A320 CEO 3
The Forward compartment has only an isolation valve switch and a temperature selector.
True
False
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.
False
True
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.
Closed
Open
With the isolation SWTICH in _____, if smoke is detected in the cargo compartment, both isolation valves automatically close, displaying as cross-line amber on ECAM.
Open
Auto
Off
Why would a pilot select the Pressurization Semi-automatic mode?
When operating with one Pack.
If no FMGS data is available to the CPC’s.
How many CPC’s are installed on the aircraft?
Two
One
The position of the Outflow Valve is displayed on the ECAM ____ page.
Cruise
Cabin Press
After landing with the Pressurization System in the MANUAL mode, ___________________.
The crew must manually depressurize the aircraft
The Residual Pressure Control Unit (RPCU) will automatically depressurize the aircraft
The Cabin Vertical Speed displays on the DOOR/OXY page only when the aircraft is in _______.
In flight
On the ground
After landing with the Pressurization System in the MANUAL mode, ______________________.
The Residual Pressure Control Unit (RPCU) will automatically depressurize the aircraft
The crew must manually depressurize the aircraft
The flap/slat position indications appear on the ________.
PFD
E/WD
If a failure occurs prior to an inhibited phase, the E/WD displays the warning immediatly and will also continue to display it during the inhibited phase and until it is corrected or the crew has cleared it from ECAM.
False
True
When a primary failure is displayed on the left side of the E/WD, you will be able to view the Secondary failures on the __________.
Right side of the E/WD
Right side of the SD
After a failure of the upper DU (or if the upper DU brightness is turned off), the R/WD is displayed on the lower DU. How can a pilot display a SD page under this condition?
Turn off the brightness of the lower DU
Press and hold the desired SD page button on the ECAM control panel, or press the ND XFR pushbutton
How many onboard sorces of AC power are available?
Five
Three
Four
The Emergency Generator can power which buses?
AC Essential and DC bus 1
AC Essential and DC Essential Buses
When the APU is started, the APU Generator will automatically connect to the electrical system and cause the Engine Generators to disconnect.
True
False
Which generators are driven by an IDG?
Engine Generators
Engine Generators and the APU Generator
How many TR’s are installed in the electrical system?
Two
Three
With External Power Available, selecting the EXT PWR switch to ON will ________.
Disconnect the APU power source and apply External Power to both sides.
Disconnect the Engine generators power source and apply External Power to both sides.
The AC ESS BUS is normally powered by ________.
AC Bus 2
AC Bus 1
Which power source is required to operate the Maintenance Bus Switch?
APU Power
External Power
When the Battery Switches are selected to AUTO on a cold aircraft, the ________ is powered by the Batteries.
DC BAT BUSS and DC ESS BUS
AC ESS BUS
Before an engine is started, it is normal for the amber FAULT light in the respective Generator switch to be on.
False
True
After both engines have been started, the APU voltage and frequency information continue to display on the ECAM ELEC page until ________.
Both Engine Generators are online
The APU is shutdown
Which circuit breakers are monitored by the FWS; and which circuit breakers feed components that are monitored by the FWS?
Black; Green
Green; Black
An amber FAULT light illuminates in an IDG pushbutton if the IDG oil temperature is too high or _____________.
The oil pressure is too low.
The oil pressure is too high.
If a failure of an AC BUS occurs, the remaining DC Bus will power the DC Bus on the depowered side.
False
True, after about 5 seconds
What will cause the RAT & EMER GEN red FAULT light to illuminate?
EMER GEN not providing power with both AC BUS 1 and AC BUS 2 depowered.
A short on any AC Bus.
Which of these MAN ON pushbuttons will deploy the RAT and also activate the GCU for the Emergency Generator?
RAT MAN ON located on the Hydraulic Control Panel.
MAN ON located on the EMER ELEC PWR panel.
What is the purpose of the PTU?
To allow the Yellow system to pressurize the Green system or vice versa
To allow the Yellow system to pressurize the Blue system or vice versa
Is there ever a condition that allows hydraulic fluid to migrate from one system to another?
Yes
No
What situation will cause the RAT to automatically deploy?
