Garmin Approach G5 - GPS-Enabled Golf Handheld, Installation Manual

Page: 247 / 285

Garmin G5 Electronic Flight Instrument Part 23 AML STC Installation Manual 190-01112-10
Rev. 21
Page 247
Airplane Make (TCDS
Holder) [common name
or previous make] Airplane Model
Designation Lightning Zone Type (Ref. Appendix F) GTP 59
Location GMU 11
Location Notes
Wing Fuselage Empennage
Boeing Airplane
Company
(Boeing)
[Boeing-Stearman]
A75L3, 75, A75,
B75, E75, A75J1,
A75L300, A75N1,
B75N1, D75N1,
IB75A, E75N1 Not Allowed Figure 6-30,
Figure 6-39
Figure 6-40 Zone 2
[1][3] All (except
wing) [5] [8]
Boeing (The Boeing
Company) [Rockwell
International]
BC-1A, AT-6 (SNJ-
2), AT-6A (SNJ-3),
AT-6B, AT-6C (SNJ-
4), AT-6D (SNJ-5),
AT-6F (SNJ-6),
SNJ-7, T-6G Figure 6-27,
Figure 6-29 Figure 6-30 Figure 6-40 Zone 3,
Zone 2A
[1][2] All
[5][7]
Cessna (Cessna Aircraft
Company)
T-50 (Army AT-17,
and UC-78 series,
and Navy JRC-1) Not Allowed Figure 6-34
(for tube-
and-fabric;
otherwise
not allowed)
Not
Allowed Zone 2A
[1][3] All (fuselage
only)
[5] [8]
Cirrus Design
Corporation
(Cirrus
Design Corporation)
SR20, SR22, SR22T Figure 6-27,
Figure 6-29 Figure 6-30 Figure 6-40 Zone 3
[4] All (fuselage
and emp.),
Zone 3
(wing) [6] [8][10]
Commander
(Commander Aircraft
Corporation)
[ CPAC,
Inc.]
112, 112TC, 112B,
112TCA, 114, 114A,
114B, 114TC Figure 6-27,
Figure 6-29 Figure 6-30 Figure 6-40 Zone 3,
Zone 2A
[1][2] Zone 3, Zone
2A
[5][7]
Costruzioni
Aeronautiche Tecnam
S.P.A.
(Costruzioni
Aeronautiche Tecnam
S.P.A.) [Tecnam]
P2006T Figure 6-27,
Figure 6-29
Figure 6-36 Figure 6-40 Zone 3,
Zone 2A
[1][2] All
[5][7] Existing Attitude
indicator must be
retained. The G5 can be
installed as a secondary
Attitude indicator. The
G5 cannot be installed
as an HSI