KING KR 21 - Page 49

030-0061-00
OR
030-0101-00
030-0101-00
OR
030-0061-00
Pl73
P173
NAV
NAV
-
ANT
ANT
030
0061-00
OR
030-0101-00
030-0101-00
OR
030-0061-00
P17
P172
COMM
COMM
ANT
ANT
030
2101-06
030
2061-00
030-2101-04
030-2146-00
Pl7
P/O
P201 P20 .
P/O
P171
P171
P/O
9651
-
SPEAKER OUTPUT
7
---
SPEAKER
OUTPUT
--ONE
MHE MO 14
34
--COMM
5000
OUTPUT
(COMM
2)--
15 14
---COMM
5002 OUTPUT (COMM
1)--
3A 23
--DME
HRz M1 15
35
--NAV
5000 OtfrPUT
(NAV
2)----
29
16
--NAV
5000
OUTPUT
(NAV 1)
35
24
--DME
MHz M2 16
39
MIC
AUDIO (COMM
2)
28 27
MIC AUDIO
(COMM
1)
p
39
25
--DME
MHz
M3 17
K
K
40
-MIC
KEY (coMM 2)
26
25
MIC
KEY (COMM
1)
9
40
27
--DME
KHz KO
32
N
X
5
-
50KHz ILS
19
WHITE LAMP
SEE
NOTE
14
""¯
28
--
DME Hz K1
33
22
-
DME MHz MD
-
20
BLUE LAMP
-
29
--DME
Hz K2 3A
23
-DME
MHz
MI---
21
AMBER
lAMP
(SEE
NOTE7
30
--DME
Hz
K3
35
5
24
-
DME
MHz
M2---
22
Au PA
SPEAKER
31
--DME
50KHz 36
25
--
DME
MHz
M3
K
5
NON-SHITCH
500 ohm INPUT
.
K
32
--
DME SWITCHING COMMDN
22
27
--
DME
KHz KO
INc
M
2
INST
LIGHT
DIMMER-
13.75VDe X 5
--
50KHz
ILS-NC
K
28
-
DME
KHz
Kl---
3
INST LIGHT DIMMER
DœMNT
L
42
--
SPARE
X
29
-
DME
KHz
K2---
4
A/C POWER--#20AWG
30
--
DME KHz
K3--~
0
9
RAMP
HAILER 89(SEE
NOTE
IS)
5
36
---
AUX AUDIO
#1-----
NC
31
-
DME
50KHz
-,
8
SPEAKER
IDAD
COMMON
y
E
10
37
--AUX
AUDIO
#2-
NC
(NGTE
12)
32
-
DME SWITCHING
COMMON
---
NC
1
AIRFRAME GROUND #16nWG 15
-
Aux AUDIO
#3
-
Nc
2
--
+10.0VDC
G.S.
SWITCHING-
NC
10
AIRCRAFT SPEAKER
42
.
K
is
--
Aux aunto
es-
ac
6
--
0.1MHz CONTROL
--
12
HF MIC
AUDIO
7
--0.3MHz
CONTROL
-
24
HF MIC
KEY
8
-0.5MHz
CONTROL
-
13
HF
(RADIO
T£LEPHONE)
5002
INPUT
9
-
0.7MHz CONTROL
--
30
ADF
5000 INPUT
(SEE
NOTES
13 & 14)
10
-
0.0MHz
CONTROL
--
NC
31
DME
5002 INPUT
11
--
108MHz CONTROL
--
32
HEADPHONES
12
--
109MHz CONTROL
--
17
R
MIC
13
--
110MHz
CONTROL
--
18
16
--
111MHz CONTROL
--,
11
.
