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Section 7 automatic flight control system, 1 s-tec fifty five x autopilot (optional), Automatic flight control system – Garmin G1000 Quest Kodiak User Manual

Page 361

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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