User Guide

190-00552-00 Rev. A Garmin G1000 Pilot’s Guide for the Columbia 350/400 7-5
AUTOMATIC FLIGHT CONTROL SYSTEM
COMMAND BARS
Upon activation of the flight director, Command Bars are displayed on the PFD as a single cue. The Command
Bars move together vertically to indicate pitch commands, and bank left or right to indicate roll commands.
If the attitude information sent to the flight director becomes invalid or unavailable, the Command Bars are
removed from the display.
Figure 7-3 Command Bars
FLIGHT DIRECTOR LIMITATIONS
The maximum commanded pitch and roll attitudes are limited to values established during AFCS certification:
-15°/+20° pitch and 22° bank. Vertical acceleration and maximum commanded roll rate are also limited. Limits
may be different from these values in certain modes as noted.