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BSI - BS G 194

Specification for Lever-Operated Manual Switches for Aircraft

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Organization: BSI
Publication Date: 31 December 1965
Status: inactive
Page Count: 16
ICS Code (Aerospace electric equipment and systems): 49.060

Document History

BS G 194
December 31, 1965
Specification for Lever-Operated Manual Switches for Aircraft
A description is not available for this item.

References

This document references:
BS 350 - Conversion factors for units
Published by BSI on May 25, 2004
A description is not available for this item.
This document references:
BS 4G 178-2 - Crimped Joints for Aircraft Electrical Cables and Wires - Part 2: Specification for Control of Crimping (Including User Control Tests)
Published by BSI on November 28, 1986
User control tests for aircraft constructors or operators.
This document is referenced by:
BS G 200 - Miniature Lever-Operated Manual Switches
Published by BSI on August 21, 1967
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...
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...
This document is referenced by:
DEF STAN 00-970:PT7:S2 S6 - Design and Airworthiness Requirements for Service Aircraft Part 7: Rotorcraft Supplement 6: Equipment (Subpart F)
Published by MODUK on July 13, 2015
A description is not available for this item.
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