System overview – Garmin G1000 King Air C90GT User Manual
Page 19
190-00663-01 Rev. A
Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT
5
SYSTEM OVERVIEW
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
• GCU 475 (1) – Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital
interface.
• GMC 710 (1) – Provides the controls for the GFC 700 AFCS through an RS-232 digital interface allowing
communication with both PFDs.
• GTP 59 (2) – Provides Outside Air Temperature (OAT) data to the on-side GDC 74B.
• GSA 80 (3), GSA 81 (1), and GSM 85A (4) – The GSA 80 servos are used for the automatic control of roll,
pitch, and yaw. The GSA 81 servo is used for the automatic control of pitch trim. These units interface with
each GIA 63W.
The GSM 85A servo gearbox is responsible for transferring the output torque of the GSA 80/81 servo actuator
to the mechanical flight-control surface linkage.