Pilot's Guide

Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT/GTi 190-00663-02 Rev. B520
ADDITIONAL FEATURES
WithESP
™
engaged, and the aircraft in a nose-up condition, opposing force steadily decreases from 20° nose-
up to 15° nose-upasaircraftpitchmovestowardzerodegrees.ESP
™
disengages at 15° nose-up.WithESP
™
engaged,andtheaircraftinanose-downcondition,opposingforcesteadilydecreasesfrom18° 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.
Figure 8-83 - ESP Pitch Operating Range When Engaged
(Force Increases as Pitch Increases & Decreases as Pitch Decreases)
30˚
25˚
20˚
15˚
10˚
5˚
0˚
5˚
10˚
15˚
20˚
25˚
30˚
30˚
25˚
20˚
15˚
10˚
5˚
0˚
5˚
10˚
15˚
20˚
25˚
30˚
35˚
40˚
45˚
50˚
35˚
40˚
45˚
50˚
50˚
45˚
40˚
35˚
50˚
45˚
40˚
35˚
ESPESP
HIGH AIRSPEED PROTECTION
ExceedingVmo/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.