Airbus A220 - Electronic Display

The Integrated Standby Instrument (ISI) supplies the information necessary to fly the aircraft when _____ and no other display systems are available. The ISI is located on the main instrument panel.

There is only emergency power (battery or RAT) available.

There is only battery power is available.

When the RAT is automatically extended or manually selected.

Correct! Wrong!

When both PFDs use the same air data source, the source is displayed _____ on the PFD.

Red.

Amber.

White.

Correct! Wrong!

The information displayed on the DUs is grouped into:

Two specific areas: Primary Flight Display (PFD), and Engine Indication and Crew Alerting System (EICAS).

Three specific areas: Primary Flight Display (PFD), Engine Indication and Crew Alerting System (EICAS), and Multifunction Window (MFW).

Four specific areas: Primary Flight Display (PFD), Multi Indication Display (MID), Engine Indication and Crew Alerting System (EICAS), and Multifunction Window (MFW).

Correct! Wrong!

The rear pair of static ports provide static pressure for sideslip compensation and redundant sensing. Drain holes provide drainage for any trapped moisture.

False.

True.

Correct! Wrong!

The default position of the EICAS page display is the right half of DU 2. If there is a malfunction of DU 2, the EICAS page is displayed on the left half of DU 3.

True.

False.

Correct! Wrong!

The PFDs are displayed on DU 1 and DU 4. They occupy the full surface of the DU screen. During multiple DU failures or during reversion mode, the PFDs will be displayed one-third of the screen surface.

False.

True.

Correct! Wrong!

During multiple DU failures or during reversion mode, the PFDs will be displayed on half of the screen surface.

Integrated standby instrument (ISI) - An amber CROSS CHECK ATTITUDE message is displayed above the aircraft reference symbol when one of the conditions that follow occurs:

Aircraft is operating without air data for more than 3 minutes, or aircraft has exceeded 35 degrees of pitch or bank angle for more than 3 minutes.

Aircraft is operating without air data for more than 60 seconds, or aircraft has exceeded 45 degrees of pitch or bank angle for more than 60 seconds.

Aircraft is operating without air data for more than 60 seconds, or aircraft has exceeded 60 degrees of pitch or bank angle for more than 2 minutes.

Correct! Wrong!

The message flashes for 5 seconds and is then removed from the display.

There are two Angle Of Attack (AOA) sensors installed on the aircraft, one on each side of the nose fuselage, just behind the corresponding pair of ADSPs. The static ports are also used to calculate Angle Of Attack (AOA). As the AOA changes, the pressure sensed at the different static ports also changes. The Air Data Smart Probe (ADSP) compares:

Static port pressures and calculates the angle of attack.

Total air pressure for airspeed indications.

Static port pressures and total air pressure.

Correct! Wrong!

The Air Data System (ADS) supplies the flight parameters to the aircraft systems. Inputs come from:

Static pressure, pitot pressure, Angle-Of-Attack (AOA), and aircraft position.

Static pressure, pitot pressure, Angle-Of-Attack (AOA), and outside temperature.

Static pressure, pitot pressure, and Angle-Of-Attack (AOA).

Correct! Wrong!

Integrated standby instrument (ISI) - When the roll angle exceeds _____, the ISI displays a red double-lined chevron on the pitch ladder.

65 degrees or the pitch exceeds 30 degrees nose-up or 20 degrees nose-down.

45 degrees or the pitch exceeds 20 degrees nose-up or 20 degrees nose-down.

40 degrees or the pitch exceeds 25 degrees nose-up or 20 degrees nose-down.

Correct! Wrong!

The pitch chevron is positioned at the +30 degrees pitch line or the -20 degrees pitch pointing upward or downward and towards the horizon line.

When only one MFW is accessible (three or more DU failure, or battery power only), both pilots can access the MFW sequentially (one at a time).

False.

True.

Correct! Wrong!

Pitch limit indicator - Pitch limits are calculated by the Fly-By-Wire (FBW) system. Pitch limits are indicated by _____ indicator for nose up and nose down.

