A-320 Chapter № 12. Indicating / Recording

38問 • 1ヶ月前

Popovich

通報

問題一覧

12.1.* ADVISORY appears on ECAM. How is the associated parameter presented on ECAM SD:

A. The parameter is pulsing green

12.2.* What does ADVISORY indication mean?

A. The parameter is about to reach the limit

12.3.* Look at the speed scale and name presented speeds.

A. 1- Vα MAX; 2- Vα PROT; 3- VLS; 4- VFE NEXT

12.4.* Which modes of ND can provide a weather radar image?

C. All modes except Plan

12.5.* If a PFD fails, does anything happen automatically?

A. The image automatically transfers to the display formerly occupied by the ND

12.6.* On which modes of ND the VOR/ADF pointers can be displayed?

C. All modes except Plan

12.7.* Look at the speed scale and name presented speeds:

A. 1- VLS; 2- VSW

12.8.* Look at the speed scales. Which flight control law corresponds to these presentations?

A. 1- Normal law; 2- Alternate \ Direct law

12.9.* Course information from the ILS1 receiver will be displayed:

A. On CM1 PFD and CM2 ND provided that both LS pushbuttons are selected ON

12.10.* In what cases a DU will display an “INVALID DATA” message?

A. Associated DMC failure

12.12.* How many DMC's are installed on aircraft?

12.13.* After a single DMC failure, how could a crew member recover display units?

C. Rotate the EIS DMC switch on the switching panel to replace failed DMC with DMC3

12.14.* If the lower ECAM DU fails, is there a way to retrieve that information?

A. By pressing and holding related systems page push button on the ECAM control panel, the page will be displayed on the UPPER ECAM

12.15.* If the upper ECAM DU fails, what will be displayed on the lower DU?

B. Engines and Warning Display (E/WD)

12.16.* Information from the VOR1 receiver will be displayed:

B. On the CM1 ND when the CM1 VOR bearing selector is selected to VOR

12.17.* After a normal engine shutdown, you observe a pulsing STS message. What does it mean?

C. It is a reminder that the status page holds a maintenance message

12.18.* The upper ECAM Display Unit (DU) has failed. You want to see the DOOR/OXY page. How can you see it?

A. You have to press and hold the DOOR key on the ECP

12.19.* Both ECAM screens have failed. Is it possible to get E/WD indications?

C. Yes. Use the ECAM/ND XFR, on the SWITCHING panel, to display the E/WD page on a navigation display

12.20.* In case of a double FWC failure master caution light, master warning light, aural warnings and ECAM cautions and warnings are lost.

True

12.21.* VLS is the lowest speed that the autoflight system will fly the aircraft. This speed is a:

A. Dynamic speed corresponding to the Angle of Attack (AOA)

12.22.* The Speed Trend Arrow is a dynamic information displaying the speed at which the aircraft will be in _____ .

C. 10 seconds

12.23.* The Flight Path vector (FPV) represents the lateral and vertical trajectory of the aircraft with respect to the ground. On the lateral scale, it indicates the aircraft's track. On the vertical scale, it indicates the aircraft's flight path angle.

True

12.24.* When the Side Stick Order indicator is displayed on PFD?

B. After first engine start and disappears after rotation

12.25.* When is the Green Dot displayed on PFD?

A. Only when flap handle is in the zero position

12.26.* When the FPV is above the horizon line, the aircraft is:

C. Climbing

12.27.* The Flight Director bars disappear, when the aircraft bank angle exceeds:

B. 45°

12.28.* The Flight Director bars disappear from the PFD when the pitch attitude exceeds:

B. 25 ° up or 13 ° down

12.29.* The Flight Director bars return to the PFD when the pitch angle returns to the region between:

B. 22 ° up or 10 ° down

12.30.* TERR mode is displayed on ND. What does the numbers in the yellow box mean?

A. Minimum and maximum elevations ahead of the aircraft, within the selected ND range

12.31.* When will the Flight Directors bars flash?

A. When a reversion to the HDG V/S occurs or loss of LOC or G/S signal

12.32.* Red LOC or G/S flag appears on the deviation scale on PFD when:

C. The localizer or glideslope receiver fails

12.33.* When ECAM LDG INHIBIT mode active?

A. From 800ft AGL down to 80kt on landing roll

12.34.* When ECAM T.O. INHIBIT mode active?

A. As soon as thrust levers set in the TOGA or FLEX detent up to reaching 1500 ft AGL or 2 minutes after lift off

12.35.* The lower ECAM DU displays the Gross Weight (GW) in green, as soon as the flight crew starts the first engine.

True

12.36.* The WX RADAR tilt angle refers to the angle between:

A. the antenna beam centerline and the horizon

12.37.* Magenta symbol “R” appears on the speed scale, when:

B. RTA is inserted in the MCDU and aircraft is in managed speed and NAV mode

12.38.* Look at the picture. Why the Hail and Lightning icons are shown on ND?

