Airplane Flight Manual Supplement

AFMS, GARMIN G500/G600 SYSTEM 190-00601-01 Rev. K
FAA APPROVED Page 18 of 51
1.13 Dual G500/G600 Operational Block Diagram
Equipment Installed per this STC
Air Data Computer
AHRS
Magnetometer
GMU 44 #1
GRS 77 #1
GDC 74() #1
Temperature Probe
GTP 59 #1
Pilot PFD/MFD Display
GDU 620
Copilot PFD/MFD Display
GDU 620
Audio Panel
Various Models (optional)***
Datalinks (optional)
Autopilot/Flight Director
(optional)**
Flight Director Only
ADF, DME
(optional)**
No. 1 VOR/Localizer/GS
(optional)**
Standby
Attitude*
Standby
Airspeed
Standby
Altimeter
Magnetic
Compass
(required on pilot side only)
No. 1 GPS/SBAS Navigator
(required)
Air Data Computer
AHRS
Magnetometer
GMU 44 #2
GRS 77 #2
GDC 74() #2
Temperature Probe
GTP 59 #2
No. 2 GPS/SBAS Navigator
(required)
No. 2 VOR/Localizer/GS
(optional)**
Adapter (optional)
GAD 43/43e
Aircraft Systems
(optional)
Existing Equipment
(already installed in aircraft)
*Standby Attitude: May be replaced with electric attitude indicator with integral /dedicated backup battery. **Optional Equipment: Connection of optional equipment to both GDUs is not required. Functions provided by the optional equipment will only be available on the GDU to which the optional equipment is connected. ***Audio Panel connection to GDU 620 is recommended for tones and aural alerts generated by the GDU 620. This MUST be connected if TAWS and/or SVT is enabled. **** Installation of the Mid-Continent electric standby attitude indicator is approved by this STC.
Weather Radar
(optional)**
Electric
Standby
Attitude***
Traffic
(optional)**
Radar Altimeter
(optional)
StormScope
(optional)**
Video Source
(optional)**
Video Source
(optional)**