Garmin GI 275 Installation Manual page 454

Gomolzig Flugzeug-
und Maschinenbau
GmbH
A34EU (Gomolzig Flugzeug-
und Maschinenbau
GmbH)
[FFA Aircraft Bravo AG]
GROB Aircraft AG
(GROB Aircraft AG)
A57EU
[GROB Aerospace
GmbH i.l.]
Grumman
TC 654 (Grumman American
Aviation Corporation)
Helio
(Helio Aircraft
3A3
Corporation)
[Taylorcraft]
HELIO
(Helio Aircraft, LLC)
1A8
[Alliance Aircraft Group,
LLC]
190-02246-10
Rev. 11
AS 202/15 "BRAVO" , AS
202/18A "BRAVO" , AS
202/18A4 "BRAVO"
G115, G115A, G115B,
G115C, G115C2, G115D,
G115D2
Grumman G-21,
Grumman G-21A
15A , 20
H-250, H-295 (USAF U-
10D), HT-295, H-391
(USAF YL-24), H-391B,
H-395 (USAF L-28A or U-
10B), H-395A, H-700
Figure G-3,
X Figure G-6 Figure G-18
Figure G-5
Figure G-4,
Figure G-6 Figure G-18 Zone 3
Figure G-5
Figure G-3,
N/A Figure G-10 Figure G-18
Figure G-5
Figure G-3,
Figure G-6 Figure G-18
Figure G-5
Figure G-3,
Figure G-6 Figure G-18
Figure G-5
Zone 2A, Zone 2A,
[1] [2] [5] [7]
Zone 3 Zone 3
[4] [6] [8] [11]
Installation
approved for VFR
operation only.
Zone 3
Interface to
resistive fuel
quantity sensors is
not approved in this
aircraft.
Zone 2A, Zone 2A,
[1] [2] [5] [7]
Zone 3 Zone 3
Zone 2A, Zone 2A,
[1] [3] [5]
Zone 3 Zone 3
Zone 2A, Zone 2A,
[1] [2] [5] [7]
Zone 3 Zone 3
GI 275 Part 23 AML STC Installation Manual
Page D-11