Garmin GI 275 User Manual

190-02246-10 GI 275 Part 23 AML STC Installation Manual
Rev. 11 Page 3-36
Figure 3-6 Example of Completed Tabulated Electrical Load Form
Sheet 2 of 2
%
÷ Alternator rating (amps):
Ldg Lt ON
(b1)
(a)
Ldg Lt OFF
(b2)
(c) (d) (e)
(< 80%)
Ldg Lt OFF
(< 80%)
Ldg Lt ON
(< 95%)
(< 80%)
N/A N/Ax 100% = Percent of alternator capacity used:
Total current used (amps):
Notes:
Cruise
(Calculated)
Emergency Operation
Operating
Time
Tail Number:Date:
Cruise
60 min
TO/Land
10 min
Land
10 min
Taxiing
10 min
Normal Operation
Circuit
Breaker
Number
Circuit/System
Phase(s) of flight during which circuit/system is used
%
%%
Pass/Fail:
68
45.7
70
60.0
44.7
43.5 34 48.1
86
64
62
[1] Duringtaxiphase,Dutopilotcircuitbreakerisclosedbutautopilotisnotengaged.
N5272K//201
PASS PASS PASS

Garmin GI 275 Specifications

General

Type	Electronic Flight Instrument
Display Type	LCD
Power Input	14 or 28 VDC
Operating Temperature Range	-20°C to +55°C
Brightness Control	Automatic and Manual
Certification	TSO-C113
Interfaces	ARINC 429, RS-232
Mounting	Panel Mount