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BS 3A117(1962) : 1962

Current

Current

The latest, up-to-date edition.

AEROSPACE SERIES - BOLTS, PAN HEAD, SLOTTED DRIVE, UNIFIED THREADS, CORROSION RESISTING STEEL, STRENGTH CLASS 880 MPA, FOR AIRCRAFT - SPECIFICATION

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-1962

$238.76
Including GST where applicable

Foreword
1 Scope
2 Normative references
3 General requirements
4 Material and manufacture
5 Dimensions
6 Screw threads
7 Protective finish
8 Hardness values
9 Identification and marking
10 Inspection procedure

Defines the materials, dimensions and inspection requirements for corrosion resisting steel pan head bolts (Unified threads), Strength class 880 MPa, for aircraft.

Committee
ACE/12
DevelopmentNote
Supersedes BS 2A117(1956) (07/2005) 1962 Edition Re-Issued in May 2016 & incorporates AMD 2 2016. Supersedes 15/30266106 DC. (06/2016)
DocumentType
Standard
Pages
12
PublisherName
British Standards Institution
Status
Current
Supersedes

BS 7S 80:2002 High chromium-nickel corrosion resisting steel forging stock, bars, forgings and parts (880 to 1080 MPa: limiting ruling section 100 mm)
BS EN ISO 6506-1:2014 Metallic materials. Brinell hardness test Test method
BS EN ISO 6508-1:2015 Metallic materials. Rockwell hardness test Test method
BS EN ISO 6507-1:2005 Metallic materials. Vickers hardness test Test method
BS HR 650:1972 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)
BS EN 2399:2008 Aerospace series. Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15). Rm ≥ 900 MPa. Bars for forged bolts. D ≤ 25 mm
BS EN 2398:2008 Aerospace series. Heat resisting steel FE-PA2601(X6NiCrTiMoV26-15). Rm ≥ 900 MPa. Bars for machined bolts. D ≤ 25 mm
BS 4A 100:2003 Specification for general requirements for bolts and free running nuts of tensile strength not exceeding 1249 MPa

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