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190-00592-06 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA40/40F
5
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
Figure 1-1 G1000 System Block Diagram
GSA 81
Roll Servo
Autopilot Calculations
(optional)
GSA 81
Pitch Servo
Autopilot Calculations
(optional)
GSA 81
Pitch T rim Servo
Autopilot Calculations
(optional)
No. 1 GIA 63/63W
Integrated Avionics Unit
System Inegration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/WAAS
Glideslope
Flight Director (with GFC 700 option)
No. 2 GIA 63/63W
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/WAAS
Glideslope
GTX 33
Tr ansponder
High-Speed Data Bus (Ethernet)
Reversionary
Control
GEA 71
Engine/Airframe
Unit
GDC 74A
Air Data
Computer
OAT
Airspeed
Altitude
Ve rtical Speed
GRS 77
AHRS
Attitude
Rate of T urn
Slip/Skid
GMU 44
Magnetometer
Heading
GPS Output
GPS Output
Reversionary
Control
GMA 1347
Audio Panel
GDU 1040 (PFD)
GDU 1040/1042/1044 (MFD)
NOTE: The GDU 1042 and GDU 1044 are equipped with additional bezel controls and are available for use
in systems equipped with the Garmin GFC 700 Automatic Flight Control System.