3s61 Aircraft Steel 3S61

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Quality - BS EN 9120:2005, / ISO 9001:2008

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Data Sheet:

Corrosion and Heat Resisting Alloy 3S61

Chemical Composition Limits

Weight %

P+S max

3S61

0.12 max

0.80 max

1.00 max

0.030P

0.025S

11.50 / 13.50

1.00 max

Chemically similar British Specifications BS.970 Pt4.
Weight %	C	Si	Mn	P+S max	Cr	Ni
403S17	0.08 max	0.80 max	1.00 max	0.040P 0.030S	12.00 / 14.00	0.50 max
410S21 (EN56A)	0.08 max	0.08 max	1.00 max	0.040P 0.030S	11.50 / 13.50	1.00 max

Other Chemically similar Specifications
Weight %	C	Si	Mn	P+S max	Cr	Ni	Others
AFNOR Z12C13	0.08 / 0.15	1.00 max	1.00 max	0.040 P 0.030 S	11.50 / 13.50	0.50 max	-
AISI 410 SAE 51410	0.15 max	1.00 max	1.00 max	0.040 P 0.030 S	11.50 / 13.50	-	-
AMS5613	0.15 max	1.00 max	1.00 max	0.040 P 0.030 S	11.50 / 13.50	0.75 max	Al 0.05 max N 0.08 max
MIL-L-24128	0.06 / 0.13	0.50 max	0.25 / 0.80	0.030 max	11.50 / 13.00	0.50 max	Mo 0.60 max Al 0.05 max
MIL-S-862B 403	0.15 max	0.50 max	1.00 max	0.040 P 0.030 S	11.50 / 13.00	-	-
MIL-S-862B 410	0.15 max	1.00 max	1.00 max	0.040 P 0.030 S	11.50 / 13.50	-	-
WERKSTOFF 1.4006	0.08 / 0.12	1.00 max	1.00 max	0.045 P 0.030 S	12.00 / 14.00	-	-

SPECIFICATIONS

S61 is available in Bar.

MECHANICAL PROPERTIES

S61

Tensile Strength Rm, tonf/in²

Proof Stress Rp 0.2, tonf/in²

Elongation in 5.65√Cross

Sectional Area (%)

Hardness HB

35 / 45

152 / 207

This material was Hardened and Tempered.

Disclaimer

Every effort is made to ensure that technical specifications are accurate. However, technical specifications included herein should be used as a guideline only. All specifications are subject to change without notice.

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