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IS 4367 40Ni6Cr4Mo3 vs EN 10028-2 10CrMo9-10

Minimal Match — 35% match based on chemical composition and mechanical property overlap.

IS 4367 40Ni6Cr4Mo3 (IS 4367:1991) and EN 10028-2 10CrMo9-10 (EN 10028-2:2017) are both steel grades. Both fall under the Alloy Steel category. IS 4367 40Ni6Cr4Mo3 is typically used for aircraft landing gear, high strength shafts, gears, axles, connecting rods, heavy engineering components, while EN 10028-2 10CrMo9-10 is commonly used for flat products for pressure purposes. IS 4367 40Ni6Cr4Mo3 is defined under Bureau of Indian Standards (IS), originating from India, while EN 10028-2 10CrMo9-10 is defined under European Standard (EN), originating from Europe.

As per chemical composition, IS 4367 40Ni6Cr4Mo3 vs EN 10028-2 10CrMo9-10 is a 53.6% match. As per mechanical properties, the match is 0%. Combined, this makes them a minimal match overall at 35%.

Frequently Compared With IS 4367 40Ni6Cr4Mo3:
NF A35-565 100C6 GB/T 3077 12Cr2Ni4A UNI 11234 100Cr6 GOST 4543 12HN3A IS 1570 (Part 4) 103Cr6 IS 1570 (Part 7) 10Cr36Mo10H IS 4367 07Cr4Mo6 IS 4367 10Cr9Mo10 IS 1570 (Part 4) 07Cr4Mo6 IS 1570 (Part 4) 103Cr4 IS 1570 (Part 4) 105Cr5 IS 1570 (Part 4) 10Cr20Mo6
Match Breakdown
CHEMISTRY MATCH
53.6%
MECHANICAL MATCH
0%
OVERALL
35%
Specifications
Property IS 4367 40Ni6Cr4Mo3 EN 10028-2 10CrMo9-10
Standard IS 4367:1991 EN 10028-2:2017
Category Alloy Steel Alloy Steel
C (%) 0.35-0.45 0.08-0.14
Si (%) 0.10-0.35 <=0.50
Mn (%) 0.40-0.70 0.40-0.80
Ni (%) 1.25-1.75 Not specified
Cr (%) 0.90-1.30 2.00-2.50
Mo (%) 0.20-0.35 0.90-1.10
S (%) <=0.035 <=0.010
P (%) <=0.035 <=0.020
N (%) Not specified <=0.012
Cu (%) Not specified <=0.30
Matched by chemical composition and mechanical properties, not a formal equivalence claim. Always verify against the applicable standard before substitution.
Mechanical Properties
Property IS 4367 40Ni6Cr4Mo3 EN 10028-2 10CrMo9-10
Tensile Strength 900-1050 MPa 480-630 MPa
Yield Strength 700 MPa min >=310 MPa
Elongation >=15% >=18%
Izod Impact 55 J min Not specified
Hardness 266-311 HB Not specified
Hardness (soft annealed) <=230 HB Not specified
Condition Hardened and tempered, ruling section up to 150 mm Usual delivery condition normalized and tempered (+NT), nominal thickness up to 16 mm; transverse direction, Yield Strength is ReH, Elongation is A
Typical Applications
IS 4367 40Ni6Cr4Mo3
aircraft landing gear, high strength shafts, gears, axles, connecting rods, heavy engineering components
EN 10028-2 10CrMo9-10
Flat products for pressure purposes
Key Differences
Can IS 4367 40Ni6Cr4Mo3 Be Substituted With EN 10028-2 10CrMo9-10?
IS 4367 40Ni6Cr4Mo3 and EN 10028-2 10CrMo9-10 share some compositional similarity but differ enough that substitution should not be assumed. Review the differences above carefully, and consult the applicable standard or a metallurgist before using one in place of the other.
Forms & Sizes Available on M-EX
IS 4367 40Ni6Cr4Mo3
Round Bar → (2 listings)
Diameter: 50–50 mm (1.97–1.97 in)
Length: 5000–5200 mm (196.85–204.72 in)
EN 10028-2 10CrMo9-10
No active listings currently.
On M-EX Right Now
IS 4367 40Ni6Cr4Mo3
2 active listings and RFQs →
EN 10028-2 10CrMo9-10
0 active listings and RFQs →
Frequently Asked Questions
What is the difference between IS 4367 40Ni6Cr4Mo3 and EN 10028-2 10CrMo9-10?
IS 4367 40Ni6Cr4Mo3 specifies Ni which is not specified for EN 10028-2 10CrMo9-10. EN 10028-2 10CrMo9-10 specifies N, Cu which are not specified for IS 4367 40Ni6Cr4Mo3.
Can IS 4367 40Ni6Cr4Mo3 be substituted with EN 10028-2 10CrMo9-10?
IS 4367 40Ni6Cr4Mo3 and EN 10028-2 10CrMo9-10 share some compositional similarity but differ enough that substitution should not be assumed. Review the differences above carefully, and consult the applicable standard or a metallurgist before using one in place of the other.