190-02246-11
GI 275 Part 23 AML STC Maintenance Manual
Rev. 1
Page 2-4
2.1.7 Electrical Load Information
Electrical load information for the GI 275 system LRUs is provided below. Appendix A of this document
contains details specific to the load changes for the specific aircraft installation.
Table 2-2 GI 275
LRU Electrical Load
Notes:
[1] All GI 275 current draws include the GMU 11/44B and GTP 59.
LRU
Current Draw
[1]
14V System
28V System
Typical
Maximum
Typical
Maximum
GI 275 Base (without battery)
0.65 A
0.75 A
0.32 A
0.40 A
GI 275 Base (with battery)
0.65 A
1.70 A
0.32 A
0.80 A
GI 275 ADAHRS
0.75 A
2.00 A
0.35A
1.00 A
GI 275 AP
0.80 A
2.00 A
0.40 A
1.00 A
GEA 110
0.30 A
0.60 A
0.15 A
0.30 A
GEA 24
0.20 A
0.40 A
0.10 A
0.20 A
GSB 15 (charging from both ports)
1.30 A
2.86 A
0.63 A
1.43 A
