This quiz assesses knowledge crucial for B777 pilots operating under low visibility conditions, covering automatic approaches, flight director approaches, and emergency procedures. It is essential for ensuring compliance with aviation safety standards and enhancing operational proficiency.
Two engines operating for a flaps 20 landing.
One engine operating for a flaps 20 or 30 landing.
APU as the only source of electrical power
Display of SGL SOURCE DISPLAYS, SGL SOURCE RAD ALT, SGL SOURCE ILS EICAS message
Normal flight controls
Antiskid operative
Autothrottle engaged
Two autoland status annunciators
Rate this question:
Only small changes in heading/pitch are required to maintain the correct flight path.
Indicated airspeed is not less than VREF or more than VREF+20 knots
The airplane is in the correct landing configuration.
Airplane sink rate is less than 1100 fpm.
Rate this question:
Above the Alert Height, re-engaged the autothrottle and continue.
Below the Alert Height execute a go-around if you do not have a visual reference established.
During rollout discontinue use of reverse thrust.
Below the Alert Height continue the approach using manual throttle control until you have a visual reference established or execute a go-around at minimums.
Rate this question:
Continue the approach with autopilot disengaged.
Re-engaged the autopilot and continue the approach.
Execute an immediate manual go-around.
Execute an immediate go around.
Rate this question:
80 degrees
90 degrees
60 degrees
120 degrees
Rate this question:
Pilot rudder pedal pressure and rudder trim inputs are required to control yaw after 1500-foot radio altitude with localizer and glideslope capture.
Roper trim includes a slideslip and the control wheel will not be centered.
Rudder trim inputs are not effective in the LOC or ROLLOUT modes.
Engaged autopilots control the yaw using the rudder before LAND 2 or LAND 3 are annunciated.
Rate this question:
A (-200) B (-300)
B (-200) C (-300)
C (-200 & -300)
C (-200) D(-300)
Rate this question:
Less than 800 foot ceiling and / or 2 miles visibility
Less than 600 foot ceiling and / or 1.5 miles visibility
Less than 1000 foot ceiling and / or 2 miles visibility
Less than 200 foot ceiling and / or RVR 2,000
Rate this question:
Using flight control Secondary operation
With SGL SOURCE RAD ALT EICAS message displayed.
During SAARU only operation
With SGL SOURCE F/D EICAS message not displayed
Rate this question:
80 degrees
90 degrees
It can not capture without LOC already captured.
120 degrees
Rate this question:
The autopilot disconnect switch has been pushed.
The autopilot is inoperative and a manual landing is required
The autoland system does not have redundancy for triple channel autoland.
NO LAND 3 means the airplane is more than 3 miles from landing.
Rate this question:
Rollout is armed below 1500 feet RA.
ROLLOUT replaces the FLARE mode annunciation.
Rollout guidance continues until the autopilots are disengaged.
The rollout mode engages below 2 feet RA.
Rate this question:
Flare engages between 60 and 40 feet RA.
The PFD autothrottle annunciation changed from SPD to IDLE.
Between 25 and 50 feet RA the autothrottle begins retarding the thrust levers to idle.
Flare commands can be used during a Flight Director approach and landing.
Rate this question:
Below 200 feet it can change from LAND 3 to LAND 2
Below 500 feet, changes in autoland status are inhibited.
Below 200 feet, changes in autoland status are inhibited other than a transition to NO AUTOLAND.
Rate this question:
2 engines must be operating
EICAS message SGL SOURCE DISPLAY must not be displayed and LAND 3 or LAND 2 is annunciated.
Minimums must be referenced to radio altitude.
LAND 3 must be annunciated.
Rate this question:
The autothrottle engaged.
Two autoland status annunciators
LAND 3 or LAND 4 annunciated.
SGL SOURCE DISPLAYS, SGL SOURCE RAD ALT, SGL SOURCE ILS EICAS messages not displayed.
Rate this question:
Continue the approach with the autopilot disengaged.
Re-engaged the autopilot and continue the approach. The autothrotlle engaged.
Continue the approach to minimums and go-around
Execute a go-around
Rate this question:
Two sources of electrical power operating (the APU may not be used as a substitute for the left or right source).
Two operating engines are required.
SGL SOURCE IS – EICAS message is not displayed.
LAND 3 or LAND 2 does not have to be annunciated, only LAND1.
Rate this question:
LAND 3 status is annunciated only on the Captain’s PFD.
Two hydraulic systems must be operating normally.
APU is operating.
LAND 2 status is annunciated on both PFD’s.
Rate this question:
The ILS approach is flown within the expanded localizer band.
The vertical speed is within 200 feet per minute of the published value.
Heading changes do not exceed 5 degrees of the approach course.
The glideslope is flown within a quarter dot.
Rate this question:
When on an ILS approach and radio communication is lost.
When a navigation radio or flight instrument failure occurs which affects the ability to safely complete the approach in instrument conditions.
When the navigation instruments show significant disagreement, but visual contact with the runway is made.
When on an ILS approach, the localizer shows half scale deflection.
Rate this question:
FTCM/Holding, approach a Center and Right hydraulic system are operating normally.
Antiskids is operative
Autothrottle is engaged.
ADIRU is operating.
Rate this question:
EICAS message SGLSOURCE ILS is not displayed.
Both engines are operating.
EICAS message SGL SOURCE DISPLAYS is not displayed.
An FMA is displayed for each pilot.
Rate this question:
Continue the approach with autopilot engaged.
Disengaged the autopilot and execute a manual landing.
Adjusting to the appropriate higher minimums of immediately execute a manual go-around.
Select the other autopilot.
Rate this question:
“Look left/right/ahead” at 200 feet above DA H).
“Strobe lights” when individual sequence flasher light bars are visible.
“Threshold” when the threshold light are seen.
“Check missed approach altitude” at 100 fee above DA (H).
Rate this question:
Continue the approach.
Select the other autopilot switch and continue the approach
Disengaged the autopilot and execute a manual landing or immediately execute a manual go-around.
All of these option are correct.
Rate this question:
The ROLLOUT mode has been fully demonstrated to be capable on contaminated runways.
The pilot must be prepared to disengaged the autopilot and take over manually should ROLLOUT directional control become inadequate.
The ROLLOUT mode uses only rudder for directional control.
The ROLLOUT mode uses nose wheel steering and main gear tracking for directional control.
Rate this question:
It shall be used regardless of reported meteorological visibility.
It shall not be used for only Category II and IIIA approaches.
It less meaningful than meteorological visibility
It should be disregarded.
Rate this question:
The ILS tuned and identified.
The aircraft on an intercept heading less than 120 degrees
Both localizer and glideslope pointers displayed and in the proper position.
The aircraft is under radar control.
Rate this question:
“FLARE ARMED”
“FLARE ENABLED”
“LAND 3” or “LAND 2”, or “NO AUTOLAND”
“500 FEET”
Rate this question:
“TALLY HO” or “ABORTING APPROACH”
“LANDING” or “GO AROUND”
“STOPPING” or “OVERSHOOTING” “STOPPING” or “OVERSHOOTING” “STOPPING” or “OVERSHOOTING”
“VISUAL” or “ON THE GO”
Rate this question:
Aircraft speed is not more than VREF+10 knots or less than VREF.
Aircraft is in the correct landing configuration.
Sink rate is not greater than 1000fpm.
All checklists except the Landing checklist are complete.
Rate this question:
Quiz Review Timeline (Updated): Mar 18, 2023 +
Our quizzes are rigorously reviewed, monitored and continuously updated by our expert board to maintain accuracy, relevance, and timeliness.
Wait!
Here's an interesting quiz for you.