Garmin SA01933LA_D- Manuals

Page 2 - Instructions for Continued Airworthiness G600, GNS 530W, GNS 430W ,; TABLE OF CONTENTS

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 2 of 29 TABLE OF CONTENTS 1. Introduction .................................................................................................................

Page 4 - Instructions for Continued Airworthiness; See Definitions in Section 1.2

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 ...

Page 5 - Description of Alteration

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 5 of 29 2.2 Description of Alteration This STC upgrades existing avionics for the Cessna 208/208B Caravan as summarized below. Equipment locations are i...

Page 6 - GMX 200 Multifunction Display and WSI AV-200:; Avionics Bus 1 Switch/Breaker Modification:

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 6 of 29 GNS 530W and GNS 430W GPS/NAV/COM: The Garmin GNS 530W and GNS 430W GPS/NAV/COM units are located in the radio stack in the center instrument pa...

Page 7 - Control/Operation Information; Section 4, for further Configuration instructions.

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 7 of 29 2.3 Control/Operation Information 2.3.1 G600 System The GDU 620, GRS 77, GMU 44, and GDC 74A are powered by Main Bus 2 which is normally energiz...

Page 10 - Servicing Information; On condition

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 10 of 29 2.4 Servicing Information In the event of a G600 system, GNS 530W, GNS 430W, GMA 347, or GTX 330D failure, troubleshoot the unit(s) in accordan...

Page 14 - Troubleshooting Information; Remove the six mounting screws from the bezel of the GDU 620.; Installation; Set the GDU 620 into place.; NOTE

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 14 of 29 1. Disconnect all harness/antenna connectors from the LRU. 2. From behind the instrument panel, measure the resistance from each of the GTX330D...

Page 15 - GDU 620 Configuration Module is Replaced; Return to Service; Power up the GDU 620 and all interfaced systems in normal mode.; Removal; Loosen the four Phillips thumbscrews with a screwdriver.; Original GRS 77 is Reinstalled

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 15 of 29 Original GDU 620 is Reinstalled If the original GDU 620 is reinstalled, then no software loading is required. This does not include units that ...

Page 17 - New, Repaired or Exchange GMU 44 is Installed; Original GDC 74A is Reinstalled

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 17 of 29 changed. If the magnetometer mount was changed, refer to Section 4 of the appropriate Modification Summary for the GRS 77/GMU 44 Magnetic Calib...

Page 21 - Top Transponder Antenna Removal & Replacement; located inside the fuselage and set aside.; Bottom Transponder Antenna Removal & Replacement; connection. Twist the BNC connector CCW to disconnect the cable.

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 21 of 29 2. Rotate the Allen wrench counterclockwise until the front lobe of the locking mechanism is in a vertical position. 3. Slide the unit into its...

Page 28 - A.2 DME Cable Connectors

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 28 of 29 5. Tin the center conductor, then solder the contact onto the center conductor, butting the contact up against the cable insulator. Do not exce...