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System Limitation/Knowledge > Instruments > Flashcards

Instruments Flashcards

1
Q

Putting the PFD brightness to off will

A

Transfer the PFD to the ND

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2
Q

The ADIRU provides

A

Speed, altitude attitude and position information

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3
Q

Each DMC has a channel for __ and __

A

EFIS and ECAM

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4
Q

DMC 1, 2 and 3 usually provide

A

CA screens, FO screens and ECAM screens

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5
Q

How would you know there’s a DMC failure

A

A crossbar in the displays affected

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6
Q

On the ECAM, the E/WD always has

A

Priority

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7
Q

When the upper ECAM has failed, you can see an SD page temporarly by pressing and holding the system page, how long does it stay before the E/WD comes back

A

3 minutes

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8
Q

ADIRS is 1 system that replaces the

A

ADC and IRS

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9
Q

ADIRS is comprised of 3 ADIRU, a CDU and

A

Many inputs and outputs

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10
Q

What are the 2 parts of the ADIRU

A

ADR and IR

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11
Q

The ADIRS supplies data to

A

FMGEC, FADEC, PRIM, SEC, FWC, SFCC, ATC, GPWS, CMC and CPC

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12
Q

The ADIRS can only align in those lattitude

A

60S to 82N (73N between 90-120W)

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13
Q

What are the 4 types of sensors on the side of the A/C

A

Pitot, Static, AOA and TAT

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14
Q

How many ADM are on the A/C

A

8

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15
Q

How many static ports are installed

A

6

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16
Q

On the ADIRS control panel, putting the switch to ATT is normally done when

A

The NAV mode a failed

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17
Q

Once the ATT mode is selected, the NAV mode can’t be used until

A

An alignement on the ground

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18
Q

If a Fault light is flashing in an IR pb, it means that

A

The attitude and heading can be recovered by putting the switch to ATT, you lose position data

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19
Q

You can perform a fast realignement by

A

Putting all switch to off and back to NAV in less than 5 seconds

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20
Q

The baro can display

A

hPa or Hg

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21
Q

When the FCU is initialized, the baro shows

A

1013 or 29.92

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22
Q

When you pull the baro knob, what happens

A

Switch to standard pressure

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23
Q

The ILS button shows

A

The LOC/GS scale on the PFD

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24
Q

If the ND mode or range data fails, the default ND is

A

Rose NAV and 80 NM scale

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25
Q

The normally gray background turns black if

A

The instrument cooling problem is detected

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26
Q

On ground, what is the white box and ‘‘cross’’ on the PFD

A

It is the max sidestick deflection symbol, and the cross shows the position of the sidestick

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27
Q

On ground, what is the green vertical line

A

It is the Ground Roll Guidance Command Bar

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28
Q

When bank exceed 45 degrees, all PFD symbols get removed except

A

Airspeed, Altitude, Attitude, Heading and V/S

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29
Q

When pitch exceeds +25 or -13, all PFD symbols get removed except

A

Airspeed, Altitude, Attitude, Heading and V/S

30
Q

When the pitch exceed 30 degree

A

Big red arrows shows where to go

31
Q

The sideslip index become blue instead of yellow in case of

A

Engine failure during TO or GA

32
Q

You should always operate the FD

A

2 on or 2 off, not just 1, for A/THR operation

33
Q

The speed trend is showing where it should be in

A

10 seconds

34
Q

The green F is

A

The minimum speed for flap retraction at current GW

35
Q

The speeds for the flap configuration are

A

VFE for Config Full is: 180 kts
VFE for Config 3 is: 186 kts
VFE for Config 2 is: 196 kts
VFE for Config 1 is: 240 kts

36
Q

The V1, VR and V2 are

A

Blue 1, blue dot and magenta triangle

37
Q

The SRS is usually aiming for V2+10, but is also limited to pitch of

A

18 degrees unless windshear warning (up to 22.5)

38
Q

If the target speed display is off scale, it is

A

Displayed in digital format

39
Q

The mach appears when

A

Above 0.5 and the LS button is not pushed

40
Q

VLS is shown as

A

The top of the amber strip

41
Q

The Green Dot speed is

A

The best lift to drag ratio (L/D MAX), also the engine out operating speed in clean config

42
Q

The altitude alert system will display

A

Amber if the altitude deviates

43
Q

The altitude turns amber when below

A

MDH or MDA

44
Q

The FCU selected altitude shows in ____ or ____ when constrained by FMGC

A

Blue, magenta

45
Q

The baro will pulse if

A

Not in the right mode when crossing transition altitude, or below 2500 feet RA when no transition level is available

46
Q

When a DH is entered in the MCDU approach page

A

The RA indication becomes green when 100 feet above the DH and amber when below

47
Q

If no DH, the RA is ____ above 400 feet and ____ below

A

Green, amber

48
Q

The red ribbon Ground Reference is based on RA and is displayed only below

A

570 feet

49
Q

When does the V/S indication show amber

A

Above 2500 feet - 6000 ft/min
Between 2500-1000 feet - 2000 ft/min
Below 1000 feet - 1200 ft/min

50
Q

Above 100 feet RA, th GS scale flashes if

A

A deviation exceeds 1 dot for more than 2 sec

51
Q

Above 15 feet RA, th LOC scale flashes if

A

A deviation exceeds 1/4 dot for more than 2 sec

52
Q

If the ILS display is not selected when the APPR mode is armed

A

A flashing ILS message will flash amber

53
Q

The altitude alert system sounds when deviating from

A

250 feet from preselected altitude

54
Q

The altitude alert system sounds when at ____ from the preselected altitude unless

A

750 feet, unless AP is engaged

55
Q

The chrono button on the glareshield starts

A

A timer on the ND

56
Q

If insufficient cooling exist, what system won’t be displayed on the ND

A

The weather radar

57
Q

The dashed yellow and green line on the ND are

A

A modification to the flight plan, and a flight plan that is not active

58
Q

The missed approach shows as ____, a flight plan to an alternate shows as ____

A

Dashed blue line, a solid blue line

59
Q

The secondary flight plan is

A

A solid white line

60
Q

Normally, ILS1 shows on ____ and ILS2 shows on ____

A

PFD 1 and ND 2, and PFD 2 and ND 1

61
Q

What is the only mode the ND would not show the weather radar

A

The Plan mode

62
Q

The PWS is only available below

A

1500 feet AGL

63
Q

What are the 3 priority level for the FWC when displaying on ECAM

A

Level 1 and 2 (yellow) and level 3 (red)

64
Q

What has the highest priority for aural warning

A

The synthetic voice

65
Q

What is an advisory

A

It’s when a systems parameters should be monitored (turn the page and flashes the info)

66
Q

On the landing memos, the FLAPS … will show CONF 3 instead of FULL when

A

In alternate or direct law, or when the GPWS LDG FLAP 3 pb is selected

67
Q

A G LOAD xxx will be displayed the load is

A

Less than 0.7 or greater than 1.4

68
Q

The BUSS is based on

A

The AOA and the configuration of slats/flaps

69
Q

BUSS is displayed when

A

All 3 ADR pb are switch off

70
Q

The backup altitude is taken from

A

The GPS

System Limitation/Knowledge (17 decks)

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