AIR 35NCD16 Structural and constructional steels
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This material has 170 properties — only a subset is shown here.
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AIR 35NCD16 Chemical Composition
AIR 9160/C: 1973 / General conditions for delivery and use of wrought steels used in aeronautical structures
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AIR 35NCD16 Physical Properties
Temperature
This material has 170 properties — only a subset is shown here.
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AIR 35NCD16 Heat Treatments
- Hardened and tempered (T1760): Hardened at 875 +/- 10°C, cooled 2h and Tempered 4h at 210 +/- 5°C;
Hardened and tempered (T1220): Hardened at 875 +/- 10°C and Tempered 3h at 560 +/- 5°C;
Annealed (R) at 875 +/- 10°C + 650 to 675, cooled in calm air;
Hardened and tempered (T1760): Hardened at 875 +/- 10°C, cooled 2h and Tempered min. 2h at 200-220°C;
Hardened and tempered (T1230): Hardened at 875 +/- 10°C, Tempered 3h at 550-580°C;
Hardened and tempered (T080): Hardened at 875 +/- 10°C, Tempered 3h at min. 550°C;
AIR 35NCD16 Mechanical Properties
Temperature
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AIR 35NCD16 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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- 64Cross References
- 8Composition
- 30Mechanical Properties
- 3Physical Properties
- 1Heat Treatment
- -Metallography
- -Machinability
- -Stress-Strain
- -Formability
- -Fatigue
- 2Fracture
- -Creep
- -Joints
- -Coatings
- -Dimensions
- -Tribology
- -Corrosion
- -Ageing
- -Weatherability
- -Irradiation
- 62Total Suppliers