BS 3A 116:1962
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Specification for steel pan head bolts (Unified threads) for aircraft
Hardcopy , PDF
31-03-2012
English
04-06-1962
Important note : Users cannot be edited or removed once added to your Multi user PDF.
FOREWORD
1 SCOPE
2 GENERAL REQUIREMENTS
3 MATERIAL AND MANUFACTURE
4 DIMENSIONS
5 SCREW THREADS
6 ANTI-CORROSION TREATMENT
7 IDENTIFICATION AND MARKING
8 INSPECTION PROCEDURE
APPENDIX - TABLE FOR CONVERSION OF INCHES TO
APPROXIMATE MILLIMETRE EQUIVALENTS
Gives the materials, dimensions, finish and inspection requirements for steel pan head bolts with Unified threads for aircraft.
| Committee |
ACE/12
|
| DevelopmentNote |
Supersedes BS 2A116(1956) (07/2005) Reviewed and confirmed by BSI, January 2008. (12/2007)
|
| DocumentType |
Standard
|
| Pages |
13
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy |
| BS 2S96(1964) : LATEST | 2.5% NICKEL-CHROMIUM-MOLYBDENUM STEEL (55/65 TONF/SQ IN: LIMITING RULING SECTION 6 IN.) |
| 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 2A 100:1968 | Specification for general requirements for bolts and nuts of tensile strength not exceeding 180000 lbf/in<sup>2</sup> (125 hbar) |
| 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 3S105(1969) : 1969 | SPECIFICATION FOR CARBON STEEL - (BAR FOR THE MANUFACTURE OF FORGED BOLTS ONLY) |
| BS 350:2004 | Conversion factors for units |
| BS 2S 117:1964 | Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch) |
| 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 |
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