APPENDIX A ASSEMBLY AND INSTALLATION DRAWINGS
GMA 1347D Installation Manual
Page A-5 (Page A-6 blank)
190-00303-21
Revision C
R.063
MAX.
1.59
4X
.130 3.30
100°
.230
4X
.683 17.34
.028 0.70
0 0.00
.450 11.43
3.073 78.04
2X 3.398 86.30
4.533 115.13
.300 7.62
3.073 78.04
2X 3.403 86.42
R.200 5.08
4X
0
0.00
.703
17.84
.670
17.02
2X .620
15.75
2X .265
6.73
.620
15.75
.648
16.45
2X .335
8.51
BEZEL CENTER
CUTOUT CENTER
NOTES:
1. DIMENSIONS: INCHES [mm]
2. IF THE FRONT LIP OF THE MOUNTING RACK IS BEHIND
THE SURFACE OF THE AIRCRAFT PANEL, THE UNIT
CONNECTORS MAY NOT FULLY ENGAGE.
3. RACK MUST BE INSTALLED FROM BACK OF AIRCRAFT PANEL ONLY.
MAXIMUM AIRCRAFT PANEL THICKNESS IS .125 [3.2].
Figure A-3. GMA 1347D Recommended Panel Cutout Dimensions