Garmin International Inc 01443 Manual De Usuario
GTX 3000 Installation Manual
Page 3-3
190-00926-01
Revision A
3.5 Electrical Load Analysis
An electrical load analysis should be completed on each aircraft prior to installation in accordance with
AC43.13-1B, Chapter 11. Use the following values for computation:
AC43.13-1B, Chapter 11. Use the following values for computation:
3.5.1 Circuit Breaker Placard
Install a Circuit Breaker Placard labeled Transponder or Transponder 1, Transponder 2 as appropriate as
indicated in AC 43.13-2A, paragraph 27c(4).
indicated in AC 43.13-2A, paragraph 27c(4).
3.6 Final Installation
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3.7 Post Installation Configuration and Checkout
The GTX 3000 Mode S Transponder will not provide valid outputs until the
aircraft post installation configuration procedures are completed.
3.7.1 Configuration
When installed as part of the Garmin Integrated Flight Deck, the GTX 3000 transponder must have FAA
approved configuration data. Configuration data is loaded to the GTX 3000 from an aircraft-specific
Software Loader Card. Transponder settings are predetermined for a specific aircraft and are typically
contained within the file named ‘GTX1’. However, the aircraft registration number must be entered
manually.
approved configuration data. Configuration data is loaded to the GTX 3000 from an aircraft-specific
Software Loader Card. Transponder settings are predetermined for a specific aircraft and are typically
contained within the file named ‘GTX1’. However, the aircraft registration number must be entered
manually.
The 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.
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.
ATC Transponder Tests and Inspections.
For transponder installations operating with a Garmin GNS 480 (CNX80), refer to GNS 480 (CNX80)
Installation Manual, 560-0982-01 for configuration procedures and operation checks.
Installation Manual, 560-0982-01 for configuration procedures and operation checks.
3.7.2 Interference Check
Turn on and verify operation of all avionics equipment except GTX 3000. Then power the GTX 3000 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.
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.
Table 3-3 Unit Power Loads
GTX 3000 Input
14 Vdc
28 Vdc
Typical
Max.
Typical
Max.
GTX 3000 Main Power
1.6 A
3.2 A
0.85 A
1.6 A
NOTE
DRAFT