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  • BS 3S95(1967) : 1967

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    SPECIFICATION FOR 1[1/2] PER CENT NICKEL-CHROMIUM-MOLYBDENUM STEEL - (880/1080 MPA: LIMITING RULING SECTION 150 MM)

    Available format(s):  Hardcopy, PDF

    Superseded date:  01-09-2015

    Language(s):  English

    Published date:  01-01-1967

    Publisher:  British Standards Institution

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    Table of Contents - (Show below) - (Hide below)

    1 Inspection and testing procedure
    2 Process of manufacture
    3 Chemical composition
    4 Surface dressing
    5 Condition
    6 Final heat treatment
    7 Mechanical properties

    General Product Information - (Show below) - (Hide below)

    Committee ACE/61
    Development Note Supersedes 67/2360 DC and BS 2S95(1964). (07/2005) Earlier was withdrawn in error by the publisher, now has been reinstated. (04/2014) 1967 Edition Re-Issued in September 2015 & incorporates AMD 1 2015. Supersedes 15/30313994 DC. (10/2015)
    Document Type Standard
    Publisher British Standards Institution
    Status Superseded
    Superseded By
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    BS 2A 57:1962 SPECIFICATION FOR STEEL HEXAGONAL-HEADED SHEAR BOLTS (B.S.F. THREADS) FOR AIRCRAFT
    BS 2A173(1962) : 1962 SPECIFICATION FOR 100 DEGREES COUNTERSUNK HEAD STEEL BOLTS (UNIFIED THREADS), CADMIUM PLATED, FOR AIRCRAFT
    BS 3A 103:1962 Specification for steel nuts (Unified hexagons and Unified threads) (ordinary, thin, slotted and castle) for aircraft
    BS A 227:1965 Specification for steel pan head bolts (short thread: Class 3A)
    13/30275815 DC : 0 BS 2A 110+A1 - SPECIFICATION FOR STEEL NUTS (UNIFIED HEXAGONS AND UNIFIED THREADS) FOR SHEAR BOLTS FOR AIRCRAFT
    11/30252412 DC : 0 BS 4A 116 - STEEL PAN HEAD BOLTS (UNIFIED THREADS) (CADMIUM PLATED) FOR AIRCRAFT
    BS 2A 27:1962 Specification for steel hexagonal nuts (B.A. and B.S.F threads) (ordinary, thin, slotted and castle) for aircraft
    BS 3A 108:1962 Specification for steel bolts (Unified hexagons and Unified threads) with close tolerance shanks for aircraft
    BS SP33-39(1951) : 1951 SPECIFICATIONS FOR TURNBARRELS, TENSION RODS AND SWAGED CABLE-END CONNECTIONS FOR AIRCRAFT
    BS 2A 60:1962 Specification for cadmium-plated steel hexagonal-headed shear bolts (B.S.F. threads) for aircraft
    BS 4A 111:1993 Specification for cadmium-plated steel bolts (Unified hexagons and Unified threads) with close tolerance shanks
    BS 4A 116:2012 Steel pan head bolts (Unified threads), cadmium plated, for aircraft
    BS 2A 58:1962 SPECIFICATION FOR STEEL HEXAGONAL NUTS (B.S.F. THREADS) FOR SHEAR BOLTS FOR AIRCRAFT
    BS 2A 122; 2A 123; 2A 124:1981 Specification for clinch nuts (Unified threads) for aircraft
    BS 3A 116:1962 SPECIFICATION FOR STEEL PAN HEAD BOLTS (UNIFIED THREADS) FOR AIRCRAFT
    BS 2A110(1962) : 1962 SPECIFICATION FOR STEEL NUTS (UNIFIED HEXAGONS AND UNIFIED THREADS) FOR SHEAR BOLTS FOR AIRCRAFT
    BS A 226:1965 SPECIFICATION FOR STEEL HEXAGON HEAD BOLTS (SHORT THREAD: CLASS 3A)
    BS 3A125 TO 3A[...](1981) : 1981 AEROSPACE SERIES - SPECIFICATION FOR STIFFNUTS (UNIFIED THREADS) FOR AIRCRAFT
    BS 2A 59:1962 SPECIFICATION FOR CADMIUM-PLATED STEEL HEXAGONAL-HEADED BOLTS (B.A. AND B.S.F. THREADS) WITH CLOSE TOLERANCE SHANKS FOR AIRCRAFT
    BS 2SP 93:1974 Specification for elastomeric grommets (acrylonitrile-butadiene) for aerospace use
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