Garmin G5 Installation Manual page 247

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