Garmin G1000 NXi Pilot’s Guide for the Cessna NAV III
190-02177-02 Rev. A
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL FEA
TURES
APPENDICES
INDEX
460
ADDITIONAL FEATURES
Figure 8-56 ESP Roll Operating Range When Engaged
(Force Increases as Roll Increases & Decreases as Roll Decreases)
0º
10º
10º
20º
20º
30º
30º
45º
45º
60º
60º
75º
75º
90º
90º
ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement attitude limit of 75
°
(following figure).
Figure 8-57 Roll Attitude Autopilot Engagement Limit (ESP Engaged)
ESP Upper Disengage Limit (75°)
Aircraft Roll Attitude = 74°
PITCH ENGAGEMENT
ESP pitch engagement parameters are set specifically for each aircraft model. The following tables shows
specific engagement angles, maximum opposing force angles and disengagement limits. Once ESP is engaged, it
will apply opposing force between approximately 15
°
and 50
°
nose-up and between approximately 12
°
and 50
°
nose-down, as indicated in the following figure. Maximum opposing force is applied between approximately
25
°
and 50
°
nose-up and between approximately 22
°
and 50
°
nose-down. ESP pitch engagement parameters
are set specifically for each aircraft model. Table 8-5 shows specific ESP engagement angles, maximum opposing
force angles, and disengagement limits.