HGS 6000 EFVS 3600 Quiz

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Question 1 of 25

1. Question

What is the primary purpose of the HGS-6000 system?

To display flight data on the multifunction display
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To provide head-up flight guidance and symbology in the pilot’s forward view
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To record flight parameters for maintenance
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To provide weather radar imagery
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Question 2 of 25

2. Question

The HGS-6000 projects flight data onto the:

Overhead panel
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Combiner glass in front of the pilot
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Primary flight display
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Center console screen
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Question 3 of 25

3. Question

The EFVS-3600 enhances pilot vision by using:

Synthetic terrain data
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Forward-looking infrared sensors
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Visible-light cameras only
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Radar signals
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Question 4 of 25

4. Question

Which display shows the EFVS imagery?

HGS combiner
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Primary flight display
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Engine indication and crew alerting system (EICAS)
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Multi-function control display unit (MCDU
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Question 5 of 25

5. Question

If authorized by the authority, the EFVS image can be used for approach operations down to:

200 feet AGL
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100 feet AGL
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Touchdown
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Only above 500 feet AGL
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Question 6 of 25

6. Question

What does the Flight Path Vector (FPV) symbol on the HGS represent?

Direction of aircraft heading
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Actual flight path relative to the horizon
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Desired glidepath angle
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Pitch attitude only
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Question 7 of 25

7. Question

The HGS-6000 system receives flight data primarily from:

IRS, ADC, and FMS
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Engine FADEC
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Weather radar
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Cabin pressurization controller
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Question 8 of 25

8. Question

When EFVS mode is active, the HGS symbology:

Disappears completely
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Overlays the infrared image
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Is replaced by synthetic vision
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Switches to monochrome mode
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Question 9 of 25

9. Question

What happens to EFVS imagery during bright daylight conditions?

It automatically switches off
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The sensor adjusts gain and contrast automatically
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The pilot must manually dim the display
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The system cannot be used
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Question 10 of 25

10. Question

What is displayed on the HGS during flare guidance?

Flight path vector and runway aim point
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Only pitch ladder
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Autopilot data only
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No visual cues
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Question 11 of 25

11. Question

The EFVS system improves:

Cabin lighting
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Runway and terrain awareness in low-visibility conditions
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ATC communications
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Fuel efficiency
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Question 12 of 25

12. Question

The EFVS camera is mounted:

On the vertical stabilizer
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In the nose area of the aircraft
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Beneath the wing
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On the tailcone
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Question 13 of 25

13. Question

When the EFVS fails during an approach, the pilot must:

Continue visually without limitations
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Discontinue use and revert to standard visual references
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Switch to weather radar
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Reboot the system in flight
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Question 14 of 25

14. Question

The EFVS display may show runway lighting that is not visible to the naked eye because:

The system enhances infrared energy from lights and terrain
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It uses radar reflection
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It displays synthetic data
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It amplifies visible light only
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Question 15 of 25

15. Question

During an approach, at what altitude must you at the latest switch off the EFVS?
(Texel Air procedures)

100 feet AGL
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100 feet above MDA/DH
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At MDA/DH
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On roll out
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Question 16 of 25

16. Question

While using the EFVS, if you notice pixels that appear brighter or darker than the neighboring pixels, what should you do?

Wait for the automatic calibration
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Perform a manual calibration
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Switch the EVS off
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Turn up max brightness
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Question 17 of 25

17. Question

What is true regarding manual calibration (EFVS)?

The CAL will be displayed and image will be removed for 10 seconds
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The CAL will be displayed and image will still be visible
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MAN CAL will be displayed
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ATT will be displayed
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Question 18 of 25

18. Question

NO EVS is displayed, what is the meaning?

EVS is switched off
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A fault prevents the display of the EVSA video feed
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The system is overheated
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calibration in progress
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Question 19 of 25

19. Question

When are you not allowed to use the EFVS?

During ILS CAT II manual approach
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During a circling approach
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During a VNAV approach
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Below 10,000 feet
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Question 20 of 25

20. Question

During a visual traffic pattern, using the HUD, which mode should you use?

HUD is not allowed for visual traffic pattern
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EVS
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PRI
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VMC
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Question 21 of 25

21. Question

During EFVS operation, if you suddenly notice that the EVS yoke switch is not working, what should you do?

Select EVS OFF in the MCDU
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Immediately stow the HUD
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Perform a go around
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Use the EVS OFF/EVS to toggle the system in the MCDU
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Question 22 of 25

22. Question

What is true regarding the use of EFVS?

HGS AIII approach can be flown from either seat
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The EFVS can not be used for CAT II autoland but the HGS can.
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The HUD must be stowed 100 feet above MDA/DH
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When performing an ILS CAT II autoland, the HUD must be stowed before 10,000 feet on descent
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Question 23 of 25

23. Question

What is true regarding the HGS?

The RWY elevation selection in the FMC (HGS DATA page) is by default the published field elevation and not the touchdown zone elevation.
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The pilot can manually select AIII mode when the aircraft is above 500 feet AGL
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If ALIGN is displayed, the HGS is performing a self test
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The FMC RWY elevation (HGS DATA page) is the runway end point and can not adjusted.
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Question 24 of 25

24. Question

In order to use the AIII mode for an ILS approach, the glideslope must be:

2.5° – 3.6°
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2.5° – 4.5°
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3° – 5°
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0° – 9.9°
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Question 25 of 25

25. Question

What is true regarding HGS modes?

IMC is primarily used for autopilot flight director approaches. FD guidance is removed at 70 ft AGL
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AIII is primarily used for autopilot flight director approaches. FD guidance is removed at 70 ft AGL
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VMC is for circling approaches
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When in Primary mode, at 70 feet, all guidance is removed.
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