ESV Study Guide HUD Flashcards
The HUD is activated by ____.
a. pushing the declutter switch
b. setting the NORM/MAN switch to NORM
c. placing the combiner screen in the breakaway position
d. unstowing the combiner
d. unstowing the combiner
In the HUD, the default glideslope angle displayed during initial power-up is ____ degrees. a. 3.20
b. 2.50 c. 3.40 d. 3.00
d. 3.00
If operational, the HUD ____.
a. must be used for all takeoffs and all approaches and landings to assist in tailstrike prevention
b. must be used for low visibility takeoffs and low visibility approaches in the Lower Minimums
Program
c. combiner must be deployed and the intensity adjusted for ambient conditions in the mandatory
regimes
d. must be used per all of the above
d. must be used per all of the above
The HUD computer is programmed/controlled for each event ____.
a. on the CDU HUD menu
b. automatically upon executing the FMC approach selection
c. whenever the MCP APP button is pressed
d. when the nav is tuned and auto-identified
a. on the CDU HUD menu
In addition to normal flight and navigation guidance, the HUD can also provide all of the following EXCEPT for ______.
a. TCAS prompts
b. unusual attitude recovery prompts
c. windshear alerts
d. RNP and ANP values
d. RNP and ANP values
If the HUD combiner screen moves to the breakaway position, ____.
a. the bottom half of the image on the combiner screen becomes distorted
b. a FAULT message is displayed on the combiner
c. an ALIGN message is displayed on the combiner
d. the combiner symbology is blanked
d. the combiner symbology is blanked
An illuminated AIII light on the HUD Annunciator Panel indicates AIII mode is ____. a. armed but not yet engaged
b. active
c. faulted
d. available
b. active
When the HUD NO AIII light is illuminated on the HAP, ____.
a. AIII mode has been armed and engaged
b. current approach conditions allow AIII operations
c. conditions have been detected which prevent AIII mode from being continued
d. AIII mode must be manually overridden to engage
c. conditions have been detected which prevent AIII mode from being continued
When the HUD Combiner NORM/MAN switch is set to NORM, combiner screen brightness is adjusted ____.
a. only by the amount of light sensed by the ambient light sensor
b. by pressing the Declutter Switch
c. by the position of the DIM Control and the amount of light sensed by the ambient light sensor
d. only by the pilot using the DIM Control
c. by the position of the DIM Control and the amount of light sensed by the ambient light sensor
For routine operations, the HUD must be used on takeoff until at least ____. a. gear up
b. 500 feet AFL or Second Segment Climb, whichever occurs first c. Final Climb Segment (clean configuration)
d. 10,000 feet MSL
c. Final Climb Segment (clean configuration)
On approach, the HUD must be used no later than ____.
a. the FAF
b. 1500 feet AFL
c. 500 feet AFL
d. 1000 feet AFL
d. 1000 feet AFL
Use of the HUD with an inoperative number 1 radio altimeter is prohibited. a. True
b. False
a. True
MAX) The naming convention for the HGS modes have changed. Which of the following modes will be annunciated on the HUD when selected?
a. PRI, VMC, IMC, AIII
b. AI, VMC, AII, AIII
c. VMC, AII, AIII
d. VMC, IMC, AIII
d. VMC, IMC, AIII
(MAX) Which of the following is correct regarding the Aircraft Braking Scale and Pointer?
a. System uses a flexible distance scale depending on new Runway Remaining Guidance system.
b. If the current braking level is not sufficient to stop the aircraft in the remaining runway, the pointer
will deflect to a position at the top end of the scale in the warning area and flash.
c. The Aircraft Braking Scale and Pointer are displayed only upon de-rotation after landing.
d. Both a and b are correct.
b. If the current braking level is not sufficient to stop the aircraft in the remaining runway, the pointer
will deflect to a position at the top end of the scale in the warning area and flash.
