Honeywell KY196B User Manual 31122

Honeywell International Inc. 31122

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Document ID31122
Application IDoBdsyYrdMhj7+56EG2H+5g==
Document Description8
Short Term ConfidentialNo
Permanent ConfidentialNo
SupercedeNo
Document TypeUser Manual
Display FormatAdobe Acrobat PDF - pdf
Filesize28.17kB (352093 bits)
Date Submitted1999-04-08 00:00:00
Date Available1999-04-22 00:00:00
Creation Date2001-06-26 11:19:24
Producing SoftwareAcrobat Distiller 4.0 for Windows
Document Lastmod2001-06-26 11:19:35
Document Title31122.pdf
Document Author: VicodinES /CB /TNN

AlliedSignal
ELECTRONIC AND AVIONICS SYSTEMS
INSTALLATION MANUAL
BENDIX/KING®
BENDIX/KING
KY 1963
VHF COMMUNICATIONS TRANSCEIVER
SECTION I
GENERAL INFORMATION
Paragraph
1.1
1.2
1.3
1.4
1.5
1.6
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
3.1.6
3.1.7
INTRODUCTION
DESCRIPTION OF EQUIPMENT
TECHNICAL CHARACTERISTICS
UNITS AND ACCESSORIES SUPPLIED
ACCESSORIES REQUIRED, BUT NOT SUPPLIED
LICENSE REQUIREMENTS
SECTION II
INSTALLATION
GENERAL INFORMATION
UNPACKING AND INSPECTING EQUIPMENT
EQUIPMENT INSTALLATION
AVIONICS COOLING REQUIREMENTS
MOUNTING RACK INSTALLATION
ANTENNA INSTALLATION
CABLE HARNESS AND CONNECTOR ASSEMBLY
KY 1968 INSTALLATION
POST INSTALLATION CHECKS
SECTION III
OPERATION
GENERAL INFORMATION
TURN ON
TRANSMIT INDICATOR
MODES OF OPERATION
REMOTE FREQUENCY TRANSFER
REMOTE CHANNEL INCREMENT
DIM SELECT
DISPLAY ADJUST MODE
IMKY1QGBLT
Rev 0 January/99
Page
1—1
1—1
1~1
1-4
1-6
2—1
2—1
2-1
2—2
2~2
2—3
2-6
3-1
3—1
3—1
3-1
3-3
3—3
3-3
Page i
BENDIX/KING
KY 1968
VHF COMMUNICATIONS TRANSCEIVER
SECTION I
GENERAL INFORMATION
1.1 INTRODUCTION
This manual contains information relative to the physical, mechanical, and electrical characteristics
of the BENDIX/KING KY196B VHF Communications Transceiver. Installation and operating
procedures are also included. Information relative to the maintenance, alignment, and
procurement of replacement parts may be found in the KY 1968 Maintenance/Overhaul Manual.
1.2 DESCRIPTION OF EQUIPMENT
The KY 1968 VHF Comm Transceiver consists electrically of five sections: receiver, transmitter,
synthesizer, display circuitry, and the microprocessor board. The KY 1968 operates at 28VDC and
features 16 Watts of transmitter power.
The KY 1968 is available with 3.33 KHz or 25KHz receiver selectivity, diffused display lenses,
backlit bezel nomenclature, and operating ranges of 118.000 to 136.9916 MHz. See Paragraph
1.4 below for descriptions of specific flavors.
The KY 1965 has the capability of programming up to nine memory channel frequencies for later
recall. Channel frequency information is stored in non-volatile memory so the when the radio is
turned off and then back on, channel information is retained. Both units also have the capability
of remote transfer of Use and Standby frequencies, and remote recall of channel frequency
information.
1.3 TECHNICAL CHARACTERISTICS
SPECIFICATION CHARACTERISTIC
TSO COMPLIANCE:
Transmitter:
KY 1963 (flavors -0101, ~0201) TSO 037c, DO—186 Class 3
TSO 037C, DO-186a Class 5
Receiver:
KY 1965 (flavors -0101, -0201) TSO 0380, 00—186 Classes C & D
TSO 0380, DO—186a Class E
ENVIRONMENTAL DATA: See TSO Appendix
PHYSICAL DIMENSIONS:
Height: 1.35 in (3.43 cm)
Width: 6.312 in (16.032 cm)
Depth (behind aircraft panel): 10.776 in (25.847 cm)
WEIGHT:
Wflh rack 3.2 lbs (1.45 Kg), :0.2 lbs (0.09 Kg.)
