BENDIXKing KY 196, KY 197 Installation Manual

411iedSignai
ELECTRONIC AND AVIONICS SYSTEMS
INSTALLATION MANUAL
BENDIX/KING@
KY 196/197
VHF COMMUNICA TIONS
TRANSCEIVERS
REVISION 3 SEPTEMBER, 1983
WARNING
Information subject to the export control laws. This document. which includes any attachments and exhibits hereto. contains information subject to International Traffic in Arms Regulation (ITAR) or Export Administration Regulation (EAR) of 1979. which may not be exported, released or disclosed to foreign nationals inside or outside the U.S. without first obtaining an export
license. Violators of ITAR or EAR may be subject to a penalty of 10 years imprisonment and a fine of $1,000.000 under 22 U.S.C. 2778 or Section
2410 of the Export Administration Act or 1979. Include this notIce with any reproduced portion of this document.
COPYRIGHT NOTICE
01:>1996AlliedSignal, Inc.
Reproduction of this publication or any portion thereof by any means without the express written permission of AlliedSignal Commercial Avionics Systems is
prohibited. For further information contact the Manager, Technical Publications, AlliedSignal Commercial Avionics Systems, 400 North Rogers Road, Olathe, Kansas, 66062. Telephone: (913) 782-0400.
p
2.1
2.2
2.3
2.3.1
2.3.2
2.3.3
2.3.4
2.3.5
2.4
"~
3.1
3.1.1
3.1.2
3.1 .3
3.1.4
3.1.5
Figure
2-1 2-2
2-3 2-4 2-5 2-6
2-7 2-8 2-9
2-10
2-11 2-12
2-13
~3-1
3-2
Page 2-4
2-7
2-9
2-11 2-13
2-15 2-17 2-19 2-21 2-23
2-25
OnLy 2-27 O"Ly
2-2~ 3-3
~-l.
Paragraph
1.1
1.2
1.3
1.4
1.5
1.6
KING
KY 196/196E/KY 197/197E
VHF COMMUNICATIONS TRANSCEIVER
TABLE OF CONTENTS
SECTION I
GENERAL INFORMATION
Introduction Equipment Description Technical Characteristics
Units and Accessories Supplied
Accessories Required, but Not Supplied
License Requirements
SECTION II
INSTALLATION
General
Unpacking and Inspecting Equipment
InstaLLation
Avionics Cooling Requirements For Panel Mounted Equipment Mounting Rack Installation Antenna InstalLation
CabLe Harness and Connector AssembLy
KY 196/196E/197/197E InstaLLation
Post InstaLLation Check
SECTION III
OPERATION
Operating Procedure
Turn On
Transmit Indicator
Mod~ of 0peration Remote Frequency Transfer Remote Channel Increment
LIST OF ILLUSTRATIONS
MoLex TerminaL and TooLs (3 Sheets)
Radio Removal TooL (KPN 071-6045-00)
KPN 030-0101-02 Connector AssembLy
KY 196/196E/197/197E OutLine and Mounting Drawing
KY 196/196E/197/197E InstaLLation AssembLy Drawing
KY 197/197E Interconnect Diagram with KMA 20 (13.75VDC)
To Provide 4 ohm Speaker OutPut, Ramp HaiLer and Intercom
KY 196/196E Interconnect Diagram with KMA 20 (27.5VDC)
To Provide 4 ohm Speaker OutPut, Ramp HaiLer and Intercom
KY 197/197E Interconnect Diagram with KA 25A (1~.75VDC)
To Provide 4 ohm Speaker Output
KY 196/196E Interconnect Diagram with KA 25A (27.5VDC)
To Provide 4 ohm Speaker Output
KY 197/197E Interconnect Diagram with KA 134 (1~.75VDC)
To Provide 4 ohm Speaker Output, Ramp HaiLer, and Intercom
KY 196/196E Interconnect Diagram with KA 134 (27.5VDC)
To Provide 4 ohm Speaker Output, Ramp HaiLer, and Intercom
