
Instructions for Continued Airworthiness G600, GNS 530W, GNS 430W, 190-01080-05 Rev. 2
GMA 347, GTX 330D, GMX 200, WSI AV-200 Cessna 208/208B Page 3 of 29
1. Introduction
1.1 Purpose
This document is designed for use by the installing agency as Instructions for Continued Airworthiness in
response to 14 CFR § 23.1529, and Part 23 Appendix G.
This ICA includes information required by the operator to adequately maintain the Garmin G600 Avionics
Display System, Garmin GNS 530W GPS/NAV/COM, Garmin GNS 430W GPS/NAV/COM, Garmin GA
35 GPS Antennas, Garmin GMA 347 Audio Panel, Garmin GMX 200, WSI AV-200, Comant CI 1530-1
WSI Antenna, Garmin GTX 330D ES transponders, and Comant CI 105 Transponder Antennas when
installed under the following STCs.
STC Number Description
SA02017SE-D
Installation of the G600, GNS 430W, GA 35 GPS Antenna, and GMA 347.
(Requires installation of SA01712SE-D and SA01512WI-D as prerequisites)
SA01712SE-D
Installation of the GNS 530W, GA 35 GPS Antenna, GMX 200, WSI AV-200,
and CI 1530-1 WSI Antenna.
SA01512WI-D
Installation of dual GTX 330D ES transponders and CI 105 Transponder
Antennas.
1.2 Definitions
The following terminology is used within this document:
AC: Advisory Circular
ACO: Aircraft Certification Office
ADC: Air Data Computer
AEG: Aircraft Evaluation Group
AHRS: Attitude Heading Reference System
CFR: Code of Federal Regulations
FAA: Federal Aviation Administration
GPS: Global Positioning System
ICA: Instructions for Continued Airworthiness
LRU: Line Replaceable Unit (GTS computer, Antenna, or PA/LNA)
MFD: Multi-Function Display
OAT: Outside Air Temperature
PFD: Primary Flight Display
PMI: Principal Maintenance Inspector
STC: Supplemental Type Certificate
TSO: Technical Standard Order
TVS: Transient Voltage Suppressor
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