Garmin G1000 Line Maintenance Manual

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Page 7-12 LMM for the Kodiak 100
190-02102-00 Rev.4
Table 7-1. Post-Installation Calibration Procedure Summary
Calibration
Procedure
Procedure
Name
Procedure
Description
Installations Requiring Procedure
A-1 Pitch/Roll Offset
Compensation
Level Aircraft Either procedure A-1 or A-2 is
required for all installations. Pro-
cedure A-1 is recommended.
A-2 Zero Pitch/Roll
Offsets by Man-
ual Entry
Manually enter
zeros for Pitch/
Roll Offsets
(passcode
required)
This procedure should be used
only if leveling the aircraft is not
feasible and the AHRS is
mounted to within 0.25° of aircraft
reference.
B Magnetometer
Calibration
Compass Rose
Taxi Maneuver
All installations. This procedure
should be repeated following
removal or replacement of the
GMU 44 unit or degaussing of
the area near the GMU 44.
C Heading Offset
Compensation
Compass Rose
Alignment with
Magnetic North
Strongly recommended for instal-
lations in which GMU 44 align-
ment is not within 0.5° of aircraft
forward longitudinal direction.
D Engine Run-Up
Vibration Test
Validate Vibration
Characteristics of
Installation
All installations.
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)