Garmin G500 Manual - Halaman 13
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Halaman Cetak
1.11 Single G500 Operational Block Diagram
(optional)
Adapter
GAD 43/43e
Magnetometer
GMU 44
AHRS
GRS 77
Air Data Computer
GDC 74()
Temperature Probe
GTP 59
No. 1 GPS/SBAS Navigator
(required)
No. 2 GPS/SBAS Navigator
(optional)
No. 1 VOR/Localizer/GS
(optional)
No. 2 VOR/Localizer/GS
(optional)
Autopilot/Flight Director
(optional)
ADF
(optional)
Standby
Standby
Airspeed
Attitude*
Standby
Magnetic
Altimeter
Compass
(required)
AFMS, GARMIN G500 PFD/MFD SYSTEM
FAA APPROVED
Equipment Installed per this STC
to Aircraft Systems
PFD/MFD Display
GDU 620
Existing Equipment
(already installed in aircraft)
Electric
Standby
Attitude***
(optional)
Audio Panel
(optional)
**
Traffic
(optional)
XM WX/Entertainment
GDL 69/69A
(optional)
Weather Radar
(optional)
Radar Altimeter
(optional)
Iridium Data Link
(optional)
Video Source
(optional)
*Standby Attitude: may be replaced
with electric attitude indicator with
integral / dedicated backup battery.
**Audio panel connection to GDU 620
is recommended for tones and aural
alerts generated by the GDU 620.
This MUST be connected if SVT is
enabled.
*** Installation of a Mid-Continent
electric standby attitude indicator is
approved by this STC.
190-01102-01 Rev. 9
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