Garmin G1000 NXi Cockpit Reference Guide for the Cessna NAV III
190-02178-02 Rev. A
136
AFCS
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
Flight
Management
Hazar
d
Avoidance
AFCS
Additional
Featur
es
Abnormal
Oper
ation
Annun/Alerts
Appendix
Index
USP Airspeeds - Non Altitude
Critical Modes
172
182
206
KIAS
KIAS
KIAS
All Flap
All Flap
All Flap
MINSPD Alert Appears
60
61
61
Non-Altitude Critical USP Activation
60
61
61
USP Activation - Non Altitude Critical Modes
SUSPECTED AUTOPILOT MALFUNCTION
NOTE:
Consult the aircraft documentation for the location of circuit breakers
as well as specifics that may supplement or amplify this procedure.
If an autopilot failure or trim failure is suspected to have occurred, perform the
following steps:
1)
Firmly grasp the control wheel.
2)
Press and hold the
AP DISC
Button. The autopilot will disconnect and
power is removed from the trim motor. Power is also removed from all
primary servo motors and engaged solenoids. Note the visual and aural
alerting indicating autopilot disconnect.
3)
Retrim the aircraft as needed. Substantial trim adjustment may be needed.
4)
Pull the appropriate circuit breaker(s) to electrically isolate the servo and
solenoid components.
5)
Release the
AP DISC
Button.
LEVEL MODE
Level (LVL) mode also becomes active as a function of Electronic Stability and
Protection (ESP). Refer to the Additional Features section for information on the
optional ESP feature.
When the normal flight envelope thresholds have been exceeded for more than
50% of the last 20 seconds, Level mode is activated. The autopilot will engage and pro-
vide input to bring the aircraft back into straight and level flight based on zero degrees
roll angle and zero feet per minute vertical speed. An aural engaging autopilot alert
sounds and the lateral and vertical flight director annunciations will display “LVL”.
The AFCS will remain in Level mode until the pilot selects another mode.
Summary of Contents for G1000 NXi
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