GH-3100
Installation & Operation Manual
TP-559
General Information
Page 1-5
Revision K
March 30, 2017
1.2.2 Detachable Configuration Module (DCM-3100)
The Detachable Configuration Module is a solid-state device that retains software and hardware
configuration information for specific aircraft.
NOTE
The DCM-3100 is electrostatic sensitive device when not connected to
the GH-3100 Indicator.
1.2.3 Magnetometer (MAG-3000)
The Magnetometer uses a three-axis magnetic sensor to sense magnetic fields. The field data is transmitted
via an RS-422 bus to the Standby Attitude Indicator (GH-3100). The field data is used with the pitch and
roll attitude of the Standby Attitude Indicator to compute the magnetic heading of the aircraft.
NOTE
Refer to the MAG-3000 Install manual, TP-633, for complete installation
information.
1.2.4 Magnetometer (MAG-3100)
The Magnetometer uses a three-axis magnetic sensor to sense magnetic fields. The field data is transmitted
via an RS-422 bus to the Standby Attitude Indicator (GH-3100). The field data is used with the pitch and
roll attitude of the Standby Attitude Indicator to compute the magnetic heading of the aircraft.
NOTE
Refer to the MAG-3100 Install manual, 0040-21200-01, for complete
installation information.
