Garmin Flight Deck 100 User Manual

190-00728-04  Rev. A

1

This section provides an overview of the Prodigy

 Integrated Flight Deck as installed in the Embraer Phenom 

100.  The system is an integrated flight control system that presents flight instrumentation, position, navigation, 
communication, and identification information to the pilot through large-format displays.  The system consists of 
the following Line Replaceable Units (LRUs):

• GDU 1240A Primary Flight Displays and Multi-

function Display

• GIA 63W Integrated Avionics Unit

• GDC 74B Air Data Computer (ADC)

• GEA 71 Engine/Airframe Unit

• GRS 77 Attitude and Heading Reference System 

(AHRS)

• GMU 44 Magnetometer

• GMA 1347D Dual Audio System with Integrated 

Marker Beacon Receiver

• GTX 33/33D Mode S Transponder (not used with 

TCAS II)

• GDL 69A Satellite Data Link Receiver

• GDL 59 Data Link (optional)

• GSR 56 Iridium Transceiver (optional)

• GWX 68 Weather Radar

• GCU 475 MFD Control Unit

• GMC 715 AFCS Control Unit

• GSD 41 Data Concentrator

• GTS 850 TCAS 1 System (optional)

• GA 36 and GA 37 GPS/SBAS Antennas

• GA 58 Traffic Avoidance System Antennas

• GSA 81 AFCS Servos

• GSM 86 Servo Gearboxes

A top-level system block diagram is shown in Figure 1-1 (it does not include the GA 36, GA 37, GA 58, or GSM 

86).

Refer to the AFCS section for details on the GFC 700 AFCS.

In the Embraer Phenom 100, the GFC 700 Automated Flight Control System (AFCS) provides the flight director 

(FD), autopilot (AP), and yaw damper (YD) functions of the system.