Garmin G1000 NXi, Reference Manual

Page: 191 / 260

Garmin G1000 NXi Cockpit Reference Guide for the Cessna NAV III 190-02178-02 Rev. A
165
Additional Features
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
Flight
Management
Hazar
d
Avoidance
AFCS
Additional
Featur
es
Abnormal
Oper
ation
Annun/Alerts
Appendix
Index
ESP High Pitch Protection Limits
C-172 C-182 C-206
Angle Opposing Force Begins 16° 19° 18°
Max Opposing Force Angle 20°
24° 23°
ESP Disengagement Angle 14°
14° 14°
ESP Pitch Protection by Aircraft Model
ESP Low Pitch Protection Limits
C-172 C-182 C-206
Angle Opposing Force Begins -16° -17° -21°
Max Opposing Force Angle -20°
-22° -26°
ESP Disengagement Angle -14°
-12° -17°
ESP Pitch Protection by Aircraft Model
HIGH AIRSPEED PROTECTION
Exceeding Vne 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.
LOW AIRSPEED PROTECTION
(Model 172) When the aircraft decelerates below 55 KIAS and remains below 55
KIAS for 1 second, ESP will activate and begin applying nose down force. ESP will
stop applying the nose down force once airspeed has increased above 55 KIAS.
(Models 182 and 206) When the stall warning has been active for at least one
half second, ESP will activate and begin applying a nose down force. ESP will stop
applying the nose down force once the angle of attack has been reduced sufficiently to
deactivate the stall warning.