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BSI - BS 2G 202

Specification for Design and Performance Requirements for Airframe-Fit Electrical Connectors for D.C. and Low Frequency A.C. Applications

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Organization: BSI
Publication Date: 29 February 1988
Status: active
Page Count: 14
ICS Code (Aerospace electric equipment and systems): 49.060
scope:

Includes engine connectors.

Document History

BS 2G 202
February 29, 1988
Specification for Design and Performance Requirements for Airframe-Fit Electrical Connectors for D.C. and Low Frequency A.C. Applications
Includes engine connectors.
BS G 202
January 29, 1968
Specification for design and performance requirements for aircraft electrical plugs and sockets for d.c. and low frequency a.c. applications
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 references:
BS 5772-3 - Basic Testing Procedures and Measuring Methods for Electromechanical Components for Electronic Methods Part 3: Current Carrying Capacity Tests
Published by BSI on November 30, 1979
A description is not available for this item.
This document is referenced by:
BS G 215 - Specification for thermocouple extension cables for aircraft (nickel-chromium and nickel-aluminium)
Published by BSI on May 17, 1972
A description is not available for this item.
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...
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