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BSI - BS M 24

Graphical Symbols for Aircraft Hydraulic and Pneumatic Systems

inactive, Most Current
Organization: BSI
Publication Date: 4 March 1955
Status: inactive
Page Count: 9
ICS Code (Graphical symbols for use on specific equipment): 01.080.20
ICS Code (Aerospace fluid systems and components): 49.080

Document History

BS M 24
March 4, 1955
Graphical Symbols for Aircraft Hydraulic and Pneumatic Systems
A description is not available for this item.

References

This document is referenced by:
BS 5070-3 - Engineering diagram drawing practice - Part 3: Recommendations for mechanical/fluid flow diagrams
Published by BSI on April 29, 1988
Gives principles and presentation for mechanical, hydraulic, pneumatic, topographic, block, circuit, piping, interconnection and supplementary diagrams.
This document is referenced by:
MODUK AVP 70 - Specifications for Air Technical Publications
Published by MODUK on March 1, 1970
PREFACE AvP 70 is one of a number of documents which together instruct and guide Government contractors (and their sub-contractors), in the administrative arrangements and technical requirements...
This document is referenced by:
DEF STAN 05-56 - Graphical Symbols for Aircraft Hydraulic and Pneumatic Systems
Published by MODUK on January 1, 1980
This Standard specifies the graphical symbols to be used in the preparation of diagrams of aircraft hydraulic and pneumatic systems for inclusion in Air Publications and servicing manuals.
This document is referenced by:
BS 5070 - Drawing practice for engineering diagrams
Published by BSI on May 12, 1974
Sets out the drawing practice common to all fields of engineering diagrams. Various types of diagram are identified and many examples are given to illustrate the principles of their presentation.
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...
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