KY 196/196E Interconnect to Provide Intercom and Headphone Output KY 197/197E Interconnect to Provide Intercom and Headphone Output
Frequency Mode Program Mode/Memory Mode
Rev. 3, September, 1983
IM0035-2
Paqe
1-1 1-1
1-2
1-4
1-4
1-4
2-1 2-1 2-1
2-1 2-1 2-1 2-2
2-3 2-3
3-1 3-1
3-1 3-1
3-3 3-3
KY 196
064-1019-00
Non-Glare lens
KY 196E
064-1019-01
Non-Glare lens
KY 196
064-1019-02
Standard lens
KY 196
064-1019-05
Non-Glare lens,
Memory
Channels
KY 196E
064-1019-06
Non-Glare lens,
Memory
Channels
KY 196
064-1019-07
Standard lens,
Memory
Channels
KY 196
064-1019-10
Non-Glare lens,
Memory
Channels,
Remote
Transfer/Inc
KY 196E
064-1019-11
Non-Glare lens,
lIo1emory
Channels,
Remote
Transfer/Inc
KY 196
064-1019-12
Standard lens,
Memory
Channels,
Remote
Transfer/Inc
KY 197
064-1021-00
Non-Glare
lens
KY 197E
064-1021-01
Non-Glare
Lens
KY 197
064-1021-05
Non-Glare
lens,
Memory Channels
KY 197E
064-1021-06
Non-Glare
lens,
Memory
Channels
KY 197
064-1021-10
Non-Glare
lens,
Memory
Channels,
Remote
Transfer/Inc
KY 197E
064-1021-11
Non-Glare
lens,
Memory
Channels,
Remote
Transfer/Inc
1.2
EQUIPMENT
DESCRIPTION
KING
KY 196/196E/KY 197/197E
VHF COMMUNICATIONS TRANSCEIVER
SECTION I
GENERAL INFORMATION
1.1 INTRODUCTION
This manual contains information relative to the physical, mechanical, and electrical characteristics of the King Radio Corporation Silver Crown KY 196/196E/197/197E 720 channel VHF communications transceivers. Installation and operating procedures are also included. Information relative to t"e
maintenance,
alignment, and procurement of replacement parts may be found in KY 196/196E/197/197E Maintenance/Overhaul Manual.
The units covered are as follows:
NOTE
All KY 196/196E RADIOS ARE 27.5 VDC, All KY 197/197E RADIOS ARE
13.75 VDC.
The KY 196/196E/197/197E transceiver is a TSO'd 720 channel communications transceiver and is desiqned to
provide two-w::lYvoice communication within the frequency range of
11~.OOOMHz
to B,).975MHz in ~5KHz
increments.
The KY 196/196E/197/197E is a panel mounted unit. Connections to the unit are made throuqh a 20 pin Molex printed circuit board edge connector and a BNC coax connector at the rear of t"e unit.
ElectricaLLy, the KY 196/196E/197/197E consists of four sections: receiver, transmitter, frequency synthesizer, and gas-discharge display circuitry. The only difference between the KY 196/197 and I<Y 196E/197E lies in their selectivity specifications (see Section 1.3). The only difference between the KY 196/196E and KY 197/197E is thei r rated t ransmi tter power out out and power requi r~ments (see Secti on
1.3) .
The KY 196/196E (-aS, -06, -07) and the KY 197/197E (-OS, -06) "ave the capability of oreproqra~minq UP to nine memory channel frequencies for later recall. Channel frequency information is stored in ::I
non-volatile earom memory so that when the radio is turned off and then back on, channel information is retained.
The KY 196/196E (-10, -11, -12) and the KY 197/197E (-10, -11) have the capability of remote transfer of use and standby frequencies and the remote recall of channel frequency information.
Rev. 3, September, 1983
IM0035-3
Paqe 1-1
KY 1961196E:
(27.5V)
Receive
-
.4AMP
Transmit
-
5.0AMP
KY 197/197E:
(13.75V)
Receive
-
.~AMP
Transmit
-
6.0AMP
KING
KY 196/196E/KY 197/197E
VHF COMMUNICATIONS TRANSCEIVER
1.3 TECHNICAL CHARACTERISTICS
KY 196/196E/197/197E TRANSCEIVER TECHNICAL CHARACTERISTICS
SPECIFICATION
CHARACTERISTIC
TSO COMPLIANCE:
Transmit:
KY 196/196E C37b (00-157, Class 3) KY 197/197E C37b (00-157, Class 4)
KY 196/197 C38b (00-156, Class C and D) KY 196E/197E C38b (DO-156, Class A and B)
00-160 Env. Cat./A1D1/A/KPS/XXXXXXZBAAA
RTCA 00-156, DO-157, 00-160
Receive:
APPLICABLE DOCUMENTS:
WEIGHT:
3.2 lbs. (1.45Kq)
PHYSICAL DIMENSIONS:
Width:
Height:
Depth:
6.~5 inches (15.88 cm)
1.3 inches
(
3.30 cm)
10.5 inches (26.67 cm)
MOUNTING:
TEMPERATURE RANGE:
Panel mounted, no shock mounting required
-200C to +550C with short time operation at +700C.
POWER REQUIREMENTS:
DESIGN:
All solid state. Printed circuit board and point to point wirinq.
FREQUENCY RANGE:
118.000MHz to 135.975MHz in 25KHz increments
FREQUENCY STABILITY:
0.0015% to meet 00-156 Class C and D
TRANSMITTER
POWER OUTPUT:
KY 196/196E - 16 watts minimum
KY 197/197E - 7 watts minimum
MODULATION:
85% modulation capabi l ity with 90Y. l imitinq,
less than 15% distortion at 85% modulation.
SIDETONE OUTPUT:
Adjustable up to 1a~mw into 500 ohm headphones.
MICROPHONE:
Standard carbon or dynamic mic containinq transistorized pre-amp. (Must provide 10~mV RMS into 100 ohm load).
HARMONIC CONTENT:
Greater than 60dB down from carrier.
Rev. 3, September, 1983 IM0035-3
Paqe 1-2
KING
KY 196/196E/KY 197/197E
VHF COMMUNICATIONS TRANSCEIVER
SPECIFICATION
CHARACTERISTI C
TRANSMITTER
HIGH-TEMPERATURE PROTECTION:
If the transmitter or modulator circuits
become hot enough to ootentially hurt any components in the transceiver, a protection ci rcuit wi II automati cally turn down the transmitter oower consumotion and output power
(4 watts minimum).
DUTY CYCLE:
1 Min. ON, 4 Min. OFF
--
RECEIVER
RECEIVER SENSITIVITY:
2uV (hard) or less for 6dB s+n/n with 1KHz
tone modulated 30%.
RECEIVER SELECTIVITY:
KY 196/197 - 6dB at !8KHz minimum 00-156 Class
C & 0
40dB at +17KHz maximum 60d8 at !22KHZ maximum
KY 196/197E - 6dB at +15KHz minimum 00-156
Class A ~ B
60dB
at
+43KHz
maximum
RECEIVER OUTPUT:
100mw into 500 ohms minimum
AGC CHARACTERISTICS:
From 5uV to 20,000uV aurlio output wi II not
vary more than 3dB.
SQUELCH:
Automatic squelch (internally ad;ustable
carrier-to-noise settinq) with manual rlisable
and carrier squelch override. Both squelch adjustments are externally accessible.
SPURIOUS RESPONSES AND CROSS MODULATION PRODUCTS:
At least 80d8 down
INTERCOM INPUT:
The mic is connected to the intercolII input.
The receiver is operational and mic aurlio appears at the audio output alonq with receive
audio. 100",V RMS of mic audio into 100 ohm load is required for 100mw output.
Rev. 3, September, 1983
lM0035-3
Paqe 1-~
PART NUMBER DESCRIPTION
030-0101-02 Conn BNC
030-1094-55
Conn
Molex
(20
Pin)
030-1107-21
Conn Pin (21)
057-2193-01
Decal
Comm 1
057-2193-02
Decal Comm 2
089-2013-37
Nut
Hex #6-32
089-2191-22
Nut Esna #6-32
089-2353-01
Clip Nut 6-32
089-5903-07 Screw PHP (4-40x7/16)
089-5907-08 Screw PHP
#6-32 x 1/2
089-6012-08 Screw FHP
(6-32x1/2)
089-8094-30
Flat Washer
090-0019-07 Retaining Ring
091-0072-02
Cable Clamp
KING
KY 196/196E/KY 197/197E
VHF ~OMMUNI~ATIONS T~ANS~EIVE~
1.4 UNITS AND ACCESSORIES SUPPLIED
A. King KY 196/196E/197/197E Transceiver with mounting rack.
(KPN 064-1019-00/01 and KPN 064-1021-00/01 respectively)
B. King KY 196/196E/197/197E Installation Kit (050-1704-00)
QUANTITY
1
1
1 1
6 2
1 6
1
1.5
ACCESSORIES REQUIRED, BUT NOT SUPPLIED
A. Communications Antenna and Cables
B. Headphones: (500 ohms nominal impedance)
C. Microphone: Low impedance carbon or dynamic with transistorized pre-amo
D. For 13.75 volt operation of the KY 196/196E a 14 to 28 volt DC to DC converter such as the Kr,~
Electronics Model RB-125 (KPN 068-1016-03) or equivalent may be used.
1.6 LICENSE REQUIREMENTS
The transmitter, as instaLLed in the aircraft, requires an Aircraft Radio Station License. This License is obtained by fiLing FCC Form 404. The KY 196/196E/197/197E may be operated for up to ~n days without a station license, after fiLing the FCC Form 404 and while awaiting the receipt of the staion license, if a copy of the FCC Form 404 is kept in the aircraft. This form is avaiLable throuqh the LocaL FCC field
office.
This equipment has been type accepted by the FCC and entered on their List of type accepted equioment as
King KY 196, KY 196E, 'KY 197 or KY 197E and must be identified as King KY 196, KY 196E, KY 197 or KY 197E
on your FCC Form 404, Aircraft Radio Station License AppLication.
Rev. 3, September, 1983
IM0035-3
Paqe 1-4
KHIG
KY 196/196E/KY 197/197E
VHF COMMUNICATIONS TRANSCEIVER
CAUTION
THE VHF TRANSMITTER IN THIS EQUIPMENT IS GUARANTEED TO MEET
FEDERAL COMMUNICATIONS COMMISSION ACCEPTANC~ OVER THE
OPERATING TEMPERATURE RANGE ONLY WHEN A KING CRYSTAL IS USED
IN THE STABILIZED MASTER OSCILLATOR.
USE OF OTHER THAN A KING CRYSTAL IS CONSIDERED AN UNAUTHORIZED MODIFICATION, AND WILL VOID THE WARRANTY.
The Federal Communications Commission requires that the operator of the transmitter of this equioment
hold a Restricted Radio Telephone Operator Permit (FCC Form 753) or hiqher class license. A oermit may be obtained by a'U.S. citzen from the nearest field office of the FCC; no examination is required.
Rev. 3, September, 1983
IMO035-3
Paqe 1-5
KING
KY 196/196E/KY 197/197E
VHF COMMUNICATIONS TRANSCEIVER
I
2.1 GENERAL
SECTION II
INSTALLATION
This section contains suggestions and fa~tors to consider before installing the KY 196/196E/197/197E.
Close adherence to these suggestions will 1assure a more satisfactory performance from the equipment.
2.2 UNPACKING AND INSPECTING EQUIPMENT
Exercise extreme care when unpacking the unit. Make a visual inspection of the unit for evidence of damage incurred during shipment. If a claim for damage is to be made, save the shipping container to substantiate the claim. The claim should be promptly filed with the transportation company. It would he advisable to retain the container and packaging material after all equipment has been removed in the event that equipment storage or reshipment should become necessary.
2.3 EQUIPMENT INSTAlLATION
The KY 196/196E/197/197E installation will conform to standards designated by the customer, installing agency and existing conditions as to the unit location and type of installation. However, the following
suggestions should be considered before installing your KY 196/196E/197/197E. The installing agency will
supply and fabricate all external cables. The connectors required are supplien by King Radio.
Interconnect diagrams are Figures 2-6 through 2-13.
NOTE
USE GOOD
QUALITY STRANDED WIRE WITH AT LEAST
600
VOL.T
INSULATION THAT
WILL NOT SUPPORT A FLAME.
