Garmin G5 Installation Manual page 28

14. Using the tabulation completed above, switch on all continuous electrical loads which are used for
the normal cruise phase and record the current measured by the ammeter (measurement (c) in
Figure 3-3).
15. Using the tabulation completed above, switch on all continuous electrical loads used for the
emergency cruise phase and record the current measured by the ammeter.
16. Using the tabulation completed above, switch on all continuous electrical loads used for the
emergency landing phase and record the current measured by the ammeter.
17. Using the values measured and recorded, complete the ELA using the blank form in Figure 3-2
and Figure 3-3.
18. Verify the maximum electrical load does not exceed 80% of the electrical system capacity. See
example in Figure 3-4 and Figure 3-5.
NOTE
Electrical loads in excess of 80% but not greater than 95% of electrical system capacity are
permitted during the takeoff/landing phase of flight when landing light(s) are switched on.
Garmin G5 Electronic Flight Instrument Part 23 AML STC Installation Manual
Page 25 of 53
190-01112-10
Rev. 2