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�� If entry is authorized by the flight crew:
‐ The flight crew unlocks the door via the COCKPIT DOOR toggle sw (UNLOCK position).
‐ The keypad’s green light comes on steady, and indicates that the door is unlocked.
CABIN CREW...........................................................................................PUSH DOOR TO OPEN
�� If there is no reaction from the flight crew:
CABIN CREW SECOND ACCESS.......................................................... REQUEST ON KEYPAD
Repeat the above procedure.
�� If there is no reaction from the flight crew, after a second request:
CABIN CREW................................................................................................CALL THE COCKPIT
To establish contact with the flight crew and request access to the cockpit.
�� If there is no reaction from the flight crew, after a cabin crew interphone call:
CABIN CREW.................................................................................................................................
...............................................APPLY THE FOLLOWING EMERGENCY ACCESS PROCEDURE
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
EQUIPMENT
A330/A340 FLEET PRO-SUP-25 P 5/6
FCOM 19 AUG 10
EMERGENCY ENTRY CODE......................................................................ENTER and PRESS #
The emergency entry code is an Operator-defined figure between 2 and 7 seven digits. A buzzer
will sound continuously in the cockpit and the keypad’s green light flashes. After a preselected
time between 15 and 120 s, the keypad’s green light comes on steady, and the cabin crew can
then push the door open.
CABIN CREW...........................................................................................PUSH DOOR TO OPEN
The cockpit door unlocks for 5 s.
The buzzer stops and indicates that the door is unlocked.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
EQUIPMENT
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A330/A340 FLEET PRO-SUP-25 P 6/6
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
FLIGHT CONTROLS (FLYING CONDITIONS) - GENERAL
A330/A340 FLEET PRO-SUP-27-10 P 1/2
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
The fly-by-wire system has been designed and certificated to make the new generation of aircraft
more cost effective and safer and smoother to fly or ride in than a conventional aircraft.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
FLIGHT CONTROLS (FLYING CONDITIONS) - GENERAL
Intentionally left blank
A330/A340 FLEET PRO-SUP-27-10 P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
FLIGHT CONTROLS (FLYING CONDITIONS) - NORMAL OPERATIONS
A330/A340 FLEET PRO-SUP-27-20 P 1/6
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
The pilot uses the sidestick to fly the aircraft in pitch and roll (and indirectly, through turn
coordination, in yaw).
The computers interpret the pilot's inputs and move the control surfaces as necessary.
However, regardless of the pilot's inputs the computers will prevent :
‐ excessive maneuvering
‐ loss of control leading to excursions outside the safe flight envelope.
AIRCRAFT ON THE GROUND
Applicable to: ALL
On the ground the sidesticks have full authority over the controls in pitch and roll.
With the aircraft in the normal configuration and engines running on the ground :
‐ when the wheel brakes are released, the aircraft usually rolls with no added thrust,
‐ nose wheel steering is “fly by wire”, with no mechanical connection between the nose wheel and
the steering tiller. The control forces are light : the flight crew should be careful to move the tiller
gently to avoid unnecessary high-rate turns.
The aircraft can make very tight turns, but the flight crew should resist any tendency to overcontrol.
When making tight turns at low ground speed, the crew should hold the selected tiller position, even
if the turn radius is shorter than intended, so as to maintain a smooth turn.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
FLIGHT CONTROLS (FLYING CONDITIONS) - NORMAL OPERATIONS
A330/A340 FLEET PRO-SUP-27-20 P 2/6
FCOM 19 AUG 10
(1) The PFD includes a symbol that is the sum of sidestick positions given to the computers. It
permits the PNF to check that the PF is making an appropriate control input during takeoff roll.
(2) Small limit marks indicate the limits of stick travel (± 16 ° in pitch, ± 20 ° in roll).
　
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