B.S. S 119 Structural and constructional steels
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B.S. S 119 Chemical Composition
BS 2S 119: 1964 / Specification for aircraft material. 1½ per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 2½ in)
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B.S. S 119 Physical Properties
Temperature
This material has 118 properties — only a subset is shown here.
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B.S. S 119 Heat Treatments
- Hardened in oil from a temperature between 820°C and 850°C (1510°F and 1560°F). Temper at a suitable temperature between 560°C and 660°C (1040°F and 1220°F). Hardened and tempered bars which have been subjected to a cold straightening or cold rolling operation shall be given a stress relieving treatment which shall be sufficient to restore the proof stress.
B.S. S 119 Mechanical Properties
Temperature
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B.S. S 119 International Equivalent Materials
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Equivalence categories reflect chemical-composition and mechanical-property comparison — always verify suitability against the governing specification for your application.
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- 54Cross References
- 8Composition
- 7Mechanical Properties
- 3Physical Properties
- 1Heat Treatment
- -Metallography
- -Machinability
- -Stress-Strain
- -Formability
- -Fatigue
- -Fracture
- -Creep
- -Joints
- -Coatings
- -Dimensions
- -Tribology
- -Corrosion
- -Ageing
- -Weatherability
- -Irradiation
- 45Total Suppliers