Garmin GI 275 Installation Manual page 449

CESSNA
A-722 (Cessna Aircraft
Company)
Cirrus Design
A00009C Corporation
H (Cirrus Design
Corporation)
COMMANDER
(Commander Aircraft
A12SO
Corporation)
[CPAC, Inc.]
Costruzioni
Aeronautiche Tecnam
S.P.A.
(Costruzioni
A62CE Aeronautiche Tecnam
S.P.A.)
[Costruzioni
Aeronautiche Tecnam
srl]
Cougar
(Cougar Aircraft
A17SO
Corporation)
[SOCATA, S.A.]
190-02246-10
Rev. 11
T-50 (Army AT-17, and
UC-78 series, and Navy
JRC-1)
SR20, SR22, SR22T
112, 112TC, 112B,
112TCA, 114, 114A,
114B, 114TC
P2006T
GA-7
N/A Not Allowed Figure G-10 Not Allowed Zone 2A Zone 2A
Figure G-3,
Figure G-6 Figure G-18 Zone 3
Figure G-5
Figure G-3,
Figure G-6 Figure G-18
Figure G-5
Figure G-3,
N/A Figure G-10 Figure G-18
Figure G-5
Figure G-3,
Figure G-10 Figure G-18
Figure G-5
[1] [3] [5] [8]
Installation using
Figure G-10 only
allowed for tube
and fabric;
otherwise, Not
Allowed
Zone 3 [4] [6] [8] [11] [13]
Zone 2A, Zone 2A,
[1] [2] [5] [7]
Zone 3 Zone 3
Zone 2A, Zone 2A,
[1] [2] [5] [7]
Zone 3 Zone 3
[1] [2] [5] [7]
Requires GEA 110
Zone 2A, Zone 2A,
for interface to
Zone 3 Zone 3
resistive fuel
quantity sensors.
GI 275 Part 23 AML STC Installation Manual
Page D-6