Retain this record in the front of the manual or chapter. Upon receipt of revisions, insert revised
pages in the manual, and enter revision number, date inserted, and initials.
INCORPORATION DATE is the date of the CMM revision that incorporates TR information.
I.B. 1516A Page TR-1/TR-2
23-12-01
Oct 25/02
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
SERVICE BULLETIN LIST
SERVICE BULLETIN
NUMBER
964-0452-00X-23-1
(012-0693-101)
964-0452-00X-23-2
(012-0693-102)
964-0452-00X-23-3
(012-0693-103)
964-0452-00X-23-4
(012-0693-104)
964-0452-0XX-23-5
(012-0693-105)
964-0452-0XX-23-6
(012-0693-106)
964-0452-00X-23-7
(012-0693-107)
964-0452-00X-23-8
(012-0693-108)
964-0452-00X-23-9
(012-0693-109)
964-0452-00X-23-10
(012-0693-110)
964-0452-00X-23-11
(012-0693-111)
964-0452-00X-23-12
(012-0693-112)
DATE
INCORPORATEDDESCRIPTION
Mar 30/01Corrects for anomalous behavior observed during
power interrupts between 4 and 250ms duration.
SW Ver. 1.50; HW Mod 10.
Mar 30/01Corrects for anomalous behavior observed during
testing at Airbus. Refer to EPRs 00001, 00002,
and 00003. SW Ver. 1.60; HW Mod 14.
Mar 30/01Eliminates problems encountered with the existing
Controller D module, and provides more reliable
XK516D1 Transceiver operation. HW Mod 22.
Mar 30/01Eliminates problems encountered with the
ON/OFF module, and provides more reliable
XK516D1 Transceiver operation. HW Mod 15.
Mar 30/01Changes made in the upgraded software: Added
bit with Air/Ground status information to ARINC
429 Word Label 270 broadcast to ACARS MU and
Radio Control Panel. HFDL SW Mod 3.
Mar 30/01Changes made in the upgraded software: Correct-
ed erroneous LRU Fault indication when Transceiver is in Data mode and on the ground, and the
Radio Control Panel input to the Radio is missing
or not available on both frequency select ports.
HFDL SW Mod 4.
Mar 30/01Eliminates problems encountered with the existing
Receiver/Exciter module, and provides more reliable XK516D1 Transceiver operation. HW Mod 13.
Mar 30/01Eliminates problems encountered during vibration
testing, and provides more reliable XK516D1
Transceiver operation. HW Mod 11.
Mar 30/01Converting the HF Transceivers to the new Part
Numbers will correct potential HF system lockup
conditions, resulting from unreliable HF Transceiver/Coupler control communications in installations
with high EMI conditions.
Mar 30/01Corrects potential HF system lockup conditions,
resulting from unreliable HF Transceiver/Coupler
control communications in installations with high
EMI conditions. The software upgrade sets the coaxial interface to Coupler, as the default, in the
Transceiver Control software. SW Ver. 1.70; HW
Mod 16.
Mar 30/01Reduces potential HF Transceiver susceptibility to
false PTT activation caused by keying of other audio components. HW Mod 18.
Mar 30/01Corrects for spurious signals on SELCAL output
caused by ringing in SELCAL output stage. Corrects for intermodulation distortion in the RF spectrum in the internal HFDL data mode. HW Mod 19.
I.B.1516A Page SB-1
23-12-01
Sep 5/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
SERVICE BULLETIN
NUMBER
964-0452-0XX-23-13
(012-0693-113)
964-0452-0XX-23-14
(012-0693-114)
964-0452-022-23-15
(012-0693-115)
964-0452-00X-23-16
(012-0693-116)
964-0452-012-23-17
(012-0693-117)
964-0452-00X-23-18
(012-0693-118)
964-0452-012-23-19
(012-0693-119)
964-0452-0XX-23-20
(012-0693-120)
964-0452-022-21
(012-0693-121)
964-0452-012-23-22
(012-0693-122)
DATE
INCORPORATEDDESCRIPTION
Mar 30/01The HFDR Software Mod 6 version contains cus-
tomer requested Red label changes to be used for
flight testing. HFDL SW Mod 6.
Mar 30/01Converts the Transceivers to the production ver-
sion of PN 964-0452-012, which are HFDL Software Mod 8.
Mar 30/01Converts HF Transceivers with Honeywell propri-
etary HF Data Link (HFDL) protocol (PN
964-0452-022) to HF Transceivers, using the industry standard ARINC 635 HFDL protocol (PN
964-0452-012). HFDL SW Mod 8.
