Figure G-18 Zoning For Empennage - Garmin GI 275 Installation Manual

G.2.3 Empennage
If the GTP 59 and GMU 11/44B cannot be mounted in other areas of the aircraft that are Zone 3 locations,
it is acceptable for metal aircraft with one of the three traditional empennages shown in Figure G-18 to
mount the GTP 59 or GMU 11/44B in the Zone 2A area of the tail. However, the GTP 59 or GMU 11/44B
cannot be mounted on/under any non-conducting surfaces. If the complete empennage of the aircraft being
considered does not match those shown in Figure G-18, then it should be mounted in allowed areas defined
for the fuselage and wings. If only portions of the empennage shown below match, then the same rule
applies and the GTP 59 or GMU 11/44B cannot be installed in the empennage. Note that it is allowable for
only the horizontal stabilizer tips to differ from those shown in Figure G-18. The GTP 59 cannot be located
in the horizontal stabilizer of the empennage. Neither the GTP 59 nor the GMU 11/44B can be mounted in
the tail of a composite empennage.
A B C
D (APPLIES TO A) E (APPLIES TO B AND C)

Figure G-18 Zoning for Empennage

190-02246-10 GI 275 Part 23 AML STC Installation Manual
Rev. 11 Page G-18