Airplane Flight Manual Supplement
AFMS, GARMIN G500/G600 SYSTEM 190-00601-01 Rev. K
FAA APPROVED Page 12 of 51
1.2 System Power Sources
The G500/G600 system depends on electrical power to function. The Garmin
Display Unit (GDU), Attitude and Heading Reference System (AHRS), and Air
Data Computer (ADC) are directly tied to the aircraft’s main or essential bus and
energized when the aircraft master switch is turned on. Other systems, like the
navigation equipment, weather datalink, autopilot and Adapter (GAD) are
typically located on the avionics bus and may not be functional when this bus is
powered off.
The major components of the G500/G600 are circuit breaker protected with
resettable type breakers available to the pilot. These breakers are located at the
main or essential bus circuit breaker panel and labeled as follows:
Circuit
Breaker
Label
Equipment
PFD
Garmin Display Unit (PFD/MFD), GDU 620
AHRS
Attitude and Heading Reference System, GRS 77
ADC
Air Data Computer, GDC 74A/B
GAD
Garmin Adapter, GAD 43/43e
STBY ATT
Electric Standby Attitude Indicator (Except L-3 Trilogy
and Mid Continent SAM installations)
In dual installations the pilot side equipment is suffixed with the number 1 and
the copilot side equipment is suffixed with the number 2. For example: PFD 1
and PFD 2.
Equipment that receives power from two different circuit breakers will be
suffixed with the letters A and B. For example: PFD 1A and PFD 1B, or
PFD 2A and PFD 2B.
1.3 Navigation Sources
The G500/G600 requires at least one Garmin GPS/SBAS navigation unit to
ensure the integrity of the Attitude and Heading Reference System. The AHRS
will still operate in a reversionary mode if the GPS fails, and the attitude display
on the PFD will still be presented, see Paragraph 2.8. The G500/G600 HSI can
be selected to display course deviation information from up to four independent
sources: two GPS, and two VHF NAV. In addition, the HSI can display two
simultaneous bearing pointers sourced from GPS, VHF NAV, or ADF. DME
distances can be displayed adjacent to the HSI.










