190-00692-00 Rev. B
Garmin G1000 Pilot’s Guide for Piper PA32
1-1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section is designed to provide an overview of the G1000 Integrated Flight Deck as installed in the Piper
PA32 aircraft. This includes the PA32 R-301 (Saratoga II HP) and the PA32 R-301 T (Saratoga II TC), as well as
the PA32-301 FT (Piper 6X) and the PA32-301 XTC (Piper 6XT).
The G1000 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 1040
Primary Flight Display (PFD)
•
GDU 1040
Multi Function Display (MFD)
•
GIA 63W
Integrated Avionics Unit (IAU)
•
GDC 74A
Air Data Computer (ADC)
•
GEA 71
Engine/Airframe Unit
•
GRS 77
Attitude and Heading Reference System
(AHRS)
•
GMU 44
Magnetometer
•
GMA 1347
Audio System with Integrated Marker
Beacon Receiver
•
GTX 33
Mode S Transponder
•
GDL 69/69A
Data Link
A top-level G1000 system block diagram is shown in Figure 1-1
.
The following equipment is also connected
to the G1000 system and interfaces with the GIA 63W:
• L-3 STORMSCOPE® WX-500 Series II Weather Mapping Sensor
• L-3 SKYWATCH® Traffic Advisory System
• S-TEC System Fifty Five X® Autopilot
• Honeywell® KN 63 DME Transceiver
• Honeywell® KR 87 ADF Receiver
Summary of Contents for G1000:Piper
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