Garmin G3X Touch
™
Pilot’s Guide for Certified Aircraft
190-02472-00 Rev. D 289
Additional Features
System
Overview
Flight
Instruments EIS
CNS
Interface
GPS
Navigation
Flight
Planning
Hazard
Avoidance
Additional
Features AFCS Annun/Alerts Appendix Index
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
Minimum
ESP Torque
(-12.5
º)
Maximum
ESP Torque
(25
º)
Minimum
ESP Torque
(15
º)
Maximum
ESP Torque
(-22.5
º)
Configured Roll Limit (20
º)
Configured Roll Limit (-17.5
º)
AIRSPEED PROTECTION
NOTE: If AGL height data is unavailable (i.e., GPS altitude or terrain data is
unavailable), low-airspeed protection is not supported.
An airspeed below the minimum configured airspeed or above maximum
configured airspeed will result in ESP applying force to raise or lower the nose
of the aircraft. When the high or low airspeed condition is remedied, ESP
force is no longer applied. An audible "Airspeed" alert may be configured.