Garmin GI 275 Installation Manual page 476

Textron Aviation
(Textron Aviation Inc.)
5A4
[Beechcraft
Corporation]
Textron Aviation
(Textron Aviation Inc.)
A23CE
[Beechcraft
Corporation]
Textron Aviation
(Textron Aviation Inc.)
A12CE
[Beechcraft
Corporation]
Textron Aviation
(Textron Aviation Inc.)
TC 779
[Beechcraft
Corporation]
Textron Aviation
(Textron Aviation Inc.)
TC 630
[Beechcraft
Corporation]
190-02246-10
Rev. 11
50 (L-23A), B50 (L-23B),
C50, D50 (L-23E), D50A,
D50B, D50C, D50E,
D50E-5990, E50 (L-23D,
RL-23D), F50, G50, H50,
J50
58P, 58PA, 58TC, 58TCA
60, A60, B60
G17S
18A, S18A
Figure G-3,
Figure G-10 Figure G-18
Figure G-5
Figure G-3,
Figure G-10 Figure G-18
Figure G-5
Figure G-3,
Figure G-10 Figure G-18
Figure G-5
Figure G-3,
Figure G-16 Figure G-18
Figure G-5
Figure G-3,
Figure G-10 Not Allowed
Figure G-5
GI 275 Part 23 AML STC Installation Manual
Zone 2A, Zone 2A,
[1] [2] [5] [7]
Zone 3 Zone 3
[1] [2] [5] [7]
Requires GEA 110
for interface to
resistive fuel
Zone 2A, Zone 2A,
quantity sensors.
Zone 3 Zone 3
The Class I/II
GI 275 variants can
be installed in this
airframe.
[1] [2] [5] [7]
Requires GEA 110
Zone 2A, Zone 2A,
for interface to
Zone 3 Zone 3
resistive fuel
quantity sensors.
Zone 2A, Zone 2A,
[1] [3] [5] [8]
Zone 3 Zone 3
Zone 2A, Zone 2A,
[1] [2] [5] [7]
Zone 3 Zone 3
Page D-33