C2435.41.10

Shield Type:	--
Shield Coverage:	--
Shield Material:	--
Conductor Insulation:	Poly-Vinyl Chloride (PVC)
Jacket (Insulation) Thickness:	0.0320" (0.813mm)
Usage:	Communication, Control
Operating Temperature:	-20°C ~ 90°C
Voltage:	300V
Features:	--
Ratings:	--
Jacket Color:	Gray
Length:	1000.0' (304.8m)
Series:	--
Jacket (Insulation) Diameter:	0.423" (10.74mm)
Jacket (Insulation) Material:	Poly-Vinyl Chloride (PVC)
Conductor Material:	Copper, Tinned
Conductor Strand:	19/0.0117"
Wire Gauge:	16 AWG
Number of Conductors:	9
Moisture Sensitivity Level (MSL):	--
Cable Type:	Multi-Conductor
Lead Free Status / RoHS Status:	--
Part Status:	Obsolete

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Introduction
Multiple Conductor Cables are a type of cable used to connect multiple devices or elements of an electrical system. The C2435.41.10 standard governs the use of multiple conductor cables for aircraft wiring applications. This standard specifies the design requirements of multiple conductor cables for aircraft wiring applications including information on the wire and voltage, insulation material, conductor wire insulation, ground wires, and mechanical design elements. It also sets out requirements for the working principles of multiple conductor cables for aircraft wiring applications.

Design Requirements for Multiple Conductor Cables
The C2435.41.10 standard specifies several design requirements when using multiple conductor cables for aircraft wiring applications. The wires and voltage of the cables must comply with the applicable aircraft power systems standards, which are typically set by the specific aircraft manufacturer. The insulation material used must comply with the applicable standards and requirements regarding fire resistance, environmental resistance, and other general requirements. Additionally, all conductor wires must be insulated from each other and any insulation material must comply with applicable standards. The ground wires must also comply with applicable standards and requirements regarding resistance and surface leakage current. Furthermore, the mechanical design of the cables must meet certain criteria, including bending radii and strain relief requirements.

Working Principles of Multiple Conductor Cables
The C2435.41.10 standard also sets out requirements for the working principles of multiple conductor cables for aircraft wiring applications. The conductor wires must be designed for a voltage of 600V and must be rated for the temperature and environment of the aircraft in which they will be used. The maximum cross-sectional area of each conductor wire must be at least 0.00101mm^2. All conductor wires must be individually insulated from each other and any insulation material must have a minimum thickness of 0.003mm. All ground wires must also be effectively connected to the aircraft ground plane and must be able to carry the maximum continuous current and meet the applicable AC/DC test requirements of the aircraft manufacturer.

Conclusion
Multiple Conductor Cables are an essential component of aircraft wiring applications and the C2435.41.10 standard sets out the design and working requirements for this type of cable. Specifically, this standard governs the design requirements of multiple conductor cables, including information on the wire and voltage, insulation material, conductor wire insulation, ground wires, and mechanical design elements. Additionally, it sets out requirements for the working principles of multiple conductor cables for aircraft wiring applications, including criteria for the conductors, insulation material, and ground connections.

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