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190-00595-01 Rev. B
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
4
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
•
GMA 1347
(1) – Integrates NAV/COM digital audio, intercom system and marker beacon controls. This
unit also enables the manual control of the display reversionary mode (red
DISPLAY BACKUP
button) and
communicates with the #1 GIA 63(W), using an RS-232 digital interface.
•
GTX 33
(1) – Solid-state transponder that provides Modes A, C and S capability. The transponder can be
controlled from the PFD. The transponder communicates with the GIA 63/63Ws through an RS-232 digital
interface.
•
GDL 69A
(1) – A satellite radio receiver that provides real-time weather information to the G1000 MFD (and,
indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A communicates
with the MFD via HSDB connection. A subscription to the XM Satellite Radio service is required to enable the
GDL 69A capability.
•
GTP 59
(2) – Provides Outside Air Temperature (OAT) data to the GDC 74A.
•
GSA 81
(4), and
GSM 85
(4) – The GSA 81 servos are used for the automatic control of roll, pitch, yaw, and
pitch trim. These units interface with each GIA 63/63W.
The GSM 85 servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator to the
mechanical flight-control surface linkage.