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A-350 > EXAM Q's > Flashcards

EXAM Q's Flashcards

1
Q

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 ?

A

To pulse green on the SD page

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2
Q

How long after shutdown is the FADEC still power by the electrical system?

A

15 min

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3
Q

A Warning alert is assigned to an Emergency that requires immediate action. What is the display to the flight crew?

A

The Master Warning flashes, a specific system Red light , CRC Warning, Title of thé alert on the Warning display with the procedure, Status page .

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4
Q

If the TAWS triggers one of the PULL-UP alerts, the immediate memory items are ?

A

A/P -Off, PITCH-PULL UP, THRUST LEVERS-TOGA, SPEED BRAKE LEVER -CHECK RETRACTED, BANK-WINGS LEVEL or ADJUST

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5
Q

If you push the COOLS push button switch what triggers ?

A

The supplemental cooling system stops operating.

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6
Q

The autopilot receives data from 2 sources, which are they ?

A

AP1 uses FMS1 and MMR1, AP2 uses FMS2 and MMR2

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7
Q

ECAM Displays information on which displays ?

A

MFD, lower part of the PFD, Engine Display, System Display and permanent Data and Warning Display

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8
Q

You are in flight with the FD’s off and the autopilot off, What happens on the PFD when you press the FD button ?

A

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

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9
Q

What ECAM pages would you expect to see Cabin Pressure information Display on in normal conditions?

A

The Cruise and SD associated page

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10
Q

The SD Page displays Systems pages, But what other pages will it Display ?

A

Cruise page, Status page and Status more page, Video page, Dispatch page

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11
Q

What is the FADEC’s purpose?

A

Manage Engine power, Engine protection, Engine fuel flow, and Engine ignition and start

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12
Q

The BLUE color emphasizes what specific situation?

A
  1. FMS entry Field Fullfilled
  2. FCU Selection
  3. Limitation
  4. Checklist Item to be completed
  5. Titles of checklists not completed
  6. Temporary system Status
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13
Q

When the Autopilot is in Protection Mode, what would you expect to see on the PFD FMA ?

A

An Amber caution message stating AP in PROT and a flashing Amber Box around the ALT FMA.

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14
Q

What NORMAL BUSBARS are NOT displayed on the ELEC SD pages ?

A

AC ETOPS 1/2 And HOT 1/2

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15
Q

Up until what point does the CRUISE page remain the Default Displayed Page ?

A

Landing Gear Extension

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16
Q

The different air sources of the bleed system are !

A

The APU
THE ENGINES
THE HP GROUND CARTS

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17
Q

The Bleed Air system supplies air to the Fuel Tank Inerting System ( FTIS) ?
True or False ?

A

True

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18
Q

The Bleed Air System supplies air to ?

A 
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
19
Q

The APU can supply Bleed Air for pressurization and air conditioning in flight up to 22,500 ft , with 2packs running !

True of False ?

A

True

20
Q

The APU can supply Bleed Air for Engine start in flight up to 25,000 ft .

True or False

A

True

21
Q

In Normal operation, the crossbleed valve interconnects or isolates the left and the right air system if ?

A

XBLEED selector is in AUTO

22
Q

The Temperature of the FWD cargo compartment is regulated with ?

A

Air from the cabin , the mixer unit and the trim-air system

23
Q

The temperature of the BULK cargo compartment is regulated with air from the cabin and from an electrical heater .

True or False

A

True

24
Q

The AFT cargo compartment is ventilated with cabin air.

True or False

A

True

25
Q

When the Ditching PB sw is pressed ?

A

It closes all valves below the floatation line

26
Q

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

A

True

27
Q

Battery , engine generator or external power can supply electrical power to the APU .

True or False

A

True

28
Q

The Avionics network is composed of ?

A

Two independent and redundant networks

29
Q

The failure of a single or multiple switches on only one network?

A

Has no functional effect

30
Q

In the case of a single CRDC failure?

A

There is no operational effect

31
Q

The two navigation keys on the Cursor Control Device ( CCD )

Are used for ?

A

Their onside ND and OIS , the MFDs and with the mailbox as well

32
Q

Each engine driven generator provides?

A

AC power at a variable frequency

33
Q

The Four Auto Transformer Inits ( ATUs ) convert :

A

The AC 230 V power into AC 115 V
And
The AC 115 V power from EXT Power Units into 230 V power

34
Q

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 :

A

1AC EMER 230 V busbar
1AC EMER 115 V busbar
1DC EMER 28V busbar

35
Q

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

A

True

36
Q

In case of generators overload and not sufficient ELMF shedding , the Electrical Network Management Function
( ENMF ) sheds groups of loads

True or False

A

True

37
Q

The Electrical Network Management Function ( ENMF )
Controls the automatic reconfiguration of the Network.

True or False

A

True

38
Q

The two engine-driven generators are lost on the same side. The APU GEN replaces both generators .

True or False

A

True

39
Q

The engines are running, the FADEC is powered by its own alternator.

True or False

A

True

40
Q

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

A Manual engine start sequence

41
Q

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 ?

A

GA SOFT

42
Q

The thrust reversera are actuated by?

A

Electrical power

43
Q

The FADEC detects an inadvertent deployment of the Thrust Reversers . The FADEC automatically?

A

Limits the related engine thrust to idle

A-350 (3 decks)

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