TM 55-1510-222-10
will be rejected by computer.
11. INSERT/ADVANCE pushbutton - Press.
Observe INSERT/ADVANCE and HOLD pushbutton
annunciators remain illuminated. North position error
and east position error in kilometers will appear in left
and right data displays, respectively.
12. If WARN annunciator illuminates,
proceed to step 13; otherwise proceed to step 9 in
procedure: Extra Precision Geographic Present Position
Check and Update.
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 10 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 annunciators extinguish. INS returns to
normal operation.
(d) 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 annunciator illuminates,
000001 appears in right data display.
3.
INSERT/ADVANCE pushbutton - Press.
Observe
INSERT/ADVANCE
pushbutton
annunciator 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.
(13)
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 TO and FROM waypoints by
pressing corresponding keys
3.
WYPT CHG pushbutton - Press.
Observe new waypoint numbers appear in TO-
FROM 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.
4.
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.
(14)
After landing procedures:
CAUTION
If INS will be unattended for an
extended period, it should be shut
down.
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.
Do not tow or taxi aircraft during
INS
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