mixed subjects cbt questions Flashcards
Q1-4 - Lighting fam // Q5-8 - Communications // Q9-21 - Elec system // Q22-26 - Emer equipment // Q27-34 - Fire protection // Q35-38 - APU // Q39-47 - Flight Instruments // Q48-55 - Air conditioning // Q56-58 - Fuel // Q59-65 - Hydraulics // Q66 - Ice and Rain protection // Q67-78 - Landing Gear // Q79-86 - Flight Controls // Q87-112 - Autoflight // Q113 - Bleed Air // Q114-131 - Warning Systems // Q132-164 - Navigation & FMS
When the wing landing lights are on, what controls their intensity?
Landing gear lever position
When are the seatbelt signs extinguished? (Seatbelts Auto)
Gear and Flaps selected up
When are the seatbelt signs illuminated? (Seatbelts Auto)
Flaps selected down
When are the “NO SMOKING” signs illuminated?
Gear selected down
Which radio receiver is being monitored?
Left VHF only
Which Navigation receiver is being monitored?
Right ILS receiver
What HF radio and mode have been selected?
Left HF AM
Normally, the right Radio Tuning Panel will have what radios selected?
Right VHF and Right HF
What does this condition indicate?
Generator Control Breaker 2 is open
What condition is indicated?
Bus Tie Breaker 2 is open
What will result if APU Generator 1 fails?
The SSB will close and power the entire synchronous bus
What does this indicate?
Left Utility Busses are not powered
Which is indicated?
Generator 3 drive has low oil pressure or high oil pressure
What is indicated?
At least 1 ELCU on the right side has disconnected its bus due to a fault
With no AC power on the airplane and the battery switch ON, what is powered?
Main Bus Battery and APU Battery Bus
What source normally powers the Main Battery Bus and APU Bus?
DC Bus 3
Which bus normally powers the Main Standby Bus?
AC Bus 3
With no AC Power sources connected, what source provides power to the Main Standby Bus?
Main Battery
Which bus cannot provide power to the Captains or First Officers Transfer Busses?
AC Bus 4
When is the Ground Handling Bus powered?
When external power is available
When is the Main deck cargo handling bus powered?
When either external power 2 or APU generator 2 is available
What is the proper way to remove a flight deck oxygen mask from stowage?
Squeeze the red release levers with thumb and forefinger
What is the condition of the flight deck oxygen at this station?
Available to the regulator
How can you restore oxygen flow to the mask/regulator?
Open the left door on the stowage box
When does the supernumerary oxygen flow control valve open?
Cabin altitude reaches approximately fourteen thousand feet
The Armed position of the Emergency switch allows automatic illumination of emergency lights when?
DC power fails or is turned off
Pulling the APU Fire Switch will:
Arm the discharge squib and shut down the APU
What should you do if the APU Fire Switch cannot be pulled during an APU fire?
Push the fire override release while pulling the switch
When is this message no longer displayed?
When the fire condition no longer exists
What do these messages indicate?
Bottle A has been discharged and the fire condition still exists
Does engine 3 have fire extinguishing available if two bottles are discharged to exthinguish a fire on engine 4?
NO
Where will the cargo fire extinguishers discharge?
FWD compartment
In what order will the bottles discharge?
A and B immediately bottles, C and D after brief delay
What is beeing tested?
The Engine Fire/Overheat detection systems and The Cargo and APU Fire detection systems
What is needed to start the APU?
APU Battery and Main Battery
Which of the following correctly describes the START position of the APU Selector?
Initiates an automatic APU start sequence
Momentary position, springg-loaded to ON
If securing the airplane:
How much time should be allowed for the APU to shutdown before turning the battery switch off?
2 minutes
An APU fault results in:
APU shuts down immediately
What is the current vertical velocity?
Descent at 700 feet per minute
What is the current heading?
120° Magnetic
What can be displayed in the lower corners of the ND?
VOR or ADF information
What is the current Ground Speed?
453 kts
What is the active waypoint? A,B or C?
B
What is the active waypoint?
GRH
What is the current Groundspeed?
338 kts
The EIU source selector selects the EIU for the:
PFD and ND Displays
What happens if the “B” controller fails?
Pack controller “A” controls the pack
What does TRIM AIR do?
Heats conditioned air to satisfy zone temperature requirements
What does the RESET switch on the Cabin Temperature Panel do?
Cancels all adjustments in all zones it affects
If the active cabin altitude controller fails..
Control of the outflow valves switches automatically to the other controller, regardless of the selector position
To set Landing Altitude when the EICAS landing altitude display is in AUTO:
Push Landing Altitude Switch and rotate Landing Altitude Control
What is indicated?
The left outflow valve is operating in Manual and the right outflow valve is operating in Automatic
on the ground
running an engine on each wing
The system is manually reconfigured for flight
What is indicated?
Aft Cargo Heat is OFF
and
Aft Cargo Heat has exceeded normal Limits
What is indicated?
The pump output pressure is low
Which fuel pumps are supplying fuel to engine number one when center wing tanks are empty
Main Tank Two Override / Jettison pumps
Prior to takeoff with fuel in all tanks and the flaps in the takeoff position which fuel tank will supply fuel to engine number four?
Center Wing Tank
Which hydraulic system is used by the center autopilot?
System One
What happens when an Engine Fire Switch is pulled? (Hydraulics)
The Hydraulic fluid shutoff valve closes and the engine pump depressurizes
When will the demand pumps operate?
To supplement the associated engine pump hydraulic pressure
With the airplane on the ground, which pump is supplying System 4 hydraulic pressure?
The electric auxiliary pump
What airplane systems are lost?
Nose and body gear steering/center autopilot
What conditions cause the system fault lights to illuminate?
Low system pressure, low fluid quantity, excessive fluid temperature
Which hydraulic system requires maintenance action prior to departure?
System 2