TM 1-1510-218-10
3B-37
The method of operation field (selected with the
OBS/LEG key) displays the selected method of
operation. This field normally displays either OBS or
AUTO/LEG.
The selected sensor field displays the sensor
chosen to provide navigation inputs to the system.
The sensor key is used to make the sensor selection.
The following is a list of possible sensor annunciations:
Blend
System uses position inputs
from all available sensors.
VOR
VOR and DME.
TACAN
Tactical air navigation.
ILS
Instrument
landing
system
(displayed when a localizer
frequency is active).
GPS
Global Positioning System.
The
mode
of
operation
displays in the mode of
operation
field.
Possible
modes of operation displayed
are:
RNAV ENR
RNAV en route (± 5 NM full
scale
HSI
deviation
bar
sensitivity).
RNAV APR
RNAV approach (± 1.25 NM
full scale HSI deviation bar
sensitivity).
NAV
Navigation (± 10° full scale
HSI deviation bar sensitivity).
(5) Self-Test Page. The self-test page is the
first page of information presented when the unit is
turned on. Following an automatic self-test the status
of the system is displayed as well as a list of
navigation data for the pilot to verify on actual aircraft
instruments and displays.
SYSTEM OK
Indicates that the unit has
passed the self test.
RMI 130°
The aircraft's RMI needle
should be pointing to 130°.
DIS 34.3
The aircraft's DME display
should be indicating 34.3 NM.
SEL CRS 315°
The course arrow on the HSI
should be indicating 315°.
HORZ DEV RT 3
The deviation bar on the HSI
3 or CDI should be 3 dots to
the right of center (or an
indication of 3 NM to the right
of center).
VNAV DEV UP 3
The VNAV indicator should be
displaying
an
up
3-dot
deflection (or an indication of
300 feet below the desired
vertical flight path).
CHECK
RMI-DIS
CHECK
CDI-CRS
CHECK
ANN LTS. The annunciator
lights illuminate to remind the
pilot to check the applicable
data values displayed on the
control display unit with the
actual aircraft instruments.
ORS
Operation revision status. A
control number that indicates
what
level
of
operational
capabilities are applicable to
the system.
TEST OK?
Cursor
position
used
to
approve the self-test page.
C 1984 King/
RADIO
Copyright logo.
(6) Initialization Page. The initialization page
will be displayed after the self-test page is approved.
DATE:
Greenwich date in the order
of day-month-year. The first
three letters of each month
are
used
for
month
abbreviations.
GMT:
Greenwich
mean
time
in
hours and minutes. The
correct date and GMT are
retained, even when aircraft
power is removed.
REF NAVAID ID
The NAVAID (within 50 NM
miles) closest to the systems
last computed position before
power was removed.
WPT ID:
A data entry field where the
waypoint
identifier
of
the
aircraft's present position may
be entered.
POS:
The last known computer
generated present position.
EST GS:
Estimated
groundspeed
manually entered. Should be