Mar 30/01Changes the default date mode of operation of the
-0X2 Transceivers when both TP7G and MP2D
are grounded to Internal HFDL Data Mode instead
of defaulting to External Data Mode. This change
does not affect the voice mode of operation of any
of the radios. HW Mods 21 and 22.
Mar 30/01Changes the Airborne Datalink Processor (ADP)
software to add the capability to display the ADP
and High Frequency Modem (HFM) software part
numbers on the ACARS/MCDU system and to fix
minor problems identified during testing of HFDL
Software Mod 8. HFDL SW Mod 9.
Mar 30/01Reverts back to Software Version 1.70. Software
Version 1.80 introduced problems with sidetone
suppression during transmit operation. SW Ver.
1.70; HW Mod 22.
Mar 30/01Incorporates changes to the Airborne Datalink Pro-
cessor (ADP) software requested by ARINC to
prevent the HFDL System from logging on to a
ground station when the ICAO address input from
the MODE-S transponder is missing, and readjusts
the data rate thresholds. HFDL SW Mod 10.
Mar 30/01Allows the HF Transceivers and Control Panel to
be powered up in any sequence. Currently, the
"HFDR INSTALLED" discrete output of the HF Data Radio (or DOUT0 Spare Discrete OUT of A2
ADP board) is grounded on power up under software control. The "HFDR INSTALLED" discrete
needs to be grounded on the A2 ADP board even
when power is OFF. HW Mod 23.
Mar 30/01Incorporates changes to the Airborne Datalink Pro-
cessor (ADP) software to reduce/eliminate nuisance HFDR Faults (Fault Code 39) caused by input power transients. HFDL SW Mod 5.
Mar 30/01Incorporates minor changes to the Airborne
Datalink Processor (ADP) software requested by
ARINC to ensure that the Maximum Uplink Data
Rate recommended by the avionics to the HFDL
ground stations is a minimum of 300bps. HFDL
SW Mod 11.
1I.B.1516A Page SB-2
23-12-01
Sep 5/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
SERVICE BULLETIN
NUMBER
964-0452-0XX-23-23
(012-0693-123)
964-0452-00X-23-24
(012-0693-124)
964-0452-00X-23-25
(012-0693-125)
964-0452-00X-23-26
(012-0693-126)
964-0452-0XX-23-27
(012-0693-127)
964-0452-0XX-23-28
(012-0693-128)
964-0452-0XX-23-29
(012-0693-129)
964-0452-0XX-23-30
(012-0693-130)
DATE
INCORPORATEDDESCRIPTION
Mar 30/01Upgrades Transceiver to be capable of operation
in HF Datalink (HFDL) mode per ARINC 753 and
635, as well as the HF Voice Radio (HFVR) capabilities. Control SW Ver. 1.70; HFDL HW Mod 11.
Mar 30/01Corrects for nuisance CMC input fault reporting.
SW Ver. 2.00; HW Mod 27.
Mar 30/01Allows the ARINC 429 interface between the HF
Transceiver and a CMU or ATSU to operate reliably at high-speed. Also improves susceptibility of
the Transceiver to short power interrupts of 10 to
40ms when operating in data mode. Mod 28.
Mar 30/01Incorporates minor changes to Airborne Datalink
Processor (ADP) software to improve data mode
operation during short power interrupts, and to enable high-speed 429 interface to the ATSU. HFDL
SW Mod 12.
Mar 30/01Converts the Airborne Datalink Processor (ADP)
CCA, A2, from either Part No. 722-4134-006 to
722-4134-008 or from Part No. 722-4134-007 to
722-4134-009. The modification consists of removing IC sockets XU6 and XU23. Mod 31.
Oct 25/02Replaces the EMC Filter, A7, Part No. 300-1096-
001 (R&S Part No. 6030.2251.02, Mod 4 or lower)
with EMC Filter, A7, Part No. 300-1096-002 (R&S
Part No. 6030.2251.02, Mod 5). HW Mod 33.
Oct 25/02Replaces EPROM set, Part No. 6030.2151.00 Ver-
sion 2.00 or lower, with Version 2.20 on Controller
D, A8. HW Mod 34.
Oct 25/02Instructions to upload upgraded HFDL software via
a Portable Data Loader while on the bench. HW
Mod 13.
This manual was prepared by Honeywell according to ATA Specification No. 100.
The front matter consists of a title page that displays the equipment name and part number, and the
ATA and document numbers assigned to the manual, a Record of Revisions page for recording
revision incorporation, a Record of Temporary Revisions page for recording temporary revision
(yellow page) insertion prior to formal revision, a Service Bulletin List that includes a brief
description of the reason for the bulletin, and the date that Service Bulletin information was
incorporated into the manual, a Table of Contents, and a List of Illustrations.