~
2.3.1 AVIONICS COOLING REQUIREMENTS
FOR PANEL MOUNTED
EQUIPMENT
The greatest single contributor to increased reliability of all modern day avionics is to limit the
maximum operating temperature of the individual units. While modern day individual circuit descdns
consume much less electrical energy, the watts per cubic inch dissipated within avionics units remains
much the same due to. high density packaging techniques utilized. Consequently, the imoortance of providing avionics stack cooling is still with us.
While each individual unit may not reguire forced air cooling, the combined heat load of several units operating in a typical avionics stack will significantly degrade the reliability of the avionics if provisions for stack cooling are not incorporated in the initial installation. Recommendations on stack cooling are contained in King Radio Installation Bullentin #55. Failure to provide stack cooling will
certainly lead to increased avionics maintenance costs and may void the King warranty.
2.3.2 Mounting Rack Installation
A. The KY 196/196E/197/197E is mounted rigidly in the aircraft panel. Select a position in the
panel that is not too close to any high external heat source. Remember to allow adequate
space for installation of cables and connectors. Avoid sharp bends and placing the cables too
near the aircraft control cables.
B. When installing two or more panel mounted units in a stack, the mounting trays shall be spaced
.050 inches (.127 cm) apart. Newer style mounting trays have had .025 inch <.064 cm) dimples
built in, top and bottom, both sides, so that two new style trays will automatically be spaced properly.
C. Refer to Figure 2-4 for the KY 196/196E/197/197E mounting dimensions.
mounting holes.
"'ark anI"! cut the
D. Secure the mounting rack to the instrument panel per Figure 2-4. The rear mounting bosses
should be attached to the airframe by means of support brackets.
Rev. 3, September, 1983
IM0035-4
Page 2-1
KING
KY 196/196E/KY 197/197E
VHF COMMUNICATIONS TRANSCEIVER
2.3.3
ANTENNA INSTALLATION
A. A conventional 50 ohm vertically polarized
COMM
antenna is requireri with the KY
196/196E/197/197E. Vertical bent whip antennas are not recommenderi. Widehand
COMM
antennas
provide efficient operation over the
COMM
band. Antennas should be installed oer
manufacturer's recommendations. Additional recommendations are as follows. B. Mount antenna on a flat metal surface or install a qround plane at least 18 inches square. C. The antenna should be well removed from any projections and the engine(s) anri propeller(s).
Also, for satisfactory operation, the antenna isolation between a communications transmitter
antenna and a NAVreceiver antenna, as well as between dual
COMM
antennas, should be a minimum
of 30dB. VHF antennas mounted on top and bottom have approximately "30dB isolation. A
horizontally polarized NAVantenna and a vertical polarized
COMM
antenna will have practical
values from 10 to 30dB.
D. If both Comm antennas must be top mounted or both bottom mounteri, antenna isolation between
Comm's may not be adequate to prevent reradiation. In single audio panel installations, reradiation can also be prevented by use of the Xmit-Rec interlock. Refer to Service Bulletin
KY 196/196E-9 or KY 197/197E-10 and Installation Bulletin 194. In dual audio panel
installations where simultaneous operation of both Comm's is desired, the Xmit-Rec interlock is not recommended. We would recommend adequate antenna isolation, 30dB min.
2.3.4 CABLE HARNESS AND CONNECTOR ASSEMBLY
The KY 196/196E/1971197E uses a speci a l connector that mates di rect ly wi th the printed ci rcui t board inside the unit. Assembly of the connector is as follows:
A. Contact Terminal Assembly using Molex Crimper (Figure 2-1)
1. Strip each wire 5/32" for contact terminal (KPN 030-1107-XX). (The last two digits of the
contact terminal part number indicates the number of terminals required).
2. Open the Molex hand crimper HT 1921 with the engraved side toward the operator. Place the
conductor tab section of a contact terminal on Anvi l B with the contact oortion facing away from the operator. Close the crimper slightly untH the contact tabs touch the
female jaw.
3. Insert the stripped conductor until the insulation is even with the side of the crimper
facing the operator. Crimp the conductor tabs by squeezing the handles together until the
jaws are fully closed or a sufficient crimp is obtained.
4. Move the lead to Anvil A. Place the insulating tab section on Anvi-l A. Crimp again until
the jaws are fully closed or a sufficient crimp is obtained.