MK
36
--
AUX AUDIO
#1----
NC
23
EED
L1
14)
37
--
AUX AUDIO
#2-
NC
(NOTE
12)
15
--
AUX
AUDIO
#3---
NC
Kl(032-0008-00
14V)
16
--
AUX AUDIO
#4-
NC -01
28V)
21
--
POWER GROUND
#16AWG--
SFE
NOTE
7
FOR 27.5VDC
OPERATION
42
--
SPARE
P/O £1
C
33
--
INST LIGHT
DIMMER---13.75VDC
DIMMER
CONTROL
INST
LIGHT DIMMER
-
33
38
--
INST LIGHT DIMMER
INST
LIGHT DIMMER
38
20
--
A/C
POWER---#16AWG
13.75VDC
1
--
NAV 13.75VDC
INPUT
#16AWG-
A/C
POWER
26
--
NAV SWITCHED
13.75VDC-NC
17
--
COMM SNITCHED A/C EDWER
#16AkG
C C
REAKE
SWTCH
18
--
COMM 13.75VDC
INPUT #16AWG
COMM SWITCHED A/C POWER #16ANC
---
17
CR 1
7-6021-00)
4
--
ILS ENERGI2E
COMM
13.75VDC INPUT #16AWG 18
19
--
ILS COMMON
---
3
--
VOR/1ßC OUT
13.75VDC
A/C EOWER
#16AWG-----
20
A/C POWER
5A
030-2106-01
P7C1
2A
AA
--
VOR/LOC
IN
NAV 13.75VDC
INPUT-
#16AWG•-
1
R
ILS COMMON
----....
#16AWG
POWER
GROUND 21
DD
ILS
ENERGIZE
---
SWITCHED
A/C POWER
NAV
SWITCHED
13.75VDC-
26
X
+10.0VDC
G.S.
3HITCilIll:;
2
A
0.11tile
tullTROL
6
E
--0.3MHz
CONTROL
7
-iŠMiiz
CONTRÕL
P
--
0.7MHz
CONTROL
U
--
0.9MHz
CONTROL
10
D
--
108MHz
CONTROL
11
J
--
109MHz CONTROL
12
N
---
110MHz CONTROL
13
T
--
111MHz
CONTROL
1'
K
Y
--
POWER GROUND (#22AWG)
030-2070-00
VOR/IDC OUT
---
3
N
3
es21
---
ILS
ENERGI2E--
4
FF
--
STATOR D
-ILS
COMMON-----
19
HH
--
STATORE a D
0
oso-2ost-oo oso-21er
ao
LL
--
STATOR F F
P/O
P1001 P/O P1001 P201
MM
--
STATORG
E
--POWER
GROUND
18
26
--•
+
VOR
FLAG
T
---ILS
ENERGIZE
3
10
-- -
TOR FIAG
_q
CC
--
ROTOR C
B
BB
--
ROTOR
H A
VOR/LOC
IN
1
9
-
+
TO
t
K
2
29
---
+
raon
.
SS
--+
W
W
a.
11
A
ROWR
H Z
W
--
+
PRC11 X
i
i
27
ROTOR C
T
JJ
--
-
VOR FMG T
N
NN
y
+
VOR FMG S
5
12
,
staron
o
aa
|
NOTE
5
28
STATOR
F
V
'¯'
O
4
13
STATOR E
,
K
L
-- -
G.S. FMG
V
n
29
STATOR D
X
r
|
Fy
+
G.S.
F1AG
U
23
+
LEFT
1
I
B
- -
NOTE
5
24
DOMHY
IDAD
,
m
EE
--
+
RIGHT
M
8
DUMMY
IDAD-#
NOTE
8
KK
+
LEFT
N
7
+
RIGHT
Ê
r
NOTE 5
-
O
I
UU
--
S
--
+
UP
P
ILS ENERGIZE U
M
-g
+
DOWN B
H
-
4
NOTE
5
L
c
-A
i
G.S.
FLAG FF
RR
--
REFERENCE
PRASE
FOR
G.S. FIAG GG
VV
--
VARIABLE PRASE
TUTING
i gg¡gi
NOTES:
1.
