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Garmin GFC 600 User Manual

Garmin GFC 600
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GFC 600 AFCS Part 23 AML STC Maintenance Manual Page 7
190-01938-00 Revision 13
2.1.6 Garmin Air Data Module (ADM)
The ADM (if installed) provides pitot and static pressure input to the GMC 605 via connection to
the existing aircraft pitot and static systems. The ADM contains an internal configuration
module, and when installed replaces the GMC 605 configuration module. The ADM uses the
same I2C interface to the GMC 605 that the configuration module would use with the exception
that the ADM wiring harness includes an additional wire for unit power.
In some installations, the ADM is utilized as a cabin pressure sensor. In this case, an approved
air data source is required, and the ADM is not connected to the existing pitot and static
systems.
2.1.7 GTA 82 Trim Adapter
The Garmin GTA 82 Trim Adapter is a remote mounted device that is used to allow the GFC
600 to drive a trim actuator provided by the airframe manufacturer. In these cases, the GTA 82
provides the required interface.
2.2 GFC 600 Interfaces
The GFC 600 AFCS is capable of interfacing with many different external units. Refer to the
installation-specific information in the aircraft records to determine which interfaces are
applicable.
2.3 Power Requirements
Table 2-1 below summarizes the power requirements for the GFC 600 LRUs.
Table 2-1 Power Requirements
LRU
Characteristics
Specifications
GMC 605
Average Current Draw @ 14 VDC
0.53 A
Max Current Draw @ 14 VDC
1.15 A
Average Current Draw @ 28 VDC
0.27 A
Max Current Draw @ 28 VDC
0.70 A
GSA 87
Average Current Draw @ 14 VDC
2.6 A
Max Current Draw @ 14 VDC
3.0 A
Average Current Draw @ 28 VDC
1.3 A
Max Current Draw @ 28 VDC
1.5 A
GI 285
Average Current Draw @ 14 VDC
65 mA
Max Current Draw @ 14 VDC
154 mA
Average Current Draw @ 28 VDC
36 mA
Max Current Draw @ 28 VDC
84 mA
GTA 82
No-Load Current Draw @ 28 VDC
60 mA
Continuous Current Draw @ 28 VDC
3.0 A
Max Current Draw @ 28 VDC
6.0 A
GSA 80
Max Current Draw @ 28 VDC
1.61 A
GSA 81
Max Current Draw @ 28 VDC
1.61 A

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Garmin GFC 600 Specifications

General IconGeneral
System TypeDigital Autopilot System
Control Wheel Steering (CWS)Yes
Yaw DamperOptional
Automatic TrimYes
Vertical Navigation (VNAV)Yes
Level Change (LVL) ModeYes
Flight DirectorYes
Safety FeaturesOverspeed Protection (OSP)
InterfaceInterfaces with Garmin navigators and displays
Aircraft TypeCertified aircraft
Control ModesIncludes heading hold, altitude hold, vertical speed, and navigation tracking
IntegrationSeamless integration with Garmin avionics
ApprovalCertified

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