25V

On the ELEC DC SD page, check that the current charge of each battery is below 60 A, and is decreasing.

two

40

The flight crew must temporarily reduce the electrical load when only two EXT power units are available, by setting the: CAB FANS pb-sw to OFF, and COOLG pb-sw to OFF.

1 h

2s; 5min

1% lower

True

All are correct

The crew must consider the OIS inoperative and consult MEL for guidance

RMP 1 and 2 on (both RMPs); Standby RAD NAV KEY OFF; Tune communication frequencies; RELEASE/ADJUST INT RECEPTION KNOB (Both)

5 s

HP, HP

As soon as the number of passengers is entered, during FMS initialization, airflow is automatically adjusted to the actual number of passengers.

The temperature ranges between 18 °C and 30 °C. The recommended temperature selection is approximately 21.5 °C (about 10 o'clock).

If the normal filling range appears in white with an amber cross indicating that it is not computed, set to NAV any ADIRS MODE selector

The current hydraulic fluid volume (green band) in the Green hydraulic system reservoir decreases of 1.5 l per open cargo door. Therefore, the green band may be below the normal filling range (or movable index).

If the ENG oil quantity indication does not appear on the ENG SD page, press all ENG FADEC GND PWR pb-sw on the overhead maintenance panel. After the check of the ENG oil quantity, press again all ENG FADEC GND PWR pb-sw.

The left and right brake pressure should be above 3 500 PSI.

is lockwired and the pressure gauge indicator is in the green area

…stowed inside the safety locker behind F/O seat.

Check that the five gear pins are on board and stowed.

Set the LOGO LT to AUTO

Press and release the pushbutton. If the test fails, the RECORDER CVR FAULT ECAM alert triggers 5 s after the flight crew presses the CVR TEST pb.

The airspeed The barometric setting The altitude indication The attitude indications The heading

To comply with the time precision requirement (+/- 1 s UTC) for ATC datalink communication, the flight crew must either: Use the clock in GPS mode, or Use the clock in internal mode (INT), provided that the clock is not set manually and is re-synchronized with the GPS once a day.

press the ACCU REINFLATE pb to reinflate the BLG brake accumulators.

Set the LOUDSPEAKER knob to approximately 1 o'clock position.

± 20 ft between both PFDs ± 30 ft between ISIS and PFD.

30ft, Set the PROBE & WINDOW HEAT pb-sw to ON during two minutes, and Check again the difference.

The first engine is started.

it may generate the AUTO FLT A/THR OFF warning at engine start.

REGUL PR LO indication… CHECK NOT DISPLAYED

If not, revise the ZFW/ZFWCG in the FMS and compare the ECAM GWCG and the loadsheet TOCG If the difference is confirmed, request a new loadsheet using the trim tank fuel quantity displayed on the FUEL SD page. If the difference between the loadsheet TOCG and the ECAM GWCG is still more than 1 %, suspect an abnormal fuel distribution. Confirm the fuel distribution with load control and compute again the loadsheet accordingly.

ECAM GWCG is Within operational limits

AUTO GND XFR pb-sw ON

ON; The flight crew can manually stop the AGT when the ECAM CG is within the operational limits.

The flight crew should not launch the automatic ground transfer if the aircraft is moving (e.g. during towing). The AGT is inhibited as soon as at least two engines are running.

both pilots should compare the runway ident, intersection and the EO acceleration altitude of the results page from their OIS TAKEOFF application with the FMS PERF T.O page.

only consider the indications on the ECAM DOOR SD page as reliable and use these indications for dispatch assessment.

The engines start regardless of the thrust lever position. If the thrust levers are not set to IDLE, then thrust rapidly increases to the corresponding thrust lever position, causing a hazardous situation

the flight crew should not start the engines during pushback in order to avoid possible damage to the nose landing gear upon green hydraulic pressurization.

Higher tan 15KT (RR) / 25 KT (EA) ; It may be necessary to reposition the airplane into the wind

any engine can be started first. The first two engines started must be done individually. The second two can be done together.