Garmin G5 Installation Manual page 266

Airplane Make (TCDS Airplane Model
Holder) [common name Designation
or previous make]
Zenair (Zenair Ltd.) CH2000
ZLIN Aircraft a.s. Z-242L, Z-143L
(ZLIN Aircraft a.s.)
[Moravan a.s.]
ZLIN AIRCRAFT a.s. ZLIN 526L
(ZLIN AIRCRAFT a.s.)
[Moravan National
Corporation]
[1] The GTP 59 cannot be installed on Zone 2A composite areas.
[2] The GTP 59 must be bonded to the aluminum skin. For details, refer to Section 4.1.7.
[3] The GTP 59 must be bonded to the metallic tube structure. For details, refer to Section 4.1.7.
[4] The GTP 59 must be isolated from the aircraft ground plane. For details, refer to Section 4.1.7.
[5] The GMU 11 must be bonded to the aircraft ground plane. For details, refer to Section 4.5.4.
[6] The GMU 11 must be isolated from the aircraft ground plane. For details, refer to Section 4.5.4.
[7] The GMU 11 may be mounted in the wingtip provided that certain criteria are met. For details, refer to Section 4.5.4.
[8] Nonmetallic aircraft.
[9] Not used.
[10] With the exception of GTP 59, GMU 11, Glareshield mounted GPS antenna wires, all other installed wires must be routed behind metallic
substructure (i.e., routed behind instrument panel/pedestal/circuit breaker panel, along lightning ground bar/strip, inside lightning ground tube, or
along other airframe ground plane).
[11] Only for aluminum wings. Not allowed for wooden wings.
Garmin G5 Electronic Flight Instrument Part 23 AML STC Installation Manual
Lightning Zone Type (Ref. Appendix F)
Wing Fuselage Empennage
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 6-30 Figure 6-40
Figure 6-29
Page 266
GTP 59 GMU 11 Notes
Location Location
Zone 3, All
Zone 2A [5][7]
[1][2]
Zone 3, All
Zone 2A [5][7]
[1][2]
Zone 3, All (fuselage [8]
Zone 2A and emp.),
[1][3] Zone 3
(wing) [5]
190-01112-10
Rev. 21