Garmin GTX 32 Installation Manual - Page 27

3.7 Post Installation Configuration and Checkout NOTE The GTX 32 Transponder will not provide valid outputs until the aircraft post installation configuration procedures are completed. 3.7.1 Configuration When installed as part of a Garmin Integrated Flight Deck, the GTX 32 transponder must have FAA approved configuration data. Configuration data is loaded to the GTX 32 from an aircraft-specific SW Loader Card. Transponder settings are predetermined for a specific aircraft and are typically contained within the file named 'GTX1'. The GDU PFD serves as the graphics user interface to the installer configuring the system. For basic configuration information, refer to the G1000 Line Maintenance and Configuration Manual, Garmin part number 190-00303-04. For actual aircraft installation/checkout, use only aircraft manufacturer approved checkout procedures. Verify proper operation of the transponder by testing in accordance with Appendix F to 14 CFR Part 43 - ATC Transponder Tests and Inspections. For transponder installations operating with a Garmin GNS 480 (CNX80) system refer to GNS 480 (CNX80) Installation Manual 560-0982-01 for configuration procedures and operation checks. For transponder installations operating with a Garmin GDL 90 system refer to GDL 90 Installation Manual 560-1049-02 for configuration procedures and operation checks. 3.7.2 Interference Check Turn on and verify operation of all avionics equipment except GTX 32. Then power GTX 32 on and verify there is no interference with any other equipment in the aircraft. The operation/performance checks should be made with all other avionics turned on. Verify that there is no interference during any mode of transponder operation. GTX 32 Installation Manual 190-00303-60 Page 3-5 Revision F