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|  MIL-N-81604C(AS)
Para 3.5.5.4d
(cont)
shall be
used to display the range in
nautical
miles from the aircraft present
position
to the waypoint selected on the
WAYPOINT
switch.
STG/TMGO - The left display shall be used to
e.
select and display the waypoint to which the
aircraft can be steered under control from
the CAINS system if automatic steering is
required. The right display shall display
the time-to-go from the aircraft present
position to the waypoint selected on the
WAYPOINT switch.
PRES POS - The PRES POS position shall allow
f.
the entry and display of the aircraft pre-
sent position coordinates. Present position
latitude shall be entered and displayed in
the left display. Present position longitude
shall be entered and displayed in the right
If the ANCU is inoperative, the CAU
display.
CONTROL COMMAND shall be supplied from the
ANCU to the CAU,thus causing the CAU to con-
trol the entry and display of latitude in the
left display.
TCK/GS - Aircraft ground track relative to
magnectic north shall be displayed in the left
display, and aircraft ground speed shall be
displayed in the right display.
h. HDG/ALT - Magnetic heading of the aircraft
shall be displayed in the left display, and
barometric altitude shall be displayed in the
right display.
WIND - The WIND position shall allow the dis-
i.
play and entry of wind direction relative to
magnetic north in the left display and wind
magnitude in the right display.
j.
NWPR/MV - The function of this DATA switch
position shall be to allow display of NWPR
(Number of Waypoints Received) in the left
display and to allow the entry and display
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