330 T Flashcards
If the BSCU fails, most likely a BRAKES SYS 1(2) FAULT may occur
The crew will be notfied with an ECAM message
The APU bleed valve automatically closed by the ECB above …..feet climbing
25000
If there is an APU fire in flight, the APU
must be shutdown and the agent manually discharged
Although no busses are unpowered, illumination of emergency exit light in the cabin is desired. Which of the following answers is correct?
EMER lights exit signs and the escape path markings will illuminate if the cockpit EMER EXIT LT switch is ON
EMER lights exit signs and the floor path markings will illuminate if the guarded EMER EXIT LT pb on the flight attendant CIDS panel is selected on
The fire extinguishing system for the cargo compartment discharges to either the FWD cargo or AFT&BULK cargo compartments depending on whether
The FWD or AFT agent PB is pressed
What does two amber lines across the last two digits of the fuel quantity mean?
The fuel quantity indication is inaccurate
The pneumatic system supplies high pressure air for
- Hydraulic reservoir pressurization and pack bay ventilation turbofan actuation
- Wing anti ice and water pressurization
- Air conditoning and eng starting
When can managed vertical navigation be engaged
Only after managed lateral navigation has been engaged
The audio managment system includes how many audio control panels
3
The APU is supplying the elec system. What is the order of priority for the different generators?
Engines, External Power, APU
When both ENG1 and 2 pushbuttons are turned ON each engine nacelle is anti-iced by
Independent bleed air source from HP compressors
The cabin pressure controllers receive signals from
Pack flow control valve and LGCIU, ADIRS and Engine Interface Unit, FMGC and Proximity Switch Control Unit
In the event of low pressure, heavy load users are isolated to give priority to
Rudders elevators ailerons spoilers and braking
In the event of low hydraulic pressure the priority valve and pressure maintaining valve give priortiy to primary flight controls and brakes. The pilots:
can neither control nor monitor the priority valve (automaic operation)
How many HP ground units can be connected to the crossbleed duct?
One or two
What happens when pressure and temperature are not sufficient to supply the corresponding engine bleed valve (low engine speed)
HP valve opens, IP stage remains open
Cabin interphone system permits you to speak to
The cabin attendants
What is required for the FADEC to compute a reduced thrust setting
A flex temp must be entered on the TakeOFF PERF page on the MCDU
With nobody in the cockpit if you have an APU fire which statement is correct
On the ground an APU EMER shutdown automatically occurs and the APU fire bottle will be discharged
How are the FMAs displayed on the PFD
There are 5 columns and 3 rows
At what power levels does window heat operate when airborne?
Normal power while inflight
Autobrakes if selected will be only activated by
The ground spoiler extension command
If a flight attendant opens the door with the escape slide armed
A white warning light warns that the slide is armed
During engine start up when is the BLUE hydraulic sys pressurized
Automatically after first engine start (ENG1)
Ground dependent position determining systems such as VOR DME or ILS
Cross check and refine the FMGS positions computed by independent systems such as ADIRS
Each passenger door has one CABIN Pressure warning light that
Warns of residual pressure in the cabin
What are the AP functions
Acquisition and tracking of a flight path
Stabilisation of the aircraft around its centre of gravity
Automatic landing and go around
The fault light for the T.Tank.Mode pb switch on the fuel control panel comes on amber when
Excess aft CG has been detected
FCMC is unable to carry out the forward transfer
FUEL LO Temp warning is triggered
Hot air from the pneumatic system provides wing anti ice to
The four outboard slats
During normal flight, the avionics ventilation system controls the temperature by
Blowing air through the underfloor extract valve
Extract air from the different panels and equipment racks
Using cabin fans recirculated air from the cabin
Alpha floor protection is avbl
From liftoff and down to 100ft radio altitude in landing configuration
How is it determined that the cockpit sliding window is closed and locked
The red coloured indicator on the top of the handle should completely flush and the red colours not be visible
Automatic transfer from the outer tanks to the inner tanks occurs when the center and trim tank have been emptied and either inner tank reaches ……kg
3500kg 7700lbs
Automatic control of CG
begins when climbing through FL255
is terminated when descending through FL245
is terminated when FMGC time to destination is below 35min
When the door arming lever is in the ARM position opening the door from the outside will
Disarm the door
The electric standby horizon ISIS normally draws current from the DC ESS bus. In case of total electric failure the indication remains usuable for ….minutes
Normal function in ELEC EMER config
What causes a DU to display a black screen with a white diagonal line
DMC failure
Engine fire detection loops are installed in the
Pylone, nacelle and engine core sections
For engine start HP air supplied from the ground air source
is not regulated
How does the FMGC derive Vapp
Vapp=Vls +1/3 surface headwind component or VLS+5kts whichever is highest
The fire ext sys for the cargo compartmend discharges through either the …. in the FWD compartment or through …in the AFT&Bulk cargo compartment
Two nozzles / one nozzle each
How many thrust lever positions are there, and how are they labeled?
4 TL positions - TOGA FLX/MCT CL IDLE
Which statement is correct regarding the illumination of the amber BULK ISOL VALVE fault light?
