A320ceo1

If a duct overheat is sensed in the hot air system, the amber fault light in the Hot Air switch will illuminate, and the hot air valve will close automatically.

The forward compartment has only an isolation valve switch and a temperature selector.

With the isolation SWITCH in _______, if smoke is detected in the cargo compatment, both isolation valves atomatically close, displaying a cross-line amber on ECAM.

Why would a pilot select the Pressurization Semiautomatic mode?

The EFCS will not maintain á more than VáMAX, even if the pilot holds the side stick full aft.

What is the "at rest" position for the Ailerons when the aircraft is on the ground?

After takeoff, the Normal Law - Ground Mode will blend to the Flight Mode when:

During Manual flight, the amount of side stick displacement ________.

The Flight Director will disappear if the Angle of Bank exceeds __________.

The modes available when operating with Alternate Law with Reduced Protections are: ___________.

The roll mode can operate with Alternate Law.

When operating in Abnormal Attitude Law, the Low Speed and High Speed protections are _________.

Mechanical back-up control allows mechanical input to control the___________, and the_____________.

The Crew Oxygen system provides oxygen to ______ crew masks.

The Passenger Oxygen system is installed to provide oxygen during ________________.

The DOOR/OXY CAM page displays the available pressure in the __________ bottle.

The fixed cabin oxygen system is designed to automatically open the container doors and present the oxygen masks at ___________ cabin altitude.

The continuous flow mask ________ provide protection for smoke inhalation.

What is the purpose of the MANUAL MASK ON pushbutton?

What is the purpose of the Manual Release Tool?

The white SYS ON light will illuminate____________________.

An oxygen generating canister can provide oxygen for about _______ minutes.

Where is the oxygen blow out disc that is inspected during the pre-flight inspection?

If the bottle pressure is below _______ the pressure display pulses.

If the bottle pressure is below _______ the pressure and

the CKPT OXY label display in amber.

Does the mask have to be removed from the container to perform a preflight oxygen mask test?

During Reverse Thrust operations, the _______ airflow is reversed.

The thrust levers are normally positioned into a sector detent during flight. The action of moving the Thrust Levers to a sector detent (such as Climb) will engage the _______ system.

Which of the Engine Parameters are always displayed?

The engine starters are _________ operated.

On the ground, positioning the Thrust Levers to the FLX/MCT detent without a Flex Temperature selected that is higher than the TAT, the resulting N1 limit mode will be ________.

If the Thrust Levers are positioned between detents, the thrust limit is computed to the limit of __________.

After takeoff, what pilot action normally engages the A/THR mode?

After takeoff, what indication flashes on the FMA to remind the pilot to set climb power?

The FADEC is powered by the aircraft electrical system for _________ after the aircraft is first powered.

The FADEC is powered by ______ the engine N2 RPM is above the required value.

The Fuel Used value is displayed on the CAM Engine page and also on the ECAM _______ page.

The green command arcs appears to display the difference from the current thrust value and the commanded thrust. This arc only appears when the A/THR is active.

When the aircraft is in flight, the thrust limit mode corresponds to the detent of the __________.

The engine start information displays on the ECAM Engine page _________.

The Fuel Used display for an engine is reset to zero when _______.

Which of the following are displayed on the ECAM ENGINE Page and on the CAM CRUISE Page.

A Bypass Valve is installed to provide continual oil flow in the event of a clogged Oil Filter.

Which of the following is not displayed by a pointer and a digital readout?

Using the Automatic Start for starting an engine on the ground, how many igniters will activate?

Using the Manual Start for starting an engine, how many igniters will activate?

Regardless of whether the Automatic or Manual Start procedure is used, when will the ignition automatically shut off?

For restarting an engine in flight, both igniters come on when the Mode Sel switch is moved to ________

After selection of thrust reverse, the annunciation of REV displays in _________ during the transition.

Which hydraulic system provides the operating pressure for the #1 Engine Thrust Reverse?

To deploy the reversers, the LCIU's must sense that both main gear struts are compressed, and a reverse signal from the Thrust Lever Angle (TLA) must be received from at least one _________.

What is the correct sequence to initiate the Automatic Engine Start?

The N2 displays on a gray background until the engine is_________.