A green.

A red.

An amber.

Correct! Wrong!

The Air Data System (ADS) uses _____. The ADSPs, AOA sensors, and the TAT probes are symmetrically installed on each side of the nose of the aircraft, below the flight deck windows.

2 independent Air Data Smart Probes (ADSPs) to measure air pressure (dynamic and static) and angle of attack, 2 Angle-Of-Attack (AOA) sensors, and 1 Total Air Temperature (TAT) probes.

4 independent Air Data Smart Probes (ADSPs) to measure air pressure (dynamic and static) and angle of attack, 2 Angle-Of-Attack (AOA) sensors, and 2 Total Air Temperature (TAT) probes.

3 independent Air Data Smart Probes (ADSPs) to measure air pressure (dynamic and static) and angle of attack, 2 Angle-Of-Attack (AOA) sensors, and 1 Total Air Temperature (TAT) probes.

Correct! Wrong!

ADS malfunction messages are displayed on the EICAS page.

The magenta pitch target marker appears when the TOGA switch is pushed. It indicates the required pitch angle for:

Takeoff and go-around.

Takeoff, Single-engine go-around and during windshear condition.

Takeoff.

Correct! Wrong!

The Multi Function Windows (MFWs) can be configured by the flight crew to show:

FMS, route and map displays, synoptic pages, charts, documents, or Electronic Checklist (ECL).

FMS, route and map displays, synoptic pages, tuning windows, charts, or Electronic Checklist (ECL).

FMS, route and map displays, synoptic pages, tuning windows, charts, documents, video, or Electronic Checklist (ECL).

Correct! Wrong!

To select and control a display, and to enter data, each pilot can use the:

Control Tuning Panel (CTP), or Multifunction Keyboard Panels (MKP), or Cursor Control Panel (CCP).

Multifunction Keyboard Panels (MKP), or Cursor Control Panel (CCP).

Control Tuning Panel (CTP), or Multifunction Keyboard Panels (MKP).

Correct! Wrong!

Airbus A220 – Electronic Display

Quiz

Airbus A220 - Electronic Display

The Integrated Standby Instrument (ISI) supplies the information necessary to fly the aircraft when _____ and no other display systems are available. The ISI is located on the main instrument panel.

When both PFDs use the same air data source, the source is displayed _____ on the PFD.

The information displayed on the DUs is grouped into:

The rear pair of static ports provide static pressure for sideslip compensation and redundant sensing. Drain holes provide drainage for any trapped moisture.

The default position of the EICAS page display is the right half of DU 2. If there is a malfunction of DU 2, the EICAS page is displayed on the left half of DU 3.

The PFDs are displayed on DU 1 and DU 4. They occupy the full surface of the DU screen. During multiple DU failures or during reversion mode, the PFDs will be displayed one-third of the screen surface.

Integrated standby instrument (ISI) - An amber CROSS CHECK ATTITUDE message is displayed above the aircraft reference symbol when one of the conditions that follow occurs:

The Air Data System (ADS) supplies the flight parameters to the aircraft systems. Inputs come from:

Integrated standby instrument (ISI) - When the roll angle exceeds _____, the ISI displays a red double-lined chevron on the pitch ladder.

When only one MFW is accessible (three or more DU failure, or battery power only), both pilots can access the MFW sequentially (one at a time).

Pitch limit indicator - Pitch limits are calculated by the Fly-By-Wire (FBW) system. Pitch limits are indicated by _____ indicator for nose up and nose down.

The Air Data System (ADS) uses _____. The ADSPs, AOA sensors, and the TAT probes are symmetrically installed on each side of the nose of the aircraft, below the flight deck windows.

The magenta pitch target marker appears when the TOGA switch is pushed. It indicates the required pitch angle for:

The Multi Function Windows (MFWs) can be configured by the flight crew to show:

To select and control a display, and to enter data, each pilot can use the: