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Homepage>BS Standards>49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.030 Fasteners for aerospace construction>49.030.20 Bolts, screws, studs>BS 2A 241:2005+A2:2011 General requirements for steel protruding-head bolts of tensile strength 1250 MPa (180000 lbf/in2) or greater. Specification
immediate downloadReleased: 2011-01-31
BS 2A 241:2005+A2:2011 General requirements for steel protruding-head bolts of tensile strength 1250 MPa (180000 lbf/in2) or greater. Specification

BS 2A 241:2005+A2:2011

General requirements for steel protruding-head bolts of tensile strength 1250 MPa (180000 lbf/in2) or greater. Specification

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Standard number:BS 2A 241:2005+A2:2011
Pages:38
Released:2011-01-31
ISBN:978 0 580 71708 6
Status:Standard
DESCRIPTION

BS 2A 241:2005+A2:2011


This standard BS 2A 241:2005+A2:2011 General requirements for steel protruding-head bolts of tensile strength 1250 MPa (180000 lbf/in2) or greater. Specification is classified in these ICS categories:
  • 49.030.20 Bolts, screws, studs

This British standard specifies the general requirements for metric and inch protruding head steel aerospace bolts of tensile strength of 1 250 MPa (180 000 lbf/in2) or greater.

The requirements related to nominal size are presented in individual tables Text deleted for use as appropriate to the relevant bolt specification. The values quoted for metric and inch bolts have a proportional relationship and are not direct conversions.


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