During the Automatic Start, the ignition will come on at _____.

After start of the first engine, both Pack Valves remain closed _______ unless has elapsed before beginning the start of the second engine.

The Approach Idle mode is activated when the _______. This causes an increased idle speed.

The Master Switch controls the ________ shut off valve.

The Reverse Idle speed is a slightly higher idle speed than forward idle thrust.

The FRV always mixes the hot fuel from the IDG cooler with the cold fuel from the ________ pump so that the temperature of the fuel returning to the fuel tank remains below 100 C.

During the Manual Start, the Master switch is selected to ON _________.

During the start, the Start Valve closes _______.

The N2 displays on a gray background during the start until_________.

When the mode select switch is moved to the START position, the FADEC is powered, the ECAM Engine page displays, and _________.

For the Manual Start procedure, how is the Start Valve opened?

How many agent bottles are available for fire discharge to an engine?

In addition to the FIRE light shown here, what other indications will appear with a detected engine fire?

Is there any fire extinguishing for the Avionics compartment?

In the event of a fault or loss of power in a single loop, the remaining loop _______.

The AGENT pushbutton is active________________.

During an engine fire procedure, how long should a pilot wait before discharging the 2nd agent bottle?

The APU will automatically shut down if an APU Fire is detected__________________.

The APU Agent bottle will automatically discharge three seconds after an APU Fire Warning when the aircraft is _______.

Where is the red disc that indicates the APU bottle has not been discharged?

What occurs when the External APU Shutoff pushbutton is pressed?

How many agent bottles are available for fire discharge to a Cargo compartment?

After the agent has been discharged to a Cargo compartment, about how long will it be until the DISCH light comes on?

If one smoke detector is inoperative in the forward cargo compartment, can smoke be detected by the remaining detector?

When the Smoke Configuration is selected, ___________.

When smoke is detected in a lavatory, the ________ given an alert.

If a lavatory fire extinguishing bottle is discharged, _______.

What condition activates a lavatory fire extinguishing bottle?

Which panel provides control over the selection of Radio Frequency?

Which panel can be used to make Passenger Address calls?

Which panel can be used to monitor the audio or ID from a navigation radio?

With the CAPT & PURS Switch in the CAPT position, pressing a CMD button at the F/A Station will _______.

Can the Evacuation Tone be silenced from the F/A Stations?

Where is the EMER EVAC Panel in the Flight Deck?

On the ground in the AUTO mode, the recording system is active continuously after the ______.

The DFDR can store flight data for at least the last _______ hours of operation.

Where is the CVR TEST pushbutton located?

After a FIA has called the Flight Deck, the amber ATT light will flash on the ACPs until _____.

Where is the CALLS panel located in the Flight Deck?

Will the white PA "IN USE" light illuminate if a PA is being made by a Flight Attendant?

What is the purpose of the SVCE INT OVRD switch?

What action will connect the Flight Deck handset to the Cabin Interphone system?

How do you make a PA with the Handset?

What is the purpose of a Radio Management Panel (RMP)?

What is the purpose of an Audio Control Panel (ACP)?

Is a Radio Management Panel (RMP) normally used to control the Navigation Radios?

On an ACP, how many radios can be selected for transmission at one time?

What is indicated by the illuminated SEL annunciation on the RMPs?

What part of the wing can be heated by the Wing Anti-ice?

Can Wing Anti-ice operate on the ground?

What part of the engine can be heated by the Engine Anti-ice?

Can Engine Anti-ice operate on the ground?

What are the two positions of the PROBE HEAT pushbutton?

The Wing Anti-ice can be used to ______ ice from the wing leading edges.

The Wing Anti-ice valves will open ______.

The Wing Anti-ice valves require an electrical signal and pneumatic pressure to open.

When the WING or Engine Anti-ice is on, the _______ is automatically decreased.

With loss of normal electrical power, the Wing Anti-ice valves fail _______, and the Engine Anti-ice valves fail ________.

What position of the PROBE/WINDOW Heat pb, will only activate the Probe and Window heat if at least one engine is running or the aircraft is in flight.

Whenever the cargo door is ______, such as upon arrival at the gate, the hot air valve automatically closes, shutting off heat to the cargo compartment.