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This British Standard,
having been approved by the
Engineering Sector Committee,
was published under authority
of the Standards Committee
and comes into effect
on 15 July 1999
© The British Standards
Institution 2016
Published by BSI Standards
Limited 2016
The following BSI references
relate to the work on this
standard:
Committee reference ACE/12
Drafts for comment
98/706175 DC,
12/30262058 DC,
15/30317035 DC
ISBN 978 0 580 92822 2
Amendments/corrigenda issued since publication
Amd. No.
Date
Comments
C1
March 2010
A1
September 2012
See Foreword
A2
September 2015
See Foreword
C2
February 2016
Clause 2 and 4.2 b) updated. Table 1
– max. and min. columns reordered.
Table 2 – upper tolerance of E updated.
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BS 4A 114:1999+A2:2015
Foreword
Publishing information
This British Standard is published by BSI Standards Limited, under licence
from The British Standards Institution, and came into effect on 15 July 1999.
It was prepared by Technical Committee ACE/12, Aerospace fasteners and
fastening systems. A list of organizations represented on this committee can
be obtained on request to its secretary.
Supersession
BS 4A 114:1999+A2:2015 supersedes BS 4A 114:1999+A1:2012, which is
withdrawn.
Information about this document
Text introduced or altered by Amendments No. 1 (and No. 2, respectively) are
indicated in the text by tags (and ). Minor editorial changes are
not tagged.
Contractual and legal considerations
This publication does not purport to include all the necessary provisions of a
contract. Users are responsible for its correct application.
Licensed
Compliance with a British Standard cannot confer immunity from
legal obligations.
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This British Standard specifies materials
and manufacture, dimensions, protective
treatment and quality assurance requirements
for corrosion-resisting and heat resisting
steel, mushroom-headed, slotted-drive, bolts
(minimum tensile strength 880 MPa).
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The following documents, in whole or in part,
are normatively referenced in this document
and are indispensable for its application. For
dated references, only the edition cited applies.
For undated references, the latest edition
of the referenced document (including any
amendments) applies.
BS 4A 100:2003, Specification for general
requirements for bolts and free running nuts of
tensile strength not exceeding 1249 MPa.
BS S 80, Specification for high chromium-nickel
corrosion-resisting steel forging stock, bars,
forgings and parts (880-1080 MPa, limiting
ruling section 100 mm).
BS S 143, Specification for chromium-nickelcopper-molybdenum corrosion-resisting steel
(precipitation hardening) billets, bars, forgings
and parts (930-1080 MPa).
Text deleted.
BS EN 2398, Aerospace series – Heat resisting
steel FE-PA2601 (X6NiCrTiMoV26-15) – Rm
=
900 MPa – Bars for machined bolts – D =
25 mm.
BS EN 2399, Aerospace series – Heat resisting
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BS EN ISO 6506-1, Metallic materials – Brinell
hardness test – Part 1: Test method.
BS EN ISO 6507-1, Metallic materials – Vickers
hardness test – Part 1: Test method.
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BS HR 650, Specification for High expansion
heat-resisting steel bar and wire for the
manufacture of bolts, studs, set screws and
nuts – (Ni 25.5, Cr 15, Ti 2, Mn 1.5, Mo 1.25,
Si 0.7, V 0.3) (Limiting ruling section 20 mm).
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a) 0.2 % proof stress (min.) : 590 MPa;
b) tensile strength (min.) : 880 MPa
Text deleted;
c) elongation (min.) : 12 %;
d) Izod impact (min.) : 55J (40 ft. lbf ).
NOTE This is not applicable to the materials given in
BS EN 2398 and BS EN 2399.
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Bolts made from material conforming to BS EN 2398
or BS EN 2399 shall be identified with a code “X ”,
e.g. a 6-32 UNC bolt with an “L” dimension of
0.1 inches and made from one of the two materials
above shall be referenced as “A114X1B” or for
bolts made from material conforming to BS S 80 or
BS S 143, this shall be identified as “A114-1B”.
Bolts shall be marked in accordance with
BS 4A 100:2003, Clause . Bolts for all nominal
sizes made from material conforming to
BS EN 2398 or BS EN 2399 shall be marked with
an “X ”.
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