Garmin Beechcraft 200 Series, Cockpit Reference Manual

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Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-02040-01 Rev. B 168
Additional Features
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
Flight
Management
Hazar
d
Avoidance
AFCS
Additional
Featur
es
Annun/Alerts
Appendix
Index
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
Flight
Management
Hazar
d
Avoidance
AFCS
Additional
Featur
es
Abnormal
Oper
ation
Annun/Alerts
Appendix
Index
Enabling/disabling ESP:
1) Turn the large FMS Knob to select the ‘Aux’ Page Group.
2) Turn the small FMS Knob to select the ‘System Setup’ Page.
3)
Press the
Setup 2
Softkey to display the ‘Aux - System Setup 2’ Page.
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 ‘Enabled’ or ‘Disabled.’
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.
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 in-
tended to encourage pilot input that returns the airplane to a more normal roll attitude.
As roll attitude decreases, ESP will disengage at 30°.
ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement
attitude limit of 75
°
.
PITCH ENGAGEMENT
ESP engages at 20
°
nose-up and 17
°
nose-down. Once ESP is engaged, it will ap-
ply opposing force between 15
°
and 50
°
nose-up and between 12
°
and 50
°
nose-down.
Maximum opposing force is applied between 25
°
and 50
°
nose-up and between 22
°
and
50
°
nose-down.
The opposing force increases or decreases depending on the pitch angle and the direc-
tion 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.