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ARINC 600 Connectors are a recognized standard rack and panel connector for
aircraft applications. The ARINC 600 is the successor to the ARINC 404 for many of
the new avionic designs. Compared to the ARINC 404, the ARINC 600 features lower
mating force contacts, increased contact count and a front release, floating keying
system.
Amphenol's extensive product offering will meet the most demanding needs of our
customers. At the design-in stage, Amphenol's sales engineers will work with you to
select a connector from our standard product line or coordinate the design of an
application specific connector. Amphenol's ARINC 600 rack and panel connectors
are designed to meet all relevant ARINC 600 connector specifications.
Amphenol ARINC 600 Connectors offer:
Amphenol ARINC 600 Connectors offer:
- Low insertion force contacts
- Both environmental and non-environmental versions
- Front removable keying posts
- Field replaceable inserts for size 22 and power contacts
- Up to 800 size 22 contact positions in one connector
- Crimp, coaxial, power, printed circuit, and wire wrap contacts
- Waveguide connections
Unit of Measure
Specifications
|
Cavity A
|
Cavity B
|
Cavity C
|
Connector Layout Arrangements
|
Polarizing Position
|
Performance Specifications
|
Material Specifications
Specifications
Performance Specifications
Dielectric withstanding voltage (DWV) |
N/A 1500Vrms 500 Vrms at 50,000 ft. (15,240m) |
Contact resistance Size 22: |
N/A 8.0 milliohms, initial (max.) 11.0 milliohms, conditioned (max.) |
Contact resistance Size 20: |
N/A 7.0 milliohms, initial (max.) 8.5 milliohms,conditioned (max.) |
Contact resistance Size 16: |
N/A 7.0 milliohms, initial (max.) 8.5 milliohms,conditioned (max.) |
Contact resistance Size 12: |
N/A 2.0 milliohms, initial (max.) 2.5 milliohms, conditioned (max.) |
Insulation Resistance |
N/A 5.0 gigaohms min. at 500 VDC |
Durability |
N/A 500 cycles min. - mating & unmating |
Temperature Range |
N/A -65°C (-86° F) to +125°C (+275° F) |
Vibration: |
N/A MIL-STD-1344, Method 2005.1, condition value E: random - 16.4G minimum severity: 8 hours in each of 3 mutually perpendicular planes with 100mA electrical load. No visible damage, breakage, cracking or loosening of parts and no discontinuities exceeding 1 microsecond. |
Shock |
N/A MIL-STD-1344, Method 2004.1, test condition A: Three shocks in each direction along each of 3 axes, mutually perpendicular to each other. No visible damage,breakage, cracking or loosening of parts and no discontinuities exceeding 1 microsecond. |
Material Specifications
Shells |
N/A Aluminum alloy, See Connector Mounting Modifier for Plating |
Retaining plates |
N/A Aluminum alloy, electroless nickel plated |
Polarizing keys |
N/A Aluminum alloy, electroless nickel plated |
Insulator material |
N/A Thermoset/Thermoplastic |
Inserts, grounded |
N/A Aluminum alloy, electroless nickel plated |
Screws, lockwashers, washers |
N/A Stainless steel, passivated |
Contact bodies |
N/A Copper alloy, gold plated |
Contact retention clips |
N/A Copper, gold plated |
Seals & grommets |
N/A Silicone/fluorosilicone elastomer |
O-Rings |
N/A Silicone/fluorosilicone rubber, colored blue |
EMI springs |
N/A Copper alloy, electroless nickel plated |