becomes available [2]. This
makes it possible to manually-send ATIS report requests to the applicable arrival airports.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
INFORMATION SYSTEMS
A330/A340 FLEET PRO-SUP-46 P 56/58
FCOM 19 AUG 10
RECEPTION
When ATIS is received, the ATIS code and time of reception appear next to the corresponding
airport.
ARPT/TYPE.................................................................................................................SELECT (1)
Displays the text of the selected ATIS report.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
INFORMATION SYSTEMS
A330/A340 FLEET PRO-SUP-46 P 57/58
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
INFORMATION SYSTEMS
Intentionally left blank
A330/A340 FLEET PRO-SUP-46 P 58/58
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
DOORS
A330/A340 FLEET PRO-SUP-52 P 1/2
FCOM 19 AUG 10
LEAVING THE AIRCRAFT VIA AVIONIC BAY ACCESS DOOR
Applicable to: ALL
Move forward the captain seat completely and open the floor ‐ hatch to get access to the avionic
bay.
‐ Descend into the avionic bay and take a position right side of the avionic bay access door
Note: Do not try to open the access door while standing on it.
‐ Open the floor panel (1) which covers the avionics bay access door handle (2), located at the aft,
center part of the access door (coin may be needed to open the lock).
‐ To open the access door (3) lift the handle (2) and pull the door completely into the bay until it is
latched in its upper stop (LH).
‐ Remove the strap which fixes the ladder assembly against motion.
‐ Lift the lever (4), located on the right side aft of the lower rung of the aft ladder element, to unlock
the ladder assembly and swing it simultaneously towards the opening.
‐ Release the lower locking device on the right inner side of the first ladder element (5) by pulling
the orange handle forward (indicated on a placard next to the locking device). Lower the element
until it latches.
‐ Repeat with the second ladder element (locking device (6) is at the left inner side).
‐ If the ladder does not touch the ground yet the last element is lowered by pulling forward its
orange handle at the lower end on the left outer side.
‐ If the ladder touches the ground leave the aircraft via the extended ladder.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
DOORS
A330/A340 FLEET PRO-SUP-52 P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
POWER PLANT
A330/A340 FLEET PRO-SUP-70 P 1/20
FCOM 19 AUG 10
THRUST CONTROL
Applicable to:
GENERAL
The flight crew uses console-mounted levers to control engine thrust. Each lever sends electrical
signals to the FADEC of the engine it controls. The FADEC responds to the thrust lever position or
an autothrust command by setting the engine thrust.
The thrust lever quadrant is the equivalent of a thrust rating panel. For each lever it has two
detents. Moving the thrust lever to the forward stop of the quadrant always gives maximum takeoff
or go around thrust, as appropriate, and signals the AP/FD to go to takeoff or go around, as
appropriate. The FMA (Flight Mode Annunciator) in the left window of each PFD displays the
status of the thrust system to the pilot.
The engine instrument display gives a read-out of the engine thrust mode (CL, MCT, etc.) and the
appropriate engine limit. It displays the actual limit set, thrust lever position, FADEC command,
and maximum engine rating limit continually.
MANUAL THRUST CONTROL
With A/THR disconnected, thrust control between idle and maximum takeoff or go around thrust is
entirely conventional.
TLA (Thrust Lever Angle) determines the thrust demanded.
The rating limit selected by the pilot and the actual engine limit appear on the engine instrument
display.
With the thrust lever short of the CL position on the quadrant, the engine instrument display shows
CL continually, if one or more thrust levers are above CL, it shows MCT/FLEX. If one or more
thrust levers are beyond the MCT detent, it shows TOGA. With the thrust levers positioned in a
　
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