190-01115-01 G3X™/G3X Touch™ Avionics Installation Manual
Rev. AV Page B-10
6. Rivet the Top Bracket Assembly (115-01017-00) to the Universal Bracket Assembly (115-00939-
00) as shown in Figure B-10 and Figure B-11.
Figure B-10 Lancair IV/IV-P GMU 22 Mounting Bracket Assembly
NOTE
The assembled bracket can be shifted to accommodate for wing dihedral. Figure A-11
illustrates the offset rivet holes which may be utilized to tilt the GMU 22 up (plus) from the
mounting surface or down (minus) from the mounting surface.
Figure B-11 Adjusting for Wing Dihedral
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