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Crimped joints for aircraft electrical cables and wires. - Specification for design requirements (including tests) for components and tools
Description
Crimped joints for aircraft electrical cables and wires. - Specification for design requirements (including tests) for components and tools1 Scope 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
Different fibre penetration strategies
Personal fall protection systems testers
or door leaves of any material
Cross referencing of information requirements associated with Level 2 BIM in accordance with PAS 1192-2
Light emitting diodes (LEDs) have been deleted from the scope of this document except for communication applications
The method applies to products having titanium contents between 0
inward and outward opening
dimensions and testing of two forms of spray taps: pillar spray taps and bib spray taps
pH value of aqueous extract (optional test)
transport of WMP-MNOs
dynamic effects and centrifugal
chimneys (including free-standing industrial chimneys) and lighthouses
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- USA
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