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
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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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