Garmin G1000 User Manual

G1000 V8.XX S/W Load and Post Install Checkout – Columbia 350/400 Page 1-5
190-00577-04 Revision 1
No. 1 GIA 63
Integrated
Avionics Unit
GEA 71
Engine/Airframe
Unit
No. GIA 63 2
Integrated
Avionics Unit
GDU 1042
MFD
Display of
Engine/Airframe
Instruments
High-Speed Data Bus (Ethernet)
GDU 1040
PFD
Display of
Engine/Airframe
Instruments
(Reversionary Mode Only)
Engine/Airframe
Transducers:
RPM, Manifold Pressure, Oil Pressure,
Oil Temperature, CHT/EGT, TIT, Fuel Flow,
Fuel Quantity, Fuel Low Discretes, Fuel Selector
Valve Position, Bus Volts, Starter Engaged System,
Battery Current, Alternator Current, Low Oil Pressure
Discrete, Aileron Trim Position, Elevator Trim Position,
Oxygen Pressure, Alternator Inop, Door Open Discrete
Figure 1-2. EIS Interface
GDU 1040
PFD
Display of Flight
Instrumentation
GDU 1042
MFD
Display of Flight
Instrumentation
(Reversionary
Mode Only)
No. 1 GIA 63
Integrated
Avionics Unit
No. 2 GIA 63
Integrated
Avionics 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
High-Speed Data Bus (Ethernet)
Figure 1-3. Flight Instrumentation Interface

Garmin G1000 Specifications

General

Display Type	LCD
Primary Flight Display (PFD)	Yes
Multi-Function Display (MFD)	Yes
Terrain Awareness	Yes
Autopilot Integration	Yes
Integrated Flight Deck System	Yes
Weather Radar	Optional
Traffic Advisory System (TAS)	Optional
Terrain Awareness and Warning System (TAWS)	Yes
Resolution	1024 x 768 pixels
Weather Data	Yes
Navigation	Yes
AHRS	Yes
Air Data Computer (ADC)	Yes
Interfaces	ARINC 429, RS-232
Certification	TSO certified
Traffic Information	Optional (requires ADS-B or TCAS)