IS 4432:1988 10C4 Steel: Specifications & Listings

IS 4432:1988 10C4: 10C4 is a case hardening steel in IS 4432:1988 (Specification for case hardening steels), which covers wrought low carbon unalloyed and alloy steel bars, billets, rods and finished forgings for case hardening.

Category: Carbon Steel
Grade Details
GradeIS 4432:1988 10C4
Standard IS 4432:1988
ApplicationsForgings and fabrication of case-hardened machine or automobile parts
Equivalent / Similar Grades
Grade Standard Region Live on M-EX
IS 11169 (Part 1) 10C4 IS 11169 (Part 1):2022 India No activity yet
EN 10084 C10R EN 10084:2008 Europe No activity yet
BS 970 (Part 3) 045M10 BS 970 (Part 3):1991 UK No activity yet
Grade ComparisonCompare With a Specific Grade →
Grade Standard Match
EN 10084 C10E EN 10084:2008 Strong Match
EN 10084 C10R EN 10084:2008 Strong Match
BS 970 (Part 3) 045M10 BS 970 (Part 3):1991 Strong Match
BS 970 (Part 3) 045A10 BS 970 (Part 3):1991 Strong Match
SAE J403 1009 SAE J403:2014 Strong Match
SAE J403 1009 SAE J403:2001 Strong Match
SAE J403 1009 SAE J403:2009 Strong Match
BS 970 EN2B BS 970:1955 Strong Match
Matched by chemical composition and mechanical properties, not a formal equivalence claim. Always verify against the applicable standard before substitution.
Chemical Composition (%)
C Si Mn S P
<=0.15 0.15-0.35 0.30-0.60 <=0.045 <=0.045
Mechanical Properties
Core Tensile Strength 550-800 MPa (16 mm) / 500-650 MPa (30 mm)
Core Yield Strength >=330 MPa (16 mm) / >=300 MPa (30 mm)
Core Elongation >=13% (16 mm) / >=16% (30 mm)
Core Reduction of Area >=40% (16 mm) / >=45% (30 mm)
Hardness, annealed (A) <=131 HB

More data from IS 4432:1988

From the standard
Other composition limits from the clauses and notes
Deoxidation
Fully killed, unless otherwise agreed
Elements not specified for this grade, if present, maximum
Cr 0.30, Ni 0.30, Cu 0.25, V 0.05, Mo 0.05 percent
Copper plus 10 times tin, maximum
0.50 percent
Ni + Cr + Mo added together, maximum
0.50 percent
Micro-alloying elements
Titanium, niobium, vanadium or boron may be added by agreement, singly or together
Elements not specified in Table 1 are not added except by agreement or to finish the heat. Reasonable precautions are taken against unwanted elements from scrap.
Source: IS 4432:1988 with Amendment 1 (April 1994), Table 1 notes, clauses 3, 3.1 and 5.3
Heat treatment temperatures 5 values
Hot working temperature range
1100 to 850 °C
Normalising temperature
880 to 910 °C
Full annealing (A) temperature
900 to 930 °C
Sub-critical anneal for softening, after normalising
650 to 700 °C
Isothermally transformed condition
To a ferrite and pearlite structure without bainite, as per the transformation diagrams
Recommended temperatures, for guidance only, for controlling hardness, machinability and shearability.
Source: IS 4432:1988 with Amendment 1 (April 1994), Table 3
Case hardening treatment 6 values
Carburising temperature
900 to 940 °C
Direct and single hardening temperature
830 to 860 °C
Double hardening, core hardening temperature
880 to 900 °C
Double hardening, case hardening temperature
780 to 820 °C
Quenching medium
Water / thermal bath at 140 to 220 °C
Tempering temperature
150 to 180 °C
Recommended conditions for reaching the core properties below, for guidance only. Time for austenitising about 45 minutes for a 25 mm section; tempering at least 1 hour, preferably 90 minutes. For direct and single quenching use fully aluminium killed fine grained steel. If direct hardened, a carburising temperature of 940 °C is generally not exceeded. Thermal bath includes suitable salt baths.
Source: IS 4432:1988 with Amendment 1 (April 1994), Table 5
Core properties after case hardening, by test bar diameter 2 sections
Tensile strength (MPa)Yield strength, min (MPa)Elongation, min (%)Reduction of area, min (%)Test bar diameter (mm)
550 to 800330134016
500 to 650300164530
Core properties of simulated case-hardened test bars, treated as in the case hardening treatment above. Values apply to test bars taken from rounds in the direction of rolling. Applies when the steel is ordered on this basis.
Source: IS 4432:1988 with Amendment 1 (April 1994), Table 4
Hardness by delivery condition 2 conditions
Annealed to maximum hardness (A), maximum
131 HB
Treated for improved machinability (M)
90 to 145 HB
Brinell hardness. A different as-rolled maximum for cold shearability, or a different range for improved machinability, may be agreed at the time of order.
Source: IS 4432:1988 with Amendment 1 (April 1994), Table 6, clause 7.2

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