Austro Engine E4 Series - Page 348

E4 Series
Maintenance Manual
Engine Control
System
Page 12
E4.08.04
Rev.29
76 – System Description
01-Jul-2020
Activation of the self-test via the Self-test push-button is only be possible if the VOTER Switch is in
AUTO Position (logical AND relation).
During the whole Self-test the push-button must remain pressed.
(For particular installation refer to the applicable Aircraft Maintenance Manual)
Fig. 76 - 9 Self-Test Wiring