Honeywell BENDIX/KING KY 97A - Dual KY 96 A with KA 25 A Interconnect

B KY 96A, KY 97A
Rev 4, Apr 2003 IM 006-00674-0004.dwd Page 2-25
FIGURE 2-12 Dual KY 96A with KA 25A interconnect
(Dwg No 155-01585-0000 Rev AA)
COMM I
P/N
030-01094-0080
K
y
9
6
A
MIC INTERCOM - N/C
(SEE
NOTE 8)
SQ. TEST AND COMPRESSION TEST - N/C
+28 LIGHTING HI
N/C
DET.
AUDIO OUT
DIM SELECT (NOTE 9)
(SEE NOTE 8)
AIRCRAFT POWER {SEE NOTE 6) __ Q __ 27.5V A/C PWR
SWITCHED A/C POWER ----------,
27 .5V POWER {SEE NOTE 7 l
4
OHM AUDIO HI {SEE NOTE 10)
4
OHM AUDIO LO
AUX AUDIO HI IN I
AUX AUDIO HI IN 2
AUX AUDIO HI IN 3
AUX AUDIO LO
POWER GROUND {SEE NOTE 6) ~
COMM I
COMM 2
...
y
P/0 P251
5001\. AUDIO OUT ------------------,-----------------+--+--1
AUDIO GROUND
MIC GROUND
MIC AUDIO
,~----.!.----------- MIC KEY
il
MIC KEY------------- ...... ---- .... ··--!-'--,
,_,
PIN 030-02002-0000
K
A
2
5
A
A+ {13.75 OR 27.5VDC) +lo20 AWG
SPEAKER
4
OHM SPEAKER LOAD
4 OHM SPEAKER LOAD
MIC AUDIO IN
AIRFRAME GROUND +lo20 AWG ~
500 OHM AUDIO IN
N/C
-MIC INTERCOM
(SEE NOTE 8)
N/C - SQ. TEST AND COMPRESSOR TEST
+2BV LIGHTING
HI
N/C
DET AUDIO OUT
DIM SELECT
{SEE
NOTE B l
27.5V
A/C
PWR __ Q __ 27.5V AIC POWER {SEE NOTE 6)
..-- SWITCHED A/C POWER
L_ 27. 5V POWER {SEE NOTE 7)
4 OHM AUDIO HI (SEE NOTE 10 l
4
OHM AUDIO LO
AUX AUDIO HI IN I
AUX AUDIO HI IN 2
AUX AUDIO HI IN 3
AUX AUDIO LO
~ POWER GROUND {SEE NOTE 6)
,_,
:r
AUDIO GROUND ------------------------------------------------------~~,
,_,
XMIT REC INTERLOCK {SEE NOTE 5 l
ANT RG 400
NOTESo
1. SELECTOR SWITCH. DOUBLE POLE - DOUBLE THROW DPDT (TD- BE SUPPLIED BY INSTALLER).
2. ALL WIRES #24 AWG UNLESS NOTED.
3. TERMINATE AUDIO SHIELDS AT ONE END ONl'V AS SHOWN.
4. PIN # IN PARENTHESIS ARE COMMON.
5. TX·RX INTERLOCK WIRING NECESSARY WHEN BOTH COMM ANTENNAS ARE TOP MOUNTED. WHEN
BOTH COMM ANTENNAS ARE BOTTOM MOUNTED. OR IN DUAL COMM INSTALLATIONS IN FABRIC
AIRCRAFT. REFER TO ANTENNA INSTALLATION RECOMMENDATIONS.
6. AIRCRAFT POWER WIRING SHOULD BE TWO #18 AWG TO THE CIRCUIT BREAKER AND POWER
GROUND .SHOULD BE TWO #18 AWG TO GROUND.
7. ~~~TE~H~ ~Fr:~~~R;_;hN~:~~~~~-13, AND 27.SV POWER, PINS N AND 12, MUST BE JUMPEti:D
8. REMOTE FREQUENCY TRANSFER/REMOTE CHANNEL INCREMENTo A MOMENTARY GROUND AT PIN
L WILL CAUSE THE RADIO TO INCREMENT TO THE NEXT CHANNEL IN MEMORY AND DISPLAY IT
IN THE STBY WINDOW. A MOMENTARY GROUND AT PIN 11 Will TRANSFER THE USE AND STBY
FREQUENCIES. A TWO POSITION SPRING LOADED ROCKER SWITCH OR TWO SEPARATE
MOMENTARY PUSHBUTION SWITCHES MAY BE USED AT THE INSTALLER'S OPTION.
P96A1
fl1-AGC TEST/REMOTE INC____.
~REMOTE TRANSFER----e ~
4 OHM AUDIO ---£+-,-(1 CABIN
~SPEAKER
MIC AUDIO
L--------------------------------------------------------------------------------------------------------------------MIC KEY
9. FOR TRACKING OF 28V LIGHTING BUS. CONNECT DIM SELECT (PIN A) TO GROUND.
WHEN PANEL DIMMER IS TURNED ALL THE WAY DOWN BACKLIGHTING GOES TO HALF BRIGHTNESS. If
CONTINUOUS HALF BRIGHTNESS IS DESIRED PIN A CAN BE CONNECTED TO AIRCRAFT SUPPLY. IF NO
CONNECTION IS MADE TO THE PANEL DIMMER BUS AND DIM SELECT, THE BACKLIGHTING WILL BE AT HALF
BRIGHTNESS.
10. ~~1 ~AO~~~~~i ~i}~~1·~~~~~J~?66~~r1~Eu::o-4~~~~:~1Lt:~~ .. RATED AUDIO IS !iOmW AT
XMIT REC INTERLOCK {SEE NOTE 5)
ANT RG 400
Dwg 155-01585-0000 Rev AA
H
7
COMM 2
PIN
030-01094-0080
K
y
9
6
A