BS 4S100(1975) : 1975
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
PROCEDURE FOR INSPECTION AND TESTING OF WROUGHT STEELS (OTHER THAN SHEET, STRIP AND TUBES)
Available format(s)
Hardcopy , PDF
Superseded date
15-09-1993
Language(s)
English
Published date
01-01-1975
Publisher
Describes inspection and testing of heat resisting alloys used for aerospace purposes. Covers forgings, plate, strip, tubes and bars. Gives chemical composition and mechanical properties.
| Committee |
ACE/61
|
| DocumentType |
Standard
|
| Pages |
45
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy |
| BS S 161:1990 | Specification for chromium-nickel-molybdenum corrosion-resisting steel. Bright bars and parts (540 MPa, limiting ruling section 160 mm) (Cr 17.5, Ni 12.5, Mo 2.25, controlled nitrogen content) |
| BS 2S 137:1976 | Specification for high chromium-nickel corrosion-resisting steel bright bars (free machining) (880-1080 MPa: limiting ruling section 70 mm) |
| BS 3S 62:1964 | Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (45/55 tonf/sq in: limiting ruling section 6 in) |
| BS 3S 91:1977 | Specification for mild steel billets, bars, forgings and parts (suitable for bearing shells) |
| BS 2S 129:1976 | Specification for 18/9 chromium-nickel corrosion-resisting steel (titanium stabilized) billets, bars, forgings and parts (540 MPa: limiting ruling section 150 mm) |
| BS 2A175(1962) : 1962 | SPECIFICATION FOR 100 DEGREE COUNTERSUNK HEAD ALUMINIUM ALLOY BOLTS (UNIFIED THREADS) FOR AIRCRAFT |
| BS 4S 106:1976 | Specification. 3% chromium-molybdenum steel billets, bars, forgings and parts (930-1080 MPa: limiting ruling section 150 mm) (suitable for nitriding) |
| BS S 139:1968 | Specification for 1½ per cent nickel-chromium-molybdenum steel (110/130 kgf/mm<sup>2</sup> (70/83 tonf/in<sup>2</sup>): limiting ruling section 70 mm (2¾ in)) |
| BS 2S 146:1976 | Specification for 4% nickel-chromium-molybdenum air-hardening steel (vacuum arc remelted) billets, bars, forgings and parts (1760-1960 MPa: limiting ruling section 100 mm) |
| BS 2S 111:1964 | Specification for aircraft material. Nickel-chromium-tungsten valve steel |
| BS 2S 124:1964 | Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (free machining) (45/55 tonf/sq in: limiting ruling section 6 in) |
| BS 5S 21:1964 | Specification for aircraft material. \'20\' carbon steel (suitable for welding) (25/35 tonf/sq in: maximum size 6 inches diameter or minor sectional dimension) |
| BS 3A107(1962) : 1962 | SPECIFICATION FOR ALUMINIUM ALLOY NUTS (UNIFIED HEXAGONS AND UNIFIED THREADS) (ORDINARY AND SLOTTED) FOR AIRCRAFT |
| BS S 138:1967 | Specification for 3 per cent chromium-molybdenum-vanadium steel (vacuum remelted - air hardening) (157 kgf/mm<sup>2</sup> (100 tonf/in<sup>2</sup>): limiting ruling section 30 mm (1⅛ in)) |
| BS 2S 93:1964 | Specification for aircraft material. \'40\' carbon steel (normalized) (35/45 tonf/sq in: limiting ruling section 6 in) |
| BS A 227:1965 | Specification for steel pan head bolts (short thread: Class 3A) |
| BS 2S 147:1976 | Specification for 0.5% nickel-chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts |
| BS S 141:1968 | Specification for 12 per cent chromium corrosion-resisting steel (60/80 kgf/mm<sup>2</sup> (38/51 tonf/in<sup>2</sup>): limiting ruling section 150 mm (6in)) |
| BS 2S 114:1964 | Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 2½ inches) |
| BS S 159:1981 | Specification for 12% chromium-nickel-molybdenum-vanadium heat-resisting steel bars for the manufacture of fasteners (1100-1300 MPa: limiting ruling section 50 mm) |
| BS S 126:1964 | Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in) |
| BS 2S 136:1977 | Specification for 1% carbon-chromium steel (vacuum arc remelted) billets, bars, forgings and parts (limiting ruling section 25 mm) |
| BS 4A 100:2003 | Specification for general requirements for bolts and free running nuts of tensile strength not exceeding 1249 MPa |
| BS 2S 92:1964 | Specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 tonf/sq in: limiting ruling section 4 in) |
| BS S 158:1977 | Specification for 1% chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts |
| BS 2S 113:1964 | Specification for aircraft material. \'40\' carbon steel bright bars for machining (45-55 tonf/sq in: limiting ruling section 1 inch) (primarily intended for the manufacture of nuts) |
| BS A 237-240:1971 | Specification for plain hexagonal nut (of Class 3B UNJ thread) |
| BS 2S 98:1964 | Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in) |
| BS 2S 131:1977 | Specification for high thermal expansion steel billets, bars, forgings and parts (620 MPa: limiting ruling section 150 mm) |
| BS 2S 130:1976 | Specification for 18/9 chromium-nickel corrosion-resisting steel (niobium stabilized) billets, bars, forgings and parts (540 MPa: limiting ruling section 150 mm) |
| BS 3A 100:1991 | Specification for general requirements for bolts and free running nuts of tensile strength not exceeding 1249 MPa |
| BS 2S 117:1964 | Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch) |
| BS 2S 112:1964 | Specification for aircraft material. Semi-free cutting carbon steel, bright bars for machining (40-50 tonf/sq in: maximum size ½ inch diameter or minor sectional dimension) (primarily intended for the manufacture of 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 S 163:1990 | Specification for nickel-chromium-molybdenum-vanadium steel forging stock, forgings, bars and parts (1900 MPa : limiting ruling section 100 mm) |
| BS A 233-236:1971 | Specification for plain hexagonal thin nut (of Class 3B UNJ thread) |
| BS 3S 61:1964 | Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (35/45 tonf/sq in: limiting ruling section 6 in) |
| 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 2W 11:1967 | Specification for aircraft material. Preformed corrosion-resisting steel wire rope |
| BS S 153:1976 | Specification. 2½% nickel-chromium-molybdenum steel billets, bars, forgings and parts (1230-1430 MPa: limiting ruling section 40 mm) |
| 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 2S 142:1977 | Specification for 1% chromium-molybdenum steel billets, bars, forgings and parts (900-1100 MPa: limiting ruling section 40 mm) |
Hardcopy - English
PDF - English
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