8. Contact Insertion into Molex Connector Housing
1. After the contact terminals have been installed on the terminals can be inserted into the proper location in 030-1094-54). The terminal cannot be inserted upside down.
all the way in, until a click can be felt or heard.
wiring harness, the contact
the connector housing (KPN
8e sure to push the terminal
2. The self locking feature can be tested by gently pulling on the wire.
C. Location of Polarizing Key in Housing
1. Prior to insertion of connector into rear of unit, check polarizing key position between
contacts 3 and 4.
2. Refer to Figure 2-5 to check correct position of polarizing key.
D. Extraction of Contact from Molex Connector
1. Slip the flat narrow blade of a Molex contact e;ector tool, HT-1884
(I(PN 047-5099-01),
under the contact on the mating side of the connector. 8y turning the connector upside
down one can see the blade slide into the stoP.
Rev. 3, September, 1983
IM0035-4
Paqe 2-;:!
KING
KY 196/196E/KY 197/197E
VHF COMMUNICATIONS TRANSCEIVER
2. When the ejector is sLid into pLace, the retaining tab of the contact is raised, aLLowing
the contact to be removed by puLLing moderateLy on the Lead.
3. Neither the contact or position is damaged by removing a contact; however, the contact
shouLd be checked visuaLLy before reinstaLLing in connector to be certain that retaining
tab "A" extends as shown (see Figure 2-1) for retention in connector.
E. Coax Connector
Refer to Figure 2-3 for the ~etaiLs for mounting the right angLe coaxiaL 9~C connector to the coax cabLe. InstaLL the connector into the mounting rack.
2.3.5 KY 196/196E/KY 197/197E INSTALLATION
A. Looking at the top of the unit, make sure the front Lobe of the hoLddown device is in a
verticaL position.
B. SLide the unit into the mouting rack untiL the front Lobe touches the mounting rack.
C. Insert a 3/32" ALLen wrench through a hoLd in the front paneL to engage the Locking screw.
Turn clockwise untiL the rear Lobe engages the mounting rack. Continue turning until the unit
is secure in the mounting rack Do not overtighten.
D. For removaL, turn the Locking screw counterclockwise, using a 3/32" ALLen wrench, untiL the
unit disengages from the mounting rack. PulL the unit out of the mounting rack by DulLing on
the metaL tabs Located behind the front paneL on each side of the unit. Radio Extractor KPN
071-6045-00 is designed to aid in the removaL of this and other King products (See Figure
2-2).
2.4
POST INST
AllA
TlON CHECK
An operation performance fLight test is recommended after the instalLation is compLeted to insure satisfactory performance of the equipment in its normaL environment. Check all aircraft control
movements to be sure no electrical cables interfere with their operation. To check the communications transceiver, maintain an appropriate aLtitude and contact a ground station faci l ity at a range of at
least fifty nautical miles. Contact a ground station close in. PuLL the voLume control knob out to
defeat the automatic squelch feature and listen for any unusual electrical noise which would renuce the
COMI\1
receiver sensitivity by increasing the squeLch threshold. If possible, verify the communications
capability on both the high and low end of the VHF
COMM
band.
NOTE
AS AN ADDED PRECAUTION BEFORE
THE FLIGHT, CHECK THE
ANTENNA.
VSWR SHOULD
BE
CHECKED
WITH
AN
IN-LINE TYPE WATTMETER
INSERTED IN THE
COAXIAL
TRANSMISSION LINE BETWEEN THE
TRANSCEIVER AND THE ANTENNA. ANY PROBLEM WITH THE AItITENItIA INSTALLATION WILL MOST LIKELY BE SEEN AS A HIGH REFLECTED ?OWER. A VSWR OF 3:1 WILL RESULT IN A 25~ LOSS IN POWER.
NOTE
THE BRIGHTNESS OF THE DISPLAY CAN BE SET FOR THE MOST PLEASING INTENSITY BY ADJUSTING R130 DURING LOW LIGHT LEVEL
CONDITIONS. R130 IS ACCESSIBLE THROUGH THE BOTTOM OF THE RADIO WHEN IT IS PARTIALLY PULLED OUT OF THE RACK.
Rev. 3, September, 1983
I1\10035-4
Page2-~
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