Cockpit Reference Guide
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
86
Additional Features
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Hazard
Avoidance
Additional
FeaturesAnnun/AlertsAppendixIndex
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-
sideRollLimitIndicatorwillmoveto30°.TheRollLimitIndicatorisnowshowing
where ESP will disengage as roll attitude decreases to within the desirable roll attitude
range.
Onceengaged,ESPforcewillbeappliedbetween30° 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
attitude.Asrollattitudedecreases,ESPwilldisengageat30°.
ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement
attitude limit of 75°.
Pitch Engagement
ESPengagesat20° nose-up and 17° nose-down. Once ESP is engaged, it will apply
opposing force between 15°and50° nose-up and between 12°and50° nose-down.
Maximum opposing force is applied between 25°and50° nose-up and between 22°
and50° 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.
Angle of Attack Protection
If the Angle of Attack Proctection feature is available in the current installation,
ESP force may be applied if the compatible lift computer determines a stall warning
condition is imminent. In this condition, the Pitch Limit Indicator will be initially
displayed 4° below this computed pitch attitude. When pitch attitude equals that
indicated by the Pitch Limit Indicator, ESP will engage, applying a force in the direction
necessary to lower the nose of the aircraft.
High Airspeed Protection
Exceeding Vmo or Mmo 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.










