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Figure 3-19. Waypoint Control Screens (Sheet 1 of 2) TM 1-1520-253-10
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Figure 3-19. Waypoint Control Screens (Sheet 2 of 2)
CONTROL/ FUNCTION INDICATOR
QUICK Access the QUICK REVIEW REVIEWg screen.
3.12.3.3 Waypoint Data Screen. The waypoint entry screen allows the pilot to edit, or de.ne a waypoint. A waypoint is marked as used in the mission data base when-ever there is any data in either the latitude or longitude or the waypoint name.
CONTROL/ FUNCTION
INDICATOR
WAYPOINT Title of screen.
DATA
gWPT Enter or edit waypoint number or
name.
gLAT Enter or edit latitude coordinate.
gLONG Enter or edit longitude coordinate.
gXALT Toggles edit box between XALT
and GSLOPE.
GSLOPE With edit box around glideslope
area, enter estimated glideslope
angle (-9° to 9°), and press ENT.
MGRSg Toggles display between MGRS
and LAT/LONG coordinate
systems.
Deleted
Deleted .
3.12.4 Create Storepoints. Storepoints are targets of opportunity, created 9on the .y9 which may be used later for navigation. Storepoints may be created by over.ying a location and pressing MARK. As many as 25 storepoints may be created, and will be designated as A through Z less
O.
3.12.4.1 Flyover Store Screen. Access this screen by pressing FIX, then FLYOVER SK-6 soft key. Functions of the soft keys are:
CONTROL/ INDICATOR FUNCTION
FLYOVER STORE Title of screen.
gOFFSET Edit box enables entry of range, and then bearing of helicopter’s present position to the waypoint position.
LAT/LONG Displays position. helicopter’s current
WPT Displays storepoint number.
AVAIL Displays number of available unused storepoints (from 25 to 0), before overwrites must occur.
gMARK First press of soft key freezes position, display becomes reverse video. Second press of soft key resumes position updating and normal display.
MGRSg Toggles between MGRS and LAT/ LONG coordinate format.
STOREg Stores the waypoint (either frozen, or, if free running, at the instant STORE soft key was pressed) , and accesses STORE-POINT DATA screen.
3.12.5 Navigation Calculator.
NOTE
There is no connection between AMS and the helicopter’s fuel measurement system. All fuel calculations are based on pilot in-puts of fuel on board and estimated fuel .ow. These calculations are estimates, and advisory only. They do not replace the pri-mary fuel quantity system for fuel load and range planning.
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