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Garmin G5 Electronic Flight Instrument Part 23 AML STC Installation Manual
190-01112-10
Rev. 21
Page 266
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
Zenair
(Zenair Ltd.)
CH2000
Zone 3,
Zone 2A
[1][2]
All
[5][7]
ZLIN Aircraft a.s.
(ZLIN Aircraft a.s.)
[Moravan a.s.]
Z-242L, Z-143L
Zone 3,
Zone 2A
[1][2]
All
[5][7]
ZLIN AIRCRAFT a.s.
(ZLIN AIRCRAFT a.s.)
[Moravan National
Corporation]
ZLIN 526L
Zone 3,
Zone 2A
[1][3]
All (fuselage
and emp.),
Zone 3
(wing) [5]
[8]
[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.