Wflhom "30k 3.0 lbs (1 .3 Kg), 20.2 lbs (0.09 Kg.)
MOUNTING: Panel mounted, no shock mounting
required
IMKY1968LT Page 1-1
Rev 0 January/99
BENDIWKING
KY 1968
VHF COMMUNICATIONS TRANSCEIVER
RECEIVER
ECEIVER SENSITIVITY:
RECEIVER SELECTIVITY:
Class C, D (flavors —0101, —0201)
Class E (flavors —0101, -0201)
RECEIVER OUTPUT:
AGC CHARACTERISTIC:
SQUELCH:
SPURIOUS RESPONSES AND CROSS
MODULATION PRODUCTS:
INTERCOM INPUT:
2uV (hard) shall produce not less than GdB S+N/N
with 1KHz tone modulated 3096 (with compressor
disabled).
BdB bandwidth at not less than 80 KHz on each
side. 40dB bandwidth with no morethen 17.0 KHz
on each side. GOdB bandwidth with no more than
22.0 KHz on each side.
6 dB bandwidth at not less than 2.773 kHz on
each side.
60 dB bandwidth at not more than 7.37 kHz on
each side.
100mW minimum into 5009 minimum.
From 5 uV to 10,000 p.V audio output will not vary
more than SdB.
Automatic squelch antemally adjustable
carrier-to—noise setting) with manual disable.
At least BOdB down.
The mic is connected to the intercom input. The
receiver is operational and mic audio appears at
the audio output along with receive audio.
100mVRMS of mic audio into 1009 is required
for 100mW output.
lMKY1QSBLT
Rev 0 January/99
Page 1-3
BENDIX/KING
KY 1963
VHF COMMUNICATIONS TRANSCEIVER
1.5 ACCESSORIES REQUIRED. BUT NOT SUPPLIED
Communications antenna and cables
Headphones: 5009 nominal impedance.
Microphone: Low impedance carbon or dynamic with transistorized preamp.
9.097?
For 13.75V operation of the KY 1965 a 14—to—28V converter such as the KGS
Electronics Model RB-125 or equivalent may be used The RB-125 is available
from BENDIX/KING under PN 068—01016-0003.
1.6 LICENSE REQUIREMENTS
The transmitter, as installed in the aircraft, requires an Aircraft Radio Station License. This
license is obtaining by filing FCC Form 404, Aircraft Radio Station License Application, which
may be obtained from your local FCC Field Office, The KY 1968 may be operated for up to 30
days without a station license after tiIing Form 404 while awaiting the receipt of the radio license
if a copy of FCC Form 404 is kept in the aircraft.
This equipment has been type accepted by the FCC and entered on their list of type accepted
equipment as AlliedSignaI KY 1968, and must be identified as AlliedSignaI KY 1965 on FCC
Form 404‘
iQAU’l'JOl!
THE VHF TRANSMITTER IN THIS EQUIPMENT IS
GUARANTEED TO MEET FEDERAL COMMUNICATIONS
COMMISSION ACCEPTANCE OVER THE OPERATING
TEMPERATURE RANGE ONLY WHEN AN ALLIEDSIGNAL
CRYSTAL IS USED IN THE STABILIZED MASTER
OSCILLATOR.
USE OF OTHER THAN AN ALLIEDSIGNAL CRYSTAL IS
CONSIDERED AN UNAUTHORIZED MODIFICATION AND
MAY VOID THE WARRANTY.
The Federal Communications Commission requires that the operator of the transmitter of this
equipment hold a Restricted Radio Telephone Operator Permit (FCC Form 753) or higher class
license A permit may be obtained by a US citizen from the nearest field oiilce of the FCC; no
examination is required.
IMKY196BLT Page 1-5
Rev 0 January/99
BENDIX/KING
KY 1968
VHF COMMUNICATIONS TRANSCEIVER
SECTION II
INSTALLATION
2.1 GENERAL INFORMATION
This section contains suggestions and factors to consider before installing the KY 1968. Close
adherence to these suggestions will assure more satisfactory performance from the equipment.
2.2 UNPACKING AND INSPECTING EQUIPMENT
Unpack the equipment carefully and inspect each item for evidence of damage incurred during
shipment. If a damage claim must be filed, save the shipping container and all packing materials
to substantiate your claim. The claim should be filed with the transportation company as soon as
possible. The shipping container and packing material should be saved in any case in the event
that storage or reshipment of the equipment is necessary.
