71-433035-13F

Overview

The 71-433035-13F is a circular MIL-spec connector plug manufactured by Amphenol Aerospace Operations. It features an 8-position configuration with male pin contacts arranged in insertion style 22-23. The housing is constructed from aluminum alloy and finished with cadmium plating for corrosion resistance. Electrical termination is achieved via solder connections, ensuring reliable signal transmission. This component adheres to military-grade standards for rugged environmental performance.

Feature Summary

• Constructed with a durable aluminum alloy shell featuring cadmium plating
• Utilizes a threaded mating interface for secure connection retention
• Designed with silver-plated copper alloy contacts for conductivity

Applications

• Military avionics systems
• Ruggedized ground support equipment
• Defense communication arrays

Procurement Notes

Verify the specific manufacturer part number against official Amphenol Aerospace documentation to ensure compatibility with existing system interfaces. Confirm that the cadmium plating and material specifications meet the required environmental compliance standards for the intended deployment environment before finalizing procurement orders.

Selection Notes

Select this model when a straight cable-mount plug with eight positions is required. Ensure the mating receptacle matches the 22-23 insertion arrangement and shell size. Verify that the solder termination method aligns with the available PCB or wire harness assembly capabilities within the design constraints.

Part Context

This component belongs to the family of circular MIL-spec connectors produced by Amphenol Aerospace Operations. These connectors are engineered for high-reliability applications where vibration and harsh environmental conditions are prevalent. The product line emphasizes standardized interfaces compatible with established military hardware ecosystems.

Replacement Considerations

Cross-reference with equivalent MIL-DTL-38999 series connectors if physical footprint adaptation is necessary. Verify that substitute parts maintain identical contact arrangements and shell sizes to ensure mechanical interchangeability without redesigning mounting structures.