NAVIGATION Flashcards
What does the IRS ON battery (BAT) light indicate on the
Overhead Maintenance Panel?
IRS operating on backup electrical power (APU hot battery bus)
FCOM, VOL 2; 11.10.11
When is full alignment of the IRS required?
When the time from the last full alignment to the next expected
arrival time exceeds 18 hours.
FCOM, VOL 2; 11.20.3
What CDU pages are available during Alternate Navigation?
•Alternate navigation LEGS
•Alternate navigation PROGRESS
•Alternate navigation RADIO
FCOM, VOL 2; 11.50.2
Can clear air turbulence be sensed by weather radar?
No, turbulence can only be sensed when there is
sufficient precipitation.
FCOM, VOL 2; 11.20.8
How many FMCs are provided?
Two FMCs (flight management computers L and R)
FCOM, VOL 2; 11.30.1
What factor determines “Econ” speed?
•Cost index
FCOM, VOL 2; 11.31.4
What VNAV Pitch mode would you expect at arrow
#3 and arrow #4 with a “climb via” clearance?
•#3 VNAV SPD
•#4 VNAV PTH
FCOM, VOL 2; 11.31.22
If you are flying an approach with the FMC in “on approach” logic,
and the airplane rises more than 150 feet above the path,
the FMA pitch mode will change from VNAV PTH to
what pitch mode display?
•VNAV SPD
FCOM, VOL 2; 11.31.29
On a -400F Legacy FMC, when does the approach phase of the
FMS start,also know as “on approach logic”?
•When the initial fix of an approach sequences
•When the runway is the active waypoint and
within 25nm
FCOM, VOL 2; 11.31.2
NG FMC, “on approach” logic occurs under any of the following conditions?
•Descent phase flaps out of up
•First waypoint sequenced of active nav database
•Aircraft less than 12NM from destination airport directto or
intercept course-to active waypoint and a manually entered
end of descent altitude constraint is lower than the destination
airport plus 500 feet
•The runway or missed approach point is the active waypoint and
the airplane is within 25NM of the runway
FCOM, VOL 2 747-8; 11.31.35
Are there VMCG issues when applying additional thrust manually during
an assumed temperature thrust takeoff?
No, because the assumed temperature thrust setting is not considered
a limitation and VMCG is calculated from the full engine rated thrust.
FCOM, VOL 2; 11.32.3
What could happen if you advance the thrust levers further then
TO 1 or TO 2 fixed derate following an engine failure?
•Loss of directional control
FCOM, VOL 2; 11.32.3
When does the CDU message INSUFFICIENT FUEL display?
•Estimated fuel at destination is less than fuel reserve (FMC RSV)
entered on the PERF INIT page.
FCOM, VOL 2 747-8; 11.32.5
Can ATC monitor airplane position on the ground when the
transponder is in STBY?
No.
FCOM, VOL 2; 11.20.7
Are LNAV and VNAV available in alternate navigation?
No
FCOM, VOL 2; 11.50.1