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Garmin G1000 Cockpit Reference Guide for the DA40/40F
190-00324-11 Rev. C
86
Additional Features
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
4) Press the
FMS
Knob to activate the cursor.
5) Turn the large
FMS
Knob to place the cursor in the STABILITY & PROTECTION
field.
6) Turn the small
FMS
Knob to select ‘ENABLE’ or ‘DISABLE’.
7) Press the
FMS
Knob to remove the cursor.
ESP
is automatically enabled on system power up.
Roll Engagement
Roll Limit Indicators are displayed on the roll scale at 45° right and left, indicating
where ESP
will engage. As roll attitude exceeds 45°, ESP
will engage and the on-side
Roll Limit Indicator will move to 30°. The Roll Limit Indicator is now showing where
ESP
will disengage as roll attitude decreases to within the desirable roll attitude range.
Once engaged, ESP
force will be applied between 30° and 75°. The force increases
as roll attitude increases and decreases as roll attitude decreases. The applied force is
intended to encourage pilot input that returns the airplane to a more normal roll at-
titude. As roll attitude decreases, ESP
will disengage at 30°
Pitch Engagement
ESP
engages at 15° nose-up and 18° nose-down. Once ESP
is engaged, it will
apply increasing opposing force between 15° and 20° nose-up and between 18° and
23° nose-down. Maximum opposing force is applied between 20° and 50° nose-up and
between 23° and 50° nose-down. ESP
disengages when 50° is exceeded in a nose-up
or nose-down attitude.
With ESP
engaged, and the aircraft in a nose-up condition, opposing force steadily
decreases from 20° nose-up to 10° nose-up as aircraft pitch moves toward zero degrees.
ESP
disengages at 10° nose-up. With ESP
engaged, and the aircraft in a nose-down
condition, opposing force steadily decreases from 23° nose-down to 13° nose-down as
aircraft pitch moves toward zero degrees. ESP
disengages at 13° nose-down.
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
engage and disengage limits in these
nose-up/nose-down conditions.
High Airspeed Protection
Exceeding Vne will result in ESP
applying force to raise the nose of the aircraft.
When the high airspeed condition is remedied, ESP
force is no longer applied.
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