Construction alloy steel- for hardening and tempering 40HNMA,1.6565,40NiCrMo6,40NiCrMo7, -

Construction alloy steel- for hardening and tempering nickel-chromium-molybdenum 40HNMA   PN-89/H-84030/04
Steel grade

Standard

Chemical composition (%)

C
Mn
Si
P
S
Cu
Cr
Ni
Mo
other
40HNMA
PN
0,37
0,44
0,50
0,80
0,17
0,37
max
0,030
max
0,025
max
0,30
0,60
0,90
1,25
1,65
0,15
0,25
-
40 NiCrMo 6
40NiCrMo6

1.6565

DIN

W.nr
0,35
0,45
0,50
0,70
0,15
0,35
max
0,035
max
0,035
-
0,90
1,40
1,40
1,70
0,20
0,30
-
40HN2MA
40KHN2MA
40ChN2MA
40ХН2МА
GOST
0,37
0,44
0,50
0,80
0,17
0,37
max
0,025
max
0,025
max
0,20
0,60
0,90
1,25
1,65
0,15
0,25
V max 0,05
Ti max 0,03
W max 0,20
N max 0,008
40 NCD 7
40NCD7
AFNOR
0,38
0,43
0,65
0,85
0,15
0,35
max
0,025
max
0,025
-
0,70
0,90
1,65
2,00
0,20
0,30
-
40 NiCrMo 7
40NiCrMo7
UNI
0,38
0,43
0,50
0,80
0,15
0,40
max
0,025
max
0,020
-
0,70
0,90
1,65
2,00
0,20
0,30
-
SNCM 439
SNCM439
JIS
0,36
0,43
0,60
0,90
0,15
0,35
max
0,030
max
0,030
max
0,30
0,60
1,00
1,60
2,00
0,15
0,30
-
G 43400
G43400
4340
A 29 (4340)

UNS

AISI
ASTM
0,38
0,43
0,65
0,85
0,22
0,35
max
0,035
max
0,040
-
0,70
0,90
1,65
2,00
0,20
0,30
-
G 43370
G43370
4337
A 519 (4337)

UNS

AISI
ASTM
0,35
0,40
0,65
0,85
0,20
0,35
max
0,025
max
0,025
-
0,70
0,90
1,65
2,00
0,20
0,30
-
Steel with high hardenability, destined for heavily loaded parts and components: motor vehicles, engines and aircrafts. 
The parts exposed to impact, torsion and vibration, with the thickness of 100 mm: crank shafts, connecting rods,
hub propellers, parts of pumps, presses, compressors, parts working at higher temperatures 400 - 450 C
The rotors, shafts, rings and discs in steam turbines, very responsible bolts and screws of large diameter,
non-carburized gears and other heavily loaded parts subjected to impact.


40HNMA grade or equivalent is provided as round-rolled bars, forgings,round bars, square bars, flat bars,
plates, cubes, rings, rings.
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