Low Viz Flashcards
What are the reasons for the Autoland Warning to flash below 200’ ?
There are 9 of them.
1/ The last AP disengages
Above 100 ft RA, with approach capability GLS CAT1 Autoland, or CAT2, or CAT3:
2/ The glide signal of the ILS transmitter fails, or
3/ The glide deviation is excessive.
Note: The glide deviation becomes excessive, when the glide deviation exceeds one dot.
Above 15 ft RA, with approach capability GLS CAT1 Autoland, or CAT2, or CAT3:
4/ The LOC signal of the ILS transmitter fails, or
5/ The LOC deviation is excessive.
Note: The LOC deviation becomes excessive, when the LOC deviation exceeds one quarter dot.
6/ One radio altimeter is failed (or rejected by the PRIM or the FWS), and the values provided by the two remaining radio altimeters differ by more than 15 ft
7/ A long flare is detected
Note: flare is long if the aircraft flies more than 1 000 m since FLARE engagement.
8/ A Thrust Control Malfunction (TCM) is detected during flare.
9/ A.FLOOR triggered at or below 200 ft.
When the AUTOLAND light flashes, the flight crew must discontinue the autoland.
Below 1000’ the LOC and/or G/S scale FLASHES on the PFD. What does this indicate?
LOC is more than one quarter dot for 2 secs (above 15’ RA) or
The G/S is more than one dot for more than 2 secs (above 100’ RA)
A Triple Click Aural sounds during approach. This means?
The precision approach capability downgrades
The red LOC flag appears on the PFD CAPTs (F/Os) side means what?
The LOC receiver on the same side is failed
The red G/S flag appears instead of the G/S scale on the CAPTs (F/Os) side means what?
The G/S receiver on the same side is failed
What happens to the FD bars when the LOC (G/S) of one ILS/GLS receiver fails?
The roll (pitch) bar flashes on both PFDs
What Operation for Automatic Landing must ROLLOUT mode be available?
CAT IIIB
The AUTOFLT APPROACH CAPABILITY DOWNGRADE alert, which is crew awareness only, has 5 triggers. What are they?
1/ One or two flight control gyrometers is failed.
2/ One or two flight control vertical accelerometers is failed
3/ Discrepancy between one AOA and the two others
4/ Discrepancy between one slideslip and the two others
5/ discrepancy between one IRS and the two others
What are the 8 equipment not monitored by the FG?
1/ CAPT & F/O sidestick AP pb
2/ AUTOLAND light
3/ AP OFF alert
4/ DH Indicator
5/ Attitude indicator on PFD
6/ Attitude indicator on Standby instrument
7/ Windshield Wiper
8/ Windshield heating
To perform an Automatic ROLLOUT in LAND2 or LAND3 SINGLE requires what from the Landing gear system?
Antiskid, nosewheel steering and Normal or Alternate braking
For Automatic Approach, Landing and ROLLOUT of GLS CAT1, ILS CAT II and ILS CAT III, what are the maximum Headwind?
Tailwind?
and Maximum crosswind?
Headwind is 38kts
Tailwind is 15kts, except 10kts if airport is > 8000’ PA
Crosswind is 30kts. FAM 21.64.1 states 15kts.
All the above is Tower or ATIS provided.
TASKSHARING
PM’s Task are to monitor what?
FMA and announce mode changes below 350’
Back up Automatic callouts
monitor A/C trajectory and announce deviation or attitude exceedance
Announce any failures.
Visual reference for CAT II ops is?
At least 3 consecutive longitudinally aligned lights, being the centreline of the approach lighting system (ALS), the TDZ lights, or the RCLL, or REDL or a combination of these lights; and
A lateral element of lighting, being an approach lighting crossbar, landing threshold or a barrette of TDZ lights.
Visual Reference for CAT IIIA with DH?
Fail Operational automatic landing system:
At DH – at least one centreline light.
Fail Passive automatic landing system:
At DH – at least 3 consecutive longitudinally aligned lights, being the centreline of the approach lighting system (ALS), or the TDZ lights, or RCLL, or REDL, or a combination of these lights.
Visual Reference for CAT IIIB with DH?
at least one centreline light.