2.3 EQUIPMENT INSTALLATION
The KY 1963 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 the KY 1968. The installing agency will supply
and fabricate all external cables. The connectors required are supplied by AlliedSignal.
Interconnect diagrams are included in this manual as Figures 2—5 through 2—10. Refer to table
below for compatible installations.
Current Installation -> KYQSA KY196
—nsii__
*1 Display brightness controlled by dimmer bus not photocell.
*2 Button/Bezel backlighting not operative.
‘3 If installation utilizes external audio amplifier.
NOTE: 064—01084-0201 is not compatible with other KY 96A/196A/197A installations.
NOTE
Use good quality stranded wire with at least 600V insulation that will
not support a flame.
2.3.1 AVIONICS COOLING REQUIREMENTS FOR PANEL MOUNTED EQUlPMENT
The most important contribution to improved reliability of avionics equipment is to limit the
maximum operating temperature of each unit. While modern designs consume less total
energy, the heat dissipated per unit volume (Watts/cubic inch) remains much the same clue
to contemporary high density packaging techniques. While each individual unit may or may
not require forced air cooling, the combined heat generated by several units operating in
a typical panel or rack can significantly degrade the reliability of the equipment if provisions
for adequate cooling are not incorporated in the initial installation.
IMKY1965 LT Page 24
Rev 0 JANUARY/99
BENDIX/KING
KY 196B
VHF COMMUNICATIONS TRANSCEIVER
It single-jaw crimpers are being used, move the contact terminal/conductor
assembly to locate the terminal’s insulation tabs on the anvil of the crimp tool. Crimp
again until thejaws are fully closed or a sufficient crimp is obtained to the insulation.
B. Contact Insertion into Molex Connector Housing
Aflerthe contact terminals have been installed on the wiring harness, the contact terminals
can be inserted into the proper location in the connector housing (PN 030-01094—0080).
The terminal cannot be inserted upside down. Be sure to push the terminal all the way in
until a click can be felt or heard. The self-locking feature can be tested by gently pulling
on the wire.
C. Location of Polarizing Key in Housing
Prior to insertion of connector into rear of unit, check polarizing key position between
contacts 8 and 9. Refer to Figure 2-4 to check correct position of polarizing key.
D. Extraction of Contact from Molex Connector
1. Slip the flat narrow blade of a Molex HT—1884 contact ejector tool,
PN 047-05099~0001, under the contact on the mating side of the connector. By turning
the connector upside down one can see the blade slide into the stop.
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 visually checked before reinstalling to be certain that retaining tab
”A” extends as shown in Figure 2-1 for retention in connector.
E. Coax Connector
Refer to Figure 2-2 for instructions for mounting the right angle coaxial BNC connector to
the coax cable. Install the connector into the mounting rack.
2.3.5 KY 1965 INSTALLATION
A. Looking at the top of the unit, make sure the front lobe of the hold-down device is in a
vertical position.
B. Slide the unit into the mounting rack until the front lobe touches the mounting rack.
C. Insert a 3/32" Allen wrench through the hole 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 OVEFtTlGHTEN.
D. To remove the unit 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 pulling on the indentations on each side of the unit’s bezel.
IMKYl 968 LT Page 2-3
Rev 0 JANUARY/99
BENDIXIKING
KY 1968
VHF COMM UNICATIONS TRANSCEIVER
2.4 POST INSTALLATION CHECKS
An operational performance flight test is recommended afterthe 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 facility
at a range of at least 50 nautical miles. Then contact a ground station close in. Pull the volume
control oulto defeat the automatic squelch feature and listen for any unusual electrical noise which
would reduce the comm 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—Iine type wattmeter inserted in the
coaxial transmission line between the transceiver and the antenna.
Any problem with the antenna installation will most likely be seen as a
high reflected power. A VSWl—‘t of 3:1 will result in a 25% loss of
power.
The brightness of the display can be set for the most pleasing
intensity by placing the unit in Dimmer Adjust made during low light
level conditions. See Paragraph 3.1 of this manual for Dimmer
Adjust mode operating instructions.
