Auxiliary Video (Optional) - Garmin G1000 Cockpit Reference Manual

Diamond da42ng integrated flight deck
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between 25° and 50° nose-down. ESP
or nose-down attitude.
With ESP
engaged, and the aircraft in a nose-up condition, opposing force steadily
decreases from 20° nose-up to 12° nose-up as aircraft pitch moves toward zero degrees.
ESP
disengages at 12° nose-up. With ESP
condition, opposing force steadily decreases from 25° nose-down to 17° nose-down as
aircraft pitch moves toward zero degrees. ESP
The opposing force increases or decreases depending on the pitch angle and the
direction of pitch travel. This force is intended to encourage movement in the pitch axis
in the direction of the normal pitch attitude range for the aircraft.
There are no indications marking the pitch ESP
nose-up/nose-down conditions.
High Airspeed Protection
Exceeding Vne will result in ESP
When the high airspeed condition is remedied, ESP

AUXILIARY VIDEO (OPTIONAL)

NOTE: Images provided on the Aux-Video page are for supplemental use only.
There are four modes of operation of the optional auxiliary video display: Full-
Screen, Full-Screen with Digital Zoom, Split-Screen with Map, and Split-Screen with
Map and Digital Zoom.
Displaying auxiliary video:
1) Turn the large FMS Knob to select the AUX page group.
2) Turn the small FMS Knob to select VIDEO and display the AUX-VIDEO Page.
The video display softkeys shown below appear on the AUX - VIDEO Page.
Control of the AUX - VIDEO Page can also be accessed through the Page Menu.
Selecting video menu options:
1) While viewing the AUX - VIDEO Page press the MENU Key to display the
Page Menu OPTIONS.
2) Turn the large FMS Knob to highlight the desired video adjustment option
and press the ENT Key.
When the ENT key is pressed on any option, the page menu closes and returns to
the AUX - VIDEO Page.
190-00963-02 Rev. C
disengages when 50° is exceeded in a nose-up
applying force to raise the nose of the aircraft.
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
Additional Features
engaged, and the aircraft in a nose-down
disengages at 17° nose-down.
engage and disengage limits in these
force is no longer applied.
85

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