DESCRIPTION AND OPERATION section contains an equipment illustration, table of leading
particulars, a general description, and a description of operation for electronic assemblies, to assist
in understanding the equipment for fault isolation purposes.
TESTING AND TROUBLESHOOTING section contains tests to enable maintenance personnel to
assess the operational condition of the equipment, a troubleshooting guide to assist in fault
isolation, and schematics.
DISASSEMBLY section contains procedures for disassembling the equipment to the part
replacement level. Complete overhaul procedures are not provided. Specific procedures are
intended to be a supplement to, and are correlated with the Illustrated Parts List (IPL).
CLEANING section contains general cleaning procedures, which should be observed during repair
and part replacement where applicable.
CHECK section contains general areas to visually observe during disassembly and assembly to
assure that equipment operational standards are met.
REPAIR section contains specific instructions for repairing areas of the equipment not specifically
covered in the ASSEMBLY section.
ASSEMBLY section contains all specific instructions necessary for part replacement and to
supplement the IPL.
FITS AND CLEARANCES section contains a list of dimensional values, torques, etc., if required
during assembly. These parameters are also specified in the ASSEMBLY section where applicable.
SPECIAL TOOLS, FIXTURES, AND EQUIPMENT section contains a list of all special equipment
required to perform procedures specified in the other manual sections.
ILLUSTRATED PARTS LIST (IPL) section contains illustrations and parts lists for all equipment
assemblies, subassemblies, and components. The illustrations and parts lists are item-number
keyed for location of parts, and list quantities, part numbers, and part descriptions. An introduction
to the IPL relates how it is used, definitions used, equipment designators, and alphanumerical
indices for parts.
I.B.1516A Page INTRO-1
23-12-01
Mar 30/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
ABBREVIATIONS AND ACRONYMS
A/DAnalog-to-Digital
ACAlternating Current
ACARSAircraft Communications Addressing and Reporting System
ADPAirborne Datalink Processor
AFAudio Frequency
AGCAutomatic Gain Control
AMAmplitude Modulation
AMPLAmplifier
ARINCAeronautical Radio, Inc.
ATAAir Transport Association
ATEAutomatic Test Equipment
ATPAcceptance Test Procedure
BITBuilt-In Test
BITEBuilt-In Test Equipment
BPBottom Plug
CCelsius
CCACircuit Card Assembly(ies)
CFDSCentral Fault Display System
CMCCentral Maintenance Computer
CMUCommunications Management Unit
CPLRCoupler
D/ADigital-to-Analog
dBDecibel
dBmDecibel with respect to 1 milliwatt
DCDirect Current
DDSDirect Signal Synthesis
DMData Module
DMMDigital Multimeter
DOD-HDBKDepartment of Defense Handbook
DOSDisk Operating System
EMCElectromagnetic Compatibility
EMFElectromotive Force
EEPROMElectrically Erasable Programmable Read Only Memory
EPROMElectrically Programmable Read Only Memory
FFahrenheit
FAAFederal Aviation Administration
1I.B.1516A Page INTRO-2
23-12-01
Mar 30/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
Fig.Figure
GNDGround
GSEGround Support Equipment
HFHigh Frequency
HFDLHigh Frequency Data Link
HFDRHigh Frequency Data Radio
HFMHigh Frequency Modem
HFVRHigh Frequency Voice Radio
HgMercury
HzHertz
IFIntermediate Frequency
kHzkilohertz
kBpskilobits per second
LEDLight Emitting Diode
LRULine Replaceable Unit
MCUModular Concept Unit
MHzMegahertz
MIL-STDMilitary Standard
MPMiddle Plug
MS WindowsMicrosoft Windows
mVmillivolt
nmNanometer
PCPersonal Computer
PLLPhase-locked Loop
PROMProgrammable Read Only Memory
PTTPush-to-Talk
PWBPrinted Wiring Board
Ref.Reference
RFRadio Frequency
RTCARadio Technical Commission for Aeronautics
RXReceive
SSBSingle Sideband
TDMATime Division Multiple Access
TPTest Point or Top Plug
TXTransmit
UTCUniversal Time Coordinated
VVolt
VACVolts Alternating Current
I.B.1516A Page INTRO-3
23-12-01
Mar 30/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
VCOVoltage-controlled Oscillator
VDCVolts Direct Current
WWatt
XCVRTransceiver
1I.B.1516A Page INTRO-4
23-12-01
Mar 30/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
TO: HOLDERS OF XK516D1 HF TRANSCEIVER COMPONENT MAINTENANCE MANUAL, PART
Item 3: (1KW) was (500W). Same source as item 1 was Rohde and Schwarz.
Item 4: Added Agilent Model No.; Agilent Technologies, Inc. was Hewlett-Packard Co.
