190-00734-17
GTX 335 w/GPS Installation Guidance
Rev. 1
Page 7-9
7.4 Documentation Checks
7.4.1 Airplane Flight Manual Supplement
Ensure that the Airplane Flight Manual Supplement (AFMS) is completed and inserted in the Airplane
Flight Manual (AFM) or Pilot's Operating Handbook (POH).
1. Fill in the required airplane information in the AFMS.
2. Fill in the appropriate check boxes in the Installation Configuration section of the AFMS as
described in section 4.6.
3. Insert the completed AFMS into the AFM or POH.
7.4.2 Configuration and Checkout Log
NOTE
A checkout log must be completed for each unit in a dual GTX installation.
The configuration log sheet contained in Appendix A of
GTX 33X and GTX 3X5 ADS-B Maintenance
Manual
should be completed during the initial installation and maintained with the aircraft permanent
records.
1. Fill in the General Information for the aircraft and GTX transponders.
2. Calculate and record the change in electrical load.
3. List the equipment interfaced to the GTX transponder.
4. Complete the wire routing diagram that is appropriate for the type of aircraft.
5. Complete the Post Installation Configuration Log that is appropriate for the GTX transponder
type.
6. Create new wiring diagrams indicative of the installation. Or markup the interconnect diagrams
from the Installation Manual detailing which equipment was installed and how it was connected.
7.4.3 Instructions for Continued Airworthiness
Make sure that the appropriate information is filled in on the Instructions for Continued Airworthiness
(ICA), in the GTX 33/330 and GTX 3X5 ADS-B Out Maintenance Manual, and ensure it is completed and
inserted in the aircraft permanent records.
1. Fill out the Configuration and Checkout Log provided in Appendix A of the Maintenance Manual
as described in Section 7.4.2.
2. Insert the Instructions for Continued Airworthiness (section 4 of the Maintenance Manual) and the
completed Appendix A of the Maintenance Manual into the aircraft permanent records.