Garmin aera 660 aera 660 Pilot s Guide - Page 175

E6B Calculator, Main Menu, Set Up Map, Track Vector, Distance, Enter, Tools

Page 175 highlights

Overview Navigation Appendix G Changing the track vector settings on the Navigation Map: 1) From the Main Menu, touch Map > Menu > Set Up Map. 2) Touch the Dedicated Page Icon and touch the 'Line' Group. 3) Touch the Track Vector button and touch Off, Distance, or Time. 4) If Distance is selected, use the keypad to enter the desired distance and touch Enter. 5) If Time is selected, use the + / - buttons to select the desired time. E6B CALCULATOR The E6B Calculator calculates Density Altitude, True Airspeed, Tail Wind, Wind From, and Wind Speed, based on information entered. Accessing the E6B calculator: From the Main Menu, touch Tools > E6B. Barometric Pressure from the Nearest METAR Flight Planning Hazard Avoidance Additional Features Appendices Calculated Figures E6B Calculator • Indicated Altitude-required entry for density altitude/true airspeed calculation. Enter the aircraft's altimeter reading. • Baro Pressure-enter the current barometric pressure. 190-02017-20 Rev. A Garmin aera 660 Pilot's Guide 159 Index

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Garmin aera 660 Pilot’s Guide
190-02017-20 Rev. A
Appendix G
159
Overview
Navigation
Flight Planning
Hazard Avoidance
Additional Features
Appendices
Index
Changing the track vector settings on the Navigation Map:
1)
From the
Main Menu
, touch
Map
>
Menu
>
Set Up Map
.
2)
Touch the Dedicated Page Icon and touch the '
Line
' Group.
3)
Touch the
Track Vector
button and touch
Off
,
Distance
, or
Time
.
4)
If
Distance
is selected, use the keypad to enter the desired distance and
touch
Enter
.
5)
If
Time
is selected, use the
+
/
-
buttons to select the desired time.
E6B CALCULATOR
The E6B Calculator calculates Density Altitude, True Airspeed, Tail Wind, Wind From,
and Wind Speed, based on information entered.
Accessing the E6B calculator:
Fr
om the
Main Menu
, touch
Tools
>
E6B
.
Calculated
Figures
E6B Calculator
Barometric Pressure
from the
Nearest
METAR
I
ndicated Altitude
required entry for density altitude/true airspeed calculation.
Enter the aircraft’s altimeter reading.
Baro Pressure
enter the current barometric pressure.