Garmin G1000 PDAs & Smartphones User Manual


 
190-00498-07 Rev. A
Garmin G1000 Pilot’s Guide for Cessna Nav III
5
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
Figure 1-1 Basic G1000 System
No. 1 GIA 63/63W
Integrated Avionics Unit
System Inegration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/WAAS
Glideslope
GFC 700 Flight Director
(172S, 182, & 206)
No. 2 GIA 63/63W
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/WAAS
Glideslope
GTX 33
Transponder
Reversionary
Control
GEA 71
Engine/Airframe
Unit
GDC 74A
Air Data
Computer
OAT
Airspeed
Altitude
Vertical Speed
GRS 77
AHRS
Attitude
Rate of Turn
Slip/Skid
GMU 44
Magnetometer
Heading
GPS Output
GPS Output
Reversionary
Control
GMA 1347
Audio Panel
PFD
GDU 1040 or
GDU 1044B*
Honeywell
KAP 140
Autopilot
MFD
GDU 1040 or
GDU 1044B*
The GDU 1040 is available in systems not using the GFC 700 Automatic Flight Control System.
The GDU 1044B is available in systems using the Garmin GFC 700 Automatic Flight Control System.
*
GSA 81
Pitch Trim
Autopilot Calculations
(172S/TD,182 & 206)
GSA 81
Pitch Servo
Autopilot Calculations
(172S/TD,182 & 206)
GSA 81
Roll Servo
Autopilot Calculations
(172S/TD,182 & 206)
GTS 800
TAS
or
GDL 90
Data Link
ADS-B Traffic Data