Loss of an engine or an AC Main Bus
Total loss of electrical power or dual engine failure
The amber FAULT Lt in which of the pushbuttons will illuminate if the Reservoir Level in the Green or Yellow system is low?
ELEC
PTU
Under which of the following conditions will the Blue ELEC Pump NOT operate?
Selected ON, but no engines running on the ground
Selected ON, but both engines running in flight
The normal position of the Yellow ELEC Pump pushbutton for flight is _______
ON
OFF
What is the normal method the pilot will use to select a VOR station?
Entry to the Radio Nav page of the MCDU
Selection on the VOR radio control panel
If radio tuning on the MCDU is not avaliable, where can the pilot manually tume a navigation radio?
On the FCU
On the RMP
The FMGS provides autotuning of the navigation radios to provide ________ information to the aircraft systems.
Altitude
Position
What is the normal mode that displays on the GPS MONITOR page?
NAV
ACQ
An ECAM GPS 1 FAULT annunciation is inhibited during ___________.
Take off and Landing
Cruise flight
What is indicated when ”ACQ” is in the mode displayed on the GPS MONITOR page?
The GPS is attempting to acquire data from the ADIRUs
The GPS is attempting to locate sufdicient satellites for the NAV mode
What happens if one GPS fails?
The pilot must move the ATT HDG selector
The ADIRUs automatically get GPS data from the remaining GPS
How can you display the ILS information on the PFD?
Rotate the ND Nav selector to the ILS position
Press the LS pushbutton
If the ND Nav Selector is positioned to the ILS position, the ________ will display on your ND
Respective ILS radio
Opposite ILS radio
The compass signal to the DDRMI is normally provided by ADIRU 1, but can be alternately provided by ______.
ADIRU 3
ADIRU 2
If an RMP is used to tune the ILS, _____ are tuned to the selected frequency and course
ILS 1
Both ILS radios
If an RMP is used to tune the VOR, _______ is/are tuned to the selected frequency and course.
The respective VOR
Both VOR’s
Predictive Windshear Advisories are available from _______ to _______ AGL.
2300; 50’
1500; 50’
Which of these systems has priority over the Predictive Windshear Alerts?
GPWS
TCAS
None. PWS has highest priority
You have recieved a Predictive Windshear Warning alert; The windshear is detected within _____ ahead of your aircraft if you’re on the ground; or ______ ahead if you’re in flight.
3 NM; 1,5 NM
1 NM; 3 NM
Which of the Predictive Windshear Alerts will not produce an aural alert?
Caution
Advisory
In order for the TCAS system to see the aircraft, the aircraft must be within a maximum range of 30 - 100 NM, and within a maximum altitude range of _______ feet.
12 000
9 900
Full TCAS operation requires an operating _______ transponder on all associated aircraft to send and recieve the signals.
Mode S
Mode C
A ”corrective” RA requires __________.
A vertical manuever by the crew
The crew to maintain the current vertical speed
The Above (ABV) position is similar to the ALL position, but traffic is displayed if it is within 9 900’ above and _______’ below your altitude.
2700’
9 900’
TCAS Advisories are inhibited for intruders below 380’ AGL when your altitude is below ______ AGL.
2500’
1700’
Increase Descent” RA’s are inhibited below _______ AGL.
1450’
1000’
Aircraft with a Mode C transponder are equipped with TCAS.
False
True
What mode selector should be selected while operating in single engine situations?
TA only
TA/RA
All TA aural alerts are inhibited below ______ AGL.
600’ when ascending, 400’ when descending
500’
The GPWS processes data received from ________________________.
RA 1, ADIRS 1, ILS 1, FMGC 1, LGCIU 1.
RA 2, ADIRS 2, ILS 2, FMGC 2, LGCIU 2.
What is the approximate time before impact for a Look Ahead Terrain Caution?
30 to 50 seconds
40 to 60 seconds
Concerning the Terrain Clearence Floor: The EGPWS provides TCF alerts only for the destination airport as determined by the FMS.
False
True
What is the primary purpose of GPWS Mode 4 alerts?
