SPECIFICATION FOR 100 DEGREES COUNTERSUNK HEAD STEEL BOLTS (UNIFIED THREADS), CADMIUM PLATED, FOR AIRCRAFT

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-1962

Publisher

British Standards Institution

Foreword
1 Scope
2 General requirements
3 Material and manufacture
4 Dimensions
5 Screw threads
6 Anti-corrosion treatment
7 Identification
8 Inspection procedure
9 Gauging
Appendix A - Principles of flushness control and
recommended gauging practice
Appendix B - Table for conversion of inches to
approximate millimeter equivalents

Gives the materials, dimensions, finish and inspection requirements for steel bolts with 100 degrees countersunk heads and unified threads for aircraft.

Committee	ACE/12
DevelopmentNote	Supersedes BS A173(1956) (07/2005) 1962 Edition Re-Issued in July 2012 and incorporates AMD 7 2012. (07/2012)
DocumentType	Standard
Pages	18
PublisherName	British Standards Institution
Status	Current

BS 2A 230:1974	Specification for 100° countersunk head steel bolts [1100 MPa with Hi-torque speed drive recesses]
BS A 232:1968	Specification for 100° countersunk head steel bolts (160 000 lbf/in<sup>2</sup> (110 hbar) with Torq-set recesses)

BS 3S95(1967) : 1967	SPECIFICATION FOR 1[1/2] PER CENT NICKEL-CHROMIUM-MOLYBDENUM STEEL - (880/1080 MPA: LIMITING RULING SECTION 150 MM)
BS 2S 114:1964	Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 2½ inches)
BS 2S 116:1964	Specification for aircraft material. \'40\' carbon steel bright bars for machining (55-65 tonf/sq in: limiting ruling section ¾ inch) (primarily intended for the manufacture of machined bolts)
BS 2S 149:1976	Specification for 1.75% nickel-chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts
BS S 154:1976	Specification. 2½% nickel-chromium-molybdenum steel billets, bars, forgings and parts (880-1080 MPa: limiting ruling section 150 mm)
BS S148(1969) : 1969	SPECIFICATION FOR LOW NICKEL-CHROMIUM STEEL (BAR FOR THE MANUFACTURE OF FORGED BOLTS ONLY)
BS 3S102(1969) : 1969	SPECIFICATION FOR CARBON-MOLYBDENUM STEEL (BAR FOR THE MANUFACTURE OF FORGED BOLTS ONLY)
BS EN 2133:2010	Aerospace series. Cadmium plating of steels with specified tensile strength ≤ 1450 MPa, copper, copper alloys and nickel alloys
BS 3S105(1969) : 1969	SPECIFICATION FOR CARBON STEEL - (BAR FOR THE MANUFACTURE OF FORGED BOLTS ONLY)
BS 2S 117:1964	Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch)
BS 4A 100:2003	Specification for general requirements for bolts and free running nuts of tensile strength not exceeding 1249 MPa
BS S 158:1977	Specification for 1% chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts
BS 2S 147:1976	Specification for 0.5% nickel-chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts
DEFSTAN 03-19/4(2010) : 2010	ELECTRO-DEPOSITION OF CADMIUM

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BS 2A173(1962) : 1962

SPECIFICATION FOR 100 DEGREES COUNTERSUNK HEAD STEEL BOLTS (UNIFIED THREADS), CADMIUM PLATED, FOR AIRCRAFT

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Abstract

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