A. HZD mode is selected on WX radar

12.39.* Look at the picture. What do magenta arcs mean on ND?

A. REACT function indicates areas where the ability of the radar system to evaluate the weather is reduced due to severe signal attenuation

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問題一覧

12.1.* ADVISORY appears on ECAM. How is the associated parameter presented on ECAM SD:

A. The parameter is pulsing green

12.2.* What does ADVISORY indication mean?

A. The parameter is about to reach the limit

12.3.* Look at the speed scale and name presented speeds.

A. 1- Vα MAX; 2- Vα PROT; 3- VLS; 4- VFE NEXT

12.4.* Which modes of ND can provide a weather radar image?

C. All modes except Plan

12.5.* If a PFD fails, does anything happen automatically?

A. The image automatically transfers to the display formerly occupied by the ND

12.6.* On which modes of ND the VOR/ADF pointers can be displayed?

C. All modes except Plan

12.7.* Look at the speed scale and name presented speeds:

A. 1- VLS; 2- VSW

12.8.* Look at the speed scales. Which flight control law corresponds to these presentations?

A. 1- Normal law; 2- Alternate \ Direct law

12.9.* Course information from the ILS1 receiver will be displayed:

A. On CM1 PFD and CM2 ND provided that both LS pushbuttons are selected ON

12.10.* In what cases a DU will display an “INVALID DATA” message?

A. Associated DMC failure

12.12.* How many DMC's are installed on aircraft?

12.13.* After a single DMC failure, how could a crew member recover display units?

C. Rotate the EIS DMC switch on the switching panel to replace failed DMC with DMC3

12.14.* If the lower ECAM DU fails, is there a way to retrieve that information?

A. By pressing and holding related systems page push button on the ECAM control panel, the page will be displayed on the UPPER ECAM

12.15.* If the upper ECAM DU fails, what will be displayed on the lower DU?

B. Engines and Warning Display (E/WD)

12.16.* Information from the VOR1 receiver will be displayed:

B. On the CM1 ND when the CM1 VOR bearing selector is selected to VOR

12.17.* After a normal engine shutdown, you observe a pulsing STS message. What does it mean?

C. It is a reminder that the status page holds a maintenance message

12.18.* The upper ECAM Display Unit (DU) has failed. You want to see the DOOR/OXY page. How can you see it?

A. You have to press and hold the DOOR key on the ECP

12.19.* Both ECAM screens have failed. Is it possible to get E/WD indications?

C. Yes. Use the ECAM/ND XFR, on the SWITCHING panel, to display the E/WD page on a navigation display

12.20.* In case of a double FWC failure master caution light, master warning light, aural warnings and ECAM cautions and warnings are lost.

True

12.21.* VLS is the lowest speed that the autoflight system will fly the aircraft. This speed is a:

A. Dynamic speed corresponding to the Angle of Attack (AOA)

12.22.* The Speed Trend Arrow is a dynamic information displaying the speed at which the aircraft will be in _____ .

C. 10 seconds

True

12.24.* When the Side Stick Order indicator is displayed on PFD?

B. After first engine start and disappears after rotation

12.25.* When is the Green Dot displayed on PFD?

A. Only when flap handle is in the zero position

12.26.* When the FPV is above the horizon line, the aircraft is:

C. Climbing

12.27.* The Flight Director bars disappear, when the aircraft bank angle exceeds:

B. 45°

12.28.* The Flight Director bars disappear from the PFD when the pitch attitude exceeds:

B. 25 ° up or 13 ° down

12.29.* The Flight Director bars return to the PFD when the pitch angle returns to the region between:

B. 22 ° up or 10 ° down

12.30.* TERR mode is displayed on ND. What does the numbers in the yellow box mean?

A. Minimum and maximum elevations ahead of the aircraft, within the selected ND range

12.31.* When will the Flight Directors bars flash?

A. When a reversion to the HDG V/S occurs or loss of LOC or G/S signal

12.32.* Red LOC or G/S flag appears on the deviation scale on PFD when:

C. The localizer or glideslope receiver fails

12.33.* When ECAM LDG INHIBIT mode active?

A. From 800ft AGL down to 80kt on landing roll

12.34.* When ECAM T.O. INHIBIT mode active?

A. As soon as thrust levers set in the TOGA or FLEX detent up to reaching 1500 ft AGL or 2 minutes after lift off

12.35.* The lower ECAM DU displays the Gross Weight (GW) in green, as soon as the flight crew starts the first engine.

True

12.36.* The WX RADAR tilt angle refers to the angle between:

A. the antenna beam centerline and the horizon

12.37.* Magenta symbol “R” appears on the speed scale, when:

B. RTA is inserted in the MCDU and aircraft is in managed speed and NAV mode

12.38.* Look at the picture. Why the Hail and Lightning icons are shown on ND?

A. HZD mode is selected on WX radar

12.39.* Look at the picture. What do magenta arcs mean on ND?

A. REACT function indicates areas where the ability of the radar system to evaluate the weather is reduced due to severe signal attenuation