EXAM Q's Flashcards
If a normal monitor parameters goes out of its normal range, but does not reach a level to trigger an alert, what would you expect the parameters indication to do ?
To pulse green on the SD page
How long after shutdown is the FADEC still power by the electrical system?
15 min
A Warning alert is assigned to an Emergency that requires immediate action. What is the display to the flight crew?
The Master Warning flashes, a specific system Red light , CRC Warning, Title of thé alert on the Warning display with the procedure, Status page .
If the TAWS triggers one of the PULL-UP alerts, the immediate memory items are ?
A/P -Off, PITCH-PULL UP, THRUST LEVERS-TOGA, SPEED BRAKE LEVER -CHECK RETRACTED, BANK-WINGS LEVEL or ADJUST
If you push the COOLS push button switch what triggers ?
The supplemental cooling system stops operating.
The autopilot receives data from 2 sources, which are they ?
AP1 uses FMS1 and MMR1, AP2 uses FMS2 and MMR2
ECAM Displays information on which displays ?
MFD, lower part of the PFD, Engine Display, System Display and permanent Data and Warning Display
You are in flight with the FD’s off and the autopilot off, What happens on the PFD when you press the FD button ?
The FD BARS will appear and flash for 10 secs, 1FD2 will appear in the FMA and V/S +HDG or FDA+TRK will appear also appear in the FMA
What ECAM pages would you expect to see Cabin Pressure information Display on in normal conditions?
The Cruise and SD associated page
The SD Page displays Systems pages, But what other pages will it Display ?
Cruise page, Status page and Status more page, Video page, Dispatch page
What is the FADEC’s purpose?
Manage Engine power, Engine protection, Engine fuel flow, and Engine ignition and start
The BLUE color emphasizes what specific situation?
- FMS entry Field Fullfilled
- FCU Selection
- Limitation
- Checklist Item to be completed
- Titles of checklists not completed
- Temporary system Status
When the Autopilot is in Protection Mode, what would you expect to see on the PFD FMA ?
An Amber caution message stating AP in PROT and a flashing Amber Box around the ALT FMA.
What NORMAL BUSBARS are NOT displayed on the ELEC SD pages ?
AC ETOPS 1/2 And HOT 1/2
Up until what point does the CRUISE page remain the Default Displayed Page ?
Landing Gear Extension
The different air sources of the bleed system are !
The APU
THE ENGINES
THE HP GROUND CARTS
The Bleed Air system supplies air to the Fuel Tank Inerting System ( FTIS) ?
True or False ?
True
The Bleed Air System supplies air to ?
The engine start system The air conditioning system The cabin pressurization System The Wing anti-ice System The Engine anti-ice System The Fuel Tank Inerting System
The APU can supply Bleed Air for pressurization and air conditioning in flight up to 22,500 ft , with 2packs running !
True of False ?
True
The APU can supply Bleed Air for Engine start in flight up to 25,000 ft .
True or False
True
In Normal operation, the crossbleed valve interconnects or isolates the left and the right air system if ?
XBLEED selector is in AUTO
The Temperature of the FWD cargo compartment is regulated with ?
Air from the cabin , the mixer unit and the trim-air system
The temperature of the BULK cargo compartment is regulated with air from the cabin and from an electrical heater .
True or False
True
The AFT cargo compartment is ventilated with cabin air.
True or False
True
When the Ditching PB sw is pressed ?
It closes all valves below the floatation line
The aircraft is in flight, and you have a Engine Bleed leak, the engine bleed valve is closed, will the crossbleed valve automatically open .
True or False
True
Battery , engine generator or external power can supply electrical power to the APU .
True or False
True
The Avionics network is composed of ?
Two independent and redundant networks
The failure of a single or multiple switches on only one network?
Has no functional effect
In the case of a single CRDC failure?
There is no operational effect
The two navigation keys on the Cursor Control Device ( CCD )
Are used for ?
Their onside ND and OIS , the MFDs and with the mailbox as well
Each engine driven generator provides?
AC power at a variable frequency
The Four Auto Transformer Inits ( ATUs ) convert :
The AC 230 V power into AC 115 V
And
The AC 115 V power from EXT Power Units into 230 V power
The electrical system has 2 Electrical Power Distribution Centers: EPDC side 1 and EPDC side 2 . For each side, the emergency network is composed of :
1AC EMER 230 V busbar
1AC EMER 115 V busbar
1DC EMER 28V busbar
In case of a generator overload, the Electrical Load Management Function ( ELMF ) automatically sheds the sheds the non essential commercial electrical loads .
True or False
True
In case of generators overload and not sufficient ELMF shedding , the Electrical Network Management Function
( ENMF ) sheds groups of loads
True or False
True
The Electrical Network Management Function ( ENMF )
Controls the automatic reconfiguration of the Network.
True or False
True
The two engine-driven generators are lost on the same side. The APU GEN replaces both generators .
True or False
True
The engines are running, the FADEC is powered by its own alternator.
True or False
True
The ignition system has two independent igniters ( A and B ) .
On ground , during engine start , the igniter AB indication displayed on the ENGINE SD page indicates:
A Manual engine start sequence
Each thrust rating mode has a thrust limit value by default. The thrust rating modes possibly displayed on the Engine Display are TOGA, Dxx, FLEX, CLB, DCLB, MCT, As well as ?
GA SOFT
The thrust reversera are actuated by?
Electrical power
The FADEC detects an inadvertent deployment of the Thrust Reversers . The FADEC automatically?
Limits the related engine thrust to idle
