Weight And Balance; Electrical Load Analysis; Table 3-6. Unit Power Loads - Garmin GMX 200 Installation Manual

3.5 W eight and Balance
2 4 B
Weight and balance computation is required after the installation of the GMX 200. Follow the guidelines
as established in AC 43.13-1B, Chapter 10, Section 2. Make appropriate entries in the equipment list
indicating items added, removed, or relocated along with the date accomplished. Include your name and
certificate number in the aircraft records.
Section 1 .5.1 has the weights for the GMX 200 and GMX 200 I/O.
X X
3.6 E lectrical Load Analysis
2 5 B
An electrical load analysis should be completed on each aircraft prior to installation in accordance with
AC 43.13-1B, Chapter 11 and recorded on FAA Form 337. Use the following values for computation:
GMX 200
Unit Status Max Current @ 28 VDC
Off
On
GMX 200 I/O
Unit Status Max Current @ 28 VDC
Off
On
Note: Unit OFF is defined as the unit has power but is turned off with the front power switch.
Circuits should be protected in accordance with the approved data in this document (see
T able 3-6 ) and the guidelines in AC 43.13-1B, chapter 11, section 4.
X X
Page 3-10
Revision F
F igure D-7. shows the unit dimensions and center of gravity.
X X

Table 3-6. Unit Power Loads

.014 A
1.19 A
.014 A
1.39 A
NOTE
Max Current @ 14 VDC
.023 A
2.29 A
Max Current @ 14 VDC
.023 A
2.56 A
GMX 200 Installation Manual
190-00607-04