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position of the LDU in the overall file transfer. The sink performs a
verification process on the EOT, and sends an Acknowledgment Word
(ACK) if all tests are passed. The source then sends another CTS, and the
process is repeated until the last LDU is acknowledged.
Bit Oriented Protocols ARINC 429 Tutorial
16 ARINC Protocol Tutorial
AIRLINE
SOURCE
------->
------->
RTS WORD AIRCRAFT
SINK
ORIGINAL
DATA FILE
CTS WORD <------
SOT WORD 1 FIRST
DATA WORD 2 LDU
" n
DATA WORD 254
EOT WORD 255
ACK WORD <------
--------> RTS WORD
CTS WORD <-------
-------> SOT WORD 1
LAST DATA WORD 2
LDU DATA WORD 3 RECEIVED
DATA
FILE
EOT WORD 4
ACK WORD
Figure 8. File Transfer Scheme Version 1 (no Windows)
ARINC 429 Tutorial Bit Oriented Protocols
ARINC Protocol Tutorial 17
Table 11. Systems Using Bit Oriented Communications and Their Address Labels
SYSTEM SAL
(OCT) SYSTEM SAL
(OCT)
777 CABIN INTERPHONE SYSTEM 152 LOW SPEED DATA LINK (ARINC 603) 300
747 DFDR AND A330/340 SSFDR 163 FMC 1 300
DFDAU (Mandatory Load Functions) 170 FMC 2 301
SDU #2 173 DFDAU (AIDS) 302
RFU 174 CFDIU 303
HGA/HPA TOP/PORT 175 ACARS MU/CMU (724B, 748) 304
HGA/HPA STARBOARD 176 WBS 305
LGA/HPA 177 TCAS 306
GPS/GNSS SENSOR 201 SDU #1 307
MCDU 1 220 CABIN TELECOMMUNICATIONS UNIT
(CTU) 334
MCDU 2 221 HF DATA RADIO/DATA UNIT #1 340
MCDU 3 222 HF DATA RADIO/DATA UNIT #2 344
PRINTER 1 223 ACESS 360
PRINTER 2 224 EFIS 361
HIGH SPEED DL (ARINC 615) 226 ENGINE INDICATION UNIT 365
MCDU 4 230 CABIN TERMINAL 3 372
EIVMU 1 234 CABIN TERMINAL 4 373
EIVMU 2 235 CABIN TERMINAL 1 374
EIVMU 3 236 CABIN TERMINAL 2 375
EIVMU 4 237 OMEGA NAV. SYSTEMS 376
CABIN VIDEO SYSTEM (AIRSHOW) 266

ARINC Protocol Tutorial 19
CHAPTER 2
Other ARINC Protocols
ARINC 419
Reference 7, ARINC 419 Digital Data System Compendium, describes a
number of digital transmission system building blocks which where
available prior to 1984. It provides a synopsis of many protocols that
predate ARINC 429 such as ARINC 561, 582, 573 and 575.
The reference describes a number of digital transmission systems with
varying standards. Some systems used 32-bit words similar to ARINC
429; some used major frames of four subframes each consisting of 64, 12-
bit words. Still others used 32-bit, rather than 64-bit words. Some
message frames were 24 bits with three subframes of two BCD words.
Some systems did not provide information identifiers; others used 8-bit
label codes, and another depended on time slots for identifying
information. Identification of BCD vs. BNR was provided by a flag bit in
either the 1st bit or the 4th bit transmitted. A variety of standard data labels
were adopted.
Some electrical interconnections depended on one wire per bit; others used
the 6 wire system described above while others used a shielded 2 wire
twisted pair or a coaxial cable. Either two state, (HI LO), or three state (HI
NULL LO) were used. Voltage levels ranged from 18.5 to 10 for the high
state and from (less than) 5 to 1 for the null where used. Digital languages
included Gilham code (an example is the altitude encoder for the ATC
Transponder), a bit stream you determined in each individual case,
International Standards Organization (ISO) Alphabet #5, BCD, and BNR.
In some cases there was no error detection or correction, others used bit
parity or character parity, or block sequence check. Bit rate varied from
384 BPS to 12+ KBPS, and there were many other variations among
systems.
The variability of “standards” doesn’t matter where a single user is
involved, but is very important when equipment from different suppliers
must interact with each other. Standardization is beneficial not only to the
aircraft integrator, but to the equipment supplier who can have greater
assurance of product acceptability so long as it is “on spec”. ARINC 429
ARINC 453 Other ARINC Protocols
20 ARINC Protocol Tutorial
is the most widely applied Digital Data Transmission specification for
modern transport aircraft. ARINC 429 draws on the experience of 419 but
does not depend on it.
ARINC 453
Not a formally released specification. See ARINC 708.
ARINC 561/568
The need for standardized digital data transmission arose during the
development of ARINC Characteristics 561, “Air Transport Inertial
Navigation System”. ARINC 568 uses the same electrical interface as
ARINC 561.
A six-wire system involving 3 pairs of wires, was used in 561. The three
 
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