TM 55-1510-219-10
13.
Data selector DSRTK/STS.
(Observe action code "02" and malfunction code
"49". This indicates radial error between loaded position
and INS position exceeds 62 kilometers. Operator must
evaluate possibility that INS is in error or reference point
position is incorrect. It is possible to force INS to accept
updated position by setting data selector to UTM POS
and proceeding to step (8) of procedure: "Extra
Precision Geographic Present Position Check and
Update.")
14.
If updating is to be rejected
Press HOLD pushbutton.
(Observe HOLD and INSERT/ADVANCE pushbutton
lights extinguish. INS returns to normal operation.) (e)
Position update eradication:
NOTE
This procedure is not considered
common. Its use is limited to
those times where an operational
error has resulted in an erroneous
position fix.
1.
Data selector DSRTK/STS.
2.
Key "1" Press.
(Observe
INSERT/ADVANCE
pushbutton
light
illuminates, 000001 appears in right data display.)
3.
INSERT/ADVANCE
pushbutton Press.
(Observe
INSERT/ADVANCE
pushbutton
light
extinguishes. Within 30 seconds, data displays return to
normal with "0" (normal inertial mode) in last digit of
right display. AI will be set to approximately three times
the number of hours in NAV.)
(18)
Flight course changes.
(a)
Manual flight plan change insertion:
1.
WYPT
CHG
pushbutton
Press.
(Observe WYPT CHG and INSERT/ ADVANCE
pushbuttons illuminate.)
2.
Select new FROM and TO
waypoints
by
pressing
corresponding
keys
in
sequence.
(Observe new waypoint numbers appear in FROM-
TO data displays as keys are pressed.)
NOTE
Selecting zero as FROM waypoint
will cause desired track to be
defined
by
computed
present
position (inertial present position
plus fixes) and TO waypoint.
3.
INSERT/ADVANCE
pushbutton Press.
(Observe WYPT CHG and INSERT/ ADVANCE
pushbuttons extinguish.)
NOTE
Waypoint zero always contains
ramp coordinates if no manual
flight plan changes are made.
When a manual flight plan change
is made, present position at
instant of insertion is stored in
waypoint zero.
(19)
After landing procedures.
CAUTION
If INS will be unattended for an
extended period, it should be shut
down.
CAUTION
Do not leave INS operating unless
aircraft or ground power and
cooling
air
are
available
to
system.
NOTE
The INS may be shut down,
downmoded to STBY or Align
mode,
or
operated
in
the
navigation mode after landing.
The
determining
factor
in
choosing course of action is
expected length of time before the
next takeoff.
NOTE
Do not tow or taxi aircraft during
INS alignment. Movement during
alignment
requires
restarting
alignment
.
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