Garmin G1000 Line Maintenance Manual

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LMM for the Kodiak 100 Page 2-1
190-02102-00 Rev.4
2 SYSTEM DESCRIPTION AND OPERATION
Basic knowledge about system operation is needed to perform line maintenance. Refer
to the G1000 NXi Pilot’s Guide for the Kodiak 100 to locate complete operating
information not covered in this section.
2.1 G1000 NXi Integrated Avionics System Description
This section provides an overview of the G1000 NXi Integrated Avionics System as
installed in the Kodiak 100. The G1000 NXi 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 Kodiak 100
G1000 NXi systems consists of the Line Replaceable Units (LRUs) listed in Table 2-1.
System level block diagrams are shown in Figure 2-1 and Figure 2-2.
Table 2-1. Kodiak 100 G1000 NXi System LRUs
Part Number LRU Type Qty
011-03470-00 GDU 1050 Display Unit Standard 3
011-03595-00 Flight Stream 510 Wireless Transceiver Standard 1
011-00809-00 GMA 1347 Audio Panel Standard 2
011-03568-20 GMA 1360D Audio Panel Standard 2
011-01020-10 GMC 710 AFCS Controller Standard 1
011-01105-20 GIA 63W Integrated Avionics Unit Standard 2
011-03711-00 GIA 64W Integrated Avionics Unit Standard 2
011-03711-01 GIA 64W Integrated Avionics Unit Standard 2
011-00831-00 GEA 71 Engine and Airframe Interface Unit Standard 1
011-03682-00 GEA 71B Engine and Airframe Interface Unit Standard 1
011-03303-00 GTX 345R Transponder Standard 1
011-03303-01 GTX 345R Transponder Standard 1
011-03732-00 GRS 79 Altitude and Heading Reference System Standard 2
011-03734-00 GDC 72 Air Data Computer Standard 2
011-00870-10 GMU 44 Magnetometer Standard 2
011-04201-00 GMU 44B Magnetometer Standard 2
011-00978-00 GTP 59 Outside Air Temperature Probe Standard 2
011-01356-00 GTS 800 TAS/TCAS Traffic System Optional 1
Uncontrolled if Printed

Garmin G1000 Specifications

General

Display Type	LCD
Primary Flight Display (PFD)	Yes
Multi-Function Display (MFD)	Yes
Terrain Awareness	Yes
Autopilot Integration	Yes
Integrated Flight Deck System	Yes
Weather Radar	Optional
Traffic Advisory System (TAS)	Optional
Terrain Awareness and Warning System (TAWS)	Yes
Resolution	1024 x 768 pixels
Weather Data	Yes
Navigation	Yes
AHRS	Yes
Air Data Computer (ADC)	Yes
Interfaces	ARINC 429, RS-232
Certification	TSO certified
Traffic Information	Optional (requires ADS-B or TCAS)