Documentation Checks; Airplane Flight Manual Supplement; Instructions For Continued Airworthiness; Return To Service - Garmin GI 275 Installation Manual

6.9 Documentation Checks

All checks contained in the previous sections must be completed prior to performing the following checks.
6.9.1

Airplane Flight Manual Supplement

Ensure that the AFMS is completed and inserted in the AFM or POH.
1. Fill in the specific airplane information on the AFMS cover sheet.
2. In AFMS Sections 1.5, 2.2, 2.8, 2.28, 4.2.4, 7, 7.3, 7.10, and 7.15, fill in all applicable check
boxes. More than one box may be checked, depending upon the installation.
6.9.2

Instructions for Continued Airworthiness

Ensure that the appropriate aircraft information in Appendix A of GI 275 Part 23 AML STC Maintenance
Manual/ICA (P/N 190-02246-11) is filled in completely and inserted into the aircraft permanent records.
6.9.3

Return to Service

Complete the return-to-service in a means acceptable to the cognizant aviation authority. An example
would be compliance with 14 CFR 43.9, 14 CFR 91.417 and submission of an FAA Form 337 "Major
Repair and Alteration Airframe, Powerplant, Propeller, or Appliance" completed in accordance with
advisory circular AC43.9-1F, Instructions for Completion of FAA Form 337.
If a GEA 24 P/N 011-02848-01 is connected to resistive fuel quantity probe(s), verify the interface is
installed in accordance with revision 8 or later of this installation manual (refer to Section 3.4.3,
Figure B-8, and Appendix Section C.19). If the interface does not comply, refer to Garmin Service Bulletin
SB2135 for additional information. Once complete, make the following entry in the aircraft maintenance
record (i.e. airframe logbook):
The GI 275 installation in this aircraft complies with Garmin Service Bulletin SB2135,
Modification of GEA 24 Resistive Fuel Probe Interface.
190-02246-10
Rev. 11
GI 275 Part 23 AML STC Installation Manual
Page 6-43