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BSI - BS 2G 223

Specification for Screen Terminating Devices for Aircraft Electric Cables

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Organization: BSI
Publication Date: 31 August 1989
Status: active
Page Count: 12
ICS Code (Aerospace electric equipment and systems): 49.060
scope:

Design and testing of insulated and uninsulated screen terminating devices for general purpose screened electrical cables or wires in the temperature range defined in the relevant cable specifications.

Document History

BS 2G 223
August 31, 1989
Specification for Screen Terminating Devices for Aircraft Electric Cables
Design and testing of insulated and uninsulated screen terminating devices for general purpose screened electrical cables or wires in the temperature range defined in the relevant cable...
BS G 223
December 31, 1976
Specification for Screen Terminating Devices for Aircraft Electric Cables
A description is not available for this item.

References

This document references:
BS 3G 100-2.3.12 - General Requirements for Equipment for Use on Aircraft - Part 2: All Equipment - Section 3: Environmental Conditions - Subsection 3.12: Fluid Contamination
Published by BSI on May 31, 1991
A description is not available for this item.
This document references:
BS 5G 178-1 - Crimped Joints for Aircraft Electrical Cables and Wires - Part 1: Specification for Design Requirements (Including Tests) for Components and Tools
Published by BSI on February 15, 1993
Provides updated tests and test requirements for crimped joints with copper, copper alloy, aluminium and aluminium alloy conductors.
This document is referenced by:
DEF STAN 00-970: PT1 SEC6 - Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 6: Equipment
Published by MODUK on September 19, 2016
INTRODUCTION This Clause specifies the requirements relating to equipment and systems embodied on any aircraft. These requirements are to be used where there are no aircraft specific requirements...
This document is referenced by:
DEF STAN 00-970: V1 B2 P4 - Design and Airworthiness Requirements for Service Aircraft Volume 1 - Aeroplanes Book 2 (Parts 4 to 6 and Chapters 700 to 710) Part 4: Detail Design and Strength of Materials
Published by MODUK on October 1, 1992
GENERAL In the detailed design of the aeroplane the variety of materials and parts to be kept to a minimum consistent with structural efficiency and without unduly sacrificing structure weight. The...
This document is referenced by:
DEF STAN 00-970: V2 P7 - Design and Airworthiness Requirements for Service Aircraft Volume 2 - Rotorcraft Book 3 (Parts 7 to 10) Part 7: Installations
Published by MODUK on March 10, 1998
INTRODUCTION The requirements of this Chapter are applicable to the design and construction of all turbine engine propulsion system installations including all the equipment and sub-systems necessary...
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