ARINC 429 Line Receivers | APC Technology Group
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ARINC 429 Line Receivers

Dual, Quad, Octal and Galvanically Isolated Line Recievers with Lightning Protection

Holt Integrated Circuits has the largest ARINC 429 IC product portfolio in existence today. Holt’s ARINC 429 ICs cover a whole range of complexity, from simple analogue bus interface chips such as line receivers and line drivers, to protocol ICs with on-chip FIFOs or RAM. Holt’s unique approach provides fully integrated solutions with both analogue transceivers and digital protocol on one chip. The latest line of ARINC 429 terminal ICs are designed to operate from a single 3.3V supply and incorporate a host Serial Peripheral Interface (SPI).

Holt Integrated Circuit's latest line receivers and line drivers both have internal lightning protection to RTCA/DO-160G, Section 22 Level 3 pin injection test.

ARINC 429 Applications

  • Guidance and Navigation Systems
  • Flight Control
  • Flight Data
  • Communications
  • In-Flight Entertainment Systems

Resources

ARINC 429 Product Selector Guide pdf 1525.33

 Device Device Type

Description

Released Datasheet
HI-8460
HI-8461
Galvanically Isolated Line Receiver 800V Galvanically Isolated ARINC 429 Line Receiver with Internal Level 3 Lightning Protection 2017 View
HI-8456
HI-8457
HI-8458
Octal Line Receiver Integrated DO-160G Level 3 Lightning Protection. Drop-in replacements for DEI1046, DEI1047 and DEI1148. Pin-compatible with Holt HI-8448. 3.3V or 5V operation. 2015 View
HI-8450
HI-8451
Line Receiver Integrated DO-160G Level 3 Lightning Protection. 3.3V or 5V operation. Compact SO-8 package. 2014 View
HI-8454
HI-8455
Quad Line Receiver Integrated DO-160G Level 3 Lightning Protection on each channel. 3.3V or 5V operation. Compact 5mm x 5mm QFN or TSSOP packages. 2014 View
HI-35851 ARINC 429 Repeater ARINC 429 Repeater. Connects directly to ARINC 429 bus. Re-transmit at ARINC 429 low or high-speed data rates. 2021 View
HI-8477
HI-8478
Line Receiver with Label Filtering and Parity Check ARINC 429 Line Receiver. Designed specifically for use without a microprocessor. All configuration and control is programmed via logic level input pins. 2015 View
HI-8591 Line Receiver 3.3V or 5V operation. +/-30V common mode capability. External resistance for easy lightning protection of ARINC inputs. Compact SO-8 package. 2004 View
HI-8475
HI-8476
Line Receiver with Label Filtering ARINC 429 Line Receiver. Designed specifically for use without a microprocessor. All configuration and control is programmed via logic level input pins. 2013 View
HI-3718 ARINC 717 / ARINC 429 Transceiver 3.3V single supply operation. Harvard Bi-Phase (HBP) and Bi-Polar Return-to-Zero (BPRZ) line receiver and line drivers. 2014 View
HI-8588-10 Line Receiver 5V operation. Self-test mode. External 10kOhm resistance for lightning protection of ARINC inputs. Compact SO-8 package. 1999 View
HI-8588 Line Receiver 5V operation. Self-test mode with tri-state outputs. Compact SO-8 package. 1999 View
HI-84820 Dual Line Receiver Input noise filtering. Self-test mode. Drop-in replacement for HI-8482 and Fairchild/Raytheon RM3183. 2021 View
HI-8483 Dual Line Receiver Functionally equivalent to Fairchild/Raytheon RM3283 and DEI3283. 2010 View
HI-8482 Dual Line Receiver Input noise filtering. Self-test mode. 1992 View
HI-8444
HI-8445
Quad Line Receiver 3.3V or 5V operation. Self-test mode on HI-8444. 2001 View
HI-8448 Octal Line Receiver 3.3V or 5V operation. Self-test mode. 2001 View

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APC Technology Group, has a 35-year heritage in the design, specification and distribution of specialist electronic components, products and systems for aerospace and space applications. Our engineer-led technical sales team have extensive pedigrees in designing-in components and products into space programmes.

As AS9120B Certified Distributors, our space-compatible technologies include, but are not limited to: Radiation-Tolerant, Semiconductors, Microelectronics and Optoelectronic Components, including Integrated Circuits. APC can also supply high-density ‘System-in-Package’ Solutions that miniaturise radiation tolerant systems.​

What is ARINC-429?

Aeronautical Radio, Inc. (ARINC) was a privately held corporation started in 1929, ultimately acquired by Collins Aerospace in 2013. This corporation was founded by and comprised of various airlines and airline manufacturers (components and equipment) with the goal of producing sets of specifications (standards) for avionics hardware for global aircraft use. ARINC-429 is the standard for local area networks on commercial and transport aircraft. Communications, guidance, altitude, altitude reference, flight management, and more are all needed to work together to accomplish a successful flight. ARINC-429 was designed in the 1970’s to accomplish this goal.

ARINC-429 SPECIFICATION

The ARINC-429 technical specification, originally referred to as the Digital Information Transfer System (DTIS), was published in 1977 to define how avionics systems and components should communicate within commercial aircraft. The Mark 33 Digital Information Transfer System, as it is known today, is still the standard most commonly used by airlines. This specification is used to establish 429 bus communications for word structures, electrical characteristics and other protocols.

What is unique about ARINC 429 data transfer is its simple one directional flow of bus communications data. A typical data bus offers multidirectional data transfer between various bus points on a single set of wires. Not so with ARINC-429, but this is not taken as a disadvantage to the airlines as it has allowed for long-term operational cost savings and system reliability.

The ARINC-429 specification entails the following:

  • Hardware consisting of only a single transmitter source supporting 1 to 20 receivers (also known as “sinks”) on a single wire pair.
  • Data transmission is one directional. Additional busses are required for multidirectional data transfer.
  • A data transmitter can only talk to a defined number of data receivers on a single bus on one wire pair.
  • For multidirectional communication, 2 wire pairs are required for data transmission in opposite directions.
  • Transmit and receive channels are different ports.
  • Data words are 32 bits (most messages consist of a single data word) broken into 24-bits containing the core information and 8-bits acting as a data label describing the data transmitted.
  • Messages are transmitted at either low speed (12.5 kbit/s) or high speed (100 kbit/s) to receiver components