Garmin g1000 beechcraftbaron58 g58 pilots guide Manuale Utente
190-00629-00 Rev. B
Garmin G1000 Pilot’s Guide for Beechcraft 58/G58
8-5
AUTOMATIC FLIGHT
CONTROL SYSTEM
AFCS STATUS BAR
Flight Director mode annunciations are displayed on
the PFD when the Flight Director is active. Autopilot and
Yaw Damper status are displayed in the center field of the
AFCS Status Bar. Flight Director roll modes are shown on
the left and pitch on the right. Armed modes are annunci-
ated in white and active in green.
Yaw Damper status are displayed in the center field of the
AFCS Status Bar. Flight Director roll modes are shown on
the left and pitch on the right. Armed modes are annunci-
ated in white and active in green.
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.
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 8-3 Command Bars
FLIGHT DIRECTOR LIMITATIONS
The maximum commanded pitch and roll attitudes are
limited to values established during AFCS certification.
Maximum commanded pitch and roll rates are also lim-
ited. Limits may be different from these values in certain
modes, as noted in the section for the mode operation.
Maximum commanded pitch and roll rates are also lim-
ited. Limits may be different from these values in certain
modes, as noted in the section for the mode operation.
Pitch Angle
+20° / -15°
Bank Angle
25°
Bank Rate
5 deg/sec
Table 8-1 Flight Director Command Limits