Section 7 automatic flight control system, 1 s-tec fifty five x autopilot (optional), Automatic flight control system – Garmin G1000 Quest Kodiak User Manual
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190-00590-02 Rev. A
Garmin G1000 Pilot’s Guide for the Quest Kodiak 100
349
AUTOMATIC FLIGHT CONTROL SYSTEM
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
NOTE:
Refer to the Aircraft Flight Manual (AFM) for the installed autopilot.
7.1 S-TEC FIFTY FIVE X AUTOPILOT (OPTIONAL)
NOTE:
This section covers only the additional ‘AP’, ‘YD’, and ‘FD’ status annunciations that may appear in the
G1000 AFCS Status Box. These status annunciations are not analogous to both the G1000 and the S-TEC
Fifty Five X. Refer to the approved S-TEC Fifty Five X Pilot’s Operating Handbook (POH) for comprehensive
list of annunciations and operating instructions.
In addition to the redundant status/mode annunciations and/or visual representations that are simultaneously
displayed on both the G1000 (AFCS Status Box and/or PFD) and the S-TEC Fifty Five X (Autopilot Display
and/or Remote Annunciator Display), the G1000 displays additional status/mode annunciations of ‘AP’ when
the autopilot is engaged, ‘YD’ when the Yaw Damper is engaged, and ‘FD’ when the Flight Director Mode is
engaged.
Autopilot
Status
Figure 7-1 Autopilot & Yaw Damper Engaged
(G1000 AFCS Status Box)
Yaw
Damper
Status
Figure 7-2 Flight Director Mode Engaged
(G1000 AFCS Status Box)
Flight
Director
Mode