Airplane Flight Manual Supplement

AFMS, GARMIN G500/G600 SYSTEM 190-00601-01 Rev. K
FAA APPROVED Page 25 of 51
2.20 Kinds of Operations
Unless placarded as limited to VFR only operations, G500/G600 equipment
installed in a certified aircraft is approved for Day and Night / VFR and IFR
operations in accordance with 14 Code of Federal Regulations Part 91, Part 121,
and Part 135 when appropriately maintained.
The table below lists the minimum fully functional G500/G600 System
Equipment ** required for IFR flight operations:
Equipment
Number
installed
VFR
IFR
Primary/Multi Flight Display
1 or 2
1a*
1
Garmin GPS/SBAS Navigator
1 or 2
-
1
Attitude / Heading Unit (AHRS)
1 or 2
-
1
Air data computer (ADC)
1 or 2
1a*
1
Magnetometer (GMU)
1 or 2
-
1
Standby Attitude Indicator
1
-
1
Standby Airspeed Indicator
1
1b
1
Standby Altimeter
1
1b
1
Magnetic Compass
1
1
1
* For VFR operations under 14 CFR Part 91, the aircraft shall have one source
of altitude and airspeed information. This may be from either the PFD or the
standby instruments. (i.e. all “1a” items or all “1b” items from the table above)
** For IFR flight a fully functional G500/G600 system shall not generate system
alerts, which indicate faults within the system or any interfaced equipment.
2.21 KFC 275/325 Altitude Preselect
When the altitude preselect option is installed with KFC 275/325 autopilots,
SOFT RIDE (SR) mode shall be disengaged during altitude capture mode
(ALTC). The following placard must be installed near the autopilot mode
controller or above PFD 1:
“DISENGAGE SOFT RIDE DURING ALTITUDE CAPTURE (ALTC)”
2.22 Type Ratings
Unless otherwise authorized by this section, operations are prohibited in aircraft
that require a type rating under 14 CFR 61.31(a).