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190-00728-04 Rev. A
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
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).
NOTE: 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.