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page and BLEED SD page in cold weather conditions (below approx. 10 °C)
ELEC
* EXT PWR (if ON)...........................................................................................................AS RQRD
External power may be kept on to reduce APU load, especially in hot condition.
BEFORE WALK AROUND
Applicable to: ALL
COCKPIT LIGHTS
* COCKPIT LIGHTS..........................................................................................................AS RQRD
Set STBY COMPASS sw, DOME selector, ANN LT selector, as required.
Set FLOOD LT and INTEG LT, as required.
Applicable to: ALL
F/CTL
FLAPS..................................................................................................................CHECK POSITION
Check the upper ECAM display to confirm that the FLAPS position agrees with the handle
position.
* SPEED BRAKE lever.......................................................CHECK RETRACTED and DISARMED
WARNING If flight control surface positions do not agree with the control handle positions,
check with the maintenance crew before applying hydraulic power.
Applicable to: ALL
PARKING BRAKE
* PARK BRK handle.................................................................................................................... ON
The parking brake must be on during the exterior inspection to allow the flight crew to check brake
wear indicator.
* ACCU PRESS indicator & BRAKES PRESS indicator...................................................... CHECK
‐ Check for normal indications.
The ACCU PRESS indication must be in the green band. ‐ If required use the electric pump on
blue hydraulic system to recharge the brake accumulators.
WARNING Blue hydraulic system is pressurized from blue electric pump. Get ground crew
clearance before using the electric pump.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES
- PRELIMINARY COCKPIT PREPARATION
A330/A340 FLEET PRO-NOR-SOP-04 P 7/10
FCOM 19 AUG 10
Applicable to: ALL
ALTERNATE BRAKING SYSTEM
Note: The purpose of this check is to verify, before the first flight of the day, the efficiency of the
alternate braking system (absence of “spongy pedals”).
CHOCKS.............................................................................................................. CHECK IN PLACE
PRK BRK handle.........................................................................................................................OFF
BRAKE PEDALS.....................................................................................................................PRESS
Apply maximum pressure on both pedals.
BRAKE PRESSURE (on BRAKE press indicator).................................................................CHECK
Pressure must build up without delay symmetrically on left and right sides for the same application
simultaneously applied on left and right pedals. With full pedal deflection, the pressure must be
between 2 200 PSI and 2 700 PSI.
BRAKE PEDALS................................................................................................................ RELEASE
PARK BRK handle........................................................................................................................ ON
The parking brake must be on during the exterior inspection to allow the flight crew to check brake
wear indicators.
Applicable to: ALL
PROBE/WINDOW HEAT
PROBE/WINDOW HEAT pb....................................................................................... CHECK AUTO
Applicable to: ALL
AIR COND
APU BLEED pb-sw........................................................................................................................ON
Do not use APU BLEED, if ground personnel confirms that the ground air unit is connected. Pilots
should also check the BLEED SD page to determine whether an HP ground air unit is connected
(pressure in the bleed system).
ALL WHITE lights........................................................................................................................ OFF
X-BLEED rotary selector...........................................................................................................AUTO
Cockpit and cabin temperature selectors...........................................................................AS RQRD
Full range temperature 24 ± 6 °C (75 ± 11 °F).
The temperature selection recommended for the cabin is 21.5 °C (about 10 o’clock).
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES
- PRELIMINARY COCKPIT PREPARATION
　
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