GI 275 Part 23 AML STC
190-02246-12 Rev. 4
Airplane Flight Manual Supplement
Page 3 of 70
FAA APPROVED
4
8
Corrected table formatting
See Cover Page
10
Added clarification of Standby Reversionary
capabilities
11
Added clarification of EIS configuration to
include all EIS capabilities and display
parameters
12
Included VFR GPS antenna and Backup
Battery Pack as GI 275 system components
13
Added clarifications for Standby instrument
configurations with the GI 275; Clarified
reversionary function when configured as a
Standby instrument; Added Battery Charge
Inhibited system message description
14
Added ADI to the Definitions
15
Added a table to identify AFMS section
applicability based on specific system
installation
16
Added tickbox for GI 275 primary heading
installations; Clarified magnetic variation
limits for configurations with GI 275 as
primary heading source
17
Added GPS aiding system message
description; Clarified limitations of aerobatic
maneuvers for primary and standby ADI
configurations; Added clarifications for battery
capacity required for aircraft above 25,000ft
service ceiling
18
Added clarification that QFE altimeter setting
is incompatible with GI 275 instrument; Added
tickbox selections to define specific system
installation and configuration; clarified loss of
control warning for IMC flight
19
Clarified sensor selection applicability to
Garmin cross-comparison AHRS and ADC
sensors
21
Clarified VFR GPS functionality and
limitations; Removed powerplant gauge
markings section
22
Added original flight instrument requirements
for GI 275 system when installed with non GI
275 standby instruments
23
Added External EIS Annunciator requirements
for GI 275 EIS systems; Added requirement to
test any installed annunciator; Added section
for recording placards that are removed or
modified
25
Added a note to clarify that not all emergency
procedures may apply to a specific installation
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