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Homepage>BS Standards>49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.060 Aerospace electric equipment and systems>BS 5G 178-1:1993 Crimped joints for aircraft electrical cables and wires. Specification for design requirements (including tests) for components and tools
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immediate downloadReleased: 1993-02-15
BS 5G 178-1:1993 Crimped joints for aircraft electrical cables and wires. Specification for design requirements (including tests) for components and tools

BS 5G 178-1:1993

Crimped joints for aircraft electrical cables and wires. Specification for design requirements (including tests) for components and tools

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Standard number:BS 5G 178-1:1993
Pages:16
Released:1993-02-15
ISBN:0 580 21549 0
Status:Standard
DESCRIPTION

BS 5G 178-1:1993


This standard BS 5G 178-1:1993 Crimped joints for aircraft electrical cables and wires. is classified in these ICS categories:
  • 49.060 Aerospace electric equipment and systems

This Part of BS 5G 178 specifies the design requirements and tests for components and tools for the crimping of insulated and non-insulated terminals and splices to general purpose electrical cables or equipment wires for aircraft with conductors of copper, copper alloy, aluminium or aluminium alloy, in locations in which the stabilized conductor temperature does not exceed the value specified for the relevant type of cable.

Tests for the components, tools and crimped joints are described in Annex A.

NOTE The latest revision or new edition of an Aerospace Series standard is indicated by a prefix number.


Provides updated tests and test requirements for crimped joints with copper, copper alloy, aluminium and aluminium alloy conductors.