Published: July 27, 2026 · Technical Guide
Walk down the avionics bay of any Boeing 737, Airbus A320, or military transport aircraft, and you'll see rows of identical black boxes — each one slid into a metal tray, locked in place, and connected through a massive rectangular connector at the back. That connector is built to ARINC 600, and it is the most widely deployed avionics interconnection standard in commercial aviation.
ARINC (Aeronautical Radio, Incorporated) 600 defines the mechanical, electrical, and environmental requirements for Air Transport Avionics Equipment Interfaces. In plain terms: it standardizes how a Line Replaceable Unit (LRU) physically mates with the aircraft wiring — making it possible for airlines to swap a flight management computer from one vendor with a radio altimeter from another, and have both plug into the same tray in the same rack.
The ARINC 600 system is a rack-and-panel architecture with three components:
This design means a technician can replace a failed LRU on the tarmac in under 5 minutes: release the hold-down hooks, slide the old box out, slide the new box in, lock. The connector blind-mates automatically — no tools, no torque wrenches, no pin alignment guesswork.
ARINC 600 connectors are designated by size (1, 2, or 3) and insert configuration (number and type of contact cavities). The size refers to the connector shell width:
| Size | Width | Max Insert Stations | Typical LRU |
|---|---|---|---|
| Size 1 | ~57 mm (2.25 in) | 2 inserts (A, B) | Radio management panel, audio control |
| Size 2 | ~95 mm (3.75 in) | 4 inserts (A, B, C, D) | VHF comm radio, DME, transponder |
| Size 3 | ~120 mm (4.75 in) | 6 inserts (A, B, C, D, E, F) | FMC, TCAS computer, satcom, display processor |
Each insert station can hold different contact configurations designated by a numeric code:
ARINC 600 uses mechanical keying pins in the connector to ensure that only the correct LRU type can be inserted into a given tray position. Keying is configured by installing keying pins in specific positions on the connector face — like a physical password. The aircraft wiring manual specifies which keying positions are populated for each LRU slot.
Common keying pin positions are designated by letters (A through Z, excluding I, O, and Q) and arranged in a matrix across the connector. This prevents dangerous mismatches — a flight management computer cannot be accidentally installed into a radio transponder slot, even if both use Size 2 trays.
Engineers sometimes confuse ARINC 600 with its predecessor, ARINC 404. The key differences:
| Feature | ARINC 404 | ARINC 600 |
|---|---|---|
| Introduced | 1950s | 1970s (still current) |
| Connector Type | Two circular connectors per LRU | Single rectangular multi-insert connector |
| Contact Density | Lower (limited by circular shell sizes) | Higher (rectangular form factor, more inserts) |
| Blind Mating | Less reliable (dual circular alignment) | Superior (single rectangular + guide pins) |
| Current Usage | Legacy aircraft, some regional jets | All modern Boeing, Airbus, and military platforms |
Despite being a 50-year-old standard, ARINC 600 continues to evolve. Modern insert configurations now support fiber optic termini for high-bandwidth avionics data buses, high-speed differential pairs for Ethernet-based aircraft networks (ARINC 664/AFDX), and composite-shell variants for weight reduction on next-generation platforms like the Boeing 777X and Airbus A350.
The standard's longevity is its strength: airlines operating mixed fleets of A320ceo, A320neo, 737 NG, and 737 MAX aircraft can stock a single set of ARINC 600 LRUs that fit across generations. That interchangeability saves millions in inventory costs and simplifies MRO logistics.
Source ARINC 600 connectors for your avionics program?
Airoadcon manufactures ARINC 600 Size 1, 2, and 3 connectors with full insert configuration support. All connectors tested to MIL-STD environmental specs. Free samples and 2–4 week lead times.
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