Garmin GFC 600 Manuale - Pagina 22

Sfoglia online o scarica il pdf Manuale per Display avionico Garmin GFC 600. Garmin GFC 600 46. Installed in piper pa46-310p/350p

PITCH TRIM FAILURE

(Amber AP LED, PTRM FAIL in Message Window on GMC 605 display)

Indicates a failure of the pitch trim servo of the autopilot. The autopilot may remain engaged, but after

disengagement it cannot be re-engaged until the problem is resolved. The yaw damper (if installed) will

remain operative.

1. Control Wheel .................................................................................................................. GRIP FIRMLY

2. AP DISC / TRIM INT Button ............................................................................... PRESS and RELEASE

3. Elevator Trim .................................................................. RE-TRIM if necessary using Pitch Trim Wheel

The autopilot disconnect may be accompanied by an AP FAIL on the GMC 605 Status

message window, indicating the automatic flight control system has failed. The autopilot

cannot be re-engaged with this annunciation present.

4. Yaw Damper ................................................................................................. ENGAGE AS REQUIRED

GFC 600 Autopilot Installed in Piper PA-46-310P/350P

Page 22 of 46

(Be prepared for possible high elevator control forces)

NOTE

190-02011-11 Rev. 2