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BSI - BS 2SP 90

Specification for corrosion‑resisting steel split cotter pins for aircraft - Inch series

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Organization: BSI
Publication Date: 30 November 2008
Status: inactive
Page Count: 10
ICS Code (Pins, nails): 49.030.40

Document History

BS 2SP 90
November 30, 2008
Specification for corrosion‑resisting steel split cotter pins for aircraft - Inch series
A description is not available for this item.
BS 2SP 90
November 30, 2008
Specification for corrosion‑resisting steel split cotter pins for aircraft - Inch series
A description is not available for this item.
BS SP 90
July 27, 1961
Corrosion-Resisting Steel Split Cotter Pins for Aircraft
A description is not available for this item.

References

This document references:
BS 2S 205 - Austenitic chromium-nickel steel wire rod, wire and springs - Specification
Published by BSI on December 14, 2004
A description is not available for this item.
This document references:
BS EN 2573 - Aerospace series - Steel X6CrNiTi18-10 (1.4541) - Air melted - Softened - Wires - 0,25 mm ≤ De ≤ 3 mm - Rm ≤ 780 MPa
Published by BSI on December 31, 2022
A description is not available for this item.
This document references:
BS 2S 130 - Specification for 18/9 chromium-nickel corrosion-resisting steel (niobium stabilized) billets, bars, forgings and parts - (540 MPa: limiting ruling section 150 mm)
Published by BSI on August 31, 1976
A description is not available for this item.
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 P4 - Detail Design and Strength of Materials
Published by MODUK on March 10, 1998
In the detailed design of the Rotor craft, the variety of materials and parts shall 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: PT1 SEC4 - Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 4: Design and Construction
Published by MODUK on July 13, 2015
PREFACE (a) This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Fixed Wing Aircraft for UK Military...
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