Appendix D Model-Specific Data - Garmin GI 275 Installation Manual

APPENDIX D MODEL-SPECIFIC DATA

Table D-1 Aircraft Model-Specific Data ...............................................................................................D-2
This appendix provides the following information for every model listed on the AML:
• GI 275 Installation Limited to MFD/Standby ADI: An "X" in this column indicates that only
installations of the GI 275 as an MFD/Standby ADI are approved for this model; refer to
Section 2.1.12 for more information
• Fuel Pressure Check Required: An "X" in this column necessitates a Fuel Pressure Check be
performed per Section 3.4.3, item 7. The Fuel Pressure Check only applies to piston aircraft with
fuel flow transducers installed per this STC
• Lightning Zone Wing, Fuselage, and Empennage: Each column references the lightning zoning
figures from Appendix G that are applicable to a particular aircraft model
• GTP 59 and GMU 11/GMU 44B Location: Each column references the suitable lightning zones
for installation of the GTP 59 Temperature Probe and GMU 11/44B Magnetometer in a particular
aircraft model. For additional information, refer to Section 4.6.2 for GTP 59 and Section 4.6.1 for
GMU 11 and GMU 44B
• Notes: This column includes any notes related to a particular aircraft model
NOTE
Any aircraft model listed in Table D-1 and not explicitly called out as nonmetallic by an
end note should be considered an all-metal aircraft.
190-02246-10
Rev. 11
GI 275 Part 23 AML STC Installation Manual
Page D-1