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Bendix/King KY 196 - KY 196;196 E Interconnectdiagram with KA 25 A; To Provide 4 Ohm Speaker Output; Ky 196;196 E

Bendix/King KY 196
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KING
KY 196/196E/KY 197/197E
VHF COMMUNICATIONS TRANSC~IVER
COMM
NO. I
KPN 030-1094-SS
PI96
K
Y
I
9
6
I
K
Y
I
9
6
E
#1
F XMIT REC INTERLOCK
(SEE
NOTE
7)
B 500n ALOIO
(VT
N/C-SPEAKER LOAD (16-)
C
' ,', ~IC Au.JIO~'
4 ~.: MIC KEY. I
3 MIC
Gt.[)
2
NAV1 AUDIO
n
y
,-; MIC ALOIO
"'--'"='--
MIC KEY
. (SEE NOTE 10i
I N/C-
_13.7SV.
~MIC INTERCOM-N/C
(SEE
NOTE
2)
L- 13.1S/21 .~:
.
:LECT
I
PIC PI341
KPN 030-1094-05
PIO PI341 XMIT REC INTERLOCK (SEE NOTE 7
5000 ALOIO OUT
SPEAKER LOAO (161).)-NIC
MIC ALOIO "2
~IC KEY
"2
MIC
GI()
NAV2AUDIO-
CABINSPKR--B--r"1./1 CABIN
SPEAKER
SPEAKERLOADGND(lBAWG)
(SEE NOTE 10
AIRFRAIE
GI() I
",lS0lG --:1
N/C
N~-MIC INTERCOM
INSTR
LIGHTING::;:;;:--l
(SEE NOTE
2)
AUX. AUDIO500.n.-NC
-=
NIC-SQ.TEST
AUX.MICKEY-NC
21.SV DI*ER
INSTR LIGHTING
CONTRa-
i
HEADPHONES-€>v
~
(SEE NOTE 10
Z7.5V ---
27.5V AC POWER
AC
!
PMRTAoP
I
smc~:::::::
(SEE NOTE')
21 . SV POftER
V
13
. ~ .-.
RAMP HAILER
4
SPEAKER ','.
OR
P.~A~
LOAO I
\ r (SEE NOTE
8)
AUX.MIC Al.JDI~..., .b
INT/HAILIN ~
RAMP
HAI~ER
'-
<3-{A
-'-f
.DN
(SEENOTE3)
GOFF
:CMo1AN7" 2
-
ANT
RG-5e
..
14
IS
22
21
2
18
5
6
AC POI,ER AC POIIER
SQ. TEST -
NIC
21 . sv ...
2OM'G
(SEE NOTE
10)
W
16
20
1
A
1
L
10
Z?::'V AC~.:.
27.5V._
(SEE NOTE
8)
7AMP AC POWER
SI,ITCHED
.
AlC POWER
-,
'II'
16AWG
(SEE NOTE')
ADF /lL()IO 5Don.
21.5v POI.ER
DME ALOIO SOO.n.
MXR AUDIO SOO.n.
PQl\ER GRO!W--, DIRECT AUDIOSOOt>.
(SEE NOTE
8)
~
DIRECT
DIRECT
M
A
F
Pl962
ANT
NOTES
1. OLL WiRES 'JQ 24A'G
UNLESS NOTEC.
~IC INTERCOM IS NOT USED. !NTERCOM IS PROVIDED BY USING RAI'P HAILER OR PO SIDETQNE IN EXT.
I()QE
~ KA 134.
IF RAMP HOlLER
()R
PA S!DETONE IS DESIREQ FOR INTERCOM. ROMP HAILER OR PA SPEOKFR OUTPUT PIN 13. MUST BE
TERt.lINATED TI-fiOUGH A SP!!TCH
TO A LOAO
RESISTOP.
POWER BUSS CIRCUIT BREOKERS ORE TO BE M'JL~TED IN THE AIRCRAFT BRUKER PANEL OR INSTRUMENT PANE.t. SUCH THAT
iHEY I'\ILL
BE: ACC~SSIBLE I~ FLIGHT Af'l.) SAFE FROM PHYS!CAL DA~GE.
UNLESS OTHERWIS<: SPECIFIED ALL SYSTEM GROUNDS ARE AIRFRAME GROUNDS
PIN NUMBERS IN PARENTHESES ARE ALL COMMCN.
TX-RX INTERCONNEc:T WIRIN. IS NECESSARY WHEN BOTH COMM ANT. ARE TOP MOUNTED, BOTH CDMM ANT. ARE
BOTTOM MOUNTED OR IN DUAL COMM INSTALLATIONS IN FABRIC AIRCRAFT. REFER TO ANTENNA INSTALLATION
RECOMMENDATIONS.
8. AIRCRAFT POWER WIRING SHOULO BE TWO""8AWG TO THE CIRCUIT BREAKER AND POWER GROUND SHOULD
BE
TWO""B
AWG TO GROUND.
9. SWITCHED A/C POWER, PINS J AND BAND 27.SV POWER PINS HAND 7 MUST BE JUMPERED TOGETHER
WITH
'*
20 AWG MINIMUM.
10. FOR REMOTE FREQUENCY TRANSFER/REMOTE FREQUENCY RECALL (064-1021-10/11/12)
OR FIE!..D
,,"Or> 15. A MOMENTARY GROUND AT PIN E WIL!.. CAUSE THE RADIO TO INCREMENT
TO THE NExT FREQUENCY IN MEM0RY AND DISPLA': IT IN THE srBY WINDOW. A MOMENTARY
GROUND
AT PIN 6 WILL TRANSFER THE USE AND ST9Y, FREQUENCIES. A TWO POSITION
SPRING LOADED ROCKER SWITCH OR TWC SEPARATE ~},orI.ENTARY PUSHSUTTQN SWITCHES
Mt.Y BE USED t..: THE INSTALLERS OPTICiJ.
Pl961
W
AGC TEST/REMOTE
6 REMOT~ XFER
INC~
::::;;-<>i
0 R
o
~
FIGURE
TO
2-11 KY 196/196E INTERCONNECT DIAGRAM WITH
PROVIDE 4 OHM SPEAKER OUTPUT, RAMP HAILER,
(Dwg. No. 155-1324-00, R-5)
KA 1~4 (27.5VDC)
A~O INTERCOM
Rev. 3, September, 1983
IMOO35-4
OOMMNO.2
KPN 030-1094-55
Pl961
F
B
E
K
Y
I
9
6
I
K
y
I
9
6
E
D
K
9
J
S
H
#2
1
L
10
Pl962
Page 2-25
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