
Garmin G1000 Pilot’s Guide for Cessna Nav III
190-00498-07 Rev. A
460
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
CONTROL WHEEL STEERING
Duringautopilotoperation,theaircraftmaybehand-ownwithoutdisengagingtheautopilot.Pressingand
holding the
CWS
Buttondisengagesthe pitchandrollservos fromtheightcontrol surfacesandallowsthe
aircrafttobehand-own.At thesametime,theightdirector issynchronizedtotheaircraftattitudeduring
themaneuver. The ‘AP’ annunciation is temporarily replaced by ‘CWS’ in white for the duration of CWS
maneuvers.
In most scenarios, releasing the
CWS
Buttonreengagestheautopilotwithanewreference.Refertotheight
directormodessectionforCWSbehaviorineachmode.
Figure 7-27 CWS Annunciation
Control Wheel Steering
DISENGAGING THE AUTOPILOT
The autopilot is manually disengaged by pushing the
AP DISC
Switch,
GA
Switch or the
AP
Key on the
MFD. Manualdisengagementis indicatedby ave-secondashing yellow‘AP’ annunciationand atwo-
second autopilot disconnect aural alert. After manual disengagement, the autopilot disconnect aural alert
may be cancelled by pushing the
AP DISC
or MET Switch (AP DISCSwitchalsocancels theashing‘AP’
annunciation).
Figure 7-28 Manual Autopilot Disengagement
Automaticautopilotdisengagementis indicatedbyaashing red‘AP’annunciationandby theautopilot
disconnect aural alert, which continue until acknowledged by pushing the AP DISC or
MET
Switch.
Automatic disengagement occurs due to:
•Systemfailure
•Inability to compute default ight director
modes(FDalsodisengagesautomatically)
•Invalidsensordata
Figure 7-29 Automatic Autopilot Disengagement