Installation
Becker Avionics
Aircraft Wiring
32
RCU6512
DV17551.03 Issue 03 June 2020
RT6512 with RCU6512 as Primary Controller
Figure 9: RT6512 with RCU6512 as Primary Controller
Ai
rc
raf
t P
ow
er
G
round
CB
CB
10 A
5 A
Dim
B
us
-
Dim
B
us
+
Ai
rc
ra
ft
P1 (male)
P1 (male)
RT6512
RCU6512
AWG22/24
AWG22/24
AWG22/24
AW
G
22/
24
AW
G
22/
24
AW
G
22/
24
AWG22/24
AWG24/26 Twisted Pair, shielded
AWG24/26 Twisted Pair, shielded
AWG20
AWG20
AWG22
AWG22
AWG22
AWG24
AWG24
AWG20
AWG20
Not
in us
e f
or
this
ins
tallat
ion c
onf
igur
at
ion
AW
G
24/
26
Twis
ted P
ai
r, s
hielded
AW
G
24/
26
Twis
ted P
ai
r, s
hielded
Note
Note 1
Optional
connection
Bonding
Terminal
*Installation switch
(INS_SW)
INS
_S
W
*
Note 1
Grounding connection:
Electrical GND to
connectors metal hood
Existing Audio System
Aircraft Power 28 VDC
(from Avionic Master)