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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
The normally gray background turns black if
The instrument cooling problem is detected
26
On ground, what is the white box and ''cross'' on the PFD
It is the max sidestick deflection symbol, and the cross shows the position of the sidestick
27
On ground, what is the green vertical line
It is the Ground Roll Guidance Command Bar
28
When bank exceed 45 degrees, all PFD symbols get removed except
Airspeed, Altitude, Attitude, Heading and V/S
29
When pitch exceeds +25 or -13, all PFD symbols get removed except
Airspeed, Altitude, Attitude, Heading and V/S
30
When the pitch exceed 30 degree
Big red arrows shows where to go
31
The sideslip index become blue instead of yellow in case of
Engine failure during TO or GA
32
You should always operate the FD
2 on or 2 off, not just 1, for A/THR operation
33
The speed trend is showing where it should be in
10 seconds
34
The green F is
The minimum speed for flap retraction at current GW
35
The speeds for the flap configuration are
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
The V1, VR and V2 are
Blue 1, blue dot and magenta triangle
37
The SRS is usually aiming for V2+10, but is also limited to pitch of
18 degrees unless windshear warning (up to 22.5)
38
If the target speed display is off scale, it is
Displayed in digital format
39
The mach appears when
Above 0.5 and the LS button is not pushed
40
VLS is shown as
The top of the amber strip
41
The Green Dot speed is
The best lift to drag ratio (L/D MAX), also the engine out operating speed in clean config
42
The altitude alert system will display
Amber if the altitude deviates
43
The altitude turns amber when below
MDH or MDA
44
The FCU selected altitude shows in ____ or ____ when constrained by FMGC
Blue, magenta
45
The baro will pulse if
Not in the right mode when crossing transition altitude, or below 2500 feet RA when no transition level is available
46
When a DH is entered in the MCDU approach page
The RA indication becomes green when 100 feet above the DH and amber when below
47
If no DH, the RA is ____ above 400 feet and ____ below
Green, amber
48
The red ribbon Ground Reference is based on RA and is displayed only below
570 feet
49
When does the V/S indication show amber
Above 2500 feet - 6000 ft/min Between 2500-1000 feet - 2000 ft/min Below 1000 feet - 1200 ft/min
50
Above 100 feet RA, th GS scale flashes if
A deviation exceeds 1 dot for more than 2 sec
51
Above 15 feet RA, th LOC scale flashes if
A deviation exceeds 1/4 dot for more than 2 sec
52
If the ILS display is not selected when the APPR mode is armed
A flashing ILS message will flash amber
53
The altitude alert system sounds when deviating from
250 feet from preselected altitude
54
The altitude alert system sounds when at ____ from the preselected altitude unless
750 feet, unless AP is engaged
55
The chrono button on the glareshield starts
A timer on the ND
56
If insufficient cooling exist, what system won't be displayed on the ND
The weather radar
57
The dashed yellow and green line on the ND are
A modification to the flight plan, and a flight plan that is not active
58
The missed approach shows as ____, a flight plan to an alternate shows as ____
Dashed blue line, a solid blue line
59
The secondary flight plan is
A solid white line
60
Normally, ILS1 shows on ____ and ILS2 shows on ____
PFD 1 and ND 2, and PFD 2 and ND 1
61
What is the only mode the ND would not show the weather radar
The Plan mode
62
The PWS is only available below
1500 feet AGL
63
What are the 3 priority level for the FWC when displaying on ECAM
Level 1 and 2 (yellow) and level 3 (red)
64
What has the highest priority for aural warning
The synthetic voice
65
What is an advisory
It's when a systems parameters should be monitored (turn the page and flashes the info)
66
On the landing memos, the FLAPS ... will show CONF 3 instead of FULL when
In alternate or direct law, or when the GPWS LDG FLAP 3 pb is selected
67
A G LOAD xxx will be displayed the load is
Less than 0.7 or greater than 1.4
68
The BUSS is based on
The AOA and the configuration of slats/flaps
69
BUSS is displayed when
All 3 ADR pb are switch off
70
The backup altitude is taken from
The GPS

System Limitation/Knowledge (17 decks)

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