IMKY1968 LT Page 25
Rev 0 JANUARY/99
BENDIX/KING
KY 1968
VHF COMMUNICATIONS TRANSCEIVER
JISSBI
PCLARIZING KEY
(mamas-0000
m d-I-I-I-l-fihfiffii : iii-I-I-H-I-l-ffi ff: film
z345613910|||zusu|s
FRONT VIEW
(LOOKING IN FROM THE FRONT OF THE RACK)
w 500 0 AUDIO HI
500 0 AUDIO L0
MIC AUDIO HI
MIC INTERCOM
MIC KEY
MIC AUDIO LO
SOUELCH AND COMPRESSOR DISABLE
AGC TEST/REMOTE CHANNEL INC
REMOTE TRANSFER
AIRCRAFT POWER +275 VDC
AIRCRAFT POWER f 27.5 VDC
- SWITCHED +2745 VDC
- SWITCHED 427.5 VDC
4» 27.5 VDC
+ 27.5 VDC
AIRCRAFT GROUND
AIRCRAFT GROUND
AIRCRAFT GROUND
QIRCRAFT GROUND
IC
+28 VDC LIGHTING HI '
DETECTED AUDIO OUT
DIM SELECT
N/C
N/C
N/C
NIC
NIC
N/C
XMIT REC INTERLOCK
III
10
T N
12
IIIII
If
15
III
Mk
J‘I 9632
£401 ~ ANTENNA
‘FIN 1 rs svuc LIGHTING HI ON (jammy-02m.
A FIGURE 2-8 KY 1965 PIN FUNCTION AND LOCATION DIAGRAM
IMKYI 968 LT Page 2-21
Rev 0 JANUARY/99
BENDlX/KING
KY 1968
VHF COMMUNICATIONS TRANSCEIVER
SECTION III
OPERATION
3.1 GENERAL INFORMATION
For a detailed description of the operating controls of the KY 1968 referto the Silver Crown +’ pilots
guide (PIN 006-18110-0000) or the aircraft's flight manual supplement.
Control layout is shown in Figure 3-1.
3.1.1 TURN ON
To turn on the radio rotate the Volume (VOL) knob clockwise from the OFF position. When power
is activated the Use and Standby (STBY) windows will display the frequencies and/or mode stored
in the non-volatile memory before power down.
After act'wating power, pull the VOL knob out to overridethe automatic squelch and rotate the VOL
knob to the desired audio level. Push the VOL knob back in to activate the automatic squelch.
SPRING".
THE KY1968 SHOULD BE TURNED ON ONLY AFTER
ENGINE STARTUP. THIS IS A SIMPLE PRECAUTION
WHICH HELPS PROTECT THE SOLID STATE CIRCUITRY
AND EXTENDS THEOPERATING LIFE OFYOURAVIONICS
EQUIPMENT.
3.1.2 TRANSMlT INDICATOR
During Comm transmissions, a Twill appear between the USE and STBY windows to indicate that
the transceiver is in the Transmit mode of operation.
3.1.3 MODES OF OPERATION
A. Frequency Mode
Frequency selection is accomplished in the Standby Entry mode by changing the frequency
display in the STBY window of the display with the tuning knobs, and then transfernng the
selected frequency into the USE window by pressing the Transfer button. The Iargertuning
knob will increment or decrement the MHz portion ofthe display in 1MHz steps with rollover
at each band edge (118.000MHZ or 136.975MHZ). the smaller tuning knob will increment
at all times.
8. Channel Mode
Momentarily pressing the Channel (CHAN) button while in the Frequency mode puts the
radio in the Channel mode. The last active frequency remains tuned and displayed in the
USE window. The last used channel number is displayed in the channel digit unless no
channels have been programmed, in which casethe radio defaults to Channel 1 and dashes
are displayed in the STBYwindow. Turning either tuning knob changes the channel number
and corresponding frequency in the STBY window.
The channels will only increment and decrement to channels that have been programmed.
If there has been no activity for five seconds the radio will return to Frequency mode and
the channel frequency is placed in the STBY window. Pressing the CHAN button before the
lMKY1SGB LT Page 3-1
Rev 0 JANUARY/99
BENDIX/KING
KY 1968
VHF COMMUNICATIONS TRANSCEIVER
Momentarily pushing the Transfer button returns the radio to Standby Frequency Entry. The
Standby frequency prior to Active Entry mode remains unchanged.
3.1i4 REMOTE FREQUENCY TRANSFER
The Remote Frequency Transfer button operates identically to the front panel Transfer button with
the exception that holding the Remote Transfer button for two seconds does not place the radio in
the Active Entry mode.
