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Becker ACU6100 - Startup and Volume Control

Becker ACU6100
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Operation
Becker Avionics
Volume Adjustment
48 ACU6100 DV64440.03 Issue 09 November 2019
3.3 Start-Up
Excessive pulses on the DC bus of the aircraft may cause damage on electrical
circuits of any installed instrument.
Do not switch ON the device during engine start or shutdown
The ACU6100 powers up with the main system power.
The test routine will be started (test time ca. 4 s)
o The test status LED (yellow) is on.
o The internal circuits and the data transfer between ACU61 and REU6100 will be
examined.
After successful test without failure the test status LED is off.
If a failure was found the test status LED (yellow) flashes.
There are two procedure to continue, if a failure was found:
(1) Push at the “TEST” button the failure will be ignored.
o If there is permanent problem inside the system, it will be found by the continuous
self-test routine and indicated again.
(2) Set the "BACK-UP" switch to slaved or emergency mode (details see "Emergency
Operation" page 60).
Some functions are only available when they are enabled for the user in
the configuration software*.
The scope of functions is variant-dependent.
*For more information refer to the software manual "CSW6100... "(www.becker-
avionics.com/downloads/ → Intercom).
3.4 Volume Adjustment
Main Volume Adjustment
Main Volume Adjustment
The main volume is adjustable at any time.
Turn the outer part of the double rotary knob (VOL) to adjust the volume.
o The main volume adjustment is for all audio channels which are on and
the fixed inputs 4...6.
Figure 16: Operation - Main Volume

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