UNLESS NOTED,
ALL WIRES
#24AWG
HINIMUM.
7, 27.3VDC
OFERATION
2. ALL
ANTENNA
COAX IS RG58A/U.
EX175/XX 1755
3.
UNLESS
OTHERMISE
SPECIFIED,
ALL SYSTEM GROUNDS ARE AIRFRAME
GROUNDS.
P
P171
4. THE
KA47 MAY
BE USED 10 CONVERT
KIl75/KIl75B IttE
SWITCHING
OITTPUT
TO
GIANNEL
2 OUT OF
33
--
INST LIGHT
DIMMER-NC
SCODE DME'S. 38
--INST
LIGHT
DIMMER---27.5VDC
DIMMER
CONTROL
5.
KN70
JUMPER
P1NS
AS
INDICATED
FOR
REQUIRED
NUHBER
OF EXTERNAL IDADS.
20
--A/C
POWER #16AWG
7.5VDC
A/C PONER
EXTERNAL
GLIDES1ßPE VOR/LOC
2A
LOADS DEV FIAG DEV FIAG
17
--COMM
SNITCHED A/C EONER #16AWG
OUTPUT
INPUT
ONE
M
F
KK NN
18
--COB91
13.75VDC
INPUT
#16AWG--
A
A
H B
PP
TT
(1,
SA
CORTINUOUS)
C
UU XX
(5.0A
201 DUTY
FACTOR)
y
KA
39
G
TWO M NONE
KK
NN
1
--NAV
13.75VDC
INPUT
#16AWG--
B
B
---
H
PP
TT
..... (0.75A
CONTINUGUS)
THREE NONE
NONE NONE
6.
POWER BUSS
CIRCUIT
BREAKERS ARE
TO
BE MOUNTEDIN THE
AIRCRAFT BREAKER PANEL
OR
INSTRUMENT
PANEL SUCH TRAT THEY
WILL
BE
ACCESSIBLE IN
FLIGHT AND SAFE
FROM
PHYSICAL
IMMAGE,
KMA20
P/O
P201
10. RAMP
HAILER AND
AIRCRAFT SPEAKER RETURN
LEADS SHOULD BE
CONNECTED
TO
PIN
1 2 INST LIGHT
DIMMER-27.5VDC
DDetER
CONTROL
AT
KMA20,
RAMP
HAILER OUTPUT (Pin
9)
TO
BE TERMINATED
WITH 7.52
5
WATT
IDAD
3
INST LIGHT
DIMMER-NC
RES1STOR
WHENRAMP HAILER
15 NOT USED"
11. EXTERNAL
SWITCHING
CAPABILITY: COMM
-
PIN 17
-
NONE
8.
KN74
-
FOR ONE
INDICATOR JUMPER PINS 7, 8.
AND
24.
NAV
-
PIN
26
-
300MA
FOR TUD
INDICATORS
JUMPER
PINS 7
AND
8.
12. AUXILIARY
AUDIO #2 IS
INTERŒlM
MIC
INPUT
ON
KX175B.
FOR THREE INDICATORS NO
JUMPER REQUIRED.
13.
OPTIONAL
INTERCONNECT
FOR BOOM
MIC O
HEADSET
INSTALIATION.
9. KNGS DME INDICATOR (KI265) NGE SHOWN.
16.
IF STANDARD
3-WIRE
MICADPHONE
PLUG IS
USED, THE
FRAME
SHOULD
BE
INSULATED
BY
16.
REMOTE OPTION
FOR VERSIONS
-00/-15
(MARKER
LIGHT
OUTPUT)
WASHERS TO AVOID
INTRODUCING NOISE
INTO MIKE
AUDIO.
FOR
-16
VERSION
THE
lAMP
OUTPUTS BECOME:
PIN 21 has no connection
15.
KEEP
GROUND SEPARATE FROM
KMA
20
GROUND,
PIN
20 has no connection.
PIN 19
MARKER RADIO 5002
INPUT