3.1.5 REMOTE CHANNEL INCREMENT
Pressing the Remote Channel button will cause the system to enter the Channel mode of operation
and will increment the channel from the previous channel number used.
3.1.6 DIM SELECT
MAX BRIGHT
FOLLOW PHOTOCELL
DIMMER BUS
Display brightness (1=tast, 8=slow)
Response to dimmer photocell (0=dim, 64=bright)
Display age compensation for brightness (0=dim, 255=bright)
IMKY1QGB LT Page 3-3
Rev 0 JANUARY/99
__,, V “v
BENDIXIKING
KY 1963
VHF COMMUNICATIONS TRANSCEIVER
ACTIVE TRANSMIT STANDBY CHANNEL concemmc
FREQ momma FREQ NUMBER TUNING KNOBS
(IN/OFF
VOL. SQUELCH
CONTROL
TRANSFER CHANNEL
BUTTON BUTTON
064-01084-0101
NOTE: All knob and control Iocafions/fundions are identical between various flavors.
FIGURE 3-1 KY 1965 VHF COMMUNICATIONS TRANSCEIVERS
IMKY196B LT Page 3-5
Rev 0 JANUARY/99
IMKY1QGBLT
Rev 0 Januaw/SS
BENDIX/KING
KY 1968
VHF COMMUNICATIONS TRANSCEIVER
TSO APPENDIX
RTCA DO-1GOB
ENVIRONMENTAL QUALIFICATION
FORMS
Page i
RTCA DO-160B
ENVIRONMENTAL QUALIFICATION FORM
NOMENCLATURE:
PART NUMBER:
TSO NUMBER:
MANUFACTURER’S SPECIFICATION:
KY 1963 8.33 KHZ / 25 KHz VHF Communications Transceiver
064—01084-0201 8.33 kHz VHF COM (CNI 5000 Version)
0644110840101 8.33 kHz VHF COM (50 version) Silver Crown
USO—026000000 Installation Kit
047-08512-0004 Mounting Tray
C37: (DO-lBG/a Classes 3 and 5)
C38c (DO-lSfi/a Classes CD and E)
MP5 004-01084—80
MANUFACTURER: ALLIEDSIGNAL AVIONlCS INC.
ADDRESS: One Technology Center
23500 West 105‘" Street
Olathe. Kansas 66061
USA
DO- I 6013
CONDITIONS PARAGRAPH CONDUCTED TESTS
Temperature and Altitude 4.0 Category Al Dl
(Temp. -20“C/+55°C. Alt. 50K)
(Decomp., 3K to 50K < 15 sec.)
(Overpressurc, 170 kPa)
(Loss of Cooling. Not Applicable)
Temperature Variation 50 Category C
Humidity 6.0 Category B
Shock 7.0 7.2 and 7.3
Vibration 80 Category KPS
Explosion 9.0 Category X (Not Tested)
Waterproofness 10.0 Category X (Not Tested)
Fluids Susceptibility l I .0 Category X (Not Tested)
Sand and Dust 120 Category X (Not Tested)
Fungus 13.0 Category X (N ol Tested)
Salt Spray 140 Category X (Not Tested)
Magnetic Effect 15.0 Class Z
Power Input 16.0 Category B
Voltage Spike Conducted ”0 Category AB
Audio Frequency Conducted Susceptibility 18.0 Category 82
Induced Signal Susceptibility 190 Category Z
Radio Frequency Susceptibility 20.0 Category A
Emission of Radio Frequency Energy 210 Category B
Lightning Induced Transient Susceptibility 220 Category X
AlliedSignaI Inc. P/N 004-01084-82
Environ Qua] Form filename. 196B_EQFidoc Revision -
Page I an
REVISION HISTORY
Revision C0 #
Description of Change
Date
» PRN Original Issue 12-98
AlliedSignal Inc.
P/N 004~0l084—82
Enw’mn Qua] Form filename: 196B_EQFAdec Revision -
Page 2 of 2

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PDF Version                     : 1.3
Linearized                      : Yes
Create Date                     : 2001:06:26 11:19:24
Producer                        : Acrobat Distiller 4.0 for Windows
Author                          : VicodinES /CB /TNN
Title                           : 31122.pdf
Modify Date                     : 2001:06:26 11:19:35-04:00
Page Count                      : 16
EXIF Metadata provided by EXIF.tools
FCC ID Filing: ASYKY196B

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