
KlNG
KMA
20
/KR
21
MARKER
BEACON RECEIVER/
ISOLATION
AMPLIFIER
TABLE
OF
CONTENTS
SECTIONIGENERALINFORMATION
Paragraph
Page
1. 1
Introduction
1-1
1.
2
Technical Characteristics
1-2
1. 3
Accessories Required
1-6
SECTIONIIINSTALLATION
2.
1
General
2-1
2.2
Unpacking and
Inspecting Equipment
2-1
2.
3
Installation
Notes and
Precautions
2-1
2.4 Installation
Procedure
2-2
2.
5
Marker
Antenna
Installation
2-2
2.
6 KA 40
Installation
(Optional)
2-3
SECTION
III
OPERATION
3.
1 Marker
Beacon
(KMA 20 and KR
21)
3-1
3.2
Isolation Amplifier (KMA
20)
3-2
LIST
OF
ILLUSTRATIONS
Figure Page
2-1
KMA 20 Installation
Drawing
2-4
2-2
KR
21
Instanation
Drawing
2-5
2-3
KA
40
Instanation
Drawing
2-6
2-4
KMA
20
Interconnect Diagram
2-7
2-5
KR
21 Interconnect Diagram (27. BV
DC')
2-9
2-6
KR 21 lnterconnect
Diagram (13. 75VD(')
2-9
2-7
KA
40
lnterconnect Diagram
2-10
2-8
Pin Function
for
000-1024-00
thru
-16
2-11
i

KING
KMA
20/KR
21
MARKER BEACON
RECEIVER/
ISOLATION AMPLIFIER
SECTION
I
GENERAL
INFORMATION
1.1
INTRODUCTION
The
King
KMA 20 is a
compact
transistorized unit
providing the
functions
of
marker
beacon
receiver,
isolation amplifier
and
audio control panel.
The
unit has been
styled
to harmonize with
the
all new
generation
of
Silver
Crown
panel mounted
equipment.
TSO
certification
of the
KMA 20 assures
operation under
varying
environmental
conditions.
The KMA
20 is
designed to
provide
a
uniformly functioning
aircraft radio
system when
utilized
with other
units
of
the new Silver
Crown
line. Although the
equipment is designed
primarily
for use with the KX
170
NAV/COMM unit,
it will also perform
effeciently
with
older Silver
Crown
transceivers and
radios.
Significant
new
features
of
the KMA 20
design
include its
AUTO
switch
feature:
semi-
concealed
marker light
presentation and
its ability
to control COMM and
NAV audio
independently. Automatic
dimming
circuitry
for the marker
lamps,
to
compensate
for
ambient
cockpit
lighting,
is also
incorporated in the design.
Within the KMA 20, the
marker beacon receiver comprises
one
section
of
the
unit.
The
marker
receiver
of
the KMA 20,
available
without
the isolation
amplifier and audio
panel is the KR 21. The
receiver
is
a crystal controlled
superheterodyne
receiver
and
has
excellent
selectivity
and
freedom
from
interference
of
television and FM stations.
Operating controls
for the
marker receiver consists
of
two
toggle switches on the KMA
20: a
HI-LO
sensitivity
and lamp
test control and an
audio
selector
switch. The KR
21
has
only
the
HI-LO
sensitivity
and
lamp
test control. A three light
presentation
is de
signed into the
front
panel of
the unit
with
colored lenses
to indicate passage over
the
markers.
Besides
the
colors,
the stations
are identified
by
the
letters
A-O-M
engraved
on the lenses plus
the
appropriate
frequency
audio
tone.
Should the
aircraft
user
desire
a
a
remote
location for
the
marker
lights,
King
Radio Corporation
manufacturers
an
optional
remote
light
assembly
designated the KA 40
for
use with the KMA
20
only.
The
isolation
amplifier
of
the KMA 20
makes
possible the
combining
of
all receiver
audio
inputs
into
a single cockpit
speaker
with 40db
of
isolation between each
radio. The
input
power levels
of
the
signals are
amplified
to the
level
necessary
to drive a
4 ohm
speaker.
An
electronic
muting
circuit (diode
switch) is provided to
automatically
isolate
the output
of
all receivers from
the isolation amplifier
whenever the microphone
button
Rev.
1,
August, 1972 Page
1-1

