Systems question Quiz using the CBT unit tests
2000NM
1800NM
1200NM
2100NM
30000FT
41000FT
39000FT
31000FT
DC power provide Emergency lighting
AC power provide Emergency Lighting
AC and DC power provide Emergency Lighting
Emergency lighting is not fitted
Nosetip
Tail
Wingtip
Nosewheel
10000FT
12000FT
14000FT
15000FT
1
2
3
Nil
13800Lbs
13500Lbs
1400Lbs
14200Lbs
On center pedestal near the screen
On the right hand glare shield light control panel
On the left hand glare shield light control panel
On both glare shield control panels
19m/60ft
17m/54ft 8in
16m/50ft 6in
18m/57ft
29.9m/98ft 1in
25m/82ft 1in
Twice 9.67m/32ft
26m/85ft 4in
10400ft
9700ft
12400ft
14000ft
Can only be controlled using the respective knob on the flight attendant control panel
Can only be controlled using the PAX/CABIN selector knob in the cockpit
Can be transferred from the cockpit control panel to the flight attendant control panel
Is set by an automatic temperature sensor behind the cabin wall paneling
Will depressurize the cabin to a max of 12400ft cabin altitude, and deactivates the ECS pack
Will depressurize the cabin to a maximum of 12000ft cabin altitude, and deactivates the recirculation fans
Will depressurize the cabin to a max of 12400ft cabin Altitude, and deactivates the recirculation fans and the ECS packs
Will depressurize the cabin to a maximum of 10000ft cabin alt
75% fresh air and 25% recirculation air
52% fresh air and 48% recirculation
40% fresh air and 60% recirculation air
52% recirculation air and 48% fresh air
If Pack 1 is commanded/failed OFF, and the altitude is less than 25000FT
If Pacl 2 is commanded/failed OFF, and the altitude is less than 20000FT
If Pack 1 and Pack 2 are commanded/failed OFF, and the altitude is less than 25000FT
If Pack 1 and Pack 2 are commanded/failed OFF and the altitude is more than 25000FT
The Conditioned air Check Valve
The Trim Control Valve
The Flow Control Valve
The fan air modulation valve
8.3 PSID
7.8 PSID
7.9 PSID
8.7 PSID
Takeoff, climb, cruise, descent, land, and abort
Takeoff, climb, cruise, descent, approach, and abort
Ground, taxi, takeoff, climb, cruise, descent, and abort
Taxi, takeoff, climb, cruise, descent, and land
7.7 PSID
8.4 PSID
8.6 PSID
7.9 PSID
One cabin pressure controller, one cabin outflow valve, one negative relief valve, one positive pressure relief valve and one static port
Two cabin pressure controllers, one cabin outflow valve, two positive pressure relief valves and two static ports
Two cabin pressure controllers, one cabin outflow valve, one negative relief valve and one static port
One cabin pressure controller, one cabin outflow valve, one negative relief valve, two positive relief valves and one static port
Electrics and conditioning air
Electrics only
Conditioning air only
No services are available
APU to stop after 2 minute cool down period
APU to stop immediately
A red bar to appear in the button
The fire extinguisher to be armed
Overspeed, FADEC, critical fault
APU fire, EGT over temp, sensor failure
APU high Oil temp, APU low oil pressure
All of the Above
20000ft
25000FT
30000FT
33000FT
33000FT
30000FT
15000FT
25000FT
Manual trim or quick disc switches activated, column shakers are activated
The fly by wire system in direct mode, aileron and elevator system disconnects
A column and control wheel force monitor sensor trips
All of the above
GS, Flare, NLOW
LNAV, LOC
FLCH, ASEL, ALT
PTH, VGP, VAPP
Lateral and Vertical Guidance control
AFCS management Control
Two independent A and B channels
All of the above
Activates the Holding Altitude
Selects a new altitude
Provides the selected ALT in meters to be displayed on the PFD
De-activates the Holding Altitude
The airplane maintains the new ALT requested
Lateral control returns to the previous selected lateral control mode
The auto pilot disconnects
Primary servos re-engage
No
Yes
Yes by cycling the IDG push button
Yes, but is not allowed due to short-circuit in generator line
The generator is de-energized and the line contractor is closed
The generator is energized and the line contractor is closed
The generator is energized and the line contractor is open
The generator is de-energized and the line contractor is open
There is a failure in the gourd power unit
The external power is connected and all quality requirements are satisfied
The AC external power is powering the aircraft systems
The DC external power is connected and all parameters correct
The APU generator
The other engine generator
The RAT Genereator
The inverter via AC STBY BUS
After the loss of one IDG
After the loss of two IDG
When the aircraft is powered by batteries only
When the RAT is operating
4 air driven actuators
2 air driven actuators
2 hydraulic actuators
2 electrical actuators
One on ground and two in flight
One on ground and one in flight
Two at all times
Two on ground and one in flight
A mechanical link to the throttle lever
The FADEC
An electrical link direct to the throttle lever
The FMU is self controlled
Low bypass twin spool turbofan
Low bypass turbojet
High bypass two spool turbofan
High bypass triple spool turbofan
The pilot opens and closes the Starter Control Valve manually
The FADEC opens and closes the Starter Control Valve automatically
The pilot opens the Starter Control Valve and the FADEC closes it
The FADEC opens the Starter Control Valve and the Pilot closes it
Test the engine and APU fire detection system
Test the engine, the fire and the lavatory fire detection system
Test the engine and APU fire detection systems as well as the cargo smoke detection system
An alarm will sound and the red alarm indicator will illuminate
An EICAS warning LAV SMOKE will be displayed in the cockpit
The flashing amber lights on both the attendant light indicator panels will be activated
All statements are correct
Shutoff the fuel system, the hydraulic fluids and the bleed air system of the respective engine
Discharge the fire extinguisher agent into the respective engine
Both of the above statements are correct
The APU will shut down immediatly
The APU will shutdown after 10 seconds, if there is no command shut down through the APU emergency stop switch
The APU will continue to run until the APU emergency stop switch is pressed
Activated automatically into the waste bin when a lavatory fire is detected by the lavatory smoke detector
Activated automatically when a certain temperature has been reached
Activated manually from the cockpit or the flight attendant panel
Trim commands from the Backup trim, Pilot trim, Co-pilot trim and PCM trim inputs
Trim commands from the control columns only
Trim commands from the autopilot only
Elevator position commands via the FCM
Both surfaces move together
Flaps extend first, while slats retract first
Slats extend first, while flaps retract first
Slats extend and retract first
In normal mode only, as it is computed in the FCM unit
In direct and normal mode, as it is computed in the P-ACE unit
Only when the autopilot is engaged, as it is computed in the AFCS
Only in the case of an engine failure
In an active/standby configuration
In an active/active configuration
In a control/monitor configuration
In standby configuration only
Left outboard
Left and right outboard
Right outboard
Left and right inboard
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