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Superseded

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BS 4A 116 - STEEL PAN HEAD BOLTS (UNIFIED THREADS) (CADMIUM PLATED) FOR AIRCRAFT

Available format(s)

Hardcopy , PDF

Superseded date

03-31-2012

Language(s)

English

Publisher

British Standards Institution

Foreword
1 Scope
2 Normative references
3 General requirements
4 Material and manufacture
5 Dimensions
6 Screw threads
7 Anti-corrosion treatment
8 Identification and marking
9 Inspection procedure
Annexes
Annex A (informative) - Table for conversion of inches
to approximate millimeter equivalents
Bibliography

BS 4A 116

Committee	ACE/12
DocumentType	Draft
Pages	15
PublisherName	British Standards Institution
Status	Superseded
SupersededBy	BS 4A 116:2012

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 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 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