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BSI - BS 2M 53

Aircraft - Fluid systems - Thermal shock testing of piping and fittings

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Organization: BSI
Publication Date: 15 November 1997
Status: active
Page Count: 12
ICS Code (Aerospace fluid systems and components): 49.080

Document History

BS 2M 53
November 15, 1997
Aircraft - Fluid systems - Thermal shock testing of piping and fittings
A description is not available for this item.
BS M 53
April 29, 1983
Method for thermal shock testing of pipes and fittings for aerospace fluid systems
A description is not available for this item.

References

This document references:
ISO 6772 - Aerospace - Fluid systems - Impulse testing of hydraulic hose, tubing and fitting assemblies
Published by ISO on October 1, 2012
This International Standard specifies the requirements and the procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace hydraulic systems. Requirements may apply...
This document is referenced by:
BS 2M 60 - Separable Tube Fittings, 24 Degree Cone, for Aerospace Fluid Systems
Published by BSI on August 15, 1993
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: VOL1 - Installations Chapter 711 on
Published by MODUK on March 10, 1998
This chapter states the design requirements for the installation of armament equipment in all aeroplanes. Armament Equipment, for the purpose of these requirements , comprises the weapon...
This document is referenced by:
DEF STAN 00-970: PART 1 - Certification Specifications for Airworthiness Part 1: FIXED WING COMBAT AIR SYSTEMS
Published by MODUK on August 28, 2020
Note 1 Where CS 25 and CS 23 make reference to ‘the Agency’, this should be considered to mean the certifying authority.
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