To provide alert to protect against controlled flight into terrain
To provide alert for flight below the Glide Slope
Normal Landing Gear Extension/Retraction is provided by the _________ hydraulic system.
Yellow
Green
The Normal Brake system pressure is provided by the _________ hydraulic system.
Green
Yellow
Parking Brake operation is provided by the _______ hydraulic system.
Green
Yellow
A safety valve is installed in the system to isolate the Green system pressure from the Landing Gear when the aitspeed exceeds ________, or when the Landing Gear Lever is UP.
260 kts
180kts
When does the red down arrow appear on the Landing Gear Indicating panel?
When one or more gear are not locked down after gear extension.
When all gear are locked down after gear extension.
The Landing Gear Indicator Panel displays the red and green lights for the landing gear. The lights are operational as long as _________ is electrically powered.
LGCIU #2
LGCIU #1
A wheel Brake Temperature arc appears in amber when the temperature exceeds ________ Celcius.
200 degrees
300 degrees
Is the Autobrake system operable when the Alternate Brakes are active?
Yes
No
Does Anti-skid operate when braking is available from the Accumulator?
Yes
No
Does the Anti-skid operate with Alternate Brakes when there is a BSCU failure?
Yes
No
Approximately, how many brake applications are available when operating on Accumulator brakes?
Seven
Five
The N/W STRG DISC memo appears when the Tow Control Lever is set to byspass the Nosewheel Steering. At what point does the memo chamge color from green to amber?
After start of the first engine.
If the Tow Bypass Lever is not set for pushback when movement is sensed.
What is the maximum steering angle that can be commanded by the rudder pedals at low ground speed?
15 degrees in either direction
6 degrees in either direction
Hydraulic pressure is provided to the Nosewheel steering by the ________ system, when the nosegear doors are closed.
Yellow
Blue
Fuel that flows through the IDG cooler, is returned to the ____________.
Inner Tank of the respective wing
Outer tank of the respective wing
The Wing Tank Pumps are physically located in the ________________.
Surge Tank
Inner Tank
Outer Tank
Center Tank
When does the APU Fuel Pump operate?
First flight of the day
When the APU is running and there is no other source of fuel pressure
On approach and landing
Anytime the APU is running
From which tank(s) can the engines gravity feed?
Center Tank Only
Wing and Center Tanks
Wing Tanks only
The Center Tank Pumps are normally in the AUTO mode. In AUTO, these pumps ________ operate when the slats are extended.
Will
Will not
The FAULT light in a Fuel Pump switch indicates ______.
The pump is selected OFf
The pump is selected ON but output pressure is low
With the Center Tank pumps operatingbin the AUTO mode, the Center Tank pumps will shut down _______ the low level sensor is reached.
5 minutes after
At the moment
What is the purpose of the Recirculation System?
It provides IDG cooling through fuel flow
It keeps fuel warm
When the Center tank is providing fuel to the engines, how does the recirculation system tend to overfill the inner tanks?
The Center tank fuel moves through the transfer valves
The return fuel flows to the Wing Tanks
The _____ sensors cause the Center Tank pumps to shut off, and the ________ sensors cause the Center Tank pumps to come on again when the Inner Tank fuel is reduced by fuel burn.
FULL; UNDERFULL
UNDERFULL; LOW FUEL
What causes the Transfer Valves to open?
They automatically open when the tank Low Level sensors are dry
A Control Switch on the Overhead Panel
How long do the Transfers Valves remain open?
They remain open until the aircraft is refueled
They remain open until the Outer Tanks are empty
Which Transfer Valves are controlled by the Low Level sensor in the Left Wing Inner Tank?
One Transfer Valve in the Left Wing and One Transfer Valve in the Right Wing
Both Transfer Valves in the Left Wing
Which Spoiler panels are deployed as speedbrakes?
2, 3 and 4
1, 2, 3 and 4
What is the name of the computers that normally provide control for the Elevators and Ailerons?
ELACs
SECs
What is the name of the computers that provide back-up control for the Elevators and Ailerons?
ELACs
SECs
What is the name of the computers that provide control for the Flaps and Slats?
ELACs
SFCCs
SECs
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