KING
KMA 20/KR 21
MARKER BEACON
RECËIVER/
ISOLATION
AMPLIFIER
is
pressed.
This
feature
eliminates
the
possiblity of
audio feedback in the cockpit.
The
amplifier design utilizes
only
one
integrated
circuit
and a
push-pull
output
stage
for
high
reliability.
Audio
control
functions
of the
Silver
Crown
radio
system are
performed at
the
front
panel of the KMA 20. A microphone
selector
rotary
switch,
a
series
of
eight audio
selector switches and a marker beacon
receiver
sensitivity
control are the operating
controls
of
the
unit.
The microphone selector routes audio
and
keying information to
the
selected transceiver or to
a EXT
ramp
hail
speaker or passenger
address system.
The
AUTO switch control
of the
standard
model is
utilized
in
conjunction with the
micro-
phone
selector
switch.
For normal operation
of
the AUTO
switch,
COMM 1 and COMM
2
are placed in
the
center
(off) position. With
the
AUTO
switch in
the
SPEAKER position,
the
receiver
audio selected
is
automatically
controlled
by the operation of
the
micro-
phone
selector.
Thus if
transmitting
on
COMM 1,
receiver
audio
for
COMM
1
will be
routed to the
cockpit
speaker.
This
feature eliminates the constant manipulation
of
COMM receiver
audio
selectors
when
switching
back and
forth
between
transmitters.
Speaker,
off
or
mute,
and
headphone audio
control
of
each of
the
aircraft
radios is
accomplished
with the
remaining
three-position
toggle
switches.
A
series type solid state
regulator
is used to
supply
the regulated
voltage
to
the
marker
receiver and
audio boards
of
the
unit. Since
each aircraft
installation is
wired
for
eithier
13.
75
or
27. 5V operation
of the
unit,
the KMA 20
and
KR 21 are
completely
interchange-
able
between
aircraft with
no
internal
wiring
changes.
1.2 TECHNICALCHARACTERISTICS
MARKER
BEACON
RECEIVER
-
KMA
20/KR
21
SPECIFICATION
CHARACTERISTIC
TSO
COMPLIANCE: TSO C35c Env.
Category
DACAAAX.
CONTROL:
Panel
mounted equipment.
Sensitivity
and
audio selector
controls on
the
front
panel of
the
unit.
DUTY
CYCLE:
Continuous.
INPUT IMPEDANCE: Designed
to
match
50 ohm
antenna.
OUTPUT:
Capable
of
10
milliwatts into
Isolation
Amp-
lifier
input of 5000. Capable
of 6.
25 watts
at
the
4O speaker
output.
Page
1-2
November,
1969

KING
KMA
20/KR
21
MARKER BEACON
RECEIVER/
ISOLATION AMPLIFIER
SPECIFICATION
CHARACTERISTIC
SPEAKER
OUTPUT:
4
ohm
output:
Rated
power
output
is
6. 25
watts at the4ohms
speaker
output.
With
a supply voltage of
27.
Svde,
output
power
capability
increases
to
8 watts.
8
ohm
output:
Rated
power
output
is
6,
25 watts at the 8
ohm
speaker
output. With a supply voltage
at
27.
5
vde,
output
power
capability
increases
to
8
watts.
DISTORTION: Less
than
10a/o
at rated
output.
FREQUENCY RESPONSE:
.
Within 6dh
from 350Hz
to
3000Hz.
KMA 20
GENERAL
POWER REQUIREMENTS:
lnstrument panel lighting: 13. 75V 27.
5V
KMA 20
idle
current:
300ma 150ma
KMA 20
operating current:
1. 1
amps 1.1amps
PHYSICAL DIMENSIONS:
Length: 6. 293
inches
behind instrument
panel.
Width:
6. 2
inches.
Height:
1. 6
inches.
WEIGHT: 2. 3
lbs.
KR
21
GENERAL
POWER REQUIREMENTS:
Idle
Current:
170ma
at 13.
75V
120ma at
27.
5V
Operating Current: 300ma
at 13. 25V
250ma
at
27.
5
V
Panel Lighting:
None
Page
1-4
Rev. 1,
August,
1972