Garmin G1000 Socata TBM 850 - Manual (Page 442)

Garmin G1000 Pilot’s Guide for the Socata TBM 850 190-00709-01 Rev. A 430
AUTOMATIC FLIGHT CONTROL SYSTEM
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL FEA
TURES
APPENDICES
INDEX
DISENGAGEMENT
NOTE: Pressing the AP Key does not disengage the yaw damper.
The autopilot may be manually disengaged by pushing the AP DISC, GA, MEYT Switch, MEPT ARM Switch,
or the AP Key on the AFCS Control Unit. Manual disengagement is indicated by a five-second flashing yellow
‘AP’ annunciation and a three-second autopilot disconnect aural alert. The AP DISC or MEPT ARM Switch
may be used to cancel the aural alert.
Figure 7-32 Manual Autopilot Disengagement
The YD Key, MEYT and AP DISC Switches can be used to disengage the yaw damper (the autopilot, if
engaged, also disengages when the AP DISC Switch is pressed). The ‘YD’ and ‘AP’ annunciations turn yellow
and flash for 5 seconds upon disengagement.
Figure 7-33 Yaw Damper Disengagement
Automatic autopilot disengagement is indicated by a flashing red and white ‘AP’ annunciation and by the
autopilot disconnect aural alert, which continue until acknowledged by pushing the AP DISC or MEPT ARM
Switch. Automatic autopilot disengagement occurs due to:
• System failure
• Invalid sensor data
• Roll Trim input
• Stall warning
• Inability to compute default flight director modes
(FD also disengages automatically)
Yaw damper disengagement is indicated by a five-second flashing yellow ‘YD’ annunciation. Automatic yaw
damper disengagement occurs when autopilot disengagement is caused by failure in a parameter also affecting
the yaw damper. This means the yaw damper can remain operational in some cases where the autopilot
automatically disengages. A localized failure in the yaw damper system or invalid sensor data also cause yaw
damper disengagement.
Figure 7-34 Automatic Autopilot and
Yaw Damper Disengagement