Garmin GPSMAP 695/696 Quick Reference Guide
190-00959-00 Rev. A
utilities
24
Overview
GPS Navigation
Flight Planning
Hazar
d
Avoidance
Additional F
eatur
es
Messages &
Alerts
Utilities
e6B cALcuLAtOr
Calculating true airspeed and density altitude:
1)
From the E6B Calculator Window, enter the altitude shown on the altimeter
into the ‘Indicated Altitude’ field, and press the
ENT
Key.
2)
Repeat for ‘Calibrated Airspeed’, ‘Baro Pressure’, and ‘Total Air
Temperature’ fields. (For Calibrated Airspeed, use the speed shown on
the airspeed indicator. Use the current altimeter setting for Baro Pressure.
Total Air Temperature is the temperature of the outside air including the
heating effect caused by speed. For most aircraft, this is the temperature
reading on a standard outside air temperature gauge.) The calculated
figures for True Airspeed and Density Altitude are shown in the designated
fields.
Calculating winds aloft:
1)
Calculate or enter the true airspeed into the ‘True Airspeed’ field, and press
the
ENT
Key.
2)
Enter the aircraft heading shown on the directional gyro or compass into
the ‘Heading’ field, and press the
ENT
Key. Tail Wind, Wind From, and Wind
Speed are calculated.
AircrAft PrOfiLe
Entering an aircraft profile:
1)
From the Aircraft Profile Page, press the
NEW
Softkey. The cursor is
activated in the ‘Current Aircraft’ field.
2)
Enter the desired aircraft name, and press the
ENT
Key.
3)
Move the
FMS
Joystick to the ‘Cruise Speed’ field, turn the
FMS
Joystick to
enter the appropriate cruise speed, and press the
ENT
Key. Repeat for the
‘Maximum Speed’ and ‘Fuel Flow’ fields.
4)
Move the
FMS
Joystick to highlight the ‘Map Symbol’ field, and turn the
FMS
Joystick to select the desired map symbol.
Summary of Contents for GPSMAP 695
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