A 320 Sys Pneumatic And Communications

Has priority over engine bleed air .

Will supply bleed air only if the ENGINE BLEED pb´s are selected OFF.

Will supply bleed air only if the X BLEED selector is selected OPEN

Only supply bleed air to the left .

Supply pneumatic air to both sides of the aircraft because the pneumatic crossbleed valva automatically opens .

Will supply bleed air only to  the left side unless the X BLEED selector is selected OPEN.

Engine intermediate pressure , APU

Crossbleed

Engine ,APU crossbleed .

Detection loops associated with BMC Nr 1

Detection  loops associated with BMC Nr 2

The APU BMC

All valves that could supply pneumatic air to the area of the bleed leak will automatically close .

The crew must isolate the affected leak.

All pneumatic valves close automatically.

The remaining BMC  will automatically assume most of the falled BMC ´s functions.

All systems associated with the falled BMC also fail.

The associated bleed valves close 

Remain in it´s current position.

Assume the closed position.

Assume the open position.

The crew must observe minimun N1 limits

Additional pneumatic air will be requested air will be requested by the BMC to the FADECs or the APU 

A  and B are corret

The valve position differs from that of the push button.

The X BLEED selector is selected to SHUT

The X BLEED selector is selected to OPEN

The wing anti ice on the associated side will be lost , and the engine anti ice on the associated side will continue to function.

The wing and engine anti ice on the associated side will be lost.

Only the engine anti ice on the associated side will be lost.

The white SEL light will be illuminated on both ARMP´s .This is a normal occurrence inflight.

The white SEL light is illuminated on the side RMP

The white SEL light is illuminated on the offside RMP

The NAV key must be selected.

Tune the new frequency on the offside RMP.

Select the appropriate VHF communication radio transmission key tune using the rotary selector , press the transfer key .

Manual tuning via the MCDU RAD NAV page is still possible.

Manual tuning via the MCDU RAD NAV page is always possible.

FMGC auto tuning is inhibited .

RMP´s 1 and 2 and ACP´s 1 and 2 are both operative .

RMP´s and ACP´s 1 and 2 are operative .

RMP 1  and  ACP 1 are operative.

ACP INT/ RAD switch selected to INT, INT reception knob on , loud speaker up.

INT transmission key to INT reception knob on , use the side stick push to talk when soeaking loud speaker volume up.

Both A and B

Select the transmission key push button labeled CAB and the audio selector labaled CAB.

Select the transmission key push push button labeled INT audio selector.

Select the INT / RAD  selector to INT audio selector on.

To alert the aft flight attendants of a routine need to speak to them.

To alert teh lead flight attendant to cook your crew meal.

To alert all flight attendants of a pending urgent need to speak to them.

Usingthe ACP CAB pb.

Using an overhead FWD or AFT call push button.

Selecting the AATND ADV pb on.

Depress and hold the PA transmission key push button .

Use the pedestal mounted handset.

Both A and B are correct.

An ACARS MESSAGE IS WAITING

Indicate a SELCALL

The lead flight attendant is callig

PA

CAB

VHF 3

VHF 1 and 2

VHF  2 and 3

VHF 1 and 3

Is automatically energized when the parking brake is set .

Is always active.

Is automatically energized after the first engine star or five minutes after AC electrical power is applied to the aircraft.

ACARS may be accessed only through the first officer MCDU

ACARS may be accessed only through the captains MCDU

ACARS may be accessed through both the first officer´s and captain´s MCDU´s