Garmin SA01933LA_D Instrukcja Obsługi Strona 4

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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 4 of 29
2. Instructions for Continued Airworthiness
2.1 Introduction
Content, Scope,
Purpose and
Arrangement:
This document identifies the Instructions for Continued Airworthiness for the
Garmin G600, Garmin GNS 530W, Garmin GNS 430W, Garmin GA 35 GPS
Antennas, Garmin GMA 347, Garmin GMX 200, WSI AV-200, Comant CI 1530-
1 WSI Antenna, Garmin GTX 330D ES transponders, and Comant CI 105
Transponder Antennas installed in a Cessna 208/208B Caravan.
Definition of
Abbreviations:
See Definitions in Section 1.2
Precautions:
None
Units of measurement:
None
STC SA02017SE-D
Maintenance Data
(or later revisions)
190-01080-02, General Arrangement, G600 GNS430W GMA347 Cessna
208/208B, Rev. 5
190-01080-03, Modification Summary FX, G600 GNS430W GMA347 Cessna
208/208B, Rev. 5 (Sections 4, 5, and Appendix A)
190-01080-04, Modification Summary FE, G600 GNS430W GMA347 Cessna
208/208B, Rev. 6 (Sections 4, 5, and Appendix A)
190-01080-00, Install Dwg 150, G600 GNS430W GMA347 Cessna
208/208B, Rev. 6
190-01080-01, Install Dwg 250, G600 GNS430W GMA347 Cessna
208/208B, Rev. 7
005-W0027-00, Installation Wiring FE, G600 GNS430W GMA347 Cessna
208/208B, Rev. 9
005-W0027-04, Installation Wiring FX, G600 GNS430W GMA347 Cessna
208/208B, Rev. 7
STC SA01712SE-D
Maintenance Data
(or later revisions)
005-00368-12, Avionics Installation, GNS 530(W), GMX200, WSI AV-200,
150, Rev 8
005-00368-13, Avionics Installation, GNS 530(W), GMX200, WSI AV-200,
250, Rev 9
190-00607-04, GMX 200 Installation Manual, Rev. B
WSI 305427-00, WSI AV100/AV-200 Installation Manual
STC SA01512WI-D
Maintenance Data
(or later revisions)
005-00521-11, GTX330D Antenna Installation in Cessna 208/208B, Rev. 5
005-00521-13, DME Antenna Reassignment, Cessna 208/208B, Rev. 6
005-00521-14, Avionics Bus 1 Switch/Breaker Modification, Cessna
208/208B, Rev. 2
Retention:
This document, or the information contained within, will be included in the
aircraft’s permanent records.
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