Either the inet or outlet isol valve is not in the selected position
The APU master SW Fault light will illuminate
When an automatic shutdown of the APU occurs
You want to open the cabin door whilst lifting the control handle the white light illuminates. What does that mean
The slide is still armed
What are the correct positions for the PFD and ND
PFD should be outboard and the ND should be inboard
How longs does an alignment take
app 10´
With the EMER EXIT LT selector in the ARM pos if partial loss of the normal AC power supply
The overhead emergency lights will illuminate automatically
The two center tank transfer pumps transfer fuel from the center tank to the ….tanks
inner
The APU generator has priority over ….for AC Bus2
External Power B
What is the signification of an amber RAT indicator during flight phases 1 and 2 ECAM HYD page
Pressure for stowing RAT has been applied or the RAT pump is not avbl
Both independent cabin px controllers receive signals from
LGCIU ADIRS FMGEC PSCU EIU and flow control valves
If the thrust levers are set IDLE detent is Alpha floor protection still avbl?
Yes TL pos is disregarded
There are …. HP ground air supply connector located on the lower center fuselage
2
Opening a passenger door from the outside disarms the door and escape slides
True
How can you get mechanics attention when he is outside the aircraft
Use the MECH pb on the CALLS panel which sounds an external horn
What is required to arm the Autobrakes?
Green hydraulic pressure avbl, anti skid, no failures in the braking system
Illumination of the SEL indicator on a Radio Managment Panel indicates
A transceiver normally asociated with one RMP is tuned by another
The override switch for the service interphone switch is located on the … and is used for maintenance purposes only
overhead panel
The green hydraulic circuit drives an emergency generator that automatically supplies emergency AC power to the aircraft electrical system in case of main generators loss
True
INFLIGHT a yellow IR fault light is teady ON. What does that mean?
The respective IR is lost
The APU air intake and an electrically operated flap allow air to reach the compressor inlet
True
The APU is fed from the engine 1 collector in the left inner tank through the APU FWD pump and the APU isol valve when
On Ground after two minutes when the trim tank is not refueled
Which situation will automatically illuminate the escape path lighting
The loss of power to the DC ESS Bus and the loss of normal electrical power
Which one of the following statements is true
When the engine anti-ice is operating continous ignition is automatically activated
While operating on Emergency Electrical Power with the landing gear lowered which of the following control laws is in effect?
Direct
TAT probes are heated on the ground
False
Which of the following have automatic fire extinguishing systems
APU and lavatory waste bins
You enter the dark cockpi what action is necessary before checking the main battery voltages
You have to verify both batteries are off
After the engine shutdown you observe a pulsing STS message What does that mean
It is a remainder that the status page holds a maintenance message
During a routine flight which of the following would result after the loss of GEN2 and the subsequent start of the APU
ENG GEN1 continues to power AC Bus1 and downstream systems. The APU powers AC Bus 2 and downstream systems…
Air bleed from the engines is
cooled by air to air heat exchanger using air bleed from engine fan
How many FADEC are installed
2 - 1 per eng
If the VHF3 transmisison key illuminated amber showing the word CALL
indicates a SELCAL
Automatic cranking is provided
by the FADEC following an automatic start abort
What does HORN shutoff on the EVAC panel do
Silences horn in the cockpit
When the TL are moved to the TO position the FMGS updates its position at TO using
The NAV databse and the TO RWY entered into the MCDU by the pilot
The …. allows the pilot to select on the ECAM either warning and caution messages or system and system status messages displayed
ECAM control panel
Wht happens to the cockpit door with electrical power failure
it automatically unlocks
You are about to TO but no FLEX is inserted. Can you still take off?
Yes only using TOGA
What does the AMBER level indicate on the HYD QTY indic?
Warning level
With the engines off if the AVAIL LT is lilluminated on both the APU start pb and the EXT PWR pb what is the active source of ELEC pwr for the AC busses?
APU
APU bleed air supplies the pneumatic system if the APU speed is above ..
95%
After extending the RAT is it possible to check its position and status
Yes select ECAM HYD page
With reference to the PROBE WINDOW heat pb in normal position AUTO which of the following is true
Window heating comes on automatically after first engine start
What does the Low Accuracy message mean
The estimated position uncertainty EPU exceeds the RNP
What does the LDG GEAR GRVYT EXTN selector handle initiate when selected DOWN
Close the HYD cutoff valve, disengage doors and gear unlocks
What is the function of APU GEN pb located on the OVHD CTRL panel
When selected to OFF the APU generator field is de-energized
What does the AMBER speed brakes mean on the lower ECAM
Speed brakes are extened and eng are not idle
After a single DMC failure how could a crew recover the DU ?
Rotate the EIS DMC switch on the switching panel to replace the failed DMC with DMC3
Which hyd system supply presure to the landing gear system
Green
When is the SRS active
At TO when TOGA or FLX power is set
SRS is displayed on the FMA and provides guidance up to the acc altitude
During GA after the TL are placed to the TOGA position up to ACC ALT
If battery voltage is below minimum how do you charge them
I have to check tht the BAT pb are on and switch the EXT power on
The landing gear consists of
two inb retracting main gears a forward retrating nose gear
When the APU fire pb is released out an elec signal is sent that
Shuts down the APU and silences the CRC Arms the APU ext squib closes LP fuel valve shuts off apu fuel pumps closes the apu bleed valve and deactivates apu generator
The pack flow control valve are pneumatically operated and electrically controled. They close automatically in case of
Pack overheating, operation of the fire or ditching pb
insufficent upstream air pressure
engine starting and any unclosed doors at eng start
While flying the airplane with A7THR active, the speed know is pulled and turned to a selected speed that happens to be slower than Alpha Prot. What speed will the aircraft slow to
VLS
What are the different types of Flight guidance
Managed and selected