Added Alternate Test Equipment to CMS 54, items 1 through 6.
10056030.1555.02 was 6030.1555.01. 6030.1555.03 was 6030.1555.02.
1010Added Figure name and number.
1011Added (VD8286) VS0715705 to items 15, 40, 45, and 55.
1012Added (VD8286) VS0715705 to item 115.
1014Item 320 was: 6030.1555.01.
Item 320A was: 6030.1555.02.
I.B.1516A Page 1/2
23-12-01
Oct 25/02
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
I.B.1516A Page 3
Transceiver Front Panel and Rear Connector
Figure 2
23-12-01
Mar 30/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
B. Electrical
The XK516D1 HF Transceiver mode of operation (SSB or AM voice, data, etc.) is controlled
via 2 ARINC 429 serial ports, which are connected on the aircraft to the radio management
panel. The Transceiver is configured for control via ARINC 429 words, both with label 037,
and words with label 205, 206, 207 (installation dependent).
The Transceiver can be connected by means of 2 additional ARINC 429 ports (receive and
transmit) to an on-board central fault display system (CFDS) according to ARINC 604 or to a
central maintenance computer (CMC). There are 3 input discretes (CFDS type programming
pins) that are available in the rear connector to identify the type of aircraft maintenance system. The Transceiver automatically detects which type of aircraft maintenance system (CFDS
or CMC) it is connected to if the CFDS Type input discretes are all open.
Part Number 964-0452-002, 012, and 022 Tranceivers can also be connected to 1 or 2
ACARS Management Units (MU) or Communications Management Units (CMU) by means
of 1 transmit and 2 receive ARINC 429 ports to provide the means to exchange data link
messages with compatible HF Data Link Ground Stations when the Transceiver is operating
in the internal HFDL Data mode. Refer to Fig. 3 for the HF Voice/Data Radio System Interconnect Diagram, showing all the possible connections to other aircraft systems.
The FK 516 Antenna Coupler (part of XK 516D HF Radio system) is connected to the Transceiver by a coaxial cable and a multiwire control cable. The coaxial cable carries the RF signal and control data for the coupler. The coupler control data consists of serial data messages
sent via the inner conductor of the coaxial cable.The multiwire control cable provides the coupler with 115V/400Hz (single phase) power. The control cable also provides the interlock wiring between couplers in dual HF installations. As an option, for single HF installations, the
multiwire control cable may not be used. In this case, the coaxial cable also carries the Coupler power supply (+28V).
C. Equipment Specifications
The specifications for the XK516D1 HF Transceiver are listed in Fig. 4.
D. Operation of XK516D1 in Voice Mode
(1) To operate the XK516D1 in Voice Mode, the operator selects either SSB Mode or AM
Mode on the Radio Control Panel and selects the frequency.
(2) The radio tunes to the selected frequency, and the received audio can immediately be
heard on the Audio Management System.
(3) To initiate transmission, the microphone keyline (PTT) must be grounded while speaking
into the microphone.
E. Operation of XK516D1 in HF Data Link Mode
(1) To select HF Data Link Mode, the operator must select DATA mode on the Radio Control
Panel.
(2) When the HFDR is placed in data mode, the HFDR performs an automatic frequency
search from a list of frequencies assigned to HF Data Sync operation. Voice communication through this radio is not possible during this mode of operation.
(3) Based on the aircraft’s position and time of day, the HFDR prioritizes its list of possible
frequencies so that frequencies with the highest probability of propagation are tried first.
1I.B.1516A Page 4
23-12-01
Mar 30/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
Interconnect Diagram, HF Voice/Data Radio System
I.B.1516A Page 5
Figure 3
23-12-01
Mar 30/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
1I.B.1516A Page 6
Transceiver Specifications
Figure 4 (Sheet 1)
23-12-01
Mar 30/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
I.B.1516A Page 7
Transceiver Specifications
Figure 4 (Sheet 2)
23-12-01
Mar 30/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
Backup to 516/517 Interface.
Primary mode.
Tune power (MPSC)
1I.B.1516A Page 8
Transceiver Specifications
Figure 4 (Sheet 3)
23-12-01
Mar 30/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
I.B.1516A Page 9
Transceiver Specifications
Figure 4 (Sheet 4)
23-12-01
Mar 30/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
1I.B.1516A Page 10
Transceiver Specifications
Figure 4 (Sheet 5)
23-12-01
Mar 30/01
Honeywell
COMPONENT MAINTENANCE MANUAL
PART NUMBER 964-0452
I.B.1516A Page 11
Transceiver Specifications
Figure 4 (Sheet 6)
